1. The document discusses sequential engineering and concurrent engineering approaches to product development. In sequential engineering, departments such as design, planning, and manufacturing work independently and pass work to each other in sequence, requiring rework if changes are needed. 2. Concurrent engineering uses cross-functional teams with representatives from all departments who work together throughout the design process. This allows issues to be identified and resolved early when changes are less costly. 3. The document advocates for concurrent engineering as a better approach for reducing product development time and integrating customer and manufacturing needs into the design.

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ED 7102 Computer Aided Design

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UNIT 1
FUNDAMENTALS OF COMPUTER GRAPHICS
Product cycle- Design process- sequential and concurrent engineering- Computer aided design – CAD
system architecture- Computer graphics – co-ordinate systems- 2D and 3D transformations-
homogeneous coordinates - Line drawing -Clipping- viewing transformation
1.1 PRODUCT CYCLE
Industries have to continuously upgrade their products as well as introduce new products in the
market in order to retain as well as to increase their market share. The product development is the
responsibility of the research and development (R&D) department of a manufacturing company. When a
product is initially introduced the sales volume will be low. If the product is good and satisfies the
customers, the sales will pick up. Sometimes, if there are any problems in the product the company will
have to make changes or improvements in the product which is a very expensive proposition. If the defect
is serious enough the company may have to recall an entire batch of products at enormous cost and loss of
goodwill. The sales and service department usually takes care of attending to the customers’ problems.
That is why manufacturers of automobiles, entertainment electronic goods, fast moving consumer goods
like washing machines and refrigerators etc have elaborate sales and service network. The sales volume
will pick up gradually and peak after some time. The product will continue to sell for some time. The
sales will then start gradually declining owing to availability of better products in the market. It is time for
the company to introduce a new and improved product in the market as well as to retire the old product.
The companies will usually advice the customers that the old product will be further supported by the
sales and service department only for a limited period of time. The cycle through which a product goes
through from development to retirement is called the product life cycle. The variation of the sales volume
during the life cycle of a product is graphically shown in Fig.1.

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Fig. 1 Variation of the Sales Volume Vs Life of a Product
The product development cycle starts with developing the product concept, evolving the design,
engineering the product, manufacturing the part, marketing and servicing. This is shown in Fig. 2. The
idea of a product may come from a patent, suggestion of the customers, feedback of the sales and service
department, market research carried out by the marketing department or from the R&D department itself.
The next stage is the conceptualization of the product. The cost at which the product could be sold in the
market is decided and the overall design in terms of shape, functional specifications, ergonomics,
aesthetics etc are considered in detail and finalized at this stage. The work of product development is then
taken to the next stage by the design department who carefully designs each assembly and each
component of the assembly. Detailed design analysis and optimization is carried out at this stage. A
design may have several variants. For example, a passenger car may have what is called a stripped down
version with the bare minimum options and luxury versions with several add on functionalities. Between
these two extreme versions, there will be a number of models or variants to meet the needs of customers
with different paying capacities. In a similar way, a satellite launch vehicle may be designed for different
payloads. A fighter aircraft may have different versions. A refrigerator will have to be marketed with
different capacities. The design department creates these designs through a top down approach or a
bottom up approach. In top down approach, the entire assembly is designed first and individual designs
are done latter. In bottom up approach, the component design is done first and the product is realized by
assembling the components suitably. The design also will involve preparation of detail drawings.

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Fig. 2 Product Development Cycle
1.2 SEQUENTIAL ENGINEERING
The traditional product development process at the prototype development stage is sequential. It
includes Product design, development of manufacturing process and supporting quality and testing
activities, all carried out one after another. This situation assumes that there is no interaction among the
major Departments involved in product manufacturing during the initial development process. Often the
need for engineering changes is discovered during planning or manufacturing or assembly. Design
department in a typical sequential product development process finalizes the design without consulting
the manufacturing, quality or purchase departments. Planning might feel it necessary to request design
changes based on a number of reasons like the procurement or facility limitations. Changes in design may
be called for when the manufacturing department is unable to meet design specifications or there are
problems in assembly.
These changes are however to be incorporated in design. The design documents are therefore sent
back to the design department for incorporating the changes. The design redesign path is shown in Fig. 3
The design documents are passed on back and forth to incorporate design changes as illustrated. This will
lead to inevitable conflicts, each department sticking to their own decisions and may often require
intervention of senior management to resolve conflicts or differences in opinion. Design changes will
involve both material and time wastages. In such a situation, time taken to product development is usually

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more than what is anticipated and correspondingly the response to the market requirements will be slow
compared to a competing company which can create an error free design at the first instance. In an age of
reduced product life cycles as we witness today the time delay between market demand and introduction
of product in the market has to be as short as possible. Sequential product development process, therefore,
may not suit the present global scenario.
Fig. 3 Design and Redesign Path
Even after the prototype development stage is over, the need for design change may arise during
service. Such changes are usually few in number, but are very costly. Thus in the traditional
manufacturing, the design documents move sequentially through the various departments of the
organization. The R & D group completes the design task and passes the data to planning, which in turn
passes the information to manufacturing and so on. If any downstream department wants to introduce any
change, the process has to backtrack and this often involves additional expenditure as well as inevitable
delay in realizing the product.

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Fig.4 across the Wall Approach in Sequential Engineering
Sequential Engineering is often called “across the wall” method. Figure 4 illustrates the insulated way
each department may function in sequential approach. Each segment of the product development team
(Design, Planning, Manufacturing etc.) completes its task in isolation and passes over the documents to
the next segment. There is no interaction among the groups before the design is finalized. If a serious
mistake in the product is detected during testing, the revision process has to start from design, resulting in
materials wastage and loss of time. In the context of extensive outsourcing, there is also need for intensive
consultation between vendors and manufacturers.
1.3 CONCURRENT ENGINEERING
Concurrent engineering or Simultaneous Engineering is a methodology of restructuring the
product development activity in a manufacturing organization using a cross functional team approach and
is a technique adopted to improve the efficiency of product design and reduce the product development
cycle time. This is also sometimes referred to as Parallel Engineering. Concurrent Engineering brings
together a wide spectrum of people from several functional areas in the design and manufacture of a
product. Representatives from R & D, engineering, manufacturing, materials management, quality
assurance, marketing etc. develop the product as a team. Everyone interacts with each other from the start,
and they perform their tasks in parallel. The team reviews the design from the point of view of marketing,
process, tool design and procurement, operation, facility and capacity planning, design for
manufacturability, assembly, testing and maintenance, standardization, procurement of components and
sub-assemblies, quality assurance etc as the design is evolved. Even the vendor development department
is associated with the prototype development. Any possible bottleneck in the development process is
thoroughly studied and rectified. All the departments get a chance to review the design and identify

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delays and difficulties. The departments can start their own processes simultaneously. For example, the
tool design, procurement of material and machinery and recruitment and training of manpower which
contributes to considerable delay can be taken up simultaneously as the design development is in
progress. Issues are debated thoroughly and conflicts are resolved amicably. Concurrent Engineering (CE)
gives marketing and other groups the opportunity to review the design during the modeling, prototyping
and soft tooling phases of development. CAD systems especially 3D modelers can play an important role
in early product development phases. In fact, they can become the core of the CE. They offer a visual
check when design changes cost the least. Intensive teamwork between product development, production
planning and manufacturing is essential for satisfactory implementation of concurrent engineering. The
teamwork also brings additional advantages ; the co-operation between various specialists and systematic
application of special methods such as QFD (Quality Function Deployment), DFMA (Design for
Manufacture and Assembly) and FMEA (Failure Mode and Effect Analysis) ensures quick optimization
of design and early detection of possible faults in product and production planning. This additionally
leads to reduction in lead time which reduces cost of production and guarantees better quality.
1.4 COMPUTER GRAPHICS
Traditionally drawings are prepared on plane drawing sheets. This has several limitations. The
sketches have to be made only in two dimensions. Though the depth can be represented by pictorial
projections like isometric and perspective projections, the projections have to be necessarily reduced to
two dimensions. Use of computer graphics has opened up tremendous possibilities for the designer. Some
of them are listed below:
• The object is represented by its geometric model in three dimensions (X, Y and Z).
• The mathematical representation reduces creation of views like orthographic, isometric,
axonometric or perspective projections into simple viewing transformations.
• Though the size of the screen is limited, there is no need to scale the drawings.
• Drawings can be made very accurate.
• The geometric models can be represented in color and can be viewed from any angle.
• Sections can be automatically created.
• The associatively ensures that any change made in one of the related views will automatically
reflect in other views.
• Revision and revision control are easy.
• Drawings (geometric models) can be modified easily.
• More important than all, drawings can be reused conveniently.
• Storage and retrieval of drawings are easy.

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Modern computer graphics displays are simple in construction. They consist of basically three
components.
ÿ
Monitor
ÿ
Digital Memory or Frame Buffer
ÿ
Display Controller
Most of the computer graphics displays use raster CRT which is a matrix of discrete cells each of which
can be made bright. A graphic entity like line or circle is represented as a series of “points or dots” on the
screen. Therefore, it is called as a point plotting device. The video display screen is divided into very
small rectangular elements called a picture element or pixel. This happens to be the smallest addressable
screen element. Graphic images are formed by setting suitable intensity and color to the pixels which
compose the image. Depending upon the resolution screens may have varying number of pixels. For
example, an SVGA monitor with a resolution of 1024 x 768 will have 1024 pixels in every row (X -
direction) and 768 pixels in every column (Y-direction). Monitors of larger size will have resolution of
1024 x 1024 or more. A raster scan system displays the image on a CRT in a certain fixed sequence. The
refresh rate is the number of complete images or frames scanned per second. In the case of interlaced
refresh cycle odd numbered raster lines are refreshed during 1/60
th
of a second. Even numbered raster
lines are refreshed during the next 1/60th of a second. In non-interlaced displays, all lines are refreshed in
1/60th of a second. The quality of no interlaced display is hence, superior. These systems, however,
require expensive frame buffer memory and display controller.
1.5 GRAPHIC PRIMITIVES
A drawing is created by an assembly of points, lines, arcs, circles.. Each of these is called an entity.
The drawing entities that a user may find in a typical CAD package include:
∑ point
∑ line
∑ construction line, multi-line, polyline
∑ circle
∑ spline
∑ arc
∑ ellipse
∑ polygon
∑ rectangle

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1.6 CO-ORDINATE SYSTEMS
Transformations can be carried out either in 2-dimensions or in 3-dimensions. The theory of two-
dimensional transformations is discussed first in this chapter. This is then extended to three dimensions.
When a design package is initiated, the display will have a set of co-ordinate values. These are called
default co-ordinates. A user co-ordinate system is one in which the designer can specify his own co-
ordinates for a specific design application. These screen independent coordinates can have large or small
numeric range, or even negative values, so that the model can be represented in a natural way. It may,
however, happen that the picture is too crowded with several features to be viewed clearly on the display
screen. Therefore, the designer may want to view only a portion of the image, enclosed in a rectangular
region called a window. Different parts of the drawing can thus be selected for viewing by placing the
windows. Portions inside the window can be enlarged, reduced or edited depending upon the
requirements. Figure 5 shows the use of windowing to enlarge the picture.
Fig. 5 Use of Window to Enlarge a Portion of the Drawing
1.7 2-D TRANSFORMATIONS
In computer graphics, drawings are created by a series of primitives which are represented by the
co-ordinates of their end points. Certain changes in these drawings can be made by performing some
mathematical operations on these co-ordinates. The basic transformations are scaling, translation and
rotation. An example of scaling in the case of a triangle is shown in Fig.5 Fig next. shows the original
picture before scaling. Figure below shows the triangle after the co-ordinates are multiplied by the scaling
matrix.

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Fig. 7. Scaling a Triangle
B.TRANSLATION
Moving drawing or model across the screen is called translation. This is accomplished by adding
to the co-ordinates of each corner point the distance through which the drawing is to be moved
(translated). Figure below shows a rectangle given figure being moved to a new position as in figure
below by adding 40 units to X co-ordinate values and 30 units to Y coordinate values. In general, in order
to translate drawing by (TX , TY ) every point X, Y will be replaced by a point X1 , Y1 where
C. ROTATION
Another useful transformation is the rotation of a drawing about a pivot point. Consider Fig. next.
Point P1 (40, 20) can be seen being rotated about the origin through an angle, 45°, in the anti-clockwise

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direction to position P2. The co-ordinates of P2 can be obtained by multiplying the co-ordinates of P1 by
the matrix:
For rotating drawings in anticlockwise direction positive angles are used.
D. SHEARING

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A shearing transformation produces distortion of an object or an entire image. There are two
types of shears: X-shear and Y-shear. A Y-shear transforms the point (X, Y) to the point (X1, Y1) by a
factor Sh1, where
X1 = X
Y1 = Sh1. X + Y
Fig. below shows Y shear applied to a drawing.
Fig. below shows the effect of X-shear.

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1.8 3-DIMENSIONAL TRANSFORMATIONS
It is often necessary to display objects in 3-D on the graphics screen. The
transformation matrices developed for 2-dimensions can be extended to 3-D.

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1.9 HOMOGENEOUS COORINATES
Each of the above transformations with the exception of translation can be represented as a row
vector X, Y and a 2 X 2 matrix. However, all the four transformations discussed above can be represented
as a product of a 1 X 3 row vector and an appropriate 3 X 3 matrix. The conversion of a two-dimensional
co-ordinate pair (X, Y) into a 3-dimensional vector can be achieved by representing the point as [X Y 1].
After multiplying this vector by a 3 X 3 matrix, another homogeneous row vector is obtained [X1 Y1 1].
The first two terms in this vector are the co-ordinate pair which is the transform of (X, Y). This three
dimensional representation of a two dimensional plane is called homogeneous coordinates and the
transformation using the homogeneous co-ordinates is called homogeneous transformation. The matrix
representations of the four basic transformations are given below.

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1.10 DRAWING OF LINES
Straight line segments are used a great deal in computer generated pictures. The following criteria
have been stipulated for line drawing displays :
i. Lines should appear straight
ii. Lines should terminate accurately
iii. Lines should have constant density
iv. Line density should be independent of length and angle
v. Line should be drawn rapidly

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The process of turning on the pixels for a line segment is called vector generation. If the end points of the
line segment are known, there are several schemes for selecting the pixels between the end pixels. One
method of generating a line segment is a symmetrical digital differential analyzer (DDA).
DDA ALGORITHM
The digital differential analyzer generates lines from their differential equations. The DDA works
on the principle that X and Y are simultaneously incremented by small steps proportional to the first
derivatives of X and Y. In the case of a straight line the first derivatives are constant and are proportional
to DX and DY, where D is a small quantity. In the real world of limited precision displays, addressable
pixels only must be generated. This can be done by rounding to the next integer after each incremental
step. After rounding, a pixel is displayed at the resultant X and Y locations. An alternative to rounding is
the use of arithmetic overflow. X and Y are kept in registers that have integer and fractional parts. The
incrementing values which are less than unity are repeatedly added to the fractional part and whenever the
result overflows the corresponding integer part is incremented. The integer parts of X and Y are used to
plot the line. This would normally have the effect of truncating. The DDA is therefore initialized by
adding 0.5 in each of the fractional parts to achieve true rounding. The symmetrical DDA generates
reasonably accurate lines since a displayed pixel is never away from a true line by half the pixel unit. A
Pascal procedure for a simple DDA is given below :

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It can be noted that lines drawn on a raster display may have a jagged or staircase appearance unless
the lines are vertical or horizontal. This is because the points that are plotted must be pixel grid points
and many of these may not lie on the actual line.
1.11 CLIPPING
Clipping is the process of determining the visible portions of a drawing lying within a window. In
clipping each graphic element of the display is examined to determine whether or not it is completely
inside the window, completely outside the window or crosses a window boundary. Portions outside the
boundary are not drawn. If the element of a drawing crosses the boundary the point of inter-section is
determined and only portions which lie inside are drawn. Readers are advised to refer to books on

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computer graphics for typical clipping algorithms like Cohen-Sutherland clipping algorithm. Fig
below
shows an example of clipping.
Figure.1.11 Example of clipping

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UNIT II GEOMETRIC MODELING
Representation of curves- Hermite curve- Bezier curve- B-spline curves-rational curves-
Techniques for surface modeling – surface patch- Coons and bicubic patches- Bezier and B-
spline surfaces. Solid modeling techniques- CSG and B-rep
Modeling of curves and surfaces is essential to describe objects that are encountered in several
areas of mechanical engineering design. Curves and surfaces are the basic building blocks in the
following designs:
i. Body panels of passenger cars
ii. Aircraft bulk heads and other fuselage structures, slats, flaps, wings etc.
iii. Marine structures
iv. Consumer products like plastic containers, telephones etc.
v. Engineering products like mixed flow impellers, foundry patterns etc
A curve has one degree of freedom while a surface has two degrees of freedom. This means that
a point on a curve can be moved in only one independent direction while on surfaces it has two
independent directions to move. This is shown in Fig. 6.1
.
REPRESENTATION OF CURVES AND SURFACES
A curve or a surface may be described or represented by a set of equations.
These equations can be categorized into two forms:
i. Generic form
The generic form in which any generic point (x, y, z) satisfies a
relationship in implicit form in x, y, and z i.e. f(x, y, z) = 0. A single
such constraint generally describes a surface while two constraints
considered together can be thought of as a curve which is the
intersection of two surfaces. This may be expressed in an explicit form
in the following manner:

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ii. Parametric form
A parametric curve is one whose defining equations are in terms of a
simple, common independent variable known as parametric variable.
In the parametric form, the representation is done by a set of functions. A curve
may be represented by
where x, y, z are co-ordinates of the points on the curve which are functions of
some parameter u and the parametric variable is constrained in the interval. For
example, a point (x, y) is located at an angle Ë from +X axis on a circle with centre
at (0, 0) and radius = 1 can be described in parametric form.
whereË is the parameter. Surfaces are described similarly for which x, y and z are functions
two independent parameters u and v. Parametric design is very popular in computer aided
design for a variety of reasons, which are listed below:
• Separation of variables
• Each variable is treated alike
• More degrees of freedom/control
• Parametric equations can be transformed directly
• Infinite slopes can be handled without computational breakdown
• Easy to express as vectors
• Amenable to plotting and digitizing
• Inherently bounded
DESIGN OF CURVED SHAPES
Design of curved shapes should satisfy the following requirements:
i. It should be possible to represent the shape mathematically.
ii. The modeling should involve minimum computation.
iii. It should be possible to generate a CNC program to machine the surfaces (2, 3, 4
and 5 axis machining) or to prepare a mould or die to make the part (as in plastic
injection molding or casting or automobile panel pressing).
A component can be designed using the curves and shapes which can be mathematically described
e.g. arc, circle, conics, ellipsoid, hyperbolic paraboloid, sphere, and cone, cylinder, linear, conical -
and circular swept surfaces etc. However very often the designer starts
with specifying a few points which roughly describe the shape.
Two approaches are available to designers to model curves and surfaces in such cases:
interpolation and approximation. The interpolation essentially tries to pass a curve on a
surface called interpolant through all these points. Approximation tries to fit a smoother
curve on surface which may be close to these points but may not actually pass through each
of them. Fig. 6.27 illustrates the difference between interpolation (a) and approximation (b).

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Figure 2 interpolation and approximation
One of the popular methods of interpolation is to use the Lagrange polynomial, which is
the unique polynomial of degree n passing through n + 1 points. However, Lagrange
polynomial is unsuitable in modeling of curves because of:
i. Large number of computations involved and
ii. Tendency for the curve to oscillate between data points when the data points
are large.
Another approach is to look for a polynomial of fewer degrees than W passing through these
W + 1 data points. This is done by combining polynomials of lesser degree passing through
several consecutive data points and smoothly piecing several such curve segments together by
blending. In general, the modeling of curves is done to satisfy the following:
i. Axis independence
ii. Global and local control
iii. Smoothness of curves
iv. Versatility
v. Continuity between adjoining segments of curve.
CUBIC SPLINES
Splines are functions that are used for fitting a curve through a number of data points. A
cubic spline has the property that the three co-ordinate functions x (u), y (u), and z (u)
are each cubic polynomials in the variable u:
Whereas parametric curves are generally considered to be defined over an infinite range
of parameter values of u, it is always necessary to limit these to a finite interval
when modeling shapes on a computer. The domain u is, therefore taken as 0 < u < = 1
in the discussion that follows:
A spline passes through two end points and satisfies differentiality condition at these
end points. These four conditions require a polynomial degree of at least 3. The derivations
of cubic splines for x, y and z are similar. The difference will be only in the end point
coordinates and derivatives at the end points. Therefore only the derivation of x(u) is
considered here.

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Curves are defined by interpolating points and tangents at these points. The parametric
cubic curve can be designed using the four vectors P(0), P(1), P’(0) and P’(1). Each one
of these vectors has three components.

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F1 , F2 , F3 , F4 , are called blending function or Hermite polynomial basis functions. B is
the matrix of geometric coefficients. F is the blending function matrix. The blending function
matrix F can be written as the product of two matrices.
Figure 3 cubi spline

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BEZIER CURVES
Bezier curves, developed by P.Bezier at Ranault Automobile Company and P. de Casteljau
atCitreon, France are used for curve and surface design of automobile panels. A Bezier curve
is blended at the joints and is completely defined by four consecutive points (X0, Y0),
(X1,y1), (X2,Y2), (X3,Y3). The curve passes only through the first and fourth point. The two
intermediate points are used to define the slope of the curve at the end points. If X0, X1, X2
and X3 are the X- co-ordinates of the control points, it is assumed that :
i. The curve passes through the end points X0 and X3
ii. The slope at the points are:
X’(0) = 3(X1 – X0)
The advantages of Bezier curve over cubic spline is that the direction of the curve at the joints
can be defined and changed simply by specifying the position of the second and third data
points. Changing a control point not only affects the shape of the curve near the control point
but has an influence throughout the curve. This lack of local control is a major weakness of
Bezier curve. Fig. 6.29 shows Bezier cubic segments for two sets of values of X.
The Bezier cubic segment discussed above is a special case of the more general
Bezier polynomial curve segment

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β-SPLINES
When the control points are distinct, this curve is continuous in slope and in curvature
between successive segments but it does not pass through any of the intermediate control
points. The cubic ‚-spline has the advantage that the control points may be moved
without affecting slope and curvature continuity and only four spans of the overall curve
will be affected by the change. Moreover, by allowing two control points to coincide it is
possible to create a curvature discontinuity. A slope discontinuity, similarly, can be
introduced by choosing three successive control points to be coincident.
It is possible to represent complex curve shapes by considering composite curves
constructed from individual segments, in the case of cubic spline, Bezier and B-
spline techniques.

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RATIONAL β SPLINE
Wiassociated with each control point is called a weight and can be viewed as an extra
shape parameter. Wi affects the curve only locally and can be interpreted geometrically
as a coupling factor. The curve is pulled towards a control point if W increases.
REPRESENTATION OF SURFACES
PARAMETRIC DESIGN OF SURFACES
Parametric surfaces may be defined in one of the following methods:
i. In terms of points of data (positions, tangents, normals)
ii. In terms of data on a number of space curves lying in these surfaces.
The resulting surface will either interpolate or approximate the data. Surfaces are normally
designed in patches, each patch corresponding to a rectangular domain in u-v

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space. A surface patch defined in terms of point data will usually be based on a
rectangular array of data points which may be regarded as defining a series of curves in
one parameter direction which in turn are interpolated or approximated in the direction of
the other parameter to generate the surface. Fig.shows the parameter curves on a surface
patch defined by a rectangular array of data points.
FIGUR:A Surface Patch
BICUBIC SURFAE PATCHES

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BEZIER BICUBIC SURFACE PATCHES
A BIUBIC SURFACE PATCHES

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CUBIC B-SPLINE SURFACES
The basis function for a cubic B-spline surface is the same as that of cubic B-spline
curve. As in the case of B-spline curve, none of the control points forming the
characteristic polyhedron lies on the surface.
Composite surfaces can be obtained by combining several surface patches. Table 6.1
gives the properties of the surfaces generated by the common methods.

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UNIT III VISUAL REALISM 9
Hidden – Line-Surface-Solid removal algorithms – shading – colouring – computer animation.
Visual Realism
3.1. Introduction
Visual Realism is a method for interpreting picture data fed into a computer and for creating
pictures from difficult multidimensional data sets. Visualization can be classified as :
tion in scientific computing.
Visualization in geometric modeling is helpful in finding connection in the design applications. By
shading the parts with various shadows, colors and transparency, the designer can recognize undesired
unknown interferences. In the design of complex surfaces shading with different texture
characteristics can use to find any undesired quick modifications in surface changes.
Visualization in computing is viewed as a technique of geometric modeling. It changes the data in
numerical form into picture display, allowing users to view their simulations and computations.
Visualization offers a process of seeing the hidden. Visualization in scientific computing is of
great interest to engineers during the design process.
Existing visualization methods are:
lel projections

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Hidden line and surface removal methods remove the uncertainty of the displays of 3D models and is
accepted the first step towards visual realism. Shaded images can only be created for surface and solid
models. In multiple step shading process, the first step is removing the hidden surfaces / solids and second
step is shades the visible area only. Shaded images provide the maximum level of visualization.
The processes of hidden removal need huge amounts of computing times and also upper end hardware
services. The creation and maintenance of such a models are become complex. Hence, creating real time
images needs higher end computers with the shading algorithms embedded into the hardware.
3.2. Hidden line removal
Hidden line removal (HLR) is the method of computing which edges are not hidden by the faces of
parts for a specified view and the display of parts in the projection of a model into a 2D plane. Hidden
line removal is utilized by a CAD to display the visual lines. It is considered that information openly
exists to define a 2D wireframe model as well as the 3D topological information. Typically, the best
algorithm is required for viewing this information from an available part representation.
3D parts are simply manufactured and frequently happen in a CAD design of such a part. In addition,
the degrees of freedom are adequate to show the majority of models and are not overwhelming in
the number of constraints to be forced. Also, almost all the surface-surface intersections and shadow
computations can be calculated analytically which results in significant savings in the number of
computations over numerical methods.
3.2.1. Priority algorithm
Priority algorithm is basis on organization all the polygons in the view according to the biggest Z-
coordinate value of each. If a face intersects more than one face, other visibility tests besides the
Z-depth required to solve any issue. This step comprises purposes of wrapper.
Imagines that objects are modeled with lines and lines are generated where surfaces join. If only
the visible surfaces are created then the invisible lines are automatically removed

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Face Priority
ABCE 1
ADFG 1
DCEF 1
ABHG 2
EFGH 2
BCEH 2
ABCD, ADFG, DCEF are given higher priority-1. Hence, all lines in this faces are visible, that is, AB, BC,
CD, DA, AD, DF, FG, AG, DC, CE, EF and DF are visible.
AGHB, EFGH, BCEH are given lower priority-2. Hence, all lines in this faces other than priority-1 are
invisible, that is BH, EH and GH. These lines must be eliminated.
3.3. Hidden surface removal
The hidden surface removal is the procedure used to find which surfaces are not visible from a certain
view. A hidden surface removal algorithm is a solution to the visibility issue, which was one of the first key
issues in the field of three dimensional graphics. The procedure of hidden surface identification is called as
hiding, and such an algorithm is called a ‘hider’. Hidden surface identification is essential to render a 3D
image properly, so that one cannot see through walls in virtual reality.
Hidden surface identification is a method by which surfaces which should not be visible to the user are
prohibited from being rendered. In spite of benefits in hardware potential there is still a requirement
for difficult rendering algorithms. The accountability of a rendering engine is to permit for bigger world
spaces and as the world’s size approaches infinity the rendering engine should not slow
down but maintain at constant speed.
There are many methods for hidden surface identification. They are basically a work out in sorting, and
generally vary in the order in which the sort is executed and how the problem is subdivided. Sorting
more values of graphics primitives is generally done by divide.
3.3.1. Z - buffer algorithm
Fig.3.3. Z- buffer algorithm
In Z-buffering, the depth of ‘Z’ value is verified against available depth value. If the present pixel is
behind the pixel in the Z-buffer, the pixel is eliminated, or else it is shaded and its depth value changes

44. 44
the one in the Z-buffer. Z-buffering helps dynamic visuals easily, and is presently introduced effectively
in graphics hardware.
Depth buffering is one of the easiest hidden surface algorithms
It keeps follow of the space to nearest object at every pixel position.
Initialized to most negative z value.
when image being drawn, if its z coordinate at a position is higher than z buffer value, it is drawn,
and new z coordinate value is stored; or else, it is not drawn
If a line in three dimensional is being drawn, then the middle z values are interpolated:
linear interpolation for polygons, and can calculate z for more difficult surfaces.
Algorithm:
loop on y;
loop on x;
zbuf[x,y] = infinity;
loop on objects
{
loop on y within y range of this object
{
loop on x within x range of this scan line of this object
{
if z(x,y) < zbuf[x,y] compute z of this object at this pixel & test zbuf[x,y] = z(x,y) update z-buffer
image[x,y] = shade(x,y) update image (typically RGB)
}
}
}
Basic operations:
1. compute y range of an object
2. compute x range of a given scan line of an object

45. 45
3. Calculate intersection point of a object with ray through pixel position (x,y).
3.3.2. Painter’s algorithm
The painter's algorithm is called as a priority fill, is one of the easiest results to the visibility issue in three
dimensional graphics. When projecting a 3D view onto a 2D screen, it is essential at various points to be
finalized which polygons are visible, and which polygons are hidden.
The ‘painter's algorithm’ shows to the method employed by most of the painters of painting remote
parts of a scene before parts which are close thereby hiding some areas of distant parts. The painter's
algorithm arranges all the polygons in a view by their depth and then paints them in this order, extreme
to closest. It will paint over the existing parts that are usually not visible hence solving the visibility issue
at the cost of having painted invisible areas of distant objects. The ordering used by the algorithm is
referred a 'depth order', and does not have to respect the distances to the parts of the scene: the
important characteristics of this ordering is, somewhat, that if one object has ambiguous part of
another then the first object is painted after the object that it is ambiguous. Thus, a suitable ordering
can be explained as a topological ordering of a directed acyclic graph showing between objects.
Algorithm:
sort objects by depth, splitting if necessary to handle intersections;
loop on objects (drawing from back to front)
{
loop on y within y range of this object
{
loop on x within x range of this scan line of this object
{
image[x,y] = shade(x,y);
}
}
}
Basic operations:
1. compute ‘y’ range of an object
2. compute ‘x’ range of a given scan line of an object

46. 46
3. compute intersection point of a given object with ray via pixel point (x,y).
4. evaluate depth of two objects, determine if A is in front of B, or B is in front of A, if they don’t
overlap in xy, or if they intersect
5. divide one object by another object
Advantage of painter's algorithm is the inner loops are quite easy and limitation is sorting operation.
3.3.3. Warnock algorithm
The Warnock algorithm is a hidden surface algorithm developed by John Warnock that is classically
used in the area of graphics. It explains the issues of rendering a difficult image by recursive subdivision
of a view until regions are attained that is trivial to evaluate. Similarly, if the view is simple to compute
effectively then it is rendered; else it is split into tiny parts which are likewise evaluated for simplicity.
This is a algorithm with run-time of O(np), where p is the number of pixels in the viewport and n is the
number of polygons.
The inputs for Warnock algorithm are detail of polygons and a viewport. The good case is that if the detail
of polygons is very simple then creates the polygons in the viewport. The continuous step is to divide the
viewport into four equally sized quadrants and to recursively identify the algorithm for each
quadrant, with a polygon list changed such that it contains polygons that are detectable in
that quadrant.
1. Initialize the region.
2. Generate list of polygons by sorting them with their z values.
3. Remove polygons which are outside the area.
4. Identify relationship of each polygon.
5. Execute visibility decision analysis:
a) Fill area with background color if all polygons are disjoint,
b) Fill entire area with background color and fill part of polygon contained in area with color of
polygon if there is only one contained polygon,
c) If there is a single surrounding polygon but not contained then fill area with color of
surrounding polygon.
d) Set pixel to the color of polygon which is closer to view if region of the pixel (x,y) and if neither of
(a) to (d) applies calculate z- coordinate at pixel (x,y) of polygons.
6. If none of above is correct then subdivide the area and Go to Step 2.

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3.4. Hidden Solid Removal
The hidden solid removal issue involves the view of solid models with hidden line or surface eliminated.
Available hidden line algorithm and hidden surface algorithms are useable to hidden solid elimination
of B-rep models.
The following techniques to display CSG models:
1. Transfer the CSG model into a boundary model.
2. Use a spatial subdivision strategy.
3. Based on ray sorting.
3.4.1. Ray-Tracing algorithm
A ray tracing is a method for creating an image by tracing the path of light via pixels in an image plane
and reproducing the effects of its meets with virtual objects. The procedure is capable of creating a
high degree of visual realism, generally higher than that of usual scan line techniques, but at a better
computational. This creates ray tracing excellent suited for uses where the image can be rendered
gradually ahead of time, similar to still images and film and TV visual effects, and more badly suited for
real time environment like video games where speed is very important. Ray tracing is simulating a wide
range of optical effects, such as scattering, reflection and refraction.
Ray-Tracing algorithm
For every pixel in image
{
Generate ray from eye point passing via this pixel
Initialize Nearest ‘T’ to ‘INFINITY’
Initialize Nearest Object to NULL For each object in scene
{
If ray intersects this image
{
If t of intersection is less than Nearest T
{
Set Nearest T to t of the intersection
Set Nearest image to this object

48. 48
}
}
}
If Nearest image is NULL
{
Paint this pixel with background color
}
Else
}
{
Shoot a ray to every light source to check if in shadow
If surface is reflective, generate reflection ray
If transparent, generate refraction ray
Apply Nearest Object and Nearest T to execute shading function
Paint this pixel with color result of shading function
}
Optical ray tracing explains a technique for creating visual images constructed in three dimensional
graphics environments, with higher photorealism than either ray casting rendering practices. It
executes by tracing a path from an imaginary eye via every pixel in a virtual display, and computing the
color of the object visible via it.
Displays in ray tracing are explained mathematically by a programmer. Displays may also
incorporate data from 3D models and images captured like a digital photography.
In general, every ray must be tested for intersection with a few subsets of all the objects in the view.
Once the nearest object has been selected, the algorithm will calculate the receiving light at the point
of intersection, study the material properties of the object, and join this information to compute the
finishing color of the pixel. One of the major limitations of algorithm, the reflective or translucent
materials may need additional rays to be re-cast into the scene.
Advantages of Ray tracing:

49. 49
1. A realistic simulation of lighting over other rendering.
2. An effect such as reflections and shadows is easy and effective.
3. Simple to implement yet yielding impressive visual results.
Limitation of ray tracing:
Scan line algorithms use data consistency to divide computations between pixels, while ray tracing
normally begins the process a new, treating every eye ray separately.
3.5. Shading
Shading defines to describe depth perception in three dimensioning models by different levels of
darkness. Shading is applied in drawing for describes levels of darkness on paper by adding media
heavy densely shade for darker regions, and less densely for lighter regions.
There are different techniques of shading with cross hatching where perpendicular lines of changing
closeness are drawn in a grid pattern to shade an object. The closer the lines are combining, the
darker the area appears. Similarly, the farther apart the lines are, the lighter the area shows.
3.5.1. Shading techniques:
In computer graphics, shading submits to the procedure of changing the color of an object in the
3D view, a photorealistic effect to be based on its angle to lights and its distance from lights. Shading is
performed through the rendering procedure by a program called a ‘Shader’. Flat shading and Smooth
shading are the two major techniques using in Computer graphics.

50. 50
UNIT IV ASSEMBLY OF PARTS 9
Assembly modelling – interferences of positions and orientation – tolerance analysis-
massproperty calculations – mechanism simulation and interference checking.
Assembly of parts
4.1. Introduction
In today’s global situation, two main things are significant for the industry: cost reduction and
environment protection. Since the late 70’s it has been developed that the assembly procedure
normally signify one third of the product cost. Hence, it is essential to design appropriate plans for
parts assembly: manufacturing, and disassembly: recycling.
A realistic assembly procedure can increase efficiency, cost reduction and improve the recycling of
product. To overcome these problems, various simulations based on digital mock-ups of products are
required. Even though modeling and analysis software, presently applied at various stages of the
Product Development Process, can suggest results to several of the above stated needs, the progress
of a committed assembly and disassembly combine simulation stage is still a need.
To attain an optimum assembly method, various complex software for assembly analysis and, as well
as simulation programs based on multi agent methods or which apply contact data between
assembly components, were created. Newly, Virtual Reality (VR) has broadly developed towards
Assembly realistic simulation.
As the contact between objects is at the basis of the assembly simulations need 3D objects shapes, the
contact detection is addressed here as the first step in the Assembly simulation process. The equivalent
procedure establishes links between shapes, contact mock-ups and component kinematics, which gives
a basic set of meaningful data
All mechanical parts are applying one of the common CAD modelers. Thus, the existing assembly
modules of 3D CAD software and their definite method to modeling assemblies have a tough influence
on how products are calculated. Also, for the realistic simulation, the data exchange CAD to Virtual
Reality is one of the significant problems presently faced by the virtual prototyping community.
4.2. Assembly modeling
Assembly modeling is a technique applied by CAD and product visualization software systems to
utilize multiple files that shows components within a product. The components within an assembly
are called as solid / surface models.

51. 51
The designer usually has approach to models that others are functioning on concurrently. For example,
different people may be creating one machine that has different components. New parts are extra to an
assembly model as they are generated. Every designer has approach to the assembly model, during a
work in progress, and while working in their own components. The design development is noticeable to
everyone participated. Based on the system, it might be essential for
the users to obtain the most recent versions saved of every individual component to update the
assembly.
The personal data files defining the 3D geometry of personal components are assembled together via a
number of sub assembly levels to generate an assembly explaining the complete product. Every CAD
methods support the bottom-up construction. A few systems, through associative copying of geometry
between components allow top-down construction. Components can be situated within the assembly
applying absolute coordinate position methods.
Mating conditions are defines of the relative location of mechanism between each other; for example
axis position of two holes or distance between two faces. The final place of all objects based on these
relationships is computing using a geometry constraint engine built into the CAD package.
The significance of assembly modeling in obtaining the full advantages of Product Life-cycle
Management has directed to ongoing benefits in this technology. These contain the benefit of
lightweight data structures that accept visualization of and interaction with huge amounts of data
related to product, interface between PDM systems and active digital mock up method that combine
the skill to
visualize the assembly mock up with the skill to design and redesign with measure, analyze and
simulate.
4.2.1. Assembly Concepts
When components are additional to an assembly, parent and child relationships are created. These
relationships are displayed by graphically as an assembly tree. Parts are parametrically connected by
position constraints. These constraints have data about how a part should be placed within the
assembly hierarchy and how it should respond if other components are edited.
Functioning within the framework of an assembly is prepared easier by accepting to apply more
commands to other parts and sub-assemblies. These contain the Annotation Text, Inquire, Point,
Datum Plane and Pattern Component commands. Bigger assembly performance is improved by
removing unwanted redraws and improved display management while zooming.
Assembly models have additional data than simply the sum of their components. With assembly
modeling interference verifies between parts and assembly specific data such as mass properties.
Fig.4.1. Assembly of parts
4.2.2. Bottom up Assembly design

52. 52
In a ‘bottom up’ assembly design, complex assemblies are divided into minor subassemblies and
parts. Every part is considered as individual part by one or more designers. The parts can be archived
in a library in one or more 3D Files. This is the high effective way to generate and manage complex
assemblies.
Every part is included into the active part making a component request and thus an assembly. The
component will be the child of the active part and then it will be the active part. Hence an instance of
the actual part is applied; it revises automatically if the archived part is edited by activating.
Bottom up Hierarchy:
The ‘bottom up’ assembly design hierarchy of the basic assembly is shown in figure 4.2. All the parts
exist prior to Part1. When Part1 is generated, it becomes the active. It would utilize the menu
sequence to add Bracket and it becomes the active part.
Insert > Component
Or
Assembly Design Tool Bar >
As per example shown in figure 4.2., ‘Bracket’ is a child of Part1. The dashed line represents that
‘Bracket’ exists in the 3D file Parts Z3. The dotted line represents that ‘Bracket’ is inserted into Part-1.
After Bracket is added, Part1 is redefined. Bolt and Washer are then added the same
process and Part-1 is reactivated again.
Fig.4.2. Bottom up Design – Part 1
Module of subassembly is added similar as ‘Bracket’, ‘Bolt’, and ‘Washer’ again becoming a child of
Part-1. But, because Module Subassembly already has the two items Seal and Module, they are added
and continue as its children.
Sequence of operations (Fig. 4.2.):
-1 has 1 part.
-1 has 4 components.
-1 is eliminated from the active assembly before it is saved and Part1 are removed. The original
parts placed in the file Parts Z3 are not changed.
-1 is saved and Part1 is also saved.

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-1 is erased and Part1 is also erased.
4.2.3. Top down Assembly Design
In a ‘top down’ assembly design all parts are classically designed by the similar person within a
single part. 3D assembly handles ‘top down’ method by allowing to design and creation of a
component while work in the active part. Hence, the active part will be an assembly part.
The part becomes a child of the active part and then it will be the active part. The part, when
generated, is an instance of a base part which will be a root object located in the active file. Every
part is activated and modified as needed. The ‘top down’ assembly design has its benefits. If the
project is terminated or to go in a different new direction, removing the file will remove the part
and all of its
components.
Top down Hierarchy
The ‘top down’ assembly method is shown in a figure 4.3 and one of the components exist prior
to Part-1. When Part-1 is generated, it will be the active part. The following command sequence
to generate Bracket and create it the active part.
Assembly Design Tool Bar >
Fig.4.3. Top down Design – Part 1
Bracket is a child of Part-1. The dashed line illustrates that by default when Bracket is generated; it
is attached to File-1. The dotted line illustrates that Bracket is attached into Part-1. When Bracket
is executed Part1 is reactivated. Bolt and Washer are then generated using the similar
process and Part-1 is reactivated again.
Subassembly Module is generated like the Bracket, Bolt, and Washer again will be a child of
Part1. But, Module Subassembly remains active when seal is developed. Seal will be the active
part and by default also exists in File-1 but is inserted into Module Subassembly hence it was
active at the
time of seal was created. Subassembly Module is then reactivated and Module is generated
like a Seal.
Sequence of operations (Fig 4.3):
-1 has 7.
-1 contains 4 components, which are illustrations of the basic parts located in File-1.

54. 54
File-1.
-1 is saved it has all of its original parts.
-1 is erased, it and all of its basic parts are erased.
4.3. Interference of position and orientation
Designers and manufacturers should check jointly that a provided product can be assembled,
without interference between parts, before the product to be manufactured. Similarly, all the CAD
tools presently have the potential to directly analyze the possibility of a specified assembly plan for
a product.
An assessment of previous assembly sequence and optimization research explains that most
previous assembly planners apply either feature-mating or interference-free techniques to find
assembly part interference interaction. In both feature-mating and interference-free techniques
focused upon the basic geometrical data and restrictions for the designed product, which are
generally contained in connected CAD files.
When completely automate the procedure of creating a professional assembly plan, geometrical
information for CAD models should be automatically taken from CAD files, analyzed for
interference relationships between components in the assembly, and then designed for utilized
the assembly analysis tools. Most of the previous assembly sequence planners do not have the
potential to complete the three tasks; they need users to manually input part attributes or
interference data, which is so time-consuming.
4.3.1. Determining Interference Relationships between Parts
In automated assembly schemes, most parts are assembled along with the principal axis. Hence,
to fine interference between parts while assembly, the projected technique referred six assembly
directions along with the principal assembly axis: +x, -x, +y, -y, +z, and -z. But, the method could
be improved, to think other assembly directions, as required. The projected system uses
projection of part coordinates onto planes in three principal axis (x, y ,z) to find the obstruction
between parts sliding along some of the six principal assembly axis. The projections overlap
between any two parts in a specified axis direction shows a potential interference between the
two parts, when one of the two parts slides along the specified direction, with respect to the
other. Vertex coordinates for overlapped
projections are then evaluated to find if real collisions would happen between parts with
overlapped projections. The planned process stores the determined interference data for allocated
assembly direction in a group of interference free matrices, for compatibility with previous
planners of assembly.

55. 55
The swept volume interference and the multiple interference detection systems are appropriate for
three-dimensional interference determination between B-REP entities. But, both techniques were
developed for real-time interference detection between two moving parts in a simulation
environment. As a result, these two techniques are expensive in computationally. For the assembly
planning issue, actual collision finding capacity along subjective relative motion vectors is not
require.
Instead, a efficient computational technique is required for finding if two parts will collide when
they are assembled in a specified order along any one of the six principle assembly axis.
4.2.3. Interference-free matrix
An interference-free matrix shows interference between two components, when one component is
moved, in a given assembly direction, into an assembled location, with another component already
in an assembled location. Assembly actions that result in interferences are denoted as ‘0’ in the
matrix, and assembly actions that do not result in interferences are denoted as ‘1’ in the matrix.
As shown in figure 4.4., the interference-free matrix of an assembly having three parts, for
assembly movement sliding from infinity of negative toward infinity of positive along the +x
direction is as follows:
Fig.4.4. Interference of three parts
Interference-free matrix for sliding in the +x direction:
The row in the Interference-free matrix indicate the components being shifted during a given
assembly operation, and the column indicate the parts that have previously been assembled.
Hence, since matrix element (2, 1) is equal to ‘0’, if Part-1 is assembled initially, and after that
Part-2 is assembled in the direction of +x, Part-2 will collide with Part-1. Similarly, matrix element
(1, 2) is equal to ‘1’, if Part-2 is assembled initially, and then Part-1 is assembled in the direction of
+x, Part-1 will not collide with Part-2. As a part cannot be assembled after itself, all elements in
the diagonal matrix are set to ‘0’. As a whole, six matrices are utilized to show interference
relationships between parts in the six principal axes. When robotically creating interference-free
matrices, the projected algorithm finds matrix elements row by row. When two parts would
interfere through assembly in a given direction, the program inserts a ‘0’ in the corresponding
matrix position; or inserts as a ‘1’.
4.4. Geometric Tolerance
The function of geometric tolerance is to explain the engineering objective of components and
assemblies. The datum reference frame can explain how the part. Tolerance can accurately define
the dimensional needs for a part, permitting over 50% more tolerance than coordinate

56. 56
dimensioning in a few cases. Suitable purpose of tolerance will confirm that the part described on
the drawing has the preferred form, fit and purpose with the highest possible tolerances (Fig.4.5).
Fig.4.5. Geometric Tolerance
4.3.1. Fundamental rules for Geometric Tolerance
1. All dimensions should have a tolerance. Each attribute on every manufactured
component is subject to change; hence, the limits of acceptable difference must be
defined. Plus and minus tolerances may be used to dimensions from a common tolerance
block.
2. Dimensions describe the geometry and allowable change. Measurement and scaling of the
drawing is not permitted excluding in certain cases.
3. Engineering drawings describe the necessities of completed parts. Each dimension and
tolerance needed to define the completed part shall be shown on the drawing. If extra
dimensions would be useful, but are not necessary, they may be noted as reference.
4. Dimensions should be used to attributes and arranged in such a way as to show the purpose of
the features. In addition, dimensions should not be subject to more than one explanation.
5. Descriptions of manufacturing systems should be avoided. The geometry should be
explained without defining the technique of manufacture.
6. If some sizes are needed during manufacturing but are not wanted in the final geometry
they should be noticeable as non-mandatory.
7. All dimensioning and tolerance should be placed for utmost readability and should be used
to visible lines in true profiles.
8. When geometry is usually restricted by code, the dimension(s) shall be integrated with
code number in comments below the dimension.
9. If not openly declared, all dimensions and tolerances are only suitable when the item is in free.
10.Dimensions and tolerances indicate to the full length, width, and depth.
4.3.2. Tolerance Symbols
Symbols for tolerances are bilateral unless otherwise defined. For example, the location of a hole
has a tolerance of .020mm. This indicates that the hole can move +/- .010 mm, which is an equal
bilateral tolerance. It does not consider that the hole can move +.015/-.005 mm, which is an
unequal bilateral tolerance.
4.5. Tolerance Analysis

57. 57
Fig.4.6. Symbols for Geometric Tolerance
Tolerance analysis is a title to a different approaches applied in product design to know how
deficiencies in parts as they are manufactured, and in assemblies, influence the ability of a product
to meet customer needs. Tolerance analysis is a way of accepting how basis of deviation in part
dimensions and assembly constraints distribute across parts and assemblies, and how that total
deviation affects the ability of a drawing to reach its design necessities within the process
capabilities of organizations and supply chains.
Tolerance openly affects the cost and performance of products. In electrical machines, safety
needs that the power supply to be situated a minimum gap from adjacent components, such as
one more sheet-metal component, in order to remove electrical short circuits. Tolerance analysis
will describe whether the small clearances specified will meet the safety requirement, assigned
manufacturing and assembly variability force on the minimum clearance.
4.5.1. Tolerance stack-up
Tolerance stack-up computations show the collective effect of part tolerance with respect to an
assembly need. The tolerances ‘stacking up’ would describe to adding tolerances to obtain total
part tolerance, then evaluating that to the existing gap in order to see if the design will work
suitably. This simple evaluation is also defined as ‘worst case analyses’. Worst case analysis is
suitable for definite needs where failure would signify failure for a company. It is also needful and
suitable for problems that occupy a low number of parts. Worst case analysis is always carried out
in a single direction that is a 1- D analysis. If the analysis has part dimensions that are not parallel
to the assembly measurement being defined, the stack-up approach must be edited since 2D
variation such as angles, or any variation that is not parallel with the 1-D direction, does not
influence the measurement of assembly with a 1-to-1 ratio.
The tolerance stacking issue occurs in the perception of assemblies from interchangeable parts
because of the inability to create or join parts accurately according to nominal. Either the
applicable part dimension changes around various nominal value from part by part or it is the act of
assembly that directs to variation. For example, as two parts are combined through matching holes
pair there is not only variation in the location of the holes relative to nominal centers on the parts
but also the slippage difference of matching holes relative to each other when safe.
Thus there is the opportunity that the assembly of such interacting parts will not move or won’t
come closer as planned. This can generally be judged by different assembly criteria, say G1, G2,...
Here we will be discussed with just one assembly criterion, say G, which can be noted as a function
of the part dimensions L1,...,Ln. A example is shown in Figure 4.7., where n = 6 and is the clearance
gap of interest. It finds whether the stack of cogwheels will locate within the case or not. Thus it is
preferred to have G > 0, but for performance of functional causes one may also require to limit G.

58. 58
G = L1 − (L2 + L3 + L4 + L5 + L6)
= L1 − L2 − L3 − L4 − L5 − L6
Fig.4.7. Tolerance Stack-up
As per the example, the required lengths ‘Li ‘may vary from the nominal lengths ‘λi’ by a small
value. If there is higher variation in the ‘Li’ there may well be important problems in accepting G >
0. Thus it is sensible to limit these changes via tolerances. For similar tolerances, ‘Ti’, represent an
‘upper limit’ on the absolute variation between actual and nominal values of the i th detail part
dimension, it is means that |Li − λi| ≤ Ti. It is mostly in the interpreta on of this last inequality that
the different methods of tolerance stacking vary.
The nominal value ‘γ’of G is typically computed by replacing in equa on L1 − L2 − L3 − L4 − L5 − L6,
the actual values of Li’s by the corresponding nominal values of λi, that is γ = λ1 − λ2 − λ3 − λ4 − λ5
− λ6 .
4.5.2. Statistical method for tolerance analysis (RSS) :
In RSS method, tolerance stacking a significant new element is added to the assumptions,
specifically which the detail differences from nominal are random and independent from part by
part. It is expensive in the sense that it frequently commanded very close tolerances. That all
variations from nominal should dispose themselves in worst case method to defer the higher
assembly tolerance is a relatively unlikely proposition. On the other hand, it had the advantage of
assurance the resulting assembly tolerance. Statistical tolerance in its typical form operates under
two basic hypotheses:
As per Centered Normal Distribution, somewhat considering that the ‘Li’ can occur anywhere
within the tolerance distribu on [λi − Ti, λi + Ti], assume that the ‘Li’ are normal random variables,
that is change randomly according to a normal distribution, centered on that similar interval and
with a ±3σ distribute equal to the span of that interval, hence 99.73% of all ‘Li’ values occur within
this gap. As per the normal distribution is such that the ‘Li’ fall with upper frequency in the middle
near ‘λi’ and with low frequency closer the interval endpoints. The match of the ±3σ distribution
with the span of the detail tolerance span is hypothetical to state that almost all parts will satisfy
the detail tolerance limits as
shown in figure 4.8.
Fig.4.8. Centered Normal Distribution
Statistical tolerance stacking formula is given below:
Where, ai = ±1 for all i = 1,...,n.

59. 59
Fig.4.9. RSS cube
Typically Tstat assy is considerably smaller than T arith assy. For n=3, the scale of this variation is
simply visualized and valued by a rectangular box with side lengths T1, T2 and T3. To obtain from
one corner of the box to the diagonally opposite corner, one can cross the gap T21 + T22 + T23
along that diagonal and follow the three edges with lengths T1, T2, and T3 for a total length T arith
assy = T1 + T2 + T3 as shown in figure 4.9.
4.5.3. Second Order Tolerance Analysis
Due to the manufacturing methods changing for various types of components, the distribution
moments vary as well. RSS only applies standard deviation and does not contain the upper
moments of skewness and kurtosis that describe the effects tool wear, form aging and other
classical manufacturing situations. Second Order Tolerance Analysis includes all types of
distribution moments as shown in figure 4.9

60. 60
Fig.4.9. Second order Tolerance Analysis
Second Order Tolerance Analysis is required to find what output is going to be when the assembly
function is not linear. In classical mechanical engineering developments kinematic changes and
other assembly performances result in non-linear assembly operations. Second order estimates are
more complex so manual calculations are not suitable but the computation is greatly improved and
becomes feasible within tolerance analysis software.
4.5.4. Importance of Tolerance Analysis
With smaller product lifecycles, quicker to market, and higher cost pressures, the uniqueness that
distinguishes a product from its competitors. Engineers are moving to the next order of resolution
in order to improve cycle time and quality and to reduce costs. They are showing nearer at why
they did not get the correct part and assembly dimension values they needed from manufacturing
and then are trying to optimize the tolerances on the following version of the product. Optimization
of tolerance during design has a high impact on the output of manufacturing, and better yields
direct impact on product cost and quality. Tolerance Analysis before trying to manufacture a
product helps engineers avoid time taking iterations later in the design cycle.
The electronics industry is attaining customer satisfaction purposes via a physical shrinking of
their components while adding more capabilities. As electronic devices high densely packaged,
the significance increases to more accurately understanding the interaction of manufacturing
variation and tolerances in design. Similarly, in the aircraft, automotive and medical device
productions, liability costs are increasing while environmental needs are being more forcefully
forced such that companies requires to understand high precisely what may reason a failure.
Advantages of Tolerance Analysis
1. Accurate part assembly.
2. Elimination of assembly rework
3. Improvement in assembly quality.
4. Reduction of assembly cost.
5. High customer satisfaction.
6. Effectiveness of out-sourcing.
Limitations of Tolerance
Analysis
1. Time consuming process.

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2. Skill require for complex assemblies.
4.6.Mass property calculations
The first step in finding mass properties is to set up the location of the X, Y, and Z axis. The correctness
of the calculations will depend completely on the knowledge used in choosing the axis. Hypothetically,
these axes can be at any position relative to the object being considered, offered the axes are equally
perpendicular. But, in reality, except the axes are chosen to be at a position that can be precisely
measured and identified, the calculations are meaningless.
Fig.4.10. Accuracy of axis – Vertical
As shown in the figure 4.10, the axes do not create a best reference hence a small error in squareness
of the base of the cylinder origins the object to tilt away from the vertical axis.
Fig.4.11. Accuracy of axis – Horizontal
An axis should always pass via a surface that is firmly linked with the bulk of the component. As shown
in the figure 4.11, it would be best to position the origin (Z=0) at the end of the component
rather than the fitting that is freely dimensioned virtual to the end.

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UNIT V CAD STANDARDS
Standards for computer graphics- Graphical Kernel System (GKS) - standards for
exchange images- Open Graphics Library (OpenGL) - Data exchange standards - IGES, STEP,
CALSetc. - Communication standards.
5.1 INTRODUCTION
The heart of any CAD model is the component database. This includes the graphics
entities like points, lines, arcs, circles etc. and the co-ordinate points, which define the location of
these entities. This geometric data is used in all downstream applications of CAD, which include
finite element modeling and analysis, process planning, estimation, CNC programming, robot
programming, programming of co-ordinate measuring machines, ERP system programming and
simulation. In order to achieve at least a reasonably high level of integration between CAD,
analysis and manufacturing operations, the component database must contain:
i. Shapes of the components (based on solid models)
ii. Bill of materials (BOM), of the assembly in which the components are used.
iii. Material of the components
iv. Manufacturing, test and assembly procedures to be carried out to produce a
component so that it is capable of functioning as per the requirements of design.
In designing a data structure for CAD database the following factors are to be considered:
i. The data must be neutral
ii. The data structure must be user-friendly
iii. The data must be portable.
In order to achieve the above requirements, some type of standardization has to be followed by
the CAD software designers. The basic elements associated with a CAD system are:
• Operator (user)
• Graphics support system
• Other user interface support system
• Application functions
• Database

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Fig. 5.1 CAD System
The reasons for evolving a graphic standard thus include:
• Need for exchanging graphic data between different computer systems.
• Need for a clear distinction between modeling and reviewing aspects.
5.2 STANDARDS FOR GRAPHICS PROGRAMMING
Attempts to develop a graphics standard resulted in the following developments in 70’s:
i. A Graphic Standards Planning Committee (GSPC) was formed in 1974 by ACM-
SIGGRAPH (Association of Computing Machinery’s Special Interest Group on Graphics
and Interactive Techniques).
ii. A committee for the development of computer graphics standard was formed by DIN
in 1975.
iii. IFIP organized a workshop on Methodology in Computer Graphics in 1976.
iv. A significant development in CAD standards is the publication of Graphical Kernel
System (GKS) in 1982.
5.3 FEATURES OF GKS
GKS (Graphical Kernel System) is an ANSI and ISO standard. GKS standardizes two
dimensional graphics functionality at a relatively low level. The primary purposes of the
standard are:
• To provide for portability of graphics application programs.

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• To aid in the understanding of graphics method by application programmers.
• To provide guidelines for manufacturers in describing useful graphics capabilities.
The GKS (ANSI X3.124-1985) consists of three basic parts:
i. An informal exposition of contents of the standard, which includes such things as
positioning of text, filling of polygons etc.
ii. A formalization of the expository material outlined in (i) by way of abstracting the
ideas into functional descriptions (input/output parameters, effect of each function etc.).
iii. Language bindings, which are the implementations of the abstract functions,
described in (ii) in a specific computer language like FORTRAN, Ada or C.
Figure 5.2 shows the GKS implementation in a CAD workstation. The features of GKS include:
i. Device independence: The standard does not assume that the input or output devices
have any particular features or restrictions.
ii. Text/Annotations: All text or annotations are in a natural language like English.
iii. Display management: A complete suite of display management functions, cursor
control and other features are provided.
iv. Graphics Functions: Graphics functions are defined in 2D or 3D.
The drivers in GKS also include metafile drivers. Metafiles are devices with no graphic
capability like a disc unit. The GKS always works in a rectangular window or world coordinate
system. The window also defines a scaling factor used to map the created picture into the internal
co-ordinate system of GKS called normalized device co-ordinates. Windows and view ports can
then work in this co-ordinate system.

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Fig. 5.2 GKS Implementation in a CAD Workstation
GKS offers two routines to define the user created pictures. They are primitive functions
and attribute functions. Examples of primitive functions are:
• POLYLINE to draw a set of connected straight-line vectors
• POLYMARKER to draw a set of markers or shapes
• FILL AREA to draw a closed polygon with interior fill
• TEXT to create characters
• GDP (Generalized Drawing Primitive) to specify the standard drawing entities like
circle, ellipse etc.
The attribute functions define the appearance of the image e.g. color, line-type etc.
Current level of GKS is GKS-3D, which provides several other functions. GKS-3D is an
extension to GKS, which allows the production of 3-D objects.
5.4 OPENGL
Silicon Graphics (SGI) developed the OpenGL application-programming interface (API)
for the development of 2D and 3D graphics applications. It is a low-level vendor-neutral
software interface. It is often referred to as the assembler language of computer graphics. It
provides enormous flexibility and functionality. It is used on a variety of platforms. OpenGL is a
low-level graphics library specification. OpenGL makes available to the programmer a small set
of geometric primitives - points, lines, polygons, images, and bitmaps. OpenGL provides a set of
commands that allow the specification of geometric objects in two or three dimensions, using the
provided primitives, together with commands that control how these objects are rendered into the
frame buffer. The OpenGL API was designed for use with the C and C++ programming
languages but there are also bindings for a number of other programming languages such as Java,
Ada, and FORTRAN. OpenGL provides primitives for modelling in 3D. Its capabilities include
viewing and modelling transformation, viewport transformation, projections (orthographic and
perspective), animation, lighting etc.
5.5 EXCHANGE OF CAD DATA BETWEEN SOFTWARE PACKAGES
Necessity to translate drawings created in one drafting package to another often arises.

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For example you may have a CAD model created in PRO/E package and you may wish that this
might be transferred to I-DEAS or Unigraphics. It may also be necessary to transfer geometric
data from one software to another. This situation arises when you would want to carry out
modeling in one software, say PRO/E and analysis in software, say ANSYS. One method to meet
this need is to write direct translators from one software to another. This means that each system
developer will have to produce its own translators. This will necessitate a large number of
translators. If we have three software packages we may require six translators among them. This
is shown in Fig. 5.3.
Fig. 5.3 Direct Data Translation
A solution to this problem of direct translators is to use neutral files. These neutral files
will have standard formats and software packages can have pre-processors to convert drawing
data to neutral file and postprocessors to convert neutral file data to drawing file. Figure 5.4
illustrates how the CAD data transfer is a accomplished using neutral file. Three types of neutral
files are discussed in this chapter. They are:

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Fig. 5.4 CAD Data Exchange Using Neutral Files
i. Drawing exchange files (DXF)
ii. IGES files
iii. STEP files
5.6 INITIAL GRAPHICS EXCHANGE SPECIFICATION (IGES) GRAPHICS
STANDARD
The IGES committee was established in the year 1979. The CAD/CAM Integrated
Information Network (CIIN) of Boeing served as the preliminary basis of IGES. IGES version
1.0 was released in 1980. IGES continues to undergo revisions. IGES is a popular data exchange
standard today. Figure 5.6 shows a CAD model of a plate with a centre hole. The wire frame
model of the component is shown in Fig. 5.5. There are eight vertices (marked as PNT 0 - PNT
8), 12 edges and two circles that form the entities of the model. Table 5.1 shows the IGES output
of the wire frame model.
Fig. 5.5 Wire-frame Model of the Component

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Fig. 5.6 3-D Model of a Plate

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IGES files can also be generated for:
i. Surfaces
ii. Datum curves and points
5.7 STEP ARCHITECTURE
STEP architecture has four main components:
• EXPRESS modeling language
• Data schemes including attributes such as geometry, topology, features and tolerance.
• Aapplication interface called Standard Data Access Interface (SDAI), which is a
standard interface to enable applications to access and manipulate STEP data • STEP
database, which has the following forms:
• ASCII format file for data exchange
• Working from file, usually in binary format, that can be shared by multiple systems
• Shared database, involving object oriented database management system or relational
database system

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• Knowledge base, with a database management system as a base coupled to an expert
shell
5.8 STEP ENABLER FOR CONCURRENT ENGINEERING
STEP was released in early 1993 as a Draft International Standard (DIS). The initial
release of STEP has four basic parts. These include:
• EXPRESS modeling language
• Two application protocols
• Drafting and Configuration Control Design for three-dimensional product data.
• Six application resources.
Subsequent releases of STEP provided added functionality in terms of the kinds of
product supported and the extent of the product life cycle. While STEP is advancing towards
maturity, it had been investigated for the feasibility of incorporation into framework system.
Both STEP and Concurrent Engineering share the common goal of influencing the product cycle
from design, assembly, etc. to the disposal stages which have been realized in the CONSENS
system under ESPRIT EP6896. The object-oriented database for CONSENS has a schema with
STEP definitions alongside company specific definitions. A module called Product Information
Archive (PIA) provides functionality for STEP data access via SDAI. It is generic to be adopted
for different domains. For example it is used for product information by the Aircraft Company,
Deutshces Aerospace and electronics manufacturing company, AEG.
STEP data export in a CAD modeling package has the following options:
(i) wire frame edges
(ii) surfaces
(iii) solids
(iv) shells
(v) Datum curves and points
A typical STEP output for the wire frame model is given in Table5.2

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Table 5.2

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ACIS is another object oriented three-dimensional geometric modeling engine. It is
designed for use as the geometry foundation in a 3D modeling application. ACIS is written in
C++ and consists of a set of C++ classes and functions. A developer uses these classes and
functions to create an end user 3D application. ACIS complements existing applications by
offering a unified environment for the modeling of curves, surfaces and solids. ACIS provides a
foundation of common modeling functionality and flexibility to be adapted and extended for
particular application requirements. ACIS integrates wire frame, surface and solid modeling by
allowing these alternative representations to coexist naturally in a unified data structure, which is
implemented in a hierarchy of C++ classes. ACIS bodies can have any of these forms or
combinations of them. Linear and quadratic geometry is represented analytically and non-
uniform rational B-Splines represent free-form geometry. ACIS is a boundary-representation (B-
rep) modeler, which means that it defines the boundary between solid material and empty space.
This
boundary is made from a closed set of surfaces.
5.9ACIS ARCHITECTURE

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The ACIS has been designed using software component technology. A ‘software
component’ is a functionally specialized unit of software - a collection of software items
(functions, classes, etc.) grouped together to serve some distinct purpose. It serves as a
constituent part of a whole software system or product. A ‘product’ is one or more software
components that are assembled together and sold as a package. Components can be arranged in
different combinations to form different products
Kernel - Basic entity and attribute support, topology and geometry entity classes;
construction geometry classes Local OPS - Optional husk for locally manipulating
models Meshing - Optional husk for representing a surface as a network of polygonal
elements Sweeping - Sweep a profile along a path