This document discusses aerospace fasteners from an manufacturing perspective. It describes the types of rivets used in aircraft assembly, including solid and blind rivets. Solid rivets are used when access is available to both sides, while blind rivets are used when one side is inaccessible. The document outlines rivet identification codes and the process for installing solid rivets. Material selection and testing of aerospace fasteners is also summarized.
This presentation is an examination of structural repair of aircraft. It details the goals, regulations and classification of repairs for different types of aircraft damage.
The paper that this presentation is based on was presented by Dr. Kishore Brahma of the AXISCADES Engineering Core Group at the International Conference & Exhibition on Fatigue, Durability & Fracture Mechanics (FatigueDurabilityIndia2015) in Bangalore from 28-30th May 2015.
Aircraft Finite Element Modelling for structure analysis using Altair ProductsAltair
The Airbus airframe design process has considerably evolved since 20 years with the constant improvement of numerical simulation capability and the computational means capacity. Today the size of Finite Element Models for aircraft structural behaviour study is exceeding the boundary of airframe components (fuselage section, wing); for the A350, a very large scale non-linear model of more than 60 million degrees of freedom has been developed to secure the static test campaign. This communication will illustrate the partnership with Altair and the use of Altair products for the creation and verification of very large models at Airbus. It will deal with: - Geometry preparation - Meshing - Property assignment - Assembly - Checking More generally, numerical simulation will play more and more a major role in the aircraft process, from the development of new concepts / derivatives to the support of the in-service fleet. Then, this presentation will also state the coming needs regarding model creation tools to cope with Airbus strategy.
Speakers
Marion Touboul, Ingénieur en Simulation Numérique - Calcul Structure, Airbus Opérations SAS
This presentation is an examination of structural repair of aircraft. It details the goals, regulations and classification of repairs for different types of aircraft damage.
The paper that this presentation is based on was presented by Dr. Kishore Brahma of the AXISCADES Engineering Core Group at the International Conference & Exhibition on Fatigue, Durability & Fracture Mechanics (FatigueDurabilityIndia2015) in Bangalore from 28-30th May 2015.
Aircraft Finite Element Modelling for structure analysis using Altair ProductsAltair
The Airbus airframe design process has considerably evolved since 20 years with the constant improvement of numerical simulation capability and the computational means capacity. Today the size of Finite Element Models for aircraft structural behaviour study is exceeding the boundary of airframe components (fuselage section, wing); for the A350, a very large scale non-linear model of more than 60 million degrees of freedom has been developed to secure the static test campaign. This communication will illustrate the partnership with Altair and the use of Altair products for the creation and verification of very large models at Airbus. It will deal with: - Geometry preparation - Meshing - Property assignment - Assembly - Checking More generally, numerical simulation will play more and more a major role in the aircraft process, from the development of new concepts / derivatives to the support of the in-service fleet. Then, this presentation will also state the coming needs regarding model creation tools to cope with Airbus strategy.
Speakers
Marion Touboul, Ingénieur en Simulation Numérique - Calcul Structure, Airbus Opérations SAS
This is Part 4 (in work) of work for my Advanced Technology Demonstration Aircraft project, to inspire interest in aerospace engineering for the RAeS and AIAA.
Optimizationof fuselage shape for better pressurization and drag reductioneSAT Journals
Abstract
The fuselage of any aircraft is essentially to accommodate the payload. It is normally not as streamlined as the wing. Cabin pressurization has been a major concern in the manufacturing of aircrafts. Generally, a cylindrical shape is preferred from a pressurization point of view as it has a higher strength and weighs less too. On the other hand, a sphere is considered as the best pressure vessel among all the shapes, but, sphere being a bluff body is not suitable for carrying payloads. On this note, a cylinder is considered to be better than a sphere to carry the payload and mainly to achieve a streamlined flow. In this paper, the shape chosen is a combination of the sphere and the cylinder to achieve optimum results for pressurization as well as a better streamlined flow. Our prime aim is to convert this bluff body into something more efficient and useful, rather than only for carrying the payload. We have focused basically on two details viz. 1) Better Pressurization and 2) to assist in minimizing the drag, thereby increasing the overall lift of the aircraft and hence increasing the fuel efficiency. The proposed fuselage structure was designed in CATIA V5 software and structural analyses were done in Auto-Desk Multi-Physics software. As a result, a better structural load capacity was found. A load of 10 N/mm2 was applied on both the bodies under consideration (cylinder and ellipse) having the same material, surface area, volume and weight. For the proposed elliptical design, 78% reduction in the minimum stress value and 10% reduction in the maximum stress value were noticed.
Keywords: Fuselage, Lifting Fuselage, Drag Reduction, Pressurization, Hoop Stress, Multi body design, Toroidal Shells, Multi-cylinder, Channel Propeller Configuration, Carbon Fiber, Graphite Fiber, Stabilization and Carbonization.
Structural detailing of fuselage of aeroplane /aircraft.PriyankaKg4
This presentation is about the structural detailing of fuselage of aeroplane .The fuselage or body of the airplane, holds all the pieces together. The pilots sit in the cockpit at the front of the fuselage. Passengers and cargo are carried in the rear of the fuselage. Some aircraft carry fuel in the fuselage; others carry the fuel in the wings.
This is Part 4 (in work) of work for my Advanced Technology Demonstration Aircraft project, to inspire interest in aerospace engineering for the RAeS and AIAA.
Optimizationof fuselage shape for better pressurization and drag reductioneSAT Journals
Abstract
The fuselage of any aircraft is essentially to accommodate the payload. It is normally not as streamlined as the wing. Cabin pressurization has been a major concern in the manufacturing of aircrafts. Generally, a cylindrical shape is preferred from a pressurization point of view as it has a higher strength and weighs less too. On the other hand, a sphere is considered as the best pressure vessel among all the shapes, but, sphere being a bluff body is not suitable for carrying payloads. On this note, a cylinder is considered to be better than a sphere to carry the payload and mainly to achieve a streamlined flow. In this paper, the shape chosen is a combination of the sphere and the cylinder to achieve optimum results for pressurization as well as a better streamlined flow. Our prime aim is to convert this bluff body into something more efficient and useful, rather than only for carrying the payload. We have focused basically on two details viz. 1) Better Pressurization and 2) to assist in minimizing the drag, thereby increasing the overall lift of the aircraft and hence increasing the fuel efficiency. The proposed fuselage structure was designed in CATIA V5 software and structural analyses were done in Auto-Desk Multi-Physics software. As a result, a better structural load capacity was found. A load of 10 N/mm2 was applied on both the bodies under consideration (cylinder and ellipse) having the same material, surface area, volume and weight. For the proposed elliptical design, 78% reduction in the minimum stress value and 10% reduction in the maximum stress value were noticed.
Keywords: Fuselage, Lifting Fuselage, Drag Reduction, Pressurization, Hoop Stress, Multi body design, Toroidal Shells, Multi-cylinder, Channel Propeller Configuration, Carbon Fiber, Graphite Fiber, Stabilization and Carbonization.
Structural detailing of fuselage of aeroplane /aircraft.PriyankaKg4
This presentation is about the structural detailing of fuselage of aeroplane .The fuselage or body of the airplane, holds all the pieces together. The pilots sit in the cockpit at the front of the fuselage. Passengers and cargo are carried in the rear of the fuselage. Some aircraft carry fuel in the fuselage; others carry the fuel in the wings.
Advanced Materials International Forum, Bari 18-19 settembre, conferenza internazionale dedicata ai materiali avanzati e alle loro possibili applicazioni nei settori industriali, con un focus particolare sui trasporti (aerospazio, automotive, navale e cantieristico).
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Business Valuation Principles for EntrepreneursBen Wann
This insightful presentation is designed to equip entrepreneurs with the essential knowledge and tools needed to accurately value their businesses. Understanding business valuation is crucial for making informed decisions, whether you're seeking investment, planning to sell, or simply want to gauge your company's worth.
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Attending a job Interview for B1 and B2 Englsih learnersErika906060
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India Orthopedic Devices Market: Unlocking Growth Secrets, Trends and Develop...Kumar Satyam
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Memorandum Of Association Constitution of Company.pptseri bangash
www.seribangash.com
A Memorandum of Association (MOA) is a legal document that outlines the fundamental principles and objectives upon which a company operates. It serves as the company's charter or constitution and defines the scope of its activities. Here's a detailed note on the MOA:
Contents of Memorandum of Association:
Name Clause: This clause states the name of the company, which should end with words like "Limited" or "Ltd." for a public limited company and "Private Limited" or "Pvt. Ltd." for a private limited company.
https://seribangash.com/article-of-association-is-legal-doc-of-company/
Registered Office Clause: It specifies the location where the company's registered office is situated. This office is where all official communications and notices are sent.
Objective Clause: This clause delineates the main objectives for which the company is formed. It's important to define these objectives clearly, as the company cannot undertake activities beyond those mentioned in this clause.
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Liability Clause: It outlines the extent of liability of the company's members. In the case of companies limited by shares, the liability of members is limited to the amount unpaid on their shares. For companies limited by guarantee, members' liability is limited to the amount they undertake to contribute if the company is wound up.
https://seribangash.com/promotors-is-person-conceived-formation-company/
Capital Clause: This clause specifies the authorized capital of the company, i.e., the maximum amount of share capital the company is authorized to issue. It also mentions the division of this capital into shares and their respective nominal value.
Association Clause: It simply states that the subscribers wish to form a company and agree to become members of it, in accordance with the terms of the MOA.
Importance of Memorandum of Association:
Legal Requirement: The MOA is a legal requirement for the formation of a company. It must be filed with the Registrar of Companies during the incorporation process.
Constitutional Document: It serves as the company's constitutional document, defining its scope, powers, and limitations.
Protection of Members: It protects the interests of the company's members by clearly defining the objectives and limiting their liability.
External Communication: It provides clarity to external parties, such as investors, creditors, and regulatory authorities, regarding the company's objectives and powers.
https://seribangash.com/difference-public-and-private-company-law/
Binding Authority: The company and its members are bound by the provisions of the MOA. Any action taken beyond its scope may be considered ultra vires (beyond the powers) of the company and therefore void.
Amendment of MOA:
While the MOA lays down the company's fundamental principles, it is not entirely immutable. It can be amended, but only under specific circumstances and in compliance with legal procedures. Amendments typically require shareholder
Cracking the Workplace Discipline Code Main.pptxWorkforce Group
Cultivating and maintaining discipline within teams is a critical differentiator for successful organisations.
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What is the TDS Return Filing Due Date for FY 2024-25.pdfseoforlegalpillers
It is crucial for the taxpayers to understand about the TDS Return Filing Due Date, so that they can fulfill your TDS obligations efficiently. Taxpayers can avoid penalties by sticking to the deadlines and by accurate filing of TDS. Timely filing of TDS will make sure about the availability of tax credits. You can also seek the professional guidance of experts like Legal Pillers for timely filing of the TDS Return.
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As a business owner in Delaware, staying on top of your tax obligations is paramount, especially with the annual deadline for Delaware Franchise Tax looming on March 1. One such obligation is the annual Delaware Franchise Tax, which serves as a crucial requirement for maintaining your company’s legal standing within the state. While the prospect of handling tax matters may seem daunting, rest assured that the process can be straightforward with the right guidance. In this comprehensive guide, we’ll walk you through the steps of filing your Delaware Franchise Tax and provide insights to help you navigate the process effectively.
2. Aerospace Rivets
Primarily used to fasten aerospace skins to the
sub-structure
Concerned mainly with shear and tension loads.
Two types of rivets:
– Solid Rivet
– Blind Rivet
2
8. Aerospace Solid Rivets - Identification
Rivets manufactured in accordance with the AN/MS standards are
identified by a four part code:
1. AN or MS specification and head type
2. one or two letters that indicate the material
3. shank diameter in 1/32nd inch increments
4. a dash followed by a number that indicates rivet length in 1/16th
inch increments.
8
9. Aerospace Solid Rivets - Identification
• Aircraft rivets are made
of many materials, and
come in a wide variety of
shapes and sizes
• How do you select the
right size?
• How do you select the
right material?
•We must know what the
part number tells us…
9
10. Aerospace Solid Rivets - Identification
Example: rivet identification
standard universal head solid rivet
Material: 2117-T4 aluminium
1/8 inch diameter
5/16 inch in length
Rivet ID = either AN470AD4-5 or MS20470AD4-5
10
11. Aerospace Solid Rivets - Identification
Same rivet, different material:1100 aluminium
– AN470A4-5 or MS20470A4-5.
AN470 or MS20470 denote the specification for universal head types
AD is the material code for 2117-T4
– (A=1100, B=5056, C=copper, D=2017, DD=2024, F=stainless
and M=Monel)
4 = 4/32 or 1/8 inch diameter
-5 = 5/16 inch length
11
12. Aerospace Solid Rivet Installation
Rivet installation summary
– Drill appropriately sized holes
– Deburr holes
– Secure pieces together with Clecos
– Install rivet, buck with rivet gun or use a rivet
squeezer
12
13. Aerospace Solid Rivet Installation
• .032” 2024-
T6 sheet
aluminum to
be joined with
rivets
•Rivet gun
•Bucking bar
•Drill
•Drill bit and
chuck key
•Center punch
•Cleco
•Cleco pliers
13
14. Aerospace Solid Rivet Installation
• Drilling holes
with a #30 drill
bit
• Use 1/8”
rivets with a
#30 (.1285”)
drill bit
14
15. Aerospace Solid Rivet Installation
• Deburr the holes
by rotating (by
hand) a much
larger drill bit in the
holes
• This removes any
metal shavings
caused by drilling
15
16. Aerospace Solid Rivet Installation
• Position the
pieces together
and secure using
Clecos
•Clecos maintain
proper alignment
of the pieces while
rivets are being
installed
16
17. Aerospace Solid Rivet Installation
• Place the rivet
in the hole
• Make sure you
are using the
correct size,
material, and
type of rivet
17
18. Aerospace Solid Rivet Installation
• Align the rivet gun
on the rivet head
• Hold the bucking
bar on the opposite
end of the rivet
• Pull the trigger on
the rivet gun to
hammer the rivet in
place
18
19. Aerospace Solid Rivet Installation
Solid rivets can be
installed using a rivet
squeezer instead of a
pneumatic rivet gun
The squeezer is hand
operated
The squeezer uses
various inserts
depending on the type
and size of rivet being
19 installed
20. Aerospace Blind Rivets
Used when you cannot physically access one side of the
work
Blind rivets are hollow, and thus weaker than solid rivets
To retain strength of the joint:
– stronger material, larger diameter rivets, or more are
necessary and of course
20–50% heavier than a solid rivet because of steel stem
20
22. Aerospace Rivets – Fuselage Repair
• Exterior of a riveted patch fuselage skin patch
•Note that solid fasteners
are used except in the
middle of the patch
• Why would you use blind
fasteners in this
application?
22
23. Aerospace Rivets – Fuselage Repair
• Interior of a riveted fuselage skin patch
•Because the stringer
on the interior of the
fuselage prevents the
bucking a solid rivet
requires
• Blind rivets are the
only option when
access is restricted
23
24. Quality Assurance of Aerospace
Fasteners
Aerospace Fasteners Material Selection
Aerospace Fasteners Testing
24
25. Aerospace Fasteners Material
Selection
Background
Some factors to be considered before material selection
are:
The max. and min. operating temperatures
The corrosiveness of the environment
Fatigue and impact loading
Always try to use standard fasteners, such as AN, MS,
MIL, NAS, SAE
25
27. Aerospace Fasteners Material
Selection
Aluminum is the predominant material used in the manufacture of
commercial aircraft.
Table 3 lists the typical aluminum alloys used in commercial aircraft.
27
28. Basic Aerospace Fasteners
Application
Thebasic applications (or needs) for
aerospace fasteners are:
– Shear
– Tension
– Fatigue
– Fuel tightness
– High temperature
– Corrosion control
28
29. Aerospace Fasteners Testing
Analyzing a Joint
– Calculate all the load required for each type of
joint failure:
RivetShear
Sheet Tensile
Bearing
Sheet Shear
– Failure will occur in the mode that corresponds
with the lowest load carrying capability.
29
30. Aerospace Fastener Standardization
Most aerospace hardware is manufactured
per government standards
The three most common aircraft fastener
standards used are:
– AN = Air Force/Navy
– NAS = National Aerospace Standards
– MS = Military Standards
30