The document provides notes from a training course on aerospace sheet metal design using CATIA. It includes an introduction, overview of the ASL workbench interface, descriptions of how to set parameters and load design data, and step-by-step instructions for various sheet metal design features such as creating a web, surfacic flanges, joggles, cutouts, stamps, and generating folded and flattened parts. The target audience is aerospace designers, and prerequisites include knowledge of CATIA part design, assembly design, and wireframe and surface design.
[ Capella Day 2019 ] Model-based safety analysis on Capella using Component F...Obeo
The importance of mission or safety-critical software systems in many application domains of embedded systems is continuously growing, and so is the effort and complexity for reliability and safety analysis. Model-based system engineering (MBSE) is currently one of the key approaches to cope with increasing system complexity.
With Component Fault Trees (CFTs) there is a model- and component-based methodology for safety analysis, which extends the advantages of model-based development to safety & reliability engineering. In this talk, we demonstrate how to ease the development of safety-critical systems in industrial practice by extending MBSE in Capella with model-based safety analysis using Component Fault Tree methodology.
Marc Zeller, Siemens Corporate Engineering
Marc Zeller works as a research scientist at Siemens AG, Corporate Technology, in Munich since 2014. His research interests are focused on the model-based safety and reliability engineering of complex software-intensive embedded systems. Marc Zeller studied Computer Science at the Karlsruhe Institute of Technology (KIT) and graduated in 2007. He obtained a PhD from the University of Augsburg in 2013 for his work on self-adaptation in networked embedded systems at the Fraunhofer Institute for Embedded Systems and Communication Technologies ESK in Munich.
MBSE with Arcadia method step-by-step Physical Architecture.pdfHelder Castro
The objective of the Physical Architecture in defining the “real” concrete components that comprise the system. To start the Physical level based on the Logical level, Capella proposes transitions similar to those that we used when we went from the Operational Analysis to the System Analysis, then from the System Analysis to the Logical Architecture. Thus, it can be created as many Physical Functions as Logical Functions, by also keeping the Functional Exchanges and Functional Chains.
Architecture frameworks provide an approach to describing systems and the presentation of these elements and relationships to deliver the stakeholder needs. Essentially, frameworks provide templates for our engineering artefacts.
The design of a framework must accommodate a level of freedom in its usage; specific enough to answer the majority of stakeholder concerns whilst generic enough to allow for differences between projects. This balancing act often results in framework design being more generic to allow for a wider audience. Having an untailored framework, which is more ‘open’, can lead to creating inconsistent viewpoints.
Arcadia is one such framework as implemented through the Capella tool. The framework provides 4 perspectives/levels for product definition:
- The Operational Analysis, where the user needs are considered. Note: no concept of the System at this level.
- The System Analysis, where we define the contribution and scope of the System as a ‘black box’, identifying external interfaces, and top-level system functions.
- The Logical Architecture, where we break the System down into logical ‘blocks’ and decompose the functionality.
- The Physical Architecture, in which we define a (candidate) physical architecture, further decompose the functions, and deploy this functionality to the physical sub-systems, hardware, software and/or firmware.
In this talk, we acknowledge the strengths of the Arcadia framework, and the benefits it brings, whilst considering the need to tailor the generic viewpoints. We will provide examples of how we have adopted the generic Arcadia framework and further specified some of the viewpoints to meet the needs of our stakeholders. We will discuss future work looking at how we can translate these specialisations across other areas of the model. Finally, we will provide some suggestions and advice on tailoring views to meet your own needs and ensuring stakeholder engagement with the model.
Introduction to the OMG Systems Modeling Language (SysML), Version 2Ed Seidewitz
Tutorial presented at the MODELS 2020 virtual conference on the proposed OMG Systems Modeling Language, Version 2, as of the initial submission of the specification.
[ Capella Day 2019 ] Model-based safety analysis on Capella using Component F...Obeo
The importance of mission or safety-critical software systems in many application domains of embedded systems is continuously growing, and so is the effort and complexity for reliability and safety analysis. Model-based system engineering (MBSE) is currently one of the key approaches to cope with increasing system complexity.
With Component Fault Trees (CFTs) there is a model- and component-based methodology for safety analysis, which extends the advantages of model-based development to safety & reliability engineering. In this talk, we demonstrate how to ease the development of safety-critical systems in industrial practice by extending MBSE in Capella with model-based safety analysis using Component Fault Tree methodology.
Marc Zeller, Siemens Corporate Engineering
Marc Zeller works as a research scientist at Siemens AG, Corporate Technology, in Munich since 2014. His research interests are focused on the model-based safety and reliability engineering of complex software-intensive embedded systems. Marc Zeller studied Computer Science at the Karlsruhe Institute of Technology (KIT) and graduated in 2007. He obtained a PhD from the University of Augsburg in 2013 for his work on self-adaptation in networked embedded systems at the Fraunhofer Institute for Embedded Systems and Communication Technologies ESK in Munich.
MBSE with Arcadia method step-by-step Physical Architecture.pdfHelder Castro
The objective of the Physical Architecture in defining the “real” concrete components that comprise the system. To start the Physical level based on the Logical level, Capella proposes transitions similar to those that we used when we went from the Operational Analysis to the System Analysis, then from the System Analysis to the Logical Architecture. Thus, it can be created as many Physical Functions as Logical Functions, by also keeping the Functional Exchanges and Functional Chains.
Architecture frameworks provide an approach to describing systems and the presentation of these elements and relationships to deliver the stakeholder needs. Essentially, frameworks provide templates for our engineering artefacts.
The design of a framework must accommodate a level of freedom in its usage; specific enough to answer the majority of stakeholder concerns whilst generic enough to allow for differences between projects. This balancing act often results in framework design being more generic to allow for a wider audience. Having an untailored framework, which is more ‘open’, can lead to creating inconsistent viewpoints.
Arcadia is one such framework as implemented through the Capella tool. The framework provides 4 perspectives/levels for product definition:
- The Operational Analysis, where the user needs are considered. Note: no concept of the System at this level.
- The System Analysis, where we define the contribution and scope of the System as a ‘black box’, identifying external interfaces, and top-level system functions.
- The Logical Architecture, where we break the System down into logical ‘blocks’ and decompose the functionality.
- The Physical Architecture, in which we define a (candidate) physical architecture, further decompose the functions, and deploy this functionality to the physical sub-systems, hardware, software and/or firmware.
In this talk, we acknowledge the strengths of the Arcadia framework, and the benefits it brings, whilst considering the need to tailor the generic viewpoints. We will provide examples of how we have adopted the generic Arcadia framework and further specified some of the viewpoints to meet the needs of our stakeholders. We will discuss future work looking at how we can translate these specialisations across other areas of the model. Finally, we will provide some suggestions and advice on tailoring views to meet your own needs and ensuring stakeholder engagement with the model.
Introduction to the OMG Systems Modeling Language (SysML), Version 2Ed Seidewitz
Tutorial presented at the MODELS 2020 virtual conference on the proposed OMG Systems Modeling Language, Version 2, as of the initial submission of the specification.
A press tool assembly ppt.
CATIA (an acronym of computer aided three-dimensional interactive application, pronounced /kəˈtiə/) is a multi-platform software suite for computer-aided design (CAD), computer-aided manufacturing (CAM), computer-aided engineering (CAE), PLM and 3D, developed by the French company Dassault Systèmes.
It is introductory presentation for Catia and its capabilities with
Proposed learning goal.
Video links are provided for ease of understanding.
just click underlined lines.
Commonly referred to as a 3D Product Lifecycle Management software suite, CATIA supports multiple stages of product development (CAx), including conceptualization, design (CAD), engineering (CAE) and manufacturing (CAM). CATIA facilitates collaborative engineering across disciplines around its 3D EXPERIENCE platform, including surfacing & shape design, electrical, fluid and electronic systems design, mechanical engineering and systems engineering.
Simulation methods to assess the brake noise behavior of passenger vehicle br...Altair
An important aspect of vehicle comfort is the silence of the brake system. Especially low velocity braking maneuvers are sometimes accompanied by heavy noise occurrences. Although these noise occurrences do not affect the brake system negatively with respect to braking performance they mostly result in customer insecurity. Therefore, most OEMs invest much time and money on developing silent brake systems. The presentation will illustrate the physical reasons behind such brake noise events. Practical methods for vibration damping will be discussed as well. Different analytical approaches for early estimation of noise potentials of brake systems based on the Finite-Element-Method as well as Multi-Body-Dynamics will be presented. Finally, future steps for the investigation of brake noise occurrences by analytical methods will be offered.
Speakers
Daniel Scharding, Adam Opel AG
STPA Analysis of Automotive Safety Using Arcadia and CapellaDavid Hetherington
This presentation demonstrates the use of the Arcadia methodology and the open source Capella tool to implement a STPA-based analysis technique that augments the conventional HARA, HAZOP. The STPA approach extends the conventional methods to include a holistic perspective considering hardware, software, humans, and control failures in a balanced manner.
Delivered by David Hetherington and Pascal Roques at the ERTS 2022 conference in Toulouse, France on 1 June 2022.
MBSE with Arcadia method step-by-step Operational Analysis.pdfHelder Castro
The article will explore the Arcadia Operational Analysis layer to capture stakeholder (e.g., users, environment, other systems) and business needs, a reasoned step-by-step activities and artefacts (i.e., diagrams) that can be produced to help during the stakeholders elicitation process helping to explore needs and identify gaps in the analysis; the full MBSE with Arcadia step-by-step is not described in this article, but it has extended to all Arcadia layers (i.e., System Analysis, Logical and Physical Architecture) and it can be used in projects for defining and guiding in the initial project activities and artefacts to be produced from the model.
The Operational Analysis as mentioned in the previous article, aims at capturing what the user of the system needs to accomplish, hence, the Operational Analysis normally starts by identifying who the users (i.e., Operational Entities and/or Operational Actors) of the future system are, and any containment relationship between them.
CATIA is an acronym for Computer Aided Three-Dimensional Interactive Application. It is the most proficient, powerful and highly popular CAD i.e. computer aided design software. It is created, developed and owned by Dassault Systemes of France.
CATIA is also known as Computer Aided Three Dimensional Interactive Application. CATIA was started in the year 1977 by French Aircraft Manufacturer Avions Marcel Dassaults System
Used in automobile, aerospace and various other industries
A common need in system architecture design is to verify that if the architect is correct and can satisfy its requirements.
Execution of system architect model means to interact with state machines to test system’s control logic. It can verify if the logical sequences of functions and interfaces in different scenarios are desired.
However, only sequence itself is not enough to verify its consequence or output. So we need each function to do what it is supposed to do during model execution to verify its output, and that is what we called “simulation”.
This presentation introduced how to embed Python or MATLAB® codes inside functions to do “simulation” within Capella.
Simplifying MBSE Tasks with Capella and MapleMBSEObeo
Discover how to use Excel-based interfaces to collaborate on Capella models
MapleMBSE 2020.1 adds support for Capella. Organizations using Capella can now edit models within MapleMBSE, allowing them to simplify MBSE tasks and increase engagement with MBSE processes at their company.
During this webinar, you will see how to work with a Capella systems model using MapleMBSE
The demonstration will highlight how all stakeholders can collaborate through the systems model using task-specific, Excel-based interfaces found in MapleMBSE.
A press tool assembly ppt.
CATIA (an acronym of computer aided three-dimensional interactive application, pronounced /kəˈtiə/) is a multi-platform software suite for computer-aided design (CAD), computer-aided manufacturing (CAM), computer-aided engineering (CAE), PLM and 3D, developed by the French company Dassault Systèmes.
It is introductory presentation for Catia and its capabilities with
Proposed learning goal.
Video links are provided for ease of understanding.
just click underlined lines.
Commonly referred to as a 3D Product Lifecycle Management software suite, CATIA supports multiple stages of product development (CAx), including conceptualization, design (CAD), engineering (CAE) and manufacturing (CAM). CATIA facilitates collaborative engineering across disciplines around its 3D EXPERIENCE platform, including surfacing & shape design, electrical, fluid and electronic systems design, mechanical engineering and systems engineering.
Simulation methods to assess the brake noise behavior of passenger vehicle br...Altair
An important aspect of vehicle comfort is the silence of the brake system. Especially low velocity braking maneuvers are sometimes accompanied by heavy noise occurrences. Although these noise occurrences do not affect the brake system negatively with respect to braking performance they mostly result in customer insecurity. Therefore, most OEMs invest much time and money on developing silent brake systems. The presentation will illustrate the physical reasons behind such brake noise events. Practical methods for vibration damping will be discussed as well. Different analytical approaches for early estimation of noise potentials of brake systems based on the Finite-Element-Method as well as Multi-Body-Dynamics will be presented. Finally, future steps for the investigation of brake noise occurrences by analytical methods will be offered.
Speakers
Daniel Scharding, Adam Opel AG
STPA Analysis of Automotive Safety Using Arcadia and CapellaDavid Hetherington
This presentation demonstrates the use of the Arcadia methodology and the open source Capella tool to implement a STPA-based analysis technique that augments the conventional HARA, HAZOP. The STPA approach extends the conventional methods to include a holistic perspective considering hardware, software, humans, and control failures in a balanced manner.
Delivered by David Hetherington and Pascal Roques at the ERTS 2022 conference in Toulouse, France on 1 June 2022.
MBSE with Arcadia method step-by-step Operational Analysis.pdfHelder Castro
The article will explore the Arcadia Operational Analysis layer to capture stakeholder (e.g., users, environment, other systems) and business needs, a reasoned step-by-step activities and artefacts (i.e., diagrams) that can be produced to help during the stakeholders elicitation process helping to explore needs and identify gaps in the analysis; the full MBSE with Arcadia step-by-step is not described in this article, but it has extended to all Arcadia layers (i.e., System Analysis, Logical and Physical Architecture) and it can be used in projects for defining and guiding in the initial project activities and artefacts to be produced from the model.
The Operational Analysis as mentioned in the previous article, aims at capturing what the user of the system needs to accomplish, hence, the Operational Analysis normally starts by identifying who the users (i.e., Operational Entities and/or Operational Actors) of the future system are, and any containment relationship between them.
CATIA is an acronym for Computer Aided Three-Dimensional Interactive Application. It is the most proficient, powerful and highly popular CAD i.e. computer aided design software. It is created, developed and owned by Dassault Systemes of France.
CATIA is also known as Computer Aided Three Dimensional Interactive Application. CATIA was started in the year 1977 by French Aircraft Manufacturer Avions Marcel Dassaults System
Used in automobile, aerospace and various other industries
A common need in system architecture design is to verify that if the architect is correct and can satisfy its requirements.
Execution of system architect model means to interact with state machines to test system’s control logic. It can verify if the logical sequences of functions and interfaces in different scenarios are desired.
However, only sequence itself is not enough to verify its consequence or output. So we need each function to do what it is supposed to do during model execution to verify its output, and that is what we called “simulation”.
This presentation introduced how to embed Python or MATLAB® codes inside functions to do “simulation” within Capella.
Simplifying MBSE Tasks with Capella and MapleMBSEObeo
Discover how to use Excel-based interfaces to collaborate on Capella models
MapleMBSE 2020.1 adds support for Capella. Organizations using Capella can now edit models within MapleMBSE, allowing them to simplify MBSE tasks and increase engagement with MBSE processes at their company.
During this webinar, you will see how to work with a Capella systems model using MapleMBSE
The demonstration will highlight how all stakeholders can collaborate through the systems model using task-specific, Excel-based interfaces found in MapleMBSE.
Abstract 3D Printing is a process of manufacturing the product on the layer by layer. And it is best processes for producing a finished objects. It was started in 1980‟s with the invention of stereo lithography. It has gone through various ups and downs throughout its development and rejection of new technologies. In this paper, we h3ave summarized the printing of hollow compounds with different shapes. Applications of 3D printed hollow compounds are turbine blades, gears, disc brakes etc. One of the major application of 3D printing is hollow turbine blade. A turbine blade is the individual components. These are used to up the turbine section of a gas turbine. The blades must designed to withstand the high pressure and high temperature comings from combustor. These 3D printed hollow compounds has same strength as solid compounds when compared. Major advantages of the Hollow shaped compounds are heat transfer, low material cost. The aim of the paper is to reduce the cost of material and easy manufacturing of hollow compounds compared to traditional process and taken hollow turbine blade as example. Keywords: hollow compounds, 3D printing, turbine blades, Additive manufacturing.
DESIGN OF MOULD TOOL & COOLING CHANNEL OPTIMIZATION OF REMOTE CONTROL TOP PANELIjripublishers Ijri
A plastic material is any of a wide range of synthetic or semi-synthetic organic solids that are moldable. Plastics are
typically organic polymers of high molecular mass, but they often contain other substances. They are usually synthetic,
most commonly derived from petrochemicals, but many are partially natural.
Molding is the process of manufacturing by shaping liquid or pliable raw material using a rigid frame called a mold or
matrix. This itself may have been made using a pattern or model of the final object.
Cooling channels are used in mold tool to reduce the temperature of the object to help molten material to solidify quickly
before the ejection. It is quite useful to increase the production rate.
DESIGN OF MOULD TOOL & COOLING CHANNEL OPTIMIZATION OF REMOTE CONTROL TOP PANELIjripublishers Ijri
A plastic material is any of a wide range of synthetic or semi-synthetic organic solids that are moldable. Plastics are
typically organic polymers of high molecular mass, but they often contain other substances. They are usually synthetic,
most commonly derived from petrochemicals, but many are partially natural.
Molding is the process of manufacturing by shaping liquid or pliable raw material using a rigid frame called a mold or
matrix. This itself may have been made using a pattern or model of the final object.
Cooling channels are used in mold tool to reduce the temperature of the object to help molten material to solidify quickly
before the ejection. It is quite useful to increase the production rate.
The aim of this project work is to design mold structure and optimize cooling channel system to reduce effect of warpage
of remote control top panel.
This project deals with the modeling of cooler tank parametric model as per the client requirement. Finding the best manufacturing process preparing mould base for the same, analyzing different manufacturing process by doing CNC program by changing milling parameters (feed, speed, cutters….).So that optimum parameters for manufacturing will be suggested which is useful to reduce the costs and efforts. Plastic flow analysis will be conducted to check the material flow and filling. So that reduction in the pre-machining cost will be done by rectifying the problem. FEM Based analysis will be conducted on mould structure to reduce weight of the mould. And thermal analysis will be conducted to suggest optimized cooling channel design. Modeling, mould base preparation, manufacturing, cnc programming will be done
This project deals with the modeling of cooler tank parametric model as per the client requirement. Finding the best manufacturing process preparing mould base for the same, analyzing different manufacturing process by doing CNC program by changing milling parameters (feed, speed, cutters….).So that optimum parameters for manufacturing will be suggested which is useful to reduce the costs and efforts. Plastic flow analysis will be conducted to check the material flow and filling. So that reduction in the pre-machining cost will be done by rectifying the problem. FEM Based analysis will be conducted on mould structure to reduce weight of the mould. And thermal analysis will be conducted to suggest optimized cooling channel design. Modeling, mould base preparation, manufacturing, cnc programming will be done
Similar to Aerospace Sheet Metal Design CATIA V5 (20)
Macroeconomics- Movie Location
This will be used as part of your Personal Professional Portfolio once graded.
Objective:
Prepare a presentation or a paper using research, basic comparative analysis, data organization and application of economic information. You will make an informed assessment of an economic climate outside of the United States to accomplish an entertainment industry objective.
Acetabularia Information For Class 9 .docxvaibhavrinwa19
Acetabularia acetabulum is a single-celled green alga that in its vegetative state is morphologically differentiated into a basal rhizoid and an axially elongated stalk, which bears whorls of branching hairs. The single diploid nucleus resides in the rhizoid.
Synthetic Fiber Construction in lab .pptxPavel ( NSTU)
Synthetic fiber production is a fascinating and complex field that blends chemistry, engineering, and environmental science. By understanding these aspects, students can gain a comprehensive view of synthetic fiber production, its impact on society and the environment, and the potential for future innovations. Synthetic fibers play a crucial role in modern society, impacting various aspects of daily life, industry, and the environment. ynthetic fibers are integral to modern life, offering a range of benefits from cost-effectiveness and versatility to innovative applications and performance characteristics. While they pose environmental challenges, ongoing research and development aim to create more sustainable and eco-friendly alternatives. Understanding the importance of synthetic fibers helps in appreciating their role in the economy, industry, and daily life, while also emphasizing the need for sustainable practices and innovation.
Normal Labour/ Stages of Labour/ Mechanism of LabourWasim Ak
Normal labor is also termed spontaneous labor, defined as the natural physiological process through which the fetus, placenta, and membranes are expelled from the uterus through the birth canal at term (37 to 42 weeks
Unit 8 - Information and Communication Technology (Paper I).pdfThiyagu K
This slides describes the basic concepts of ICT, basics of Email, Emerging Technology and Digital Initiatives in Education. This presentations aligns with the UGC Paper I syllabus.
June 3, 2024 Anti-Semitism Letter Sent to MIT President Kornbluth and MIT Cor...Levi Shapiro
Letter from the Congress of the United States regarding Anti-Semitism sent June 3rd to MIT President Sally Kornbluth, MIT Corp Chair, Mark Gorenberg
Dear Dr. Kornbluth and Mr. Gorenberg,
The US House of Representatives is deeply concerned by ongoing and pervasive acts of antisemitic
harassment and intimidation at the Massachusetts Institute of Technology (MIT). Failing to act decisively to ensure a safe learning environment for all students would be a grave dereliction of your responsibilities as President of MIT and Chair of the MIT Corporation.
This Congress will not stand idly by and allow an environment hostile to Jewish students to persist. The House believes that your institution is in violation of Title VI of the Civil Rights Act, and the inability or
unwillingness to rectify this violation through action requires accountability.
Postsecondary education is a unique opportunity for students to learn and have their ideas and beliefs challenged. However, universities receiving hundreds of millions of federal funds annually have denied
students that opportunity and have been hijacked to become venues for the promotion of terrorism, antisemitic harassment and intimidation, unlawful encampments, and in some cases, assaults and riots.
The House of Representatives will not countenance the use of federal funds to indoctrinate students into hateful, antisemitic, anti-American supporters of terrorism. Investigations into campus antisemitism by the Committee on Education and the Workforce and the Committee on Ways and Means have been expanded into a Congress-wide probe across all relevant jurisdictions to address this national crisis. The undersigned Committees will conduct oversight into the use of federal funds at MIT and its learning environment under authorities granted to each Committee.
• The Committee on Education and the Workforce has been investigating your institution since December 7, 2023. The Committee has broad jurisdiction over postsecondary education, including its compliance with Title VI of the Civil Rights Act, campus safety concerns over disruptions to the learning environment, and the awarding of federal student aid under the Higher Education Act.
• The Committee on Oversight and Accountability is investigating the sources of funding and other support flowing to groups espousing pro-Hamas propaganda and engaged in antisemitic harassment and intimidation of students. The Committee on Oversight and Accountability is the principal oversight committee of the US House of Representatives and has broad authority to investigate “any matter” at “any time” under House Rule X.
• The Committee on Ways and Means has been investigating several universities since November 15, 2023, when the Committee held a hearing entitled From Ivory Towers to Dark Corners: Investigating the Nexus Between Antisemitism, Tax-Exempt Universities, and Terror Financing. The Committee followed the hearing with letters to those institutions on January 10, 202
Safalta Digital marketing institute in Noida, provide complete applications that encompass a huge range of virtual advertising and marketing additives, which includes search engine optimization, virtual communication advertising, pay-per-click on marketing, content material advertising, internet analytics, and greater. These university courses are designed for students who possess a comprehensive understanding of virtual marketing strategies and attributes.Safalta Digital Marketing Institute in Noida is a first choice for young individuals or students who are looking to start their careers in the field of digital advertising. The institute gives specialized courses designed and certification.
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Read| The latest issue of The Challenger is here! We are thrilled to announce that our school paper has qualified for the NATIONAL SCHOOLS PRESS CONFERENCE (NSPC) 2024. Thank you for your unwavering support and trust. Dive into the stories that made us stand out!
1. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 1
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Aerospace Sheet
Metal Design
CATIA V5 Training
Foils
Version 5 Release 19
January 2009
EDU_CAT_EN_ASL_FF_V5R19
2. Student Notes:
Aerospace Sheet Metal Design
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About this course
Objectives of the course
Upon completion of this course you will be able to:
- Manage Sheetmetal parameters
- Create and modify the design of a Hydro-formed Sheetmetal Part
- Generate and draw a flattened part
- Create a Knowledge Expert Check using characteristic curves
Targeted audience
Aerospace Designers
Prerequisites
Students attending this course should have knowledge of Part Design,
Assembly Design, and Wireframe & Surface Design
8 hrs
3. Student Notes:
Aerospace Sheet Metal Design
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Table of Contents (1/4)
Introduction to Aerospace Sheet Metal Design 7
ASL Workbench Presentation 8
ASL Parameters 12
Loading Data 13
Modifying Default Thickness and Bend Radius 15
Modifying Default Bend Allowance 16
Choosing Joggle Compensations 17
Runout Formulas 18
Creating the Web 20
Creating the Web 21
Creating a Surfacic Web 23
Modifying the Web 25
Creating a Surfacic Flange 26
Creating a Surfacic Flange 27
Intersecting Surfacic Flanges on a Web 34
Modifying a Surfacic Flange 35
Creating a Corner Relief 36
Creating a Corner Relief 37
4. Student Notes:
Aerospace Sheet Metal Design
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Table of Contents (2/4)
Modifying a Corner Relief 39
Create Corner or Chamfer on Sharp Edges 40
Creating a Joggle 41
Creating a Joggle by Depth 42
Creating a Joggle with an Input Surface 45
Joggle Run out Formulas 47
Modifying a Joggle 48
Creating Flanges other than Surfacic Flanges 49
Creating a Flange 50
Create a Hem 51
Create a Tear Drop 52
Create a User Flange 53
Modifying Flanges other than Surfacic Flanges 54
Creating a Cutout 55
Creating a Cutout 56
Modifying a Cutout 61
Creating Stamps 62
Creating a Flanged Hole 63
5. Student Notes:
Aerospace Sheet Metal Design
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Table of Contents (3/4)
Creating a Bead 64
Creating a Circular Stamp 65
Creating a Surface Stamp 66
Creating a Flanged Cutout 67
Creating a Stiffening Rib 68
Creating a Curve Stamp 69
Creating a User Stamps 70
Modifying a Stamp 72
Creating a Hole 73
Creating a Hole 74
Creating a Circular Cutout 78
Creating a Circular Cutout 79
Modifying a Circular Cutout 80
Point or Curve Mapping 81
Duplicate ASL Feature by applying a Pattern 82
Modifying a Feature 83
Modifying a Feature 84
Generating Folded and Flattened parts 87
6. Student Notes:
Aerospace Sheet Metal Design
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Table of Contents (4/4)
Folding / Unfolding the Part 88
Using Multi-View 89
Flat Solid linked to ASL Designed Part 90
Drawing Generation 91
Drawing Generation 92
Administration 93
About Standards 94
Setting Standard Parameters 95
Setting Parameters for a Designer 96
Customizing Standards Files to define Design Tables 97
How to use Knowledge Expert 98
7. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 7
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Introduction to Aerospace Sheet Metal Design
In this lesson you will learn about main features of Aerospace Sheet Metal Design
workbench
8. Student Notes:
Aerospace Sheet Metal Design
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ASL Workbench Presentation (1/4)
Accessing the Workbench
Modifying CATIA environment
Tools > Option > General
General
User Interface Style: CATIA P3
9. Student Notes:
Aerospace Sheet Metal Design
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ASL Workbench Presentation (2/4)
ASL features
Product tree
User Interface : General Presentation
ASL tools
Sketcher
Standard
tools
10. Student Notes:
Aerospace Sheet Metal Design
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User Interface : ASL Tools
ASL Workbench Presentation (3/4)
Sheet Metal Default
Parameters
Creating a Web
Creating a Surfacic Flange
Creating a Joggle
Unfolding / Folding the Part
Creating a Cut Out
Creating Stamps
Creating a Corner Relief
Creating a Hole
Creating a Flange
Point and Curve Mapping
Creating Corner and Chamfer
Creating a Pattern
11. Student Notes:
Aerospace Sheet Metal Design
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User Interface : ASL Tools
ASL Workbench Presentation (4/4)
Creating Stamps
Creating a Flange
Creating Pattern
Creating Corner and Chamfer
User Flange
Flange
Tear Drop
Hem
User Stamp
Flanged
Hole
Curve Stamp
Stiffening Rib
Surface Stamp
Bead
Circular Stamp
Flanged Cutout
Chamfer
Corner
User Pattern
Circular Pattern
Rectangular
Pattern
12. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 12
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ASL Parameters
In this lesson you will learn the setting parameters of an Aerospace Sheet Metal part
13. Student Notes:
Aerospace Sheet Metal Design
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Loading Data (1/2)
You can link parameters table files such as Extruded Hole Std or Bead Std for
example as well as Joggle Compensation Methods to the Sheet Standard . xls file,
just by indicating their name in the corresponding column.
14. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 14
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Loading Data (2/2)
Prior to utilizing such design table you should declare correct path where
parameters tables are stored
Tools > Options > General > Document
Other Folders / Configure ,or
DL Name Allowed and Configure
15. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 15
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Modifying Default Thickness and Bend Radius
Click the Sheet
Metal Parameters
icon
Before starting to generate the part it is necessary to set
default parameters such as Thickness and Bend Radius
Set Thickness and Bend
Radius entering directly the
values
Another way to set parameters is to open a Sheet Standards Files and
accessing to the design table by the corresponding button
Select the Parameters Tab
16. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 16
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Modifying Default Bend Allowance
Select Bend
Allowance tab
A formula is associated to the K factor and could be deactivated (Right Button
Formula Deactivate)
17. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 17
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SYSTEMES
Choosing Joggle Compensations
Select Joggle
Compensation
method
Select Run out
calculation
method and
coefficient
Select one run
out formula out
of 3 types
18. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 18
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SYSTEMES
Runout Formulas (1/2)
Default Formula :
Runout = Coeff * Depth
No Formula : erases
formulas on ALL
part joggles
Design Table Formula :
choose a path to an .xls or .txt file
19. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 19
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SYSTEMES
Runout Formulas (2/2)
There is a particular syntax to use in order to create the design table.
As you can see on the picture, it can be described as follows :
The A Column (Formula Names) contains String Parameters
The B and C Columns contain Real Parameters (no unit)
The D Column contains Length Parameters (unit)
The E Column (Formula Bodies) uses previous Real & Length parameters (a1, a2,
a3) for its own
formulas (as you can see, not all existing parameters must be used in the formula)
20. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 20
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SYSTEMES
Creating the Web
In this lesson you will learn creating the web.
21. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 21
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Creating the Web (1/2)
A. Click the Web icon
B. Select a plane or a close
sketch which support the
web
C. Select curves, planes or surfaces to
define the limits of the web.
The limiting elements must intersect.
The web is the fix feature when we unfold the part
22. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 22
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Creating the Web (2/2)
D. As soon as selected elements
make a closed area, a preview
of web is suggested
The contour must be selected
in the logic sequence.
If necessary Select Web
Material Direction.
Reverse by clicking on the red
arrow which is perpendicular
to the web support.
23. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 23
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SYSTEMES
Creating a Surfacic Web (1/2)
A. Click the Web icon
B. Select a surface that can be
developed, even a curved one,
which supports the web
C. Select a reference wire and an invariant
point as references for the unfolding of the
web.
The reference wire must be located on one
of the limits and the invariant point on the
reference wire.
Select curves, planes or surfaces to define
the limits of the web.
The limiting elements must intersect.
As soon as selected elements make a
closed area, a preview of web is suggested
The contour must be selected in the logic
sequence.
24. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 24
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DASSAULT
SYSTEMES
Creating a Surfacic Web (2/2)
D. If necessary Select Web
Material Direction.
Reverse by clicking on the
red arrow which is
perpendicular to the web
support
Use this corner as
Invariant Point
Extrude.4
Folded View
Project.1 Folded
View
Extrude.3 Folded
View
Extrude.2
Folded View
25. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 25
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SYSTEMES
Modifying the Web
1. Double-click the Web feature in the tree
2. Change Support Geometry or Boundary Elements
3. Select a Boundary Element it becomes then a
Reference Element and you can then:
Add After
Add Before
Replace
Remove
Insert
You can also Remove All elements
Multiple Sel. option is available when
Add After or Add Before are activated
Modify the web by accessing the Web Definition dialog box
26. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 26
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SYSTEMES
Creating a Surfacic Flange
In this lesson you will learn to create a Surfacic Flange.
27. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 27
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Creating a Surfacic Flange (1/7)
A. Click the Surfacic Flange icon
B. Click the Base Feature
tab
C. Select the web or a flange as
Base Feature
Selecting the Base Feature
28. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 28
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A
A. Exact : the support is the surface
geometry selected
B. Approximation : the selected surface is
approximated into a ruled surface and
the maximum deviation can be
computed according to an
approximation length
C. Angle : the surface of the flange is
defined by a curve an angle and a
support length
Selecting the Support : Support Type
Creating a Surfacic Flange (2/7)
Select the
support type
Click the
Support tab
Support type :
B
C
29. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 29
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SYSTEMES
Creating a Surfacic Flange (3/7)
Select Directions (Reverse by clicking on
the corresponding red arrows) :
A. Flange Direction
B. Flange Material direction
C. Flange Base Feature Direction
Flange Support
Flange Base
Feature
Selecting the Support : Flange Directions
A
B
C
30. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 30
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SYSTEMES
Creating a Surfacic Flange (4/7)
Select the type
flange length
A. Length From OML : length between the curve
defining the top of the flange and the Outer Mold
Line (OML)
B. Element FD (Folded) : Boundary element is a surface
or a plane which intersects the flange surface or a
wire projected on the flange surface
C. Element FP (Flattened) : Boundary element is a
surface or a plane which intersects the flattened
flange surface or a wire projected on the flattened
flange surface
Define the Edge Of Part (EOP)
A
B
C
31. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 31
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Creating a Surfacic Flange (5/7)
SIDE TYPES
Standard: they are automatically defined at
the web limit and the perpendicular plans are
kept (the user doesn’t have to define them)
None: no side computed (only the EOP is able
to define them)
Element FD: they can be defined by a
geometrical element FD (Curve or surface)
Element FP: they can be defined by a
geometrical element FP (Curve or surface)
CORNER TYPES (angle defined
between the EOP and the sides)
Corner: between the side and the
EOP (defined with a radius value)
None: No corner computed (only the
EOP is able to define the contour of
the flange)
Two texts indicate
Flange Sides
(Side & corner 1
Side & Corner 2)
Defining Sides and Corners :
Select each
Corner type
Click the Sides and
Corners tab
Select each Side type
32. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 32
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DASSAULT
SYSTEMES
Creating a Surfacic Flange (6/7)
Manufacturing process
Hydro pressed or Break
Formed
(information only for the
current CATIA release)
General K_Factor
can be locally
altered for a
specific Surfacic
Flange
Process tab: Manufacturing Process and specific K_ Factor
33. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 33
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SYSTEMES
Creating a Surfacic Flange (7/7)
Apply or not Joggle Compensation method
selected in Sheetmetal Parameters definition
Choose Flange Sides
Compensation method
Compensation tab: Joggle and Flange Sides Compensations
34. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 34
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DASSAULT
SYSTEMES
Intersecting Surfacic Flanges on a Web
It is possible to intersect two surfacic flanges on a web. This means that you
can choose as a support a web with an existing surfacic flange that will go
through the new surfacic flange.
The intersecting flanges are automatically detected, and the geometry of the
first flange is relimited to enable the creation of the second flange; the
unfolded view is computed accordingly. You can then remove the sharp
vertex in the corner by creating a corner relief or a cutout at the intersection
of the surfacic flanges.
35. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 35
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B
Modifying a Surfacic Flange
A. Double Click the Flange in the part or in the tree and the Flange Definition
dialog box is displayed
B. Modify desired parameters and click OK to validate
36. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 36
Copyright
DASSAULT
SYSTEMES
Creating a Corner Relief
In this lesson you will learn to create a Corner Relief
37. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 37
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DASSAULT
SYSTEMES
C
D
Creating a Corner Relief (1/2)
B. Click the Corner Relief icon
C. Select both involved flanges
A. Click the Fold/Unfold icon to
flatten the part
D. Select the sketch of the corner relief
profile or access to standard contour
catalog or enter the Sketcher
workbench to create the profile
Setting corner relief parameters
Part must be flattened
Support Redefinition option is used
when user wants flanges sides to
be impacted (lengthened) by corner
relief profile
A B
38. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 38
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DASSAULT
SYSTEMES
Creating a Corner Relief (2/2)
E. The red arrow determines the material
side to be removed. Change direction
if necessary
F. Update the part if necessary
G. Fold back the part
Setting corner relief parameters
F G
Flanges
selected
Web
Corner relief profile
E
39. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 39
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DASSAULT
SYSTEMES
Modifying a Corner Relief
A. Double Click the Corner Relief in the tree when the part is flattened
and the Corner Relief Definition dialog box is displayed
B. Modify desired parameters and click OK to validate
B
40. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 40
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DASSAULT
SYSTEMES
Create Corner or Chamfer on Sharp Edges
Select Corner
or Chamfer icon
Key Radius value
Select Edges to be worked or
Select all
In case of chamfer
definition you will first
have to choose the
type Length1/Length2
or Length1/Angle
1 2
3
2
3
41. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 41
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DASSAULT
SYSTEMES
Creating a Joggle
In this lesson you will learn about creating a Joggle
42. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 42
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DASSAULT
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Creating a Joggle by Depth (1/3)
Click the
Joggle icon
A. Select the flange as joggle
support
B. Select the joggle plane
The vector normal to the joggle
plane determines the side on which
the joggle is to be created (run out)
Result
C. Select the role of the plane
Using a flange
Web
Joggle
direction
Joggle plane
Flange
The vector normal to
the flange support
determines the depth
direction
A
B C
D
D. Select Depth Type
The selected plane
either start the joggle
or end it.
43. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 43
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SYSTEMES
Creating a Joggle by Depth (2/3)
D. Depth : offset at the support
surface
E. Run out : length between the
original surface of the flange and
the new surface.If desired you can
deactivate formula
F. Clearance : offset between the
Joggle Plane and the end radius
G. Start Radius : radius linked
with the original surface
H. End Radius : radius
linked with the new
surface
Setting joggle parameters
D
E
F
G
H
44. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 44
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DASSAULT
SYSTEMES
Creating a Joggle by Depth (3/3)
A. Click the Joggle icon
B. Select the Web as joggle
support
C. Select the joggle plane and the
role of the plane
Result
D. Select Offset Type as Depth
Using a web
A
Web
C
B
C
D
45. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 45
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DASSAULT
SYSTEMES
Creating a Joggle with an Input Surface (1/2)
A. Click the Joggle icon
B. Select the flange as
joggle support
C. Select the joggle plane
and the role of the plane
D. Select Surface Type
Using an offset surface
Joggle plane
Flange
Joggle direction
Offset Surface
A
B
C
D
46. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 46
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DASSAULT
SYSTEMES
Creating a Joggle with an Input Surface (2/2)
The parameters work the same way as with a depth except for the offset surface which
obviously replaces the depth parameter. We get this result at the end :
47. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 47
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Joggle Run out Formulas
Default: Coeff *Depth None : no formula
Design Table : chosen
Formula of the table
Design Table :
Resulting run out
48. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 48
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DASSAULT
SYSTEMES
Modifying a Joggle
A. Double Click the Joggle in the tree and the Joggle
Definition dialog box is displayed
B. Modify desired parameters and click OK to
validate
B
49. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 49
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DASSAULT
SYSTEMES
Creating Flanges other than Surfacic Flanges
In this lesson you will learn to create Flanges using various options
Click the pull down arrow
and select the desired icon
Creating a Flange
User Flange
Tear Drop
Hem
Flange
50. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 50
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DASSAULT
SYSTEMES
Creating a Flange
Click Flange icon
Select Spine
Choose Basic or Relimited option, If
Relimited you will then select two
relimiting elements
Key Flange parameters: Radius, Length, Angle
Select OK
1
2
3
4
5
4
51. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 51
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DASSAULT
SYSTEMES
Create a Hem
Click Hem icon
Select Spine
Select Basic or Relimited option, If
Relimited you will then select two
relimiting elements
Key Flange parameters: Radius, Length
Select OK
1
2
3
4
5
52. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 52
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DASSAULT
SYSTEMES
Create a Tear Drop
Click Tear Drop icon
Select Spine
Choose Basic or Relimited option, if you
select Relimited option then you need to
select two relimiting elements
Key Flange parameters: Radius, Length
Select OK
1
2
3
4
5
53. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 53
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SYSTEMES
Create a User Flange
Click User Flange icon
Select Spine
Choose Basic or Relimited option, if you
select Relimited option then you need to
select two relimiting elements
Select Profile
Select OK
1
2
3
4
5
54. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 54
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DASSAULT
SYSTEMES
Modifying Flanges other than Surfacic Flanges
1. Double Click the Flange in the specification tree or on the geometry itself and the
appropriate Flange Definition dialog box is displayed
2. Modify desired parameters and/or specification elements and then click OK to
validate Step 1
Step 2
55. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 55
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DASSAULT
SYSTEMES
Creating a Cutout
In this lesson you will learn to create a Cutout
56. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 56
Copyright
DASSAULT
SYSTEMES
Creating a Cutout (1/5)
Click the Cutout icon to display the
Cutout Definition dialog box
Create a sketch on the web
surface or on a flange surface
Define a closed contour
Exit the sketcher
Creating a profile as Cutout profile
1
2
3
4
2
3
4
1
57. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 57
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DASSAULT
SYSTEMES
Creating a Cutout (2/5)
Three End Limit Types are available :
Dimension : depth is define by a specific value
Up to next : the limit is the first face the application
detects while extruding the profile
Up to last : the application will limit the cutout onto the
last possible face encountered by the extrusion
Select the profile previously created with the sketcher
Determine the cutout side : click on the
Reverse Direction button or on the red arrow
Select the material part to keep : click on the Reverse
Side button or on the orange arrow
Select Sheetmetal standard or Sheetmetal pocket
option. Sheet metal standard for sheet passing
through cutout. Sheet metal pocket for depth
smaller than sheet thickness
Lying on skin allows selection of a 3D
curve as profile definition
Using a profile : Setting cutout Parameters
6
7
8
9
10
5
8
6
10
9
8
7
5
58. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 58
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DASSAULT
SYSTEMES
Select the Power Copy
Family Object or User
Feature Family Object
Creating a Cutout (3/5)
Select the Open Catalogue
icon
Click the Cutout icon to
display the Cutout
Definition dialog box
Inserting a profile instance from a catalogue
Prior to inserting profile instance from catalogue, you should set up
catalogue access through Tools / Options / Mechanical Design / Aerospace
Sheet Metal
1
2
3
1
3
2
3
59. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 59
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DASSAULT
SYSTEMES
Creating a Cutout (4/5)
Select the web plane as
Ref_Plane input, a point as
Ref_Point and a line as
Ref_Axis for orientation
purpose
Select Parameters
Click OK and Close all
windows related to contour
instantiation
Double click on
Slot_contour
Select Design table icon and/or
modify Angle value
Select 8th row
Inserting a profile instance from a catalogue (cont’d)
7
8
9
5
6
7
8
9
4
4
5
6
60. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 60
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Creating a Cutout (5/5)
Check that orange arrow is
pointed inside the profile
and click OK
Inserting a profile instance from a catalogue (cont’d)
10
10
61. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 61
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Modifying a Cutout
A. Double Click the Cutout on the part or in the tree and the Cutout Definition dialog
box is displayed.
B. Modify desired parameters and click OK to validate.
B
62. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 62
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DASSAULT
SYSTEMES
Creating Stamps
In this lesson you will learn to create and modify Stamps
Click the pull down arrow
and select the desired icon
Creating Stamps
User Stamp
Curve Stamp
Stiffening
Rib
Flanged
Cutout
Surface
Stamp
Circular
Stamp
Bead
Flanged
Hole
63. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 63
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DASSAULT
SYSTEMES
Creating a Flanged Hole
Click the Flanged Hole icon
Select a point
previously created
Select the surface
where you want to
place the hole
Change parameters, such as radius,
angle, flat pattern by entering values
or using Standards Files
Select Design table icon to select
parameters (example to follow)
Change the hole
direction by clicking on
the orange arrow and
select OK
2
1
5
4
3
64. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 64
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DASSAULT
SYSTEMES
Creating a Bead
Click the Bead icon
Select the wire the
bead will rely on
Web
Surface
Modify Bead direction by
clicking the orange arrow if
needed and click OK
1
5
3
2
Change parameters by entering
values or using Standard Files
Select Design table icon to select
parameters
4
65. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 65
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DASSAULT
SYSTEMES
Creating a Circular Stamp
Click the Circular stamp icon
Select a point
previously created
Select the surface
where you want to
place the hole
Change parameters by entering
values or using Standards Files
Select Design table icon to select
parameters
Change the stamp direction
by clicking on the orange
arrow if needed and select
OK
1
5
4
3
2
66. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 66
Copyright
DASSAULT
SYSTEMES
Creating a Surface Stamp
Click the Surface stamp icon
Select a closed contour
previously created
Change parameters by entering
values or using Standards Files
Select Design table icon to select
parameters
Change the stamp direction by
clicking on the orange arrow if
needed and select OK
1
2
3
4
Example with Opening Edge
67. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 67
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SYSTEMES
Creating a Flanged Cutout
Click the Flanged Cutout icon
Select a closed contour
previously created
Change parameters by entering
values or using Standards Files
Select Design table icon to select
parameters
Change the stamp direction
by clicking on the orange
arrow if needed and select
OK
1
4
3
2
68. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 68
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DASSAULT
SYSTEMES
Creating a Stiffening Rib
Click the Stiffening Rib icon Select the external face
of a straight bend
Change parameters by entering
values or using Standards Files
Select Design table icon to select
parameters
1 2
3
69. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 69
Copyright
DASSAULT
SYSTEMES
Creating a Curve Stamp
Click the Curve
stamp icon
Select a
wire
previously
created
Change parameters by entering values or
using Standards Files
Select Design table icon to select parameters
Change the stamp
direction by clicking
on the orange arrow
if needed and select
OK
Example of Half Pierce 5
3
2
1
4
70. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 70
Copyright
DASSAULT
SYSTEMES
Creating a User Stamps (1/2)
Import the Punch from a
catalog into a specific Body
Create a User Stamp
Before actually creating the user stamp, you should first define or import
the punch and eventually the die that will later be used for actual
stamping
1
71. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 71
Copyright
DASSAULT
SYSTEMES
Creating a User Stamps (2/2)
Select User
Stamp icon
Select outer face of bend
you want to punch
Select appropriate icon:
With Die or With opening
Select Punch Body
and Position on
context option
2
4
5
3
Punch Body
72. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 72
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SYSTEMES
Modifying a Stamp
A. Double Click the stamp to be
modified
B. Modify desired parameters and
click Preview if you wish
C. Click OK to validate
C B
73. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 73
Copyright
DASSAULT
SYSTEMES
Creating a Hole
In this lesson you will learn to create a Hole
74. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 74
Copyright
DASSAULT
SYSTEMES
Creating a Hole (1/4)
B. Select a point on the web
A. Click Hole tool
E. Specify the values as
needed
G. Position the hole on
the web
D. Choose a bottom limit for
the hole
H. Choose a bottom type
for the hole
F. Specify the direction of the
hole
B
A
C. Select the web
C
Blind Up To Next Up To Last
Up To Plane Up To Surface
Flat bottom V bottom
D
E
F
G
H
D
H
75. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 75
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Creating a Hole (2/4)
I. Select the type of hole
Counter bored
Simple
Tapered
Countersunk
Counter drilled
J. Select the Bottom Type of a threaded
hole
J
I
76. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 76
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SYSTEMES
Creating a Hole (3/4)
Hole Diameter, Pitch, Right or Left-Threaded, Add or Remove
Standards
K. Specify other Thread Parameters
You can choose a Left or Right-
Threaded hole by selecting one of these
two options.
By default, the Pitch is automatically
calculated in accordance with the Thread
Diameter and the Standard. You can
modify it to get a non standard thread.
To add or remove one or several
standards, you can use these two
buttons.
By default, the Hole Diameter is
automatically calculated in accordance
with the Thread Diameter and the
Standard. You can modify it to get a non-
standard thread .
K
77. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 77
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SYSTEMES
Creating a Hole (4/4)
L. Specify Deformation
You can create a cylindrical hole in
folded and unfolded view by clicking
on No Deformation option in the
Deformation tab.
L
78. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 78
Copyright
DASSAULT
SYSTEMES
Creating a Circular Cutout
In this lesson you will learn to create a Circular Cutout
79. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 79
Copyright
DASSAULT
SYSTEMES
Creating a Circular Cutout
A. Create a point on the web
B. Select Circular Cutout
icon
D. Select web as support
F. Select type of hole
C. Select the point previously
created
G. Enter Diameter value
and click OK
E. Select additional points if
necessary
A
B
E
C
G
F
D
80. Student Notes:
Aerospace Sheet Metal Design
Copyright DASSAULT SYSTEMES 80
Copyright
DASSAULT
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Modifying a Circular Cutout
A. Double Click the Circular Cutout
on the part or in the tree and the
Circular Cutout Definition dialog
box is displayed
B. Modify desired parameters and
click OK to validate
C. Click Preview if you wish
B C
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Point or Curve Mapping
Select Point or Curve
mapping icon
Select the Context ASL
Feature (the one from which
transformation is deduced)
Select Elements to be
mapped
Mapping can be done from
3D to 2D and conversely
1
2
3
3
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Rectangular, Circular or
User defined Pattern
Duplicate ASL Feature by applying a Pattern
Select appropriate
Pattern icon
Select Feature to be
duplicated
Fill in all fields
necessary for Pattern
definition and select OK
1
2
3
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Modifying a Feature
In this lesson you will learn to modify a feature
84. Student Notes:
Aerospace Sheet Metal Design
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Modifying a Feature (1/3)
A. Double Click the Feature to be
modified on the part or in the
tree and the Feature Definition
dialog box is displayed (ex. :
the first flange definition)
B. Modify desired parameters and
click OK to validate ( here we
suppress the first corner of the
flange).
Update if necessary
Accessing feature definition window
85. Student Notes:
Aerospace Sheet Metal Design
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Modifying a Feature (2/3)
Two ways:
A. Double-click on the
sketch in the tree
B. Edit the feature
definition window
and click the
Sketcher button
2. Modify the closed
contour
3. Exit the sketcher and
update if necessary
Modifying Sketcher Support
A
B
1. Edit the sketch linked to
the feature to be modified
(ex. : the first Cutout
definition)
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A. Change to WFS workbench
Modifying a Feature (3/3)
B. Modify a support surface. Here we modify
the offset of a flange support surface
C. Change to ASL workbench and update
A
B
C
87. Student Notes:
Aerospace Sheet Metal Design
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Generating Folded and Flattened parts
In this lesson you will learn to Fold / Unfold a part.
88. Student Notes:
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Folding / Unfolding the Part
1. Select the Unfold icon to
flatten the part according to
the web
2. Select the Unfold icon
again and the part is
folded back
89. Student Notes:
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Using Multi-View
1. Click the Multi-View icon to
unfold the part in a second
window
2. Select Window > Tile -
Horizontally menu item to
display both windows
90. Student Notes:
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Flat Solid linked to ASL Designed Part
1. Copy the Part Body out
of the ASL designed part
2. Paste As Result With Link
Flat mode into another part
or in another Body of the
same part
You obtain a Solid (linked to
initial ASL part) where you
can add on Excess and Tabs
91. Student Notes:
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Drawing Generation
In this lesson you will learn to generate a drawing of an ASL part.
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Change to Drafting
Workbench and select an
empty sheet
Drawing Generation
1
Select the Unfolded
View icon
2
Select the web
on the part
3
Select a place on the sheet
where to locate the
flattened view
4
NB : the characteristic curves
are generated in the drawing
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Administration
In this lesson you will learn Administration Tasks.
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About Standards
Standards are embedded in the sheet metal part
Standards are administrator-defined
A standard file is available by default
Editing the standard file
The standard file can be edited using an interactive editor. This editor provides
an easy-to-use graphic interface to let you customize the parameters included
in the standard file.
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Setting Standard Parameters
Invisible curves Visible curves
Administrators can for instance :
Customize the graphic properties of characteristic curves in both 3D (Aerospace
Sheet metal Design workbench) and 2D views (Generative Drafting workbench).
Manage the visibility of all characteristic curves (BTL, IML, OML and 2nd OML) in
folded and unfolded 2D views through standards.
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Setting Parameters for a Designer
The designer can also Manage the visibility of all characteristic curves
(BTL, IML, OML and 2nd OML) in folded and unfolded 2D views through
standards. in Tools/Options/Mechanical Design/Aerospace Sheet Metal
Design with the display tab)
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Customizing Standards Files to define Design Tables
In the Sheet metal Parameters Window, you can choose the sheet standard files
and then select the values you want in the given design table.
In the example below, you can see that the thickness and default bend radius are
driven by design tables, hence they are grayed out (i.e. you can’t modify the values)
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How to use Knowledge Expert
In order to perform a clearance check, you can use the characteristic curves like IML
and OML in Check formulas, in the Knowledge Expert Workbench
Thus you can see if the security clearance is verified or not
99. Student Notes:
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To Sum Up
In this course you have learned how to:
Manage sheet metal parameters
Create and modify the design of an Hydro formed Sheet Metal Part by defining
its internal features:
Web
Surfacic Flanges
Joggles
Different kinds of flanges
Corner Relieves
Cutouts
Different kinds of Stamps
Holes
Points and Curves Mapping
Corners and Chamfers
Patterns
Generate a flattened part
Draw a flattened part
Fulfill some administration tasks
Create a Knowledge Expert Check using characteristic curves