introduction to catia -gsc-aio sesion ed4
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CATIA documentTRANSCRIPT
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1MODULE 8: Engineering - Tool CAD/CAMAuthor: Fermn S. Rodrguez LagunaESI AIRBUS MILITARY
2011/2012
ESI - AIRBUS MILITARY
SESSION: Introduction to CATIA. CAD/CAM
MasterGSC&AIOGLOBALSUPPLYCHAIN&AERONAUTICALINDUSTRIALOPERATIONS
Module8:Engineering
Module: Engineering- Herramienta CAD/CAMAuthor: Fermn S. Rodrguez LagunaCompany: INALSYS Ingeniera y Anlisis de Sistemas
2011/2012
INDEX1.TolerancesChain2.ManufacturingSystembasedonCAD/CAM3.ToolCAD/CAMCATIAV.54.VirtualManufacturing TRAINING
4.1ApplicationCNC4.2ApplicationComposites4 3 Application Riveting4.3ApplicationRiveting4.4ToolingManufacturing
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2REFERENCE:
Diseo de Mquinas, A.S. Hall , A.R. Hollowenco H.G. Laughlin McGraw-Hill Anlisis estadstico de tolerancias, Jos M Gurruchaga Vzquez Di e i e T le ci Ge t ic A P i iti Re e Dimensiones y Tolerancias Geomtricas, A. Primitivo Reyes Tolerancias Dimensionales y Geomtricas-TGyD, Guillermo Navarrete
Herrera Comunicacin: Acotando el PDM. Aplicaciones Comerciales, D. Jenaro
Fernndez Martnez Expresin Grfina en la Ingeniera. OCW-UPM, Javier Prez lvarez Jos
Luis Prez Benedito Santiago Poveda Martnez Sistemas de Fabricacin AIRBUS Dassault Aviation and Dassault Falcon Jet Corp., 2011 Dassault Aviation and Dassault Falcon Jet Corp., 2011 Airbus S.A.S 2011 Curso de CATIA v.5 ESI FAG Documentacin Tcnica, ALU-Stock S.A.
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1. CHAIN OF TOLERANCE
1.1 Chain of tolerances in Aeronautics1.2 Process of Analysis. Reference Systems1.3 Metrology - Measurement Systems
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31.1 CHAIN OF TOLERANCES IN AERONAUTICS
Manufacturing tolerances:
The manufacturing processes introduced in the dimensions of the partserrors or deviations from established measures at the definition of them.
These deviations are due to:
- Games of the tools or machine tools used in the manufacture- Errors of measuring instruments or measuring operators- Errors of measuring instruments or measuring operators.- Dilation of the parts of bodies as a result of temperatures thatacquire parts to make them.- Deformations produced by the internal tensions of the pieces.
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What is the chain of tolerances for parts that are sets?
Likewise, in the aircraft industry where product complexity does not allow themanufacture of all components that make up an aircraft by a single manufacturer it ismanufacture of all components that make up an aircraft by a single manufacturer, it isnecessary a chain of companies that provide all the necessary elements for inclusionin the final product .
This can multiply the effects of manufacturing tolerances of each supplier.
Excellence in industrial products associated with the assembly of a product, it canbecome prohibitively expensive when offered a high precision, and often due to poortreatment tolerance.treatment tolerance.
It is necessary to offer a compromise between accuracy and dimensional tolerances.
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4FAL A400M
Airbus Militarys A400M multi-role transport aircraft has completed a series of tests to validate the lowest speed at which it can take off. (24 March 2011) March 2011 Airbus S.A.S 2011
Global Supply Chain A400MIntegration of more than 100,000 components
Proveedor SYSTEMSPOWER PLANT. ENGINE AND PROPELLER
Proveedor AvinicaProveedor Estruct.1
CENTRAL BOXProveedor Estruct.2
CONTROL SURFACEENGINE AND PROPELLER
Proveedor Estruct.3NOSE-PROA Proveedor SYSTEMS
Airbus Militarys A400M multi-role transport aircraft has completed a series of tests to validate the lowest speed at which it can take off. (24 March 2011) March 2011 Airbus S.A.S 2011
Proveedor TrenProveedor Estruct.4
GNDOLAS
NOSE PROA
Proveedor Estruct.5 Fuselaje
Proveedor SYSTEMS
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5Global Supply Chain A400MIntegration of more than 100,000 components
Proveedor SYSTEMSPOWER PLANT. ENGINE AND PROPELLER
Proveedor AvinicaProveedor Estruct.1
CENTRAL BOXProveedor Estruct.2
CONTROL SURFACE
Proveedor P1
Proveedor P1Proveedor A1 Proveedor A2
Proveedor CS1
Proveedor CS2
Proveedor CB1 Proveedor CB2
ENGINE AND PROPELLER
Proveedor Estruct.3NOSE-PROA Proveedor SYSTEMS
Proveedor P1
Proveedor 3NP1
Proveedor 3NP2Proveedor S1
Airbus Militarys A400M multi-role transport aircraft has completed a series of tests to validate the lowest speed at which it can take off. (24 March 2011) March 2011 Airbus S.A.S 2011
Proveedor TrenProveedor Estruct.4
GNDOLAS
NOSE PROA
Proveedor Estruct.5 Fuselaje
Proveedor SYSTEMS
Proveedor T1 Proveedor T2
Proveedor F1 Proveedor F2
Proveedor S2
Proveedor S3
Proveedor 3NP3
Proveedor G1 Proveedor G2
Global Supply Chain A400MPossible Existing Tolerances
Proveedor SYSTEMSPOWER PLANT. ENGINE AND PROPELLER
Proveedor AvinicaProveedor Estruct.1
CENTRAL BOXProveedor Estruct.2
CONTROL SURFACE
Proveedor P1
Proveedor P1Proveedor A1 Proveedor A2
Proveedor CS1
Proveedor CS2
Proveedor CB1 Proveedor CB2didi di di
di di
didi
ENGINE AND PROPELLER
Proveedor Estruct.3NOSE-PROA Proveedor SYSTEMS
Proveedor P1
Proveedor 3NP1
Proveedor 3NP2Proveedor S1
Tol. i
dididi
di didi
didi
didid
did
di
d
Airbus Militarys A400M multi-role transport aircraft has completed a series of tests to validate the lowest speed at which it can take off. (24 March 2011) March 2011 Airbus S.A.S 2011
Proveedor TrenProveedor Estruct.4
GNDOLAS
NOSE PROA
Proveedor Estruct.5 Fuselaje
Proveedor SYSTEMS
Proveedor T1 Proveedor T2
Proveedor F1 Proveedor F2
Proveedor S2
Proveedor S3
Proveedor 3NP3
Proveedor G1 Proveedor G2
didi
didi
di di di di
di
di
di
didi
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6Standards of Representation
By the standards we define and describe the tolerances of the lineardimensions for use in technical drawings.g
Tolerances indication of a method of representation does not involve theuse of a particular manufacturing method, measurement or control.
Standards:EN 20286 Sistema ISO de tolerancias
UNE 1129 T l i d t li lUNE 1129 Tolerancias de cotas linealesUNE 1122 Acotacin tolerancias conosUNE 1149 Principios de tolerancias fundamentales
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ISO System of Tolerance
Tolerances allo s stems establish criteria for conj gating the Tolerances allow systems establish criteria for conjugating thefunctional conditions of the errors of manufacturing processes,keeping the interchangeability.
Currently the most widely accepted is the ISO standard containedin the UNE 4-040 040-81, with variations of single-axis systems
i l h lor single hole.
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Characterization: Sample Rules EXTERNAL DIMENSIONAL FIGURE (axis) is at MMC when in its upper limit of size. INNER DIMENSIONAL FIGURE (hole) is to LMC when its set reference is sized greater than o.INNER DIMENSIONAL FIGURE (hole) is to LMC when its set reference is sized greater than o.
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81.2 REVIEW PROCESS. REFERENCE SYSTEMS
Analysis of Tolerances:Analysis of Tolerances:There will be based on standards and criteria and a system ofdimensional and geometric tolerances for the identification,evaluation, measurement and correction.
Reference Systems:C ll b t th t l i l i ti f th d tCollaborate on the metrological inspection of the productmanufactured and will be a function of the measurement methodadopted
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Dimensional and Geometric TolerancesGD&T: It is an internationally accepted language to specify areas ofparts tolerances on engineering drawings. Through this technicalparts tolerances on engineering drawings. Through this technicalsystem communicate to perform the design-Manufacturing-Inspectionof parts.
They should provide:- Communication between technical- The manufacture of the parts- The manufacture of the parts- Interchangeability of components
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9Reference Systems - Coordinates :Reference Systems must be based on a homogeneous
f C t i t Th RS h ld t b f dreference Cartesian system. The RS should not be confused.
Among the features that will need to define the different points of references are:
AccessiblePermanentReliables
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PROBLEMS OF TOLERANCEREJECTION!
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CYCLE ASSESSMENT OF TOLERANCE
PLANNING AND DESIGN
MANUFACTURINGCORRECTION
PROCESS
MEASUREMENTMETROLOGY
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In CAD designs start from dimensionally accurate parts.The product has dimensional changes in its geometry.Beware TGyD geometric figures that appear to be and they are not!Beware TGyD geometric figures that appear to be and they are not!
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Dimensional control of manufactured parts.
1.3 METROLOGY MEASURING SYSTEMS
CMM (Coordinate measuring machines)(PC-DMIS CMM software )Laser TrackerMeasuring ArmsMeasuring MicroscopesPhotometryPhotometryProbes
1. Radio-frecuency2. Software
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SYSTEM MMC CONVENTIONAL FIXTURE
Some comparative Measurement Systems :
INFORMATION High Basic RegularACCURACY Very Good Good NA
VELOCITY Good Low ExcelentINVESTMENT Highest Media LowTRAINEDPEOPLE
High Good Basic
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The need to avoid high values in the chain of manufacturingtolerances search sometimes leads to specialized laboratories :
Properly applied the concepts of TDyG, Have proper instrumentation for measurement, Have proper facilities for measurement,, Accredited / certified by a third party organization. Have the technology to provide an appropriate balance between:
CORRECTNESSTIME COST
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The problems of interpretation of dimensional tolerances generate: Conflicts provider vs. customer, both rely heavily on IM, but the case takes them to others. Use tools that do not meet the measurement capability sufficient to specified tolerances,(c 0.005mm / 1 m2)
CONSEQUENCES OF FAILURE CHAIN OF TOLERANCE: Stopping the production line.Lot cessation product or to its effective verification.P lt / i f t f i t ti i ll f t iPenalty / suspension for arrest of integration in all manufacturing
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Hamburg, Germany
Global Supply Chain A380
Broughton, Great Britain
Toulouse
Cdiz,Spain
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Global Supply Chain A380
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Chain integration tolerances in structural elements:
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Product Data Management (PDM)System management and production planning based on data management
2. Manufacturing system based on CAD/CAM
y g p p g gsupported by computer systems.
These systems are based on:
MAIN FEATURES PDM:Storage system and data and document managementProcess management and workflow(Workflow Management)Management structure of the productGrading and StandardizationgManaging the programmingPlanning, monitoring and control of activities and resources.(Work History Management)
Traditionally, each company has developed his "own"
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CAD and PDM systems whose relationship is directCompany CAD PDM Company
SDRC I-DEAS Metaphase SDRC p
SAP PDM SAP
MatrixOne MatrixOne
PTC Pro/Engineer Windchill PTC
EDS-UGS UNIGRAPHICS iMAN EDS-UGS
Dassault-IBM CATIA IBM-PLM Dassault-IBM
I t h I t h Intergraph Intergraph
Ariba(Agile) Agile Software-Ariba
Axalant Eigner + Partner
SmarTeam Smart Solutions MasterGSC&AIO
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This baseline lies the high weight that is assigned in the selectiong g gprocess to the relationship between the PDM system and the systemused CAD .
Here we must consider that although PDM systems have interfaceswith many CAD systems, the ideal situation suggests that PDMsystem should be the owner of the data and be CAD systems whichy ymade the connections, bridges, with the PDM system .
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The data are owned by the CAD system that produces them, being inthe role of PDM management system of references to documents.
Access to document data is possible only through the interface thatallows CAD program.
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CAD/CAM
SystemVirtual Manufacturing
PDM
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Evolution CATIA V.6 A PDM system to be considered as such, must develop the
capabilities attributed to him, but also must respect the structure thatis presupposed, otherwise some of the advantages of using thesep pp g gsystems can be depleted in the medium term.
Ownership of the data, the information model is to store them, mustrest with the PDM system and ultimately the owner-user PDMsystem. The possibility of modifying the model designed is anintrinsic feature of PDM system.
CATIA V.6PDM MODEL CAD/CAM
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INFRASTRUCTURE INTEGRATIONPRODUCTIONParts under virtual model
Management System - CAD / CAM Integrated
Infrastructure CAD/CAM
Manufacturing Management System (Material Resources)
Tooling design / manufacturing workbenches
Junction System(r)
Manufacturing Management System (Human Resources)
Specialists / Assemblers
OUTSOURCING
Parts under virtual model
y ( )
VirtualManufacturing
Tooling requirements
Materials integration
Infrastructure and auxiliary
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INFRASTRUCTURE INTEGRATIONPRODUCTIONParts under REAL model
Management System - MANUFACTURING
Infrastructure CAD/CAM
Manufacturing Management System (Material Resources)
Tooling design / manufacturing workbenches
Junction System(r)
Manufacturing Management System (Human Resources)
Specialists / Assemblers
OUTSOURCING
Parts under REAL model
y ( )
VirtualManufacturing
Tooling requirements
Materials integration
Infrastructure and auxiliary
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Dassault Falcon 7XAUTONOMY:. 5,950 nm (10.260 km)SPEED: To Mach .90 Maximum Operating Speed (MMO)SEATS 10 17SEATS:10-17
Passengers: 8Crew: 3 pilots, 1 flight attendant
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3. Tool CAD/CAM: CATIA V.5
CATIA (computer-aided three dimensional interactive application)It is an application CAD / CAM integrated with PDM support for thedesign, manufacturing and computer-aided engineering.
The program is developed to provide support from concept design toproduction and product analysis.production and product analysis.
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CATIA ,Organized in different application modules, each of which fulfills specific functions.
Given its breadth in terms of operational possibilities, CATIA is provided to you in p p p ydifferent configurations.
The most commonly corresponds to the one called Hybrid Design which comprises the following modules CATIA:
- SKETCHER: Generation from 2D sketches which generates the 3D.- PART DESIGN: Implementation of solid created based on the sketcher.- ASSEMBLY DESIGN: Assemblies of parts made individuallyp y- WIREFRAME AND SURFACE DESIGN: Generation of base areas- GENERATIVE SHAPE DESIGN: Advanced Surface Generation- DRAFTING: Creating implementation plans based on 3D
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APPLICATIONS CATIA V.5
Virtual Manufacturing PDM
Manufacturing Management
Tooling design Industrial Design
Machine Tools
oo g des g
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DEFINITION OF THE MOUSE IN CATIA
BUTTON SYMBOL EFFECT 2 PULSADO MUEVE EN PLANO PANTALLA
1
2 + UNA VEZ 1 (Y NO SUELTO 2) ZOOM
2 + 1 (FIJNDOLOS) GIRO en 3 D
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Ability to design and ergonomicanalysis of elements of the controli t t ti i ti linstrumentation in operationalposts.
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Implementation capacity of complete items of equipment and systems.
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Application to automotive
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Application for industrial manufacture as the production of metal profiles
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Application to the design of aeronautical structures and implementation of numerical control applications
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CATIA implementation of structural elements of the frames for the NC machining
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ThefirstoffiveA380sforChinaSouthernAi li t h d i H b GAirlinestouchesdowninHamburg,Germany,completingitssuccessfulmaidenflight(3March2011)
March2011AirbusS.A.S.2011
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Manufacture of a fuselage 22% A380
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Sending structural elements for final assembly line (FAL)
Application to the processing of all operational phases in the aircraft industry: Design- Manufacture and production (Lay-Out, desarrollo de utillaje,...) - FAL
All based on implementation of 3D digital models
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Component library 100% integrated with all major modules of CATIA V5
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TRAINING: 4.1 MANUFACTURING CNC
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TRAINING: 4.2 COMPOSITES MANUFACTURING
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INVAR structure with components used in the manufacture of tooling forforming processes composite material.
Invar also called Nivarox FeNi36 or is an iron alloy (64%) and nickelInvar, also called Nivarox FeNi36 or is an iron alloy (64%) and nickel(36%) with minor proportions of carbon and chromium.
Because of its small thermal expansion coefficient has a low coefficientof thermal expansion which enables parts processes either by dry or wetobtain very good tolerances.
H it i t i t d t l tHowever, its use is restricted to platessmall thickness on steel or aluminum basesdue to its high cost and weight.
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The A350 XWB programme reached a new industrial milestone with the successful curing of this new-generation jetliners largest composite fuselage panel, which was completed by Airbus partner Premium AEROTEC (18 March 2011). March 2011 Airbus S.A.S 2011 MasterGSC&AIO
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Due to strong market demand, Airbus will increase the production rate for its A330 Family of jetliners to ten aircraft per month (3 February 2011)February 2011 MasterGSC&AIO
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TRAINING: 4.3 MANUFACTURING RIVETING
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Integration componentsFixings:
Riveted joints - HilokjAbility to use nuts for torque controlManufacturing cost less than other piping systemsAvailable in a wide range of sizes
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load
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TRAINING: 4.4 MANUFACTURING EQUIPMENT
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Designing a useful setting for transport by ship manufacturing nose of aircraft. Use reference crane and coupling assembly mounted to the structural assembly.
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1. Lift truck2. Support beam3. Lifting gear and hook4 and 5. Support rail / guide (front ends) and Motor translation bridge6. Keypad / Remote7. Supply box bridge
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pp y g8 and 9. Carriage guide support beam connection10. Supply cable support structure / control car11. Cable car guide12. Cable car supply
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BRIDGE CRANE AT AIRBUS FACILITY GETAFE (MADRID)
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" "
Aristteles (384 AC-322 AC); Greek philosopher.
Questions
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