CA2583780A1 - Virtual programming of formed component trajectories - Google Patents

Virtual programming of formed component trajectories Download PDF

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Publication number
CA2583780A1
CA2583780A1 CA002583780A CA2583780A CA2583780A1 CA 2583780 A1 CA2583780 A1 CA 2583780A1 CA 002583780 A CA002583780 A CA 002583780A CA 2583780 A CA2583780 A CA 2583780A CA 2583780 A1 CA2583780 A1 CA 2583780A1
Authority
CA
Canada
Prior art keywords
computer
forming
blank
formed component
computer file
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002583780A
Other languages
French (fr)
Other versions
CA2583780C (en
Inventor
Daniel B. Bergstrom
Jeffrey M. Shoup
Albert Mcguire Hines
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Howmet Aerospace Inc
Original Assignee
Alcoa Inc.
Daniel B. Bergstrom
Jeffrey M. Shoup
Albert Mcguire Hines
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alcoa Inc., Daniel B. Bergstrom, Jeffrey M. Shoup, Albert Mcguire Hines filed Critical Alcoa Inc.
Publication of CA2583780A1 publication Critical patent/CA2583780A1/en
Application granted granted Critical
Publication of CA2583780C publication Critical patent/CA2583780C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D7/00Bending rods, profiles, or tubes
    • B21D7/12Bending rods, profiles, or tubes with programme control
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/18Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form
    • G05B19/4097Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by using design data to control NC machines, e.g. CAD/CAM
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/23Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/30Nc systems
    • G05B2219/35Nc in input of data, input till input file format
    • G05B2219/35192From design derive sequence of bending so that bending is possible
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/30Nc systems
    • G05B2219/36Nc in input of data, input key till input tape
    • G05B2219/36203Bending of workpiece, also for long slender workpiece
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/30Nc systems
    • G05B2219/45Nc applications
    • G05B2219/45143Press-brake, bending machine

Abstract

This invention discloses a method for calculating gripper trajectories in forming equipment. The method utilizes a computer aided design (CAD) or a computer aided engineering (CAE) computer program to calculate the appropriate location, speed, controller commands, and trajectory for each gripper used during a forming process.

Claims (11)

1. A method for calculating forming equipment component trajectories comprised of:

providing a forming die;

using a computer aided design (CAD) or a computer aided engineering (CAE) computer program to extend tangents from said forming die at various positions through the forming cycle, said tangents correspond to the location of one or more grippers during a forming process;

calculating the wrap angle, tension, elevation, tilt, and twist of each of said grippers at each of said tangents;

recording the wrap angle, tension, elevation, tilt and twist of each of said grippers at said tangent locations into a first computer file;

recording the initial gripper positions, amount of pre- and post-stretch imparted on a blank, and initial blank size into said first computer file; and inputting said first computer file into a first computer program to calculate an appropriate location, speed, controller commands, and trajectory for said grippers during said forming process, said first computer program produces an output that is then recorded in a second computer file that is read and executed by said forming equipment thereby producing a product with the desired part geometry.
2. The method for calculating forming equipment component trajectories according to claim 1 wherein providing a stationary or non-stationary forming die.
3. The method for calculating forming equipment component trajectories according to claim 1 further comprising inputting said first computer file into a second computer program that can model said forming process using the data stored on said first computer file.
4. The method for calculating forming equipment component trajectories according to claim 1 further comprising transmitting said second computer file to said forming equipment via a computer network, telephone network, or a wireless network.
5. A formed component manufactured from the method comprising:
providing a forming die;

using a computer aided design (CAD) or a computer aided engineering (CAE) computer program to extend tangents from said forming die at various positions through the forming cycle, said tangents correspond to the location of one or more grippers during a forming process;

calculating the wrap angle, tension, elevation, tilt, and twist of each of said grippers at each of said tangents;

recording the wrap angle, tension, elevation, tilt and twist of each of said grippers at said tangent locations into a first computer file;

recording the initial gripper positions, amount of pre- and post-stretch imparted on a blank, and initial blank size into said first computer file; and inputting said first computer file into a first computer program to calculate an appropriate location, speed, controller commands, and trajectory for said grippers during said forming process, said first computer program produces an output that is then recorded in a second computer file that is read and executed by said forming equipment thereby producing said formed component with the desired part geometry.
6. The formed component according to claim 5 wherein said blank is manufactured from a deformable material.
7. The formed component according to claim 6 wherein said blank is manufactured from a metal or a metal alloy.
8. The formed component according to claim 7 wherein said metal or metal alloy an aluminum or an aluminum alloy.
9. The formed component according to claim 8 where said blank is manufactured from an aluminum alloy selected from the Aluminum Association's 1XXX, 2XXX, 3XXX, 4XXX, 5XXX, 6XXX, 7XXX, or 8XXX series of aluminum alloys.
10. The formed component according to claim 6 wherein said blank is manufactured from a non-metallic material.
11. The formed component according to claim 10 wherein said non-metallic material is a plastic or a polymer.
CA2583780A 2004-10-25 2005-10-25 Virtual programming of formed component trajectories Expired - Fee Related CA2583780C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US62224204P 2004-10-25 2004-10-25
US60/622,242 2004-10-25
PCT/US2005/038469 WO2006047549A2 (en) 2004-10-25 2005-10-25 Virtual programming of formed component trajectories

Publications (2)

Publication Number Publication Date
CA2583780A1 true CA2583780A1 (en) 2006-05-04
CA2583780C CA2583780C (en) 2012-01-24

Family

ID=36228396

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2583780A Expired - Fee Related CA2583780C (en) 2004-10-25 2005-10-25 Virtual programming of formed component trajectories

Country Status (8)

Country Link
US (1) US7257461B2 (en)
EP (1) EP1817707B1 (en)
AT (1) ATE446534T1 (en)
CA (1) CA2583780C (en)
DE (1) DE602005017301D1 (en)
DK (1) DK1817707T3 (en)
MX (1) MX2007004988A (en)
WO (1) WO2006047549A2 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150149124A1 (en) * 2008-12-09 2015-05-28 The Boeing Company Aircraft system verification
DE102009024262A1 (en) * 2009-06-05 2010-12-09 Rosenberger Ag Method for bending elongated workpieces
JP5848535B2 (en) * 2011-07-05 2016-01-27 川崎重工業株式会社 Stretch forming device
JP5848534B2 (en) * 2011-07-05 2016-01-27 川崎重工業株式会社 Stretch forming method and system
CN104438496B (en) * 2014-10-10 2016-09-14 北京航空航天大学 A kind of curved couveuse of section bar hot-drawn and temperature control system thereof
US11113437B2 (en) * 2017-09-30 2021-09-07 Siemens Aktiengesellschaft Joint hardware and controller design
US11766712B2 (en) * 2020-10-21 2023-09-26 Ford Global Technologies, Llc Method of manufacturing a vehicle panel to reduce deviation between pre-panels and subsequent secondary forming dies
CN112007982B (en) * 2020-10-28 2021-01-29 广东高谱弯曲技术有限公司 Working platform for stretch bending of section bar

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5528921A (en) * 1994-05-03 1996-06-25 Herman; Fred L. Tube bending appartus
US5969973A (en) * 1994-11-09 1999-10-19 Amada Company, Ltd. Intelligent system for generating and executing a sheet metal bending plan
US5822207A (en) * 1996-05-06 1998-10-13 Amadasoft America, Inc. Apparatus and method for integrating intelligent manufacturing system with expert sheet metal planning and bending system
US5971589A (en) * 1996-05-06 1999-10-26 Amadasoft America, Inc. Apparatus and method for managing and distributing design and manufacturing information throughout a sheet metal production facility
IT1283019B1 (en) * 1996-05-16 1998-04-03 Salvagnini Italia Spa MANAGEMENT METHOD OF A WORKING ISLAND INCLUDING A ROBOT SUBJECTED TO A BENDING PRESS FOR PROCESSING SHEETS.
EP1087278A3 (en) * 1999-09-24 2004-12-22 Honda Giken Kogyo Kabushiki Kaisha Method of generating control data for bending and torsion apparatuses
US6769733B2 (en) * 2001-10-16 2004-08-03 Alcoa Inc. Bulkhead assembly for a motor vehicle
FI112922B (en) * 2002-06-14 2004-02-13 Finn Power Oy Procedure for controlling a machine tool cell
DE102004008870A1 (en) * 2003-03-31 2004-10-14 Anders, Peter, Prof. Dr.-Ing. Bending method for a workpiece such as a rod or tube for use in e.g. spinal surgery where a target curve is defined about which the rod is bent

Also Published As

Publication number Publication date
US7257461B2 (en) 2007-08-14
US20060122726A1 (en) 2006-06-08
EP1817707A2 (en) 2007-08-15
CA2583780C (en) 2012-01-24
WO2006047549A2 (en) 2006-05-04
DK1817707T3 (en) 2010-03-01
EP1817707B1 (en) 2009-10-21
ATE446534T1 (en) 2009-11-15
WO2006047549A3 (en) 2007-03-01
EP1817707A4 (en) 2008-12-10
MX2007004988A (en) 2007-06-12
DE602005017301D1 (en) 2009-12-03

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Effective date: 20141027