DE69910174D1 - Wissensbasierter Entwurfsoptimierungsprozess für Verbundwerkstoffe und System dafür - Google Patents

Wissensbasierter Entwurfsoptimierungsprozess für Verbundwerkstoffe und System dafür

Info

Publication number
DE69910174D1
DE69910174D1 DE69910174T DE69910174T DE69910174D1 DE 69910174 D1 DE69910174 D1 DE 69910174D1 DE 69910174 T DE69910174 T DE 69910174T DE 69910174 T DE69910174 T DE 69910174T DE 69910174 D1 DE69910174 D1 DE 69910174D1
Authority
DE
Germany
Prior art keywords
composites
knowledge
optimization process
system therefor
based design
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.)
Expired - Lifetime
Application number
DE69910174T
Other languages
English (en)
Other versions
DE69910174T3 (de
DE69910174T2 (de
Inventor
Virginia M Vasey-Glandon
Richard D Hale
Jeffrey J Schmitz
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.)
McDonnell Douglas Corp
Original Assignee
McDonnell Douglas Corp
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=8241317&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69910174(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by McDonnell Douglas Corp filed Critical McDonnell Douglas Corp
Priority to DE69910174T priority Critical patent/DE69910174T3/de
Publication of DE69910174D1 publication Critical patent/DE69910174D1/de
Application granted granted Critical
Publication of DE69910174T2 publication Critical patent/DE69910174T2/de
Publication of DE69910174T3 publication Critical patent/DE69910174T3/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F2111/00—Details relating to CAD techniques
    • G06F2111/06—Multi-objective optimisation, e.g. Pareto optimisation using simulated annealing [SA], ant colony algorithms or genetic algorithms [GA]
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F2113/00—Details relating to the application field
    • G06F2113/26—Composites

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Composite Materials (AREA)
  • Chemical & Material Sciences (AREA)
  • Evolutionary Computation (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Computer Hardware Design (AREA)
  • General Factory Administration (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
DE69910174T 1999-04-07 1999-04-07 Wissensbasierter Entwurfsoptimierungsprozess für Verbundwerkstoffe und System dafür Expired - Lifetime DE69910174T3 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE69910174T DE69910174T3 (de) 1999-04-07 1999-04-07 Wissensbasierter Entwurfsoptimierungsprozess für Verbundwerkstoffe und System dafür

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE69910174T DE69910174T3 (de) 1999-04-07 1999-04-07 Wissensbasierter Entwurfsoptimierungsprozess für Verbundwerkstoffe und System dafür
EP99302710A EP1050396B2 (de) 1999-04-07 1999-04-07 Wissensbasierter Entwurfsoptimierungsprozess für Verbundwerkstoffe und System dafür

Publications (3)

Publication Number Publication Date
DE69910174D1 true DE69910174D1 (de) 2003-09-11
DE69910174T2 DE69910174T2 (de) 2004-06-17
DE69910174T3 DE69910174T3 (de) 2012-03-08

Family

ID=8241317

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69910174T Expired - Lifetime DE69910174T3 (de) 1999-04-07 1999-04-07 Wissensbasierter Entwurfsoptimierungsprozess für Verbundwerkstoffe und System dafür

Country Status (2)

Country Link
EP (1) EP1050396B2 (de)
DE (1) DE69910174T3 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DK200401225A (da) * 2004-08-13 2006-02-14 Lm Glasfiber As Metode til afskæring af laminatlag, eksempelvis et glasfiber- eller kulfiber-laminatlag i en vindmöllevinge
EP1840775A1 (de) * 2006-03-31 2007-10-03 Airbus Espana, S.L. Computergestütztes Verfahren zum Erhalt eines Schichtmodells einer Verbundkomponente
US8321180B2 (en) 2007-10-25 2012-11-27 The Boeing Company Method and apparatus for composite part data extraction
US8285407B2 (en) 2007-10-25 2012-10-09 The Boeing Company Method and apparatus for composite part data extraction
US8442804B2 (en) 2007-10-25 2013-05-14 The Boeing Company Method and apparatus for composite part data extraction
ES2343824B1 (es) * 2007-12-21 2011-07-18 Airbus España S.L. Pieza de material compuesto con zonas de diferente espesor.
GB0820800D0 (en) 2008-11-13 2008-12-24 Airbus Uk Ltd Method of designing a composite laminate
ES2384920B1 (es) * 2009-03-31 2013-05-21 Airbus Operations, S.L. Pieza de material con una rampa entre dos zonas.
US8620627B2 (en) 2009-10-13 2013-12-31 The Boeing Company Composite information display for a part
ES2385004B1 (es) * 2009-12-31 2013-05-27 Airbus Operations, S.L. Pieza de material compuesto con larguerillo en rampa.
US8993084B2 (en) 2010-08-17 2015-03-31 The Boeing Company Multi-layer metallic structure and composite-to-metal joint methods
US8652606B2 (en) 2010-08-17 2014-02-18 The Boeing Company Composite structures having composite-to-metal joints and method for making the same
US9522512B2 (en) 2010-08-17 2016-12-20 The Boeing Company Methods for making composite structures having composite-to-metal joints
US9582616B2 (en) * 2015-01-23 2017-02-28 Siemens Product Lifecycle Management Software Inc. Method for representing and generating a flat pattern for a composite ply that folds over itself
US10345791B2 (en) * 2015-09-21 2019-07-09 Siemens Product Lifecycle Management Software Inc. System and method for distributing multiple layers of a composite within a structural volume containing an inclusion
GB201518285D0 (en) 2015-10-15 2015-12-02 Composite Technology & Applic Ltd A method of designing a plybook for a composite component
DE102018126910A1 (de) * 2018-10-29 2020-04-30 Airbus Operations Gmbh Verfahren zum Herstellen eines bereichsweise flächigen Bauteils aus einem Faserverbundwerkstoff
US20200210546A1 (en) 2019-01-02 2020-07-02 Shinc Inc. Systems and methods for generating a design for a gliding board
US11806948B2 (en) 2019-12-12 2023-11-07 The Boeing Company Method of forming flyaway stringer end caps
US11718047B2 (en) 2019-12-12 2023-08-08 The Boeing Company Flyaway stringer end caps
EP4060547A1 (de) * 2021-03-17 2022-09-21 Subaru Corporation Verfahren zum entwerfen von verbundlaminaten und flugzeug

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4849913A (en) * 1987-04-10 1989-07-18 The Boeing Company Method for the design and construction of composite parts
US5038291A (en) * 1989-04-03 1991-08-06 General Electric Company Computerized ply pattern generation
CA2198717C (en) † 1994-08-31 2005-03-15 William C. Reinfelder Fiber reinforced composite spar for a rotary wing aircraft and method of manufacture thereof
JP2955201B2 (ja) * 1995-02-24 1999-10-04 美津濃株式会社 キャンバーの温度依存性が少ないスキー板の材料選定方法

Also Published As

Publication number Publication date
EP1050396B1 (de) 2003-08-06
EP1050396A1 (de) 2000-11-08
EP1050396B2 (de) 2011-10-05
DE69910174T3 (de) 2012-03-08
DE69910174T2 (de) 2004-06-17

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