CA1177459A - Structure composite pour joindre les traverses entrecroisees d'un planeur ou d'une structure similaire - Google Patents

Structure composite pour joindre les traverses entrecroisees d'un planeur ou d'une structure similaire

Info

Publication number
CA1177459A
CA1177459A CA000375674A CA375674A CA1177459A CA 1177459 A CA1177459 A CA 1177459A CA 000375674 A CA000375674 A CA 000375674A CA 375674 A CA375674 A CA 375674A CA 1177459 A CA1177459 A CA 1177459A
Authority
CA
Canada
Prior art keywords
fibers
bundles
structural
bundle
cruciform structure
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
Application number
CA000375674A
Other languages
English (en)
Inventor
Ernie F. Loyek
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.)
Lear Fan Corp
Original Assignee
Lear Fan 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
Application filed by Lear Fan Corp filed Critical Lear Fan Corp
Application granted granted Critical
Publication of CA1177459A publication Critical patent/CA1177459A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B64C1/062—Frames specially adapted to absorb crash loads
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Woven Fabrics (AREA)
CA000375674A 1980-04-21 1981-04-16 Structure composite pour joindre les traverses entrecroisees d'un planeur ou d'une structure similaire Expired CA1177459A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14211880A 1980-04-21 1980-04-21
US142,118 1980-04-21

Publications (1)

Publication Number Publication Date
CA1177459A true CA1177459A (fr) 1984-11-06

Family

ID=22498614

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000375674A Expired CA1177459A (fr) 1980-04-21 1981-04-16 Structure composite pour joindre les traverses entrecroisees d'un planeur ou d'une structure similaire

Country Status (5)

Country Link
JP (1) JPS5734944A (fr)
CA (1) CA1177459A (fr)
DE (1) DE3115791A1 (fr)
GB (1) GB2074117B (fr)
IT (1) IT1143497B (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4962904A (en) * 1984-06-07 1990-10-16 The Boeing Company Transition fitting for high strength composite
US4671470A (en) * 1985-07-15 1987-06-09 Beech Aircraft Corporation Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
JP2935722B2 (ja) * 1990-02-28 1999-08-16 富士重工業株式会社 航空機の胴体構造およびその成形方法
ES2131479B1 (es) * 1997-11-10 2000-03-01 Torres Martinez M Util y proceso de ensamblaje para soldadura laser.
DE102007054053A1 (de) * 2007-11-13 2009-05-20 Airbus Deutschland Gmbh Kupplungselement zur Verbindung von zwei Längsversteifungselementen
DE102007055233A1 (de) 2007-11-20 2009-05-28 Airbus Deutschland Gmbh Kupplungsvorrichtung zum Zusammenfügen von Rumpfsektionen, Kombination aus einer Kupplungsvorrichtung und zumindest einer Rumpfsektion sowie Verfahren zur Herstellung der Kupplungsvorrichtung
US8079549B2 (en) * 2008-06-30 2011-12-20 EMBRAER—Empresa Brasileira de Aeronautica S.A. Monolithic integrated structural panels especially useful for aircraft structures
US8973871B2 (en) * 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
DE102013219820A1 (de) * 2013-09-30 2015-04-02 Bayerische Motoren Werke Aktiengesellschaft Faserverbundwerkstoffbauteil, Verfahren zur Herstellung eines Faserverbundwerkstoffbauteils sowie Verwendung von Faserbündeln und Verstrebungsmitteln zur Herstellung eines Faserverbundwerkstoffbauteils
DE102014222933B4 (de) 2014-11-11 2021-09-09 Bayerische Motoren Werke Aktiengesellschaft Faserverbundwerkstoffbauteil sowie Verfahren zur Herstellung eines Faserverbundwerkstoffbauteils
JP2025167342A (ja) 2024-04-25 2025-11-07 株式会社シマノ 釣糸ガイド

Also Published As

Publication number Publication date
IT1143497B (it) 1986-10-22
GB2074117A (en) 1981-10-28
IT8167534A0 (it) 1981-04-17
DE3115791A1 (de) 1982-08-12
GB2074117B (en) 1984-07-25
JPS5734944A (en) 1982-02-25

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Legal Events

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