JPS5734944A - Member, structure and its manufacture - Google Patents

Member, structure and its manufacture

Info

Publication number
JPS5734944A
JPS5734944A JP6109781A JP6109781A JPS5734944A JP S5734944 A JPS5734944 A JP S5734944A JP 6109781 A JP6109781 A JP 6109781A JP 6109781 A JP6109781 A JP 6109781A JP S5734944 A JPS5734944 A JP S5734944A
Authority
JP
Japan
Prior art keywords
fibres
joint
bundles
interdigitated
intersection
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.)
Pending
Application number
JP6109781A
Other languages
English (en)
Japanese (ja)
Inventor
Efu Roieku Aanii
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.)
RIA FUAN CORP
Original Assignee
RIA FUAN 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 RIA FUAN CORP filed Critical RIA FUAN CORP
Publication of JPS5734944A publication Critical patent/JPS5734944A/ja
Pending 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)
JP6109781A 1980-04-21 1981-04-21 Member, structure and its manufacture Pending JPS5734944A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14211880A 1980-04-21 1980-04-21

Publications (1)

Publication Number Publication Date
JPS5734944A true JPS5734944A (en) 1982-02-25

Family

ID=22498614

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6109781A Pending JPS5734944A (en) 1980-04-21 1981-04-21 Member, structure and its manufacture

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)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170967A (en) * 1990-02-28 1992-12-15 Fuji Jukogyo Kabushiki Kaisa Aircraft fuselage structure
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
JP2014144770A (ja) * 2013-01-26 2014-08-14 Boeing Co 荷重を担持するボックス構造体、およびその製作方法
KR20250156605A (ko) 2024-04-25 2025-11-03 가부시키가이샤 시마노 낚싯줄 가이드

Families Citing this family (8)

* 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
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
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

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170967A (en) * 1990-02-28 1992-12-15 Fuji Jukogyo Kabushiki Kaisa Aircraft fuselage structure
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
JP2014144770A (ja) * 2013-01-26 2014-08-14 Boeing Co 荷重を担持するボックス構造体、およびその製作方法
KR20250156605A (ko) 2024-04-25 2025-11-03 가부시키가이샤 시마노 낚싯줄 가이드

Also Published As

Publication number Publication date
CA1177459A (fr) 1984-11-06
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

Similar Documents

Publication Publication Date Title
US4177306A (en) Laminated sectional girder of fiber-reinforced materials
US4715560A (en) Composite cruciform structure for joining intersecting structural members of an airframe and the like
JPS5734944A (en) Member, structure and its manufacture
DE3583781D1 (de) Faserverstaerkte harzverbundmaterialien niedriger dichte.
MY103946A (en) Fibre reinforced plastics sheet
BR8300087A (pt) Estrutura de juncao de laminado composito e processo e aparelho para a formacao de uma estrutura de juncao de laminado composito
GB8400290D0 (en) Fibre reinforced plastics structures
ES296239U (es) Tirante de presion y compresion a base de plastico reforzado con fibras.
Matthews et al. The bolt bearing strength of glass/carbon hybrid composites
GB2010434A (en) Bolted, Flanged Joint
SE8702080L (sv) Stod- och festkonstruktion for en kolv-cylinderkombination eller motsvarande
US4491292A (en) Strut structure for suspending loads under aircraft
Baker Component form and manufacture
SE8202605L (sv) Sandwichelement
Hamada et al. Strength of mechanically fastened joint in flat braided composite
SUAREZ et al. Novel Composites for Wing and Fuselage Applications(Final Report, Jun. 1992- Sep. 1994)
Matthews et al. The Strength of Mechanically Fastened Joints inKevlar' Fibre-Reinforced Epoxy Resin
VANDREUMEL A short note on the compressive behaviour of aramid fibre reinforced plastics
Aboudi et al. The Mechanical Behaviour of Elastic--Plastic Fiber-Reinforced Laminated Plates
VANDREUMEL et al. Design and function of an experimental wing box using carbon fiber reinforced epoxy VATLIT-C'85
Buesking et al. Material Design of Racing Catamaran Structural Beams
Ger et al. Joint Strength of Graphite/Kevlar Hybrid Composites. I. Adhesive Bonded Joints
Dark Composites Structure Applications-Piper Cheyenne Iii
Knutsson Static test of a wing box structure made of composite materials, phase 1[Final Report]
Maekawa et al. Probabilistic design on strength of fiber reinforced composite laminates