FR2539701B1 - Fuselage composite pour helicoptere - Google Patents

Fuselage composite pour helicoptere

Info

Publication number
FR2539701B1
FR2539701B1 FR8400971A FR8400971A FR2539701B1 FR 2539701 B1 FR2539701 B1 FR 2539701B1 FR 8400971 A FR8400971 A FR 8400971A FR 8400971 A FR8400971 A FR 8400971A FR 2539701 B1 FR2539701 B1 FR 2539701B1
Authority
FR
France
Prior art keywords
helicopters
composite fuselage
fuselage
composite
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
FR8400971A
Other languages
English (en)
Other versions
FR2539701A1 (fr
Inventor
Reginald Ernest Swinfield
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.)
Westland Group PLC
Original Assignee
Westland PLC
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 Westland PLC filed Critical Westland PLC
Publication of FR2539701A1 publication Critical patent/FR2539701A1/fr
Application granted granted Critical
Publication of FR2539701B1 publication Critical patent/FR2539701B1/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
    • B64C1/068—Fuselage sections

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
FR8400971A 1983-01-25 1984-01-23 Fuselage composite pour helicoptere Expired FR2539701B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8301991 1983-01-25

Publications (2)

Publication Number Publication Date
FR2539701A1 FR2539701A1 (fr) 1984-07-27
FR2539701B1 true FR2539701B1 (fr) 1986-09-12

Family

ID=10536903

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8400971A Expired FR2539701B1 (fr) 1983-01-25 1984-01-23 Fuselage composite pour helicoptere

Country Status (4)

Country Link
US (1) US4531695A (fr)
DE (1) DE3401189A1 (fr)
FR (1) FR2539701B1 (fr)
IT (1) IT1178084B (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2632604B1 (fr) * 1988-06-08 1991-07-12 Aerospatiale Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication
DE3826636A1 (de) * 1988-08-05 1990-02-08 Messerschmitt Boelkow Blohm Cockpit, insbesondere fuer einen hubschrauber
JPH06255587A (ja) * 1993-03-09 1994-09-13 Honda Motor Co Ltd 航空機
DE4431612C2 (de) * 1993-09-06 1998-07-16 Sanyo Electric Co Akustisches Oberflächenwellenfilter
ES2112711B1 (es) * 1994-05-25 1998-12-01 Torres Martinez M Estructura para aviones.
JP3888630B2 (ja) * 2002-12-04 2007-03-07 川崎重工業株式会社 エネルギー吸収部材及びそれを用いるヘリコプタの耐衝撃構造
US7886873B2 (en) * 2003-02-06 2011-02-15 Swissfiber Ag Panel-type construction element
FR2896770B1 (fr) * 2006-01-27 2008-04-11 Eurocopter France Structure composite anti-crash a maintien lateral pour aeronef.
FR2903961B1 (fr) * 2006-07-21 2009-09-25 Eurocopter France Element structurel de cellule de giravion,son procede de fabrication,cellule de giravion et giravion comportant de tels elements structurels
CN101715411A (zh) * 2007-01-29 2010-05-26 空客运营有限公司 由复合材料制备的飞行器负载框架
RU2448865C2 (ru) * 2007-01-29 2012-04-27 Эйрбас Оперейшнз, С.Л. Силовой шпангоут летательного аппарата, изготовленный из композитного материала
FR2921899B1 (fr) * 2007-10-04 2011-04-15 Airbus France Procede de renforcement local d'un element en materiau composite, et caisson central de voilure pour aeronef renforce
FR2933066B1 (fr) * 2008-06-26 2010-09-10 Airbus France Element de fuselage d'aeronef
JP4918567B2 (ja) * 2009-04-20 2012-04-18 三菱重工業株式会社 衝撃吸収構造体およびその製造方法
US8317135B2 (en) * 2010-04-19 2012-11-27 Sabreliner Corporation Flexible mounting assembly for an air frame structure
EP2404824B1 (fr) * 2010-07-08 2015-09-09 Airbus Opérations SAS Structure d'aeronef et Procédé de réalisation d'une telle structure
US10099765B2 (en) * 2012-08-08 2018-10-16 The Boeing Company Monolithic composite structures for vehicles
FR3000018B1 (fr) * 2012-12-21 2016-12-09 Airbus Operations Sas Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur
EP2889212B1 (fr) * 2013-12-30 2016-01-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Structure de sous-plancher avec une coque intégral pour un aéronef à voilure tournante
EP2905228B1 (fr) * 2014-02-06 2018-01-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Cellule de fuselage et réservoir
PL2979975T3 (pl) * 2014-07-30 2018-01-31 Airbus Helicopters Deutschland GmbH Statek powietrzny ze strukturą ramową, która zawiera co najmniej jedną pustą ramę
US10053203B2 (en) * 2015-10-13 2018-08-21 The Boeing Company Composite stiffener with integral conductive element
RU2694638C2 (ru) * 2017-11-09 2019-07-16 Акционерное общество Научно-производственное объединение "Опытно-конструкторское бюро имени М.П. Симонова" Кессон фюзеляжа

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1966933A (en) * 1931-06-25 1934-07-17 Budd Edward G Mfg Co Structural assembly and method of assembling the same
US2604280A (en) * 1944-09-12 1952-07-22 Sncase Hollow structural element for vehicles and more especially for aircraft
CA928696A (en) * 1970-10-30 1973-06-19 C. Perazella John Composite stringer and method of making it
DE2639431A1 (de) * 1976-09-02 1978-03-09 Burkhart Dipl Ing Grob Vorrichtung an flugzeugruempfen aus faserverstaerkten kunststoffschalen
US4113910A (en) * 1977-04-27 1978-09-12 Rockwell International Corporation Composite load coupler for reinforcing composite structural joints

Also Published As

Publication number Publication date
FR2539701A1 (fr) 1984-07-27
IT1178084B (it) 1987-09-09
IT8447563A0 (it) 1984-01-19
US4531695A (en) 1985-07-30
DE3401189A1 (de) 1984-07-26

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Legal Events

Date Code Title Description
ST Notification of lapse