IT1178084B - Fusoliera composita per elicottero - Google Patents

Fusoliera composita per elicottero

Info

Publication number
IT1178084B
IT1178084B IT47563/84A IT4756384A IT1178084B IT 1178084 B IT1178084 B IT 1178084B IT 47563/84 A IT47563/84 A IT 47563/84A IT 4756384 A IT4756384 A IT 4756384A IT 1178084 B IT1178084 B IT 1178084B
Authority
IT
Italy
Prior art keywords
helicopter
composite fuselage
fuselage
composite
Prior art date
Application number
IT47563/84A
Other languages
English (en)
Other versions
IT8447563A0 (it
Inventor
Reginald Ernest Swinfield
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 IT8447563A0 publication Critical patent/IT8447563A0/it
Application granted granted Critical
Publication of IT1178084B publication Critical patent/IT1178084B/it

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
IT47563/84A 1983-01-25 1984-01-19 Fusoliera composita per elicottero IT1178084B (it)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
IT8447563A0 IT8447563A0 (it) 1984-01-19
IT1178084B true IT1178084B (it) 1987-09-09

Family

ID=10536903

Family Applications (1)

Application Number Title Priority Date Filing Date
IT47563/84A IT1178084B (it) 1983-01-25 1984-01-19 Fusoliera composita per elicottero

Country Status (4)

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

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
DE4447740B4 (de) * 1993-09-06 2008-10-09 Sanyo Electric Co., Ltd., Moriguchi 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
DE50311738D1 (de) * 2003-02-06 2009-09-03 Swissfiber Ag Plattenförmiges konstruktionselement
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
RU2448865C2 (ru) * 2007-01-29 2012-04-27 Эйрбас Оперейшнз, С.Л. Силовой шпангоут летательного аппарата, изготовленный из композитного материала
WO2008092970A1 (es) * 2007-01-29 2008-08-07 Airbus España, S.L. Cuaderna de carga de aeronave en material compuesto
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 (en) * 2013-12-30 2016-01-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Subfloor structure with an integral hull for a rotary wing aircraft
EP2905228B1 (en) * 2014-02-06 2018-01-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Fuselage Airframe and Tank
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
DE3401189A1 (de) 1984-07-26
US4531695A (en) 1985-07-30
FR2539701A1 (fr) 1984-07-27
IT8447563A0 (it) 1984-01-19
FR2539701B1 (fr) 1986-09-12

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