RU93036838A - HELICOPTER FUSELAGE - Google Patents

HELICOPTER FUSELAGE

Info

Publication number
RU93036838A
RU93036838A RU93036838/11A RU93036838A RU93036838A RU 93036838 A RU93036838 A RU 93036838A RU 93036838/11 A RU93036838/11 A RU 93036838/11A RU 93036838 A RU93036838 A RU 93036838A RU 93036838 A RU93036838 A RU 93036838A
Authority
RU
Russia
Prior art keywords
fuselage
power frame
central
helicopter fuselage
shape
Prior art date
Application number
RU93036838/11A
Other languages
Russian (ru)
Other versions
RU2090450C1 (en
Inventor
Бьетанадер Клод
Original Assignee
Эрокоптер Франс
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
Priority claimed from FR929209052A external-priority patent/FR2693976B1/en
Application filed by Эрокоптер Франс filed Critical Эрокоптер Франс
Publication of RU93036838A publication Critical patent/RU93036838A/en
Application granted granted Critical
Publication of RU2090450C1 publication Critical patent/RU2090450C1/en

Links

Claims (1)

Данное изобретение касается конструкции фюзеляжа вертолета, содержащему центральную конструкцию, с которой связаны передняя конструкция, задняя конструкция и посадочное шасси и которая содержит и является опорой для редуктора трансмиссии, несущего винта и по меньшей мере одного двигателя, центральная конструкция фюзеляжа содержит силовой каркас, снабженный элементами обшивки, определяющими внешние формы этого фюзеляжа. Силовой каркас центральной конструкции фюзеляжа обладает формой правильного шестигранника, образованного соединенными между собой панелями силового каркаса. Данное изобретение находит применение, в частности, при изготовлении фюзеляжей легких вертолетов.The present invention relates to a helicopter fuselage structure comprising a central structure to which a front structure, a rear structure and a landing gear are connected and which comprises and is a support for a transmission reducer, a rotor and at least one engine, the central fuselage structure comprises a power frame provided with elements casing, determining the external shape of this fuselage. The power frame of the central fuselage structure has the shape of a regular hexagon formed by interconnected panels of the power frame. This invention finds application, in particular, in the manufacture of fuselages of light helicopters.
RU9393036838A 1992-07-22 1993-07-21 Helicopter fuselage RU2090450C1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9209052 1992-07-22
FR929209052A FR2693976B1 (en) 1992-07-22 1992-07-22 Fuselage structure for helicopter.

Publications (2)

Publication Number Publication Date
RU93036838A true RU93036838A (en) 1996-11-27
RU2090450C1 RU2090450C1 (en) 1997-09-20

Family

ID=9432148

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9393036838A RU2090450C1 (en) 1992-07-22 1993-07-21 Helicopter fuselage

Country Status (10)

Country Link
US (1) US5562264A (en)
EP (1) EP0581626B2 (en)
JP (1) JP3342744B2 (en)
CN (1) CN1030303C (en)
CA (1) CA2100428C (en)
DE (1) DE69302242T3 (en)
ES (1) ES2088245T5 (en)
FR (1) FR2693976B1 (en)
PL (1) PL299742A1 (en)
RU (1) RU2090450C1 (en)

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CN104210642B (en) * 2014-09-16 2016-09-07 天峋创新（北京）科技有限公司 A kind of depopulated helicopter airframe structure of housing load
CN104527963B (en) * 2014-12-16 2017-08-25 深圳清华大学研究院 Basin type composite helicopter fuselage
CN104590583B (en) * 2014-12-19 2016-06-29 四川精石航空科技开发有限公司 A kind of frock for microlight-type helicopter main frame
CN105836100B (en) * 2015-01-15 2018-11-06 空客直升机 There is the rotary-wing craft fuselage structure of load-bearing middle layer between two space of cabin and equipment
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CN106516076A (en) * 2016-11-08 2017-03-22 芜湖万户航空航天科技有限公司 Unmanned helicopter upper plate and installation method thereof
CN106428511A (en) * 2016-11-08 2017-02-22 芜湖万户航空航天科技有限公司 Unmanned helicopter body middle plate and fixing method
EP3333072B1 (en) * 2016-12-07 2020-02-05 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An aircraft with an airframe that comprises a load carrying framework
EP3378788B1 (en) * 2017-03-22 2021-04-28 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An aircraft with a fuselage that comprises at least one hollow beam element
CN107651161B (en) * 2017-09-08 2020-12-01 中国航空工业集团公司沈阳飞机设计研究所 Universal aircraft cabin beam and design method thereof
CN108910013A (en) * 2018-08-23 2018-11-30 西安三翼航空科技有限公司 A kind of fast disassembly type fuselage wing attachment structure
FR3089946B1 (en) * 2018-12-18 2021-01-08 Airbus Operations Sas structure of a FUSELAGE OF AN aircraft presenting a panel reinforced by a trellis
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