ES2088245T3 - Estructura de fuselaje para helicoptero. - Google Patents

Estructura de fuselaje para helicoptero.

Info

Publication number
ES2088245T3
ES2088245T3 ES93401698T ES93401698T ES2088245T3 ES 2088245 T3 ES2088245 T3 ES 2088245T3 ES 93401698 T ES93401698 T ES 93401698T ES 93401698 T ES93401698 T ES 93401698T ES 2088245 T3 ES2088245 T3 ES 2088245T3
Authority
ES
Spain
Prior art keywords
skeleton
helicopter
fuselage
central structure
fuselage 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 - Lifetime
Application number
ES93401698T
Other languages
English (en)
Other versions
ES2088245T5 (es
Inventor
Claude Bietenhader
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.)
Airbus Helicopters SAS
Original Assignee
Eurocopter France SA
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9432148&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ES2088245(T3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Eurocopter France SA filed Critical Eurocopter France SA
Publication of ES2088245T3 publication Critical patent/ES2088245T3/es
Application granted granted Critical
Publication of ES2088245T5 publication Critical patent/ES2088245T5/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2211/00—Modular constructions of airplanes or helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D2011/0069—Rest berths, beds or the like
    • B64D2011/0092—Arrangements for mounting stretchers in aircraft cabins
    • 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)
  • Body Structure For Vehicles (AREA)
  • Toys (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
  • General Details Of Gearings (AREA)

Abstract

LA INVENCION CONCIERNE A UN FUSELAJE DE HELICOPTERO DEL TIPO QUE COMPORTA UNA ESTRUCTURA TRASERA Y UN TREN DE ATERRIZAJE, Y QUE SOPORTA UNA CAJA DE TRANSMISION, UN ROTOR PRINCIPAL Y AL MENOS UN MOTOR (50), Y DEL TIPO EN EL CUAL LA ESTRUCTURA CENTRAL COMPORTA UN ESQUELETO (16) PROVISTO DE ELEMENTOS DE GUARNECIDO QUE DEFINEN LA FORMA EXTERIOR DEL FUSELAJE. SEGUN LA INVENCION, EL ESQUELETO (16) DE LA ESTRUCTURA CENTRAL PRESENTA SENSIBLEMENTE LA FORMA DE UN HEXAEDRO REGULAR CONSTITUIDO POR PANELES DE ESQUELETO (28, 30, 32, 34, 36, 38) ENSAMBLADOS ENTRE ELLOS. LA INVENCION ENCUENTRA EN PARTICULAR SU APLICACION PARA LA REALIZACION DE HELICOPTEROS LIGEROS.
ES93401698T 1992-07-22 1993-06-30 Estructura de fuselaje para helicoptero. Expired - Lifetime ES2088245T5 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9209052 1992-07-22
FR929209052A FR2693976B1 (fr) 1992-07-22 1992-07-22 Structure de fuselage pour hélicoptère.

Publications (2)

Publication Number Publication Date
ES2088245T3 true ES2088245T3 (es) 1996-08-01
ES2088245T5 ES2088245T5 (es) 2004-04-01

Family

ID=9432148

Family Applications (1)

Application Number Title Priority Date Filing Date
ES93401698T Expired - Lifetime ES2088245T5 (es) 1992-07-22 1993-06-30 Estructura de fuselaje para helicoptero.

Country Status (10)

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

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FR2769584B1 (fr) * 1997-10-14 2002-12-06 Rene Mouille Agencement d'helicoptere permettant d'obtenir une famille d'helicopteres de longueurs differentes
DE19802242C2 (de) * 1998-01-22 1999-11-11 Akzo Nobel Nv Stich- und Kugelschutzkleidung
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ITTO20010327A1 (it) * 2001-04-04 2002-10-04 Augusta S P A Veicolo di soccorso.
RU2186000C1 (ru) * 2001-08-24 2002-07-27 Открытое акционерное общество "Казанский вертолетный завод" Фюзеляж вертолета
US6729576B2 (en) * 2002-08-13 2004-05-04 Sikorsky Aircraft Corporation Composite tail cone assembly
RU2278059C1 (ru) * 2004-12-24 2006-06-20 Открытое акционерное общество "Камов" Фюзеляж вертолета
FR2884801B1 (fr) 2005-04-22 2008-11-14 Eurocopter France Atterrisseur auxillaire de nez, structure porteuse et aeronef a voilure tournante
FR2884802B1 (fr) * 2005-04-22 2008-11-14 Eurocopter France Structure porteuse et aeronef a voilure tournante
US7275717B2 (en) * 2005-05-18 2007-10-02 Bell Helicopter Textron Inc. Helicopter one-piece door
US8920594B2 (en) * 2005-08-03 2014-12-30 Sikorsky Aircraft Corporation Composite thermoplastic matrix airframe structure and method of manufacture therefore
FR2896768B1 (fr) * 2006-01-27 2009-10-09 Eurocopter France Structure composite anti-crash a flambage controle pour aeronef.
RU2324622C2 (ru) * 2006-05-18 2008-05-20 Открытое акционерное общество "Камов" Фюзеляж легкого вертолета
FR2921898B1 (fr) * 2007-10-08 2009-12-11 Airbus France Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage
WO2009048881A2 (en) * 2007-10-12 2009-04-16 Abe Karem Composite bulkhead and skin construction
DE102008016104A1 (de) * 2008-03-28 2009-10-08 Airbus Deutschland Gmbh Durchbrandsicherer Flugzeugrumpf
FR2933066B1 (fr) * 2008-06-26 2010-09-10 Airbus France Element de fuselage d'aeronef
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US8667663B2 (en) 2008-12-05 2014-03-11 Sikorsky Aircraft Corporation Eccentric fitting assembly
AU2012267260B2 (en) * 2011-06-07 2017-03-30 Innova Helicopters Technology Holdings Nz Limited A helicopter
CN102514707B (zh) * 2011-12-22 2014-07-16 天津曙光敬业科技有限公司 电动无人驾驶直升机桥梁式机身结构
USD678172S1 (en) * 2012-02-10 2013-03-19 Bell Helicopter Textron Inc. Helicopter front windshields
CN103818543B (zh) * 2012-11-16 2016-03-30 哈尔滨飞机工业集团有限责任公司 一种直升机盒型复合材料机身结构
ITMO20130082A1 (it) * 2013-03-29 2014-09-30 Konner S R L Struttura per aeromobili
RU2539612C2 (ru) * 2013-04-23 2015-01-20 Закрытое акционерное общество "АВИА-ПРОЕКТ" Конструкция силового каркаса ветролета
FR3012791B1 (fr) 2013-11-05 2015-12-11 Eurocopter France Structure de fuselage d'un giravion integrant un plancher median travaillant interpose entre un local habitable et un local technique
FR3012795B1 (fr) * 2013-11-05 2015-12-04 Eurocopter France Giravion equipe de reservoirs a carburant montes par suspension sous un plancher median travaillant du fuselage du giravion
EP2878433B1 (en) 2013-11-29 2016-04-20 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Shrouded rotary assembly from segmented composite for aircraft and method for its manufacture
EP2889212B1 (en) * 2013-12-30 2016-01-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Subfloor structure with an integral hull for a rotary wing aircraft
US9399507B2 (en) * 2014-01-22 2016-07-26 The Boeing Company Joints between a composite skin and a load-bearing component and methods of forming same
CN104210642B (zh) * 2014-09-16 2016-09-07 天峋创新（北京）科技有限公司 一种壳体承力的无人直升机机身结构
CN104527963B (zh) * 2014-12-16 2017-08-25 深圳清华大学研究院 盆型复合材料直升机机身
CN104590583B (zh) * 2014-12-19 2016-06-29 四川精石航空科技开发有限公司 一种用于超轻型直升飞机主框架的工装
CN105836100B (zh) * 2015-01-15 2018-11-06 空客直升机 机舱和设备两空间之间有承重中间层的旋翼飞行器机身结构
CH710657A1 (de) * 2015-01-28 2016-07-29 Marenco Swisshelicopter Ag Hubschrauberkabine.
CN106516076A (zh) * 2016-11-08 2017-03-22 芜湖万户航空航天科技有限公司 无人直升机上板及其安装方法
CN106428511A (zh) * 2016-11-08 2017-02-22 芜湖万户航空航天科技有限公司 无人直升机机身中板以及固定方法
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 (zh) * 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 一种通用飞机座舱梁及其设计方法
CN108910013A (zh) * 2018-08-23 2018-11-30 西安三翼航空科技有限公司 一种快拆式机身机翼连接结构
FR3089946B1 (fr) * 2018-12-18 2021-01-08 Airbus Operations Sas structure d’un FUSELAGE D’UN aeronef présentant un panneau renforcé par un treillis
FR3105777B1 (fr) * 2019-12-27 2022-09-09 Airbus Operations Sas Poutre ventrale en forme de diapason pour aéronef à soute ventrale
USD928071S1 (en) * 2020-01-22 2021-08-17 Kopter Group Ag Helicopter
CN112407229A (zh) * 2020-10-30 2021-02-26 中国直升机设计研究所 一种无人直升机机身传力结构组件
CN113086237B (zh) * 2021-04-20 2023-03-14 中国直升机设计研究所 一种共轴旋翼直升机主减速器连接撑杆设计方法
RU208098U1 (ru) * 2021-05-24 2021-12-02 Закрытое акционерное общество "Инновационный центр "Бирюч" (ЗАО "ИЦ "Бирюч") Кабина летательного аппарата вертикального взлета и посадки со сдвигающимся фонарем
WO2023135275A1 (fr) * 2022-01-14 2023-07-20 Roze Mobility Aeronef a voilure tournante a usage mixte, a chaine cinematique alignee
CN115743646B (zh) * 2022-11-25 2025-07-04 北京中航智科技有限公司 一种一体式的无人直升机主机体

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Also Published As

Publication number Publication date
RU2090450C1 (ru) 1997-09-20
FR2693976A1 (fr) 1994-01-28
PL299742A1 (en) 1994-01-24
JPH06156390A (ja) 1994-06-03
CN1030303C (zh) 1995-11-22
EP0581626A1 (fr) 1994-02-02
EP0581626B2 (fr) 2003-07-02
CN1083788A (zh) 1994-03-16
ES2088245T5 (es) 2004-04-01
DE69302242T2 (de) 1996-09-19
FR2693976B1 (fr) 1994-09-30
EP0581626B1 (fr) 1996-04-17
DE69302242D1 (de) 1996-05-23
JP3342744B2 (ja) 2002-11-11
CA2100428A1 (fr) 1994-01-23
US5562264A (en) 1996-10-08
CA2100428C (fr) 2002-02-05
DE69302242T3 (de) 2004-03-11

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