BRPI0702980A - cone de cauda para aeronave - Google Patents

cone de cauda para aeronave

Info

Publication number
BRPI0702980A
BRPI0702980A BRPI0702980-2A BRPI0702980A BRPI0702980A BR PI0702980 A BRPI0702980 A BR PI0702980A BR PI0702980 A BRPI0702980 A BR PI0702980A BR PI0702980 A BRPI0702980 A BR PI0702980A
Authority
BR
Brazil
Prior art keywords
tail cone
generator unit
auxiliary generator
support structure
cover
Prior art date
Application number
BRPI0702980-2A
Other languages
English (en)
Inventor
Esteban Martino Gonzalez
Pablo Timoteo Sanz Martinez
David Alvaro Granero
Original Assignee
Airbus Espa A S L
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 Airbus Espa A S L filed Critical Airbus Espa A S L
Publication of BRPI0702980A publication Critical patent/BRPI0702980A/pt

Links

Classifications

    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/08—Inspection panels for power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • B64D2041/002—Mounting arrangements for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Sealing Devices (AREA)
  • Tents Or Canopies (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

CONE DE CAUDA PARA AERONAVE Trata-se de um cone de cauda para aeronave com carenagem móvel e estrutura de suporte para unidade de gerador auxiliar e os elementos acessórios da mesma. Cone de cauda (2) para aeronave (1) com um alojamento de cobertura (8) de uma unidade de gerador auxiliar (3) e os sistemas acessórios da mesma (6,7), e a cobertura (8) apresenta uma seção frontal fixa (11) por meio da qual o cone de cauda (2) está preso ao restante da fuselagem (4), e uma carenagem móvel (9), alojando a estrutura de suporte (10) fixada à seção frontal fixa (11) que dá suporte à unidade de gerador auxiliar (3) e os sistemas acessórios da mesma (6,7). A carenagem móvel (9) move-se por meio de processos articulados ou, de preferência, longitudinalmente por meio de trilhos telescópicos (16) fixados à seção frontal fixa (11), a partir de uma posição fechada na qual a cobertura (8) permanece fechada alojando no interior da mesma a estrutura de suporte (10) com a unidade de gerador auxiliar (3) e os elementos acessórios da mesma (6,7), e em uma posição aberta na qual a cobertura (8) permanece aberta deixando a estrutura de suporte (10) com a unidade de gerador auxiliar (3) e os elementos acessórios da mesma (6,7) expostos, proporcionando a possibilidade de acesso à mesma para propósitos de manutenção, reparo ou substituição.
BRPI0702980-2A 2006-10-31 2007-06-22 cone de cauda para aeronave BRPI0702980A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200602770A ES2316257B1 (es) 2006-10-31 2006-10-31 Cono de cola para aeronave con carena movil y estructura de soporte de unidad auxiliar de energia y de sus elementos anexos.

Publications (1)

Publication Number Publication Date
BRPI0702980A true BRPI0702980A (pt) 2008-06-24

Family

ID=38658591

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0702980-2A BRPI0702980A (pt) 2006-10-31 2007-06-22 cone de cauda para aeronave

Country Status (6)

Country Link
US (1) US20080099611A1 (pt)
EP (1) EP1918203B1 (pt)
BR (1) BRPI0702980A (pt)
CA (1) CA2590892A1 (pt)
DE (1) DE602007005577D1 (pt)
ES (1) ES2316257B1 (pt)

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DE102006027707A1 (de) * 2006-06-14 2007-12-20 Airbus Deutschland Gmbh Heckstruktur für ein Luft- oder Raumfahrzeug
FR2928137B1 (fr) 2008-02-29 2010-08-20 Airbus France Systeme de propulsion arriere d'avion fixe par poutres et avion comportant un tel systeme.
EP2285674A4 (en) * 2008-05-23 2013-12-18 David Birkenstock SYSTEM FOR BORDER HEAD CONTROL AND CORRESPONDING METHODS
ES2358650B1 (es) * 2008-05-30 2012-03-23 Airbus Operations, S.L. Configuración de la instalación neum�?tica en la zona de cola de un avión.
DE102008040213B4 (de) * 2008-07-07 2011-08-25 Airbus Operations GmbH, 21129 Verfahren zur Montage eines kalottenförmigen Druckschotts in einer Hecksektion eines Flugzeugs sowie Vorrichtung zur Durchführung des Verfahrens
ES2345808B1 (es) * 2009-03-31 2011-07-28 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil deslizante.
ES2350429B1 (es) 2009-05-28 2011-11-18 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil abatible
FR2946955B1 (fr) * 2009-06-17 2012-09-21 Airbus Aeronef pourvu d'un systeme de pile a combustible.
ES2394581B1 (es) * 2010-04-26 2013-12-12 Airbus Operation, S.L Cono de cola del fuselaje trasero de un avion con una unidad de potencia auxiliar
US8631637B2 (en) 2010-07-30 2014-01-21 Hamilton Sundstrand Corporation Auxiliary power unit fire enclosure
US8820045B2 (en) 2010-07-30 2014-09-02 United Technologies Corporation Auxiliary power unit fire enclosure drain seal
US8991759B2 (en) * 2010-09-24 2015-03-31 Airbus Operations, S.L. Rear fuselage of an aircraft
ES2398861B1 (es) * 2010-10-08 2014-04-29 Airbus Operations, S.L. Concepto de unión intercambiable para un cono de un fuselaje trasero de un avión.
US8622342B2 (en) * 2011-06-17 2014-01-07 Embraer S.A. On-board aircraft auxiliary power systems having dual auxiliary power units
US8444083B2 (en) * 2011-06-30 2013-05-21 Hamilton Sundstrand Corporation Auxiliary power unit inlet
US9188065B2 (en) * 2011-08-03 2015-11-17 Hamilton Sundstrand Corporation APU selective cool down cycle
CN102673792B (zh) * 2012-06-08 2014-12-24 中国航空工业集团公司西安飞机设计研究所 一种蚕茧包裹式辅助动力装置防火罩
EP3040264B1 (en) * 2014-12-30 2018-07-11 Airbus Operations S.L. Fuselage rear end of an aircraft
ES2763875T3 (es) 2015-12-15 2020-06-01 Airbus Operations Sl Sistema de suspensión para una unidad de potencia auxiliar
EP3199455B1 (en) * 2016-01-29 2020-04-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotary aircraft with an interface frame joining the fuselage tail boom and the tail cone
JP2017154553A (ja) * 2016-02-29 2017-09-07 三菱航空機株式会社 航空機
ES2918124T3 (es) * 2017-11-24 2022-07-13 Airbus Operations Sl Aeronave con un sistema de montaje y desmontaje hacia atrás de un motor y método para el desmontaje hacia atrás de un motor
CN107878764B (zh) * 2017-11-29 2020-12-29 中国直升机设计研究所 一种整流罩防火墙排气管整体滑动结构
ES2732306B2 (es) * 2018-05-21 2021-06-18 Alestis Aerospace S L Metodo de fabricacion de un cono de cola
US11794873B2 (en) 2019-03-08 2023-10-24 The Boeing Company Auxiliary power unit enclosure and method of making the same
CN110877746B (zh) * 2019-12-09 2023-02-10 中航沈飞民用飞机有限责任公司 一种辅助动力装置排气管支撑配套装置
FR3115764B1 (fr) * 2020-11-02 2023-04-14 Safran Nacelles Ensemble propulsif d’aéronef comprenant une nacelle et une turbomachine indépendamment supportées par un élément de voilure ou de fuselage ou d’empennage
CN113636089B (zh) * 2021-08-25 2023-07-21 成都飞机工业（集团）有限责任公司 一种细长双发进气道结构及装配方法
EP4296158A1 (en) * 2022-06-23 2023-12-27 Airbus Operations GmbH Variable fairing for a hydrogen duct system installation and uses of the same

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US3532275A (en) * 1967-11-09 1970-10-06 Rohr Corp Jet reverser drive system
US3575260A (en) * 1969-05-15 1971-04-20 Rohr Corp Method and apparatus for augmenting the thrust of a jet-propelled aircraft and suppressing the noise thereof
US3604662A (en) * 1970-01-19 1971-09-14 Rohr Corp Thrust-reversing apparatus for jet-propelled aircraft
GB1375868A (pt) * 1972-09-22 1974-11-27
FR2291091A1 (fr) * 1974-11-13 1976-06-11 Snecma Dispositif de montage sur avion d'un turboreacteur
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Also Published As

Publication number Publication date
CA2590892A1 (en) 2008-04-30
ES2316257A1 (es) 2009-04-01
EP1918203A1 (en) 2008-05-07
ES2316257B1 (es) 2010-01-12
US20080099611A1 (en) 2008-05-01
EP1918203B1 (en) 2010-03-31
DE602007005577D1 (de) 2010-05-12

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS, S.L. (ES)

Free format text: ALTERADO DE: AIRBUS ESPANA, S.L.

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 4A E 5A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2161 DE 05/06/2012.