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BRPI0603142A - sistema de suporte para unidade de potência auxiliar - Google Patents

sistema de suporte para unidade de potência auxiliar

Info

Publication number
BRPI0603142A
BRPI0603142A BRPI0603142-0A BRPI0603142A BRPI0603142A BR PI0603142 A BRPI0603142 A BR PI0603142A BR PI0603142 A BRPI0603142 A BR PI0603142A BR PI0603142 A BRPI0603142 A BR PI0603142A
Authority
BR
Brazil
Prior art keywords
power unit
auxiliary power
support system
unit support
socket
Prior art date
Application number
BRPI0603142-0A
Other languages
English (en)
Inventor
Jose Roman Martinez Rueda
Jose Alberto Rojo Carrion
Jose Luis Sen Pacios
Juan Pablo Melian Brinquis
Nicolas Rojos Sainz
David Martin Calvo
Stefan Prys Thomas
Antonio Marquez Gavilan
Maria Aranzazu Garcia Patino
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 BRPI0603142A publication Critical patent/BRPI0603142A/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
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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)
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Battery Mounting, Suspending (AREA)
  • Motor Or Generator Frames (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

SISTEMA DE SUPORTE PARA UNIDADE DE POTêNCIA AUXILIAR Trata-se de um sistema de suporte para unidade de potência auxiliar (1) de uma aeronave a uma estrutura fixa (2) que pertence a um compartimento da unidade de potência auxiliar (6) da dita aeronave, feito de um material de alta resistência mecânica e com alta resistência à ignição, que compreende pelo menos três encaixes (3, 4, 5) de um formato substancialmente cilíndrico, sendo que os ditos encaixes (3, 4, 5) são capazes de ser ocos e, cada um deles apresenta uma primeira extremidade (7) que compreende um meio de fixação do sistema de suporte (8) à estrutura fixa (2) e uma segunda extremidade (9) que compreende um meio de segurar o sistema de suporte (8) que é unido à unidade de potência auxiliar (1) na periferia da extensão da dita unidade de potência auxiliar (1), com pelo menos um primeiro encaixe dianteiro (4) e um segundo encaixe dianteiro (5) estando localizado na parte dianteira da unidade de potência auxiliar (1) e pelo menos um encaixe traseiro (3) estando localizado na parte traseira da unidade de potência auxiliar (1).
BRPI0603142-0A 2005-10-28 2006-08-09 sistema de suporte para unidade de potência auxiliar BRPI0603142A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200502626A ES2336395B1 (es) 2005-10-28 2005-10-28 Sistema de soporte de motor auxiliar.

Publications (1)

Publication Number Publication Date
BRPI0603142A true BRPI0603142A (pt) 2007-08-14

Family

ID=37684870

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0603142-0A BRPI0603142A (pt) 2005-10-28 2006-08-09 sistema de suporte para unidade de potência auxiliar

Country Status (7)

Country Link
US (1) US7909286B2 (pt)
EP (1) EP1780125B1 (pt)
BR (1) BRPI0603142A (pt)
CA (1) CA2555070C (pt)
DE (1) DE602006004942D1 (pt)
ES (2) ES2336395B1 (pt)
RU (1) RU2412870C2 (pt)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9469412B2 (en) 2012-11-02 2016-10-18 United Technologies Corporation Redundant mount system
US8955809B2 (en) * 2012-12-05 2015-02-17 Hamilton Sundstrand Corporation Three-way mount bracket for aircraft cabin air supply system
US8979056B2 (en) * 2013-05-24 2015-03-17 Hamilton Sundstrand Corporation Cabin air compressor support bracket
US9146004B2 (en) * 2013-05-24 2015-09-29 Hamilton Sundstrand Corporation Cabin air compressor support bracket
US9278759B2 (en) 2013-05-24 2016-03-08 Hamilton Sundstrand Corporation Cabin air compressor cross-support bracket
EP2886448B1 (en) * 2013-12-20 2017-03-08 Airbus Operations GmbH A load bearing element and a method for manufacturing a load bearing element
US20150102179A1 (en) * 2014-12-22 2015-04-16 Caterpillar Inc. Bracket to mount aftercooler to engine
GB201621455D0 (en) * 2016-12-16 2017-02-01 Rolls Royce Plc Mount Structure

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2818225A (en) * 1954-03-15 1957-12-31 Rolls Royce Power plant installations for aircraft
US3151464A (en) * 1959-05-25 1964-10-06 Nippon Sharyo Seizo Kk Foundation piles
US3204897A (en) * 1962-10-25 1965-09-07 Aeroflex Lab Inc Vibration damping and load-supporting apparatus
US6247668B1 (en) * 1999-07-15 2001-06-19 The Boeing Company Auxiliary power and thrust unit
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
WO2002040347A2 (en) * 2000-09-27 2002-05-23 Lord Corporation Mounting assembly for an aircraft auxiliary power unit
US20060032974A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Modular installation kit for auxiliary power unit
US7419121B2 (en) * 2004-12-09 2008-09-02 Honeywell International Inc. Integrated mount duct for use with airborne auxiliary power units and other turbomachines
EP1866203B1 (en) * 2005-04-04 2011-06-08 Lord Corporation Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit

Also Published As

Publication number Publication date
US20070120037A1 (en) 2007-05-31
CA2555070C (en) 2011-10-04
RU2006128615A (ru) 2008-02-20
EP1780125A3 (en) 2008-01-16
DE602006004942D1 (de) 2009-03-12
ES2336395A1 (es) 2010-04-12
ES2321025T3 (es) 2009-06-01
RU2412870C2 (ru) 2011-02-27
EP1780125A2 (en) 2007-05-02
US7909286B2 (en) 2011-03-22
ES2336395B1 (es) 2011-02-14
EP1780125B1 (en) 2009-01-21
CA2555070A1 (en) 2007-04-28

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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: NOME 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 A 10A ANUIDADE.

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: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2385 DE 20-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.