BRPI0513869A - conjunto motor para aeronave, e, aeronave - Google Patents

conjunto motor para aeronave, e, aeronave

Info

Publication number
BRPI0513869A
BRPI0513869A BRPI0513869-8A BRPI0513869A BRPI0513869A BR PI0513869 A BRPI0513869 A BR PI0513869A BR PI0513869 A BRPI0513869 A BR PI0513869A BR PI0513869 A BRPI0513869 A BR PI0513869A
Authority
BR
Brazil
Prior art keywords
aircraft
turbomotor
engine assembly
lyans
compensation
Prior art date
Application number
BRPI0513869-8A
Other languages
English (en)
Inventor
Lionel Diochon
Isabelle Petrissans
Guillaume Seguin
Original Assignee
Airbus France
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 France filed Critical Airbus France
Publication of BRPI0513869A publication Critical patent/BRPI0513869A/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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Vibration Prevention Devices (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Retarders (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Motor Power Transmission Devices (AREA)
  • Connection Of Plates (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)

Abstract

CONJUNTO MOTOR PARA AERONAVE, E, AERONAVE A invenção se refere a um conjunto motor (1) para aeronave que compreende um turbomotor (2), um mastro de fixação (4) assim como uma pluralidade de liames de motor (6a, 6b, 8) interpostos entre o mastro de fixação (4) e o turbomotor (2). De acordo com a invenção, a pluralidade de liames de motor compreende dois liames dianteiros (6a, 6b) dispostos de modo deslocado um em relação ao outro em uma direção vertical (Z) desse turbomotor (2), o primeiro liame dianteiro (6a) sendo projetado de maneira a assegurar unicamente a compensação dos esforços que são exercidos de acordo com a direção transversal (Y) do turbomotor (2), enquanto que o segundo liame dianteiro (6b) é projetado de maneira a assegurar unicamente a compensação dos esforços que são exercidos de acordo com as direções transversal (Y) e vertical (Z).
BRPI0513869-8A 2004-08-04 2005-08-01 conjunto motor para aeronave, e, aeronave BRPI0513869A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0451785A FR2873986B1 (fr) 2004-08-04 2004-08-04 Ensemble moteur pour aeronef
PCT/FR2005/050638 WO2006021722A1 (fr) 2004-08-04 2005-08-01 Ensemble moteur pour aeronef

Publications (1)

Publication Number Publication Date
BRPI0513869A true BRPI0513869A (pt) 2008-05-20

Family

ID=34948381

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0513869-8A BRPI0513869A (pt) 2004-08-04 2005-08-01 conjunto motor para aeronave, e, aeronave

Country Status (11)

Country Link
US (1) US7770840B2 (pt)
EP (1) EP1773659B9 (pt)
JP (1) JP4607963B2 (pt)
CN (1) CN100471759C (pt)
AT (1) ATE432874T1 (pt)
BR (1) BRPI0513869A (pt)
CA (1) CA2575982C (pt)
DE (1) DE602005014777D1 (pt)
FR (1) FR2873986B1 (pt)
RU (1) RU2381148C2 (pt)
WO (1) WO2006021722A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI118761B (fi) * 2006-02-09 2008-03-14 Patria Aerostructures Oy Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki
FR2926788B1 (fr) * 2008-01-25 2010-04-02 Snecma Fixation d'un turboreacteur multiflux a un aeronef
FR2928181B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central.
FR2928136B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR2928180B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur.
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2933073B1 (fr) * 2008-06-25 2010-06-04 Aircelle Sa Ensemble d'entree d'air de nacelle de moteur d'avion
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2948636B1 (fr) * 2009-07-31 2012-01-13 Airbus Operations Sas Ensemble moteur pour aeronef dont le mat d'accrochage comprend une enveloppe structurale formant delimitation radiale interne du flux secondaire
US9637241B2 (en) 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
FR3027873B1 (fr) * 2014-11-03 2016-12-23 Airbus Operations Sas Attache moteur avant pour un moteur d'aeronef
FR3040369B1 (fr) * 2015-09-02 2018-07-13 Airbus Operations Sas Ensemble moteur d'aeronef comprenant une attache moteur avant amelioree
US10093436B2 (en) * 2016-06-23 2018-10-09 General Electric Company Wireless aircraft engine communication system

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1328410A (en) * 1969-11-29 1973-08-30 Ver Flugtechnische Werke Aircraft engine mounting means
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
FR2676707B1 (fr) * 1991-05-23 1993-08-13 Snecma Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.
GB9125011D0 (en) * 1991-11-25 1992-01-22 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
US5303880A (en) * 1992-10-28 1994-04-19 General Electric Company Aircraft engine pin mount
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
WO1996011843A1 (en) * 1994-10-18 1996-04-25 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
US5620154A (en) * 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
FR2770486B1 (fr) * 1997-11-06 2000-01-28 Aerospatiale Dispositif d'accrochage d'un moteur sur un aeronef
FR2793768B1 (fr) * 1999-05-17 2001-09-07 Aerospatiale Airbus Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif
FR2793769B1 (fr) * 1999-05-19 2001-09-07 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef a un mat
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
FR2820402B1 (fr) * 2001-02-08 2003-05-02 Eads Airbus Sa Dispositif d'accrochage d'un moteur sur un aeronef
FR2883256B1 (fr) * 2005-03-18 2008-10-24 Airbus France Sas Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef
FR2894934B1 (fr) * 2005-12-15 2009-11-13 Airbus France Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente

Also Published As

Publication number Publication date
ATE432874T1 (de) 2009-06-15
JP2008509319A (ja) 2008-03-27
WO2006021722A1 (fr) 2006-03-02
RU2381148C2 (ru) 2010-02-10
CN101014497A (zh) 2007-08-08
RU2007107927A (ru) 2008-09-10
EP1773659B1 (fr) 2009-06-03
US7770840B2 (en) 2010-08-10
JP4607963B2 (ja) 2011-01-05
CA2575982C (fr) 2013-06-25
US20070205323A1 (en) 2007-09-06
CA2575982A1 (fr) 2006-03-02
EP1773659A1 (fr) 2007-04-18
EP1773659B9 (fr) 2009-09-09
FR2873986A1 (fr) 2006-02-10
DE602005014777D1 (de) 2009-07-16
FR2873986B1 (fr) 2007-12-21
CN100471759C (zh) 2009-03-25

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B06T Formal requirements before examination [chapter 6.20 patent gazette]
B11E Dismissal acc. art. 34 of ipl - requirements for examination incomplete
B11T Dismissal of application maintained [chapter 11.20 patent gazette]