BRPI0401810A - Suspensão de turbomotor a um montante de avião - Google Patents

Suspensão de turbomotor a um montante de avião

Info

Publication number
BRPI0401810A
BRPI0401810A BR0401810-9A BRPI0401810A BRPI0401810A BR PI0401810 A BRPI0401810 A BR PI0401810A BR PI0401810 A BRPI0401810 A BR PI0401810A BR PI0401810 A BRPI0401810 A BR PI0401810A
Authority
BR
Brazil
Prior art keywords
suspension
ferrule
rocker
airplane
riser
Prior art date
Application number
BR0401810-9A
Other languages
English (en)
Inventor
Jean-Claude Felix Pasquer
Philippe Loewenstein
Marc Tesniere
Original Assignee
Snecma Moteurs
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 Snecma Moteurs filed Critical Snecma Moteurs
Publication of BRPI0401810A publication Critical patent/BRPI0401810A/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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transmission Devices (AREA)
  • Vehicle Body Suspensions (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Supercharger (AREA)

Abstract

"SUSPENSãO DE TURBOMOTOR A UM MONTANTE DE AVIãO". A presente invenção tem como objetivo uma suspensão de turbomotor a um montante de avião, que compreende uma virola (12) adaptada para ser fixada ao montante, um balancim (15) fixado em sua parte central (150) à virola por um meio de ligação com um eixo de pivotamento (15OP), e duas bielas de compensação de impulsão (20, 22) ligadas cada uma delas por uma extremidade com o balancim e que compreendem na outra extremidade meios de fixação com o motor. Ela é caracterizada pelo fato de que o dito meio de ligação é constituído na dita parte central (150) do balancim por dois ramos (151, 152) paralelos distantes um do outro, e na virola por uma aba de fixação central (133), a aba de fixação e os dois ramos sendo mantidos juntos por intermédio do dito eixo de pivotamento (150P). A invenção permite simplificar a fabricação das peças que constituem a suspensão, trazendo uma resistência estrutural melhorada.
BR0401810-9A 2003-05-27 2004-05-24 Suspensão de turbomotor a um montante de avião BRPI0401810A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0306437A FR2855496B1 (fr) 2003-05-27 2003-05-27 Suspension arriere de moteur d'avion avec reprise de poussee

Publications (1)

Publication Number Publication Date
BRPI0401810A true BRPI0401810A (pt) 2005-01-18

Family

ID=33104492

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0401810-9A BRPI0401810A (pt) 2003-05-27 2004-05-24 Suspensão de turbomotor a um montante de avião

Country Status (9)

Country Link
US (1) US7108224B2 (pt)
EP (1) EP1481897B1 (pt)
JP (1) JP2004352232A (pt)
BR (1) BRPI0401810A (pt)
CA (1) CA2469871A1 (pt)
DE (1) DE602004000113T2 (pt)
ES (1) ES2250955T3 (pt)
FR (1) FR2855496B1 (pt)
RU (1) RU2004116116A (pt)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0328671D0 (en) * 2003-12-11 2004-01-14 Rolls Royce Plc Aircraft engine mounting
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
US20070057128A1 (en) * 2005-09-14 2007-03-15 Honeywell International, Inc. Auxiliary power unit case flange to plate adapter
FR2891253B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
GB0603539D0 (en) * 2006-02-22 2006-04-05 Airbus Uk Ltd Control surface failsafe drop link
FR2903382B1 (fr) * 2006-07-10 2008-10-10 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal
FR2903383B1 (fr) * 2006-07-10 2009-05-15 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a double liaison mecanique arriere
FR2914908B1 (fr) * 2007-04-13 2009-10-30 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif.
FR2914907B1 (fr) * 2007-04-16 2009-10-30 Snecma Sa Suspension souple avec peigne pour turbomoteur
FR2915175B1 (fr) * 2007-04-20 2009-07-17 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson
FR2917712B1 (fr) * 2007-06-20 2009-09-25 Airbus France Sas Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere formant palonnier.
FR2918644B1 (fr) * 2007-07-09 2009-10-23 Airbus France Sas Mat d'accrochage de moteur pour aeronef disposant d'un palonnier articule en quatre points.
FR2920138B1 (fr) * 2007-08-24 2010-03-12 Airbus France Dispositif d'accrochage de moteur d'aeronef comportant un dispositif de reprise des efforts de poussee a encombrement reduit
GB0810585D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
GB0810589D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
GB0810791D0 (en) * 2008-06-13 2008-07-23 Rolls Royce Plc Thrust mounting arrangement
GB0902909D0 (en) * 2009-02-23 2009-04-08 Rolls Royce Plc A thrust mount arrangement for an aircraft engine
FR2959210B1 (fr) * 2010-04-21 2013-08-23 Snecma Palonnier de suspension de turboreacteur d'aeronef et suspension avec accroche-soufflante ainsi equipee
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
US9016623B2 (en) * 2011-11-30 2015-04-28 The Boeing Company Jam protection and alleviation for control surface linkage mechanisms
US9410441B2 (en) 2012-09-13 2016-08-09 Pratt & Whitney Canada Corp. Turboprop engine with compressor turbine shroud
US9211955B1 (en) 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
US8979020B2 (en) * 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
FR3008450B1 (fr) * 2013-07-09 2015-08-07 Snecma Carter de turbomachine a bride decoupee
CA2918320C (en) 2013-07-26 2018-05-15 Mra Systems, Inc. Aircraft engine pylon
FR3013077B1 (fr) * 2013-11-08 2015-11-20 Snecma Turbomachine comportant des moyens de support d'au moins un equipement
FR3020343B1 (fr) * 2014-04-23 2017-10-27 Airbus Operations Sas Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage constituee par trois elements independants
FR3032180B1 (fr) * 2015-01-30 2018-05-18 Airbus Operations Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure
USD880279S1 (en) * 2017-12-11 2020-04-07 Marchesan Implementos E Maquinas Agricolas Tatu S.A. Support bracket
US11077954B2 (en) * 2017-12-20 2021-08-03 General Electric Company Connection assembly for mounting engine and engine mounting system comprising the same
US11970278B2 (en) * 2020-07-14 2024-04-30 General Electric Company Thrust mounts with load-balancing thrust link-lever
CN112977804B (zh) * 2021-03-26 2023-03-24 陕西飞机工业有限责任公司 一种舵面锁
FR3122164B1 (fr) * 2021-04-27 2023-06-02 Airbus Operations Sas Dispositif de liaison reliant un moteur d’aéronef et une structure primaire d’un mât d’aéronef comprenant un palonnier ainsi qu’un système de limitation du débattement du palonnier intégrant une double butée, aéronef comprenant un tel dispositif de liaison
FR3127202A1 (fr) 2021-09-20 2023-03-24 Airbus Operations (S.A.S.) Ensemble de motorisation d’aéronef comprenant un dispositif de reprise d’efforts de poussée

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US183160A (en) * 1876-10-10 Improvement in composite metallic girders
US4012549A (en) * 1974-10-10 1977-03-15 General Dynamics Corporation High strength composite structure
US5320307A (en) 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5505030A (en) * 1994-03-14 1996-04-09 Hardcore Composites, Ltd. Composite reinforced structures
US5657595A (en) * 1995-06-29 1997-08-19 Hexcel-Fyfe Co., L.L.C. Fabric reinforced beam and column connections
US5725181A (en) 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
US6037060A (en) * 1996-11-04 2000-03-14 The Boeing Company Sol for bonding expoxies to aluminum or titanium alloys
US5958578A (en) * 1996-11-04 1999-09-28 The Boeing Company Hybrid laminate having improved metal-to-resin adhesion
US5849110A (en) * 1996-11-04 1998-12-15 The Boeing Company Sol coating of metals
US5869141A (en) * 1996-11-04 1999-02-09 The Boeing Company Surface pretreatment for sol coating of metals
US5814137A (en) * 1996-11-04 1998-09-29 The Boeing Company Sol for coating metals
US5873547A (en) 1997-05-20 1999-02-23 The Boeing Company Aircraft engine thrust mount
US6224020B1 (en) * 1998-12-24 2001-05-01 Alliant Techsystems, Inc. Payload fairing with improved acoustic suppression
FR2806699B1 (fr) 2000-03-22 2002-05-10 Aerospatiale Matra Airbus Dispositif de reprise de poussee apte a relier un turbomoteur et un mat d'aeronef
US6394394B1 (en) * 2000-05-09 2002-05-28 Alliant Techsystems Inc. Payload fairing with jettisonable mass acoustic suppression
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
FR2830516B1 (fr) * 2001-10-04 2004-01-02 Snecma Moteurs Suspension de turboreacteur
FR2830515B1 (fr) * 2001-10-04 2004-01-30 Snecma Moteurs Suspension de turboreacteur
US7197852B2 (en) * 2002-09-20 2007-04-03 The Boeing Company Internally stiffened composite panels and methods for their manufacture
US6910659B2 (en) * 2002-10-22 2005-06-28 The Boeing Company Method and apparatus for liquid containment, such as for aircraft fuel vessels

Also Published As

Publication number Publication date
JP2004352232A (ja) 2004-12-16
DE602004000113D1 (de) 2005-11-10
US20040251380A1 (en) 2004-12-16
FR2855496B1 (fr) 2006-09-22
EP1481897A1 (fr) 2004-12-01
ES2250955T3 (es) 2006-04-16
EP1481897B1 (fr) 2005-10-05
CA2469871A1 (fr) 2004-11-27
US7108224B2 (en) 2006-09-19
FR2855496A1 (fr) 2004-12-03
DE602004000113T2 (de) 2006-06-29
RU2004116116A (ru) 2005-11-10

Similar Documents

Publication Publication Date Title
BRPI0401810A (pt) Suspensão de turbomotor a um montante de avião
BRPI0402464A (pt) Suspensão de turbomotor a um montante de avião
CN106428578A (zh) 用于飞行器的发动机组件和包括此发动机组件的飞行器
CN102947181B (zh) 通过安全悬挂系统附接到飞机机身的外挂架上的涡轮轴发动机
BRPI0817591A2 (pt) Conjunto de propulsão para aeronave
FR2883256B1 (fr) Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef
DE602007002714D1 (de) Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel
BRPI0510912A (pt) aeronave de múltiplos motores
RU2011123883A (ru) Воздухозаборник авиационного двигателя с толкающими воздушными винтами, не заключенными в обтекатель
BR112012001965B8 (pt) viga para a suspensão de um turbomotor na estrutura de uma aeronave, utilização de uma viga, e, aeronave
CN101809311B (zh) 用于飞机喷气发动机用叶栅型推力反向器遮挡件的弹簧
CN103954427B (zh) 舵面模型两自由度支撑机构
FR2900206B1 (fr) Liaison autobloquante entre une piece plane et une tige a extremite spherique.
BR112012010291A2 (pt) turbomáquina de fdluxo duplo para aeronave
ATE341484T1 (de) Aufhängevorrichtung eines flugzeugtriebwerks an einem flügelpylon
CN106553759B (zh) 一种航空器用双油门控制系统及其航空器
CN119142539A (zh) 具有喷气发动机、挂架和用于将喷气发动机附接到挂架的装置的飞行器推进组件
FR2981048B1 (fr) Pylone d'accrochage pour suspension de moteur d'aeronef, et suspension avec un tel pylone
CN105564657A (zh) 用于飞行器发动机的前发动机附接件和飞行器
JP2015533716A5 (pt)
US2718267A (en) Blade cuff
Cen et al. Structural bionics for reinforcing frame of fuselage and wing joint
PL435001A1 (pl) Mechanizm ruchu skrzydła statku powietrznego, w szczególności bezzałogowego samolotu
Phillips New twist on an old wing theory
CN111439391B (zh) 一种双发动机侧向约束装置

Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]