BR112014006998A2 - conjunto de propulsão de aeronave compreendendo um motor turbojato - Google Patents

conjunto de propulsão de aeronave compreendendo um motor turbojato

Info

Publication number
BR112014006998A2
BR112014006998A2 BR112014006998A BR112014006998A BR112014006998A2 BR 112014006998 A2 BR112014006998 A2 BR 112014006998A2 BR 112014006998 A BR112014006998 A BR 112014006998A BR 112014006998 A BR112014006998 A BR 112014006998A BR 112014006998 A2 BR112014006998 A2 BR 112014006998A2
Authority
BR
Brazil
Prior art keywords
turbojet engine
propulsion assembly
aircraft propulsion
aircraft
assembly
Prior art date
Application number
BR112014006998A
Other languages
English (en)
Inventor
Dezeustre Nicolas
Original Assignee
Aircelle 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
Application filed by Aircelle Sa filed Critical Aircelle Sa
Publication of BR112014006998A2 publication Critical patent/BR112014006998A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/10Aircraft characterised by the type or position of power plants of gas-turbine type 
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/404Suspension arrangements specially adapted for supporting vertical loads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/406Suspension 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)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
BR112014006998A 2011-10-06 2012-10-05 conjunto de propulsão de aeronave compreendendo um motor turbojato BR112014006998A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1159010A FR2981047B1 (fr) 2011-10-06 2011-10-06 Ensemble propulsif d'aeronef
PCT/FR2012/052259 WO2013050714A1 (fr) 2011-10-06 2012-10-05 Ensemble propulsif d'aéronef

Publications (1)

Publication Number Publication Date
BR112014006998A2 true BR112014006998A2 (pt) 2017-04-11

Family

ID=47071403

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014006998A BR112014006998A2 (pt) 2011-10-06 2012-10-05 conjunto de propulsão de aeronave compreendendo um motor turbojato

Country Status (8)

Country Link
US (1) US20140217234A1 (pt)
EP (1) EP2763897A1 (pt)
CN (1) CN103874633A (pt)
BR (1) BR112014006998A2 (pt)
CA (1) CA2849239A1 (pt)
FR (1) FR2981047B1 (pt)
RU (1) RU2014117114A (pt)
WO (1) WO2013050714A1 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9637241B2 (en) * 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
FR3010700B1 (fr) * 2013-09-18 2017-11-03 Snecma Dispositif de suspension d'un carter, turbomachine et ensemble propulsif
US9896217B2 (en) * 2016-01-07 2018-02-20 The Boeing Company Enhanced performance jet engine mounting struts
FR3060531B1 (fr) * 2016-12-20 2019-05-31 Airbus Operations Partie arriere d'aeronef comprenant un cadre de fuselage supportant deux moteurs partiellement enterres
FR3086925B1 (fr) * 2018-10-08 2020-09-11 Safran Aircraft Engines Ensemble de suspension pour une turbomachine
US11970278B2 (en) * 2020-07-14 2024-04-30 General Electric Company Thrust mounts with load-balancing thrust link-lever
US11702200B1 (en) 2021-12-29 2023-07-18 Beta Air, Llc System for a vertical takeoff and landing aircraft with an in-boom lift propulsor
FR3140068A1 (fr) * 2022-09-23 2024-03-29 Airbus Operations Ensemble de motorisation d’aéronef comportant un dispositif de reprise d’efforts de poussée
CN115716536B (zh) * 2022-10-25 2023-07-21 中国航发沈阳发动机研究所 一种薄壁高强斜支板承力框架结构

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
GB2275308B (en) * 1993-02-20 1997-02-26 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
FR2856656B1 (fr) * 2003-06-30 2006-12-01 Snecma Moteurs Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2891246B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
FR2891248B1 (fr) * 2005-09-28 2009-05-01 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2891254B1 (fr) * 2005-09-29 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef
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
FR2917379B1 (fr) * 2007-06-12 2010-02-26 Airbus France Mat de fixation d'un moteur a une aile d'aeronef.
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.
FR2921900B1 (fr) * 2007-10-05 2011-03-18 Aircelle Sa Ensemble propulsif pour aeronef.
FR2924684B1 (fr) * 2007-12-07 2010-01-01 Snecma Suspension d'un turboreacteur a un aeronef
FR2931800B1 (fr) * 2008-05-29 2010-07-30 Airbus France Dispositif de reprise des efforts de poussee pour mat d'accrochage de moteur d'aeronef, comprenant des bielles laterales a butees de palonnier integrees
US8672260B2 (en) * 2009-12-02 2014-03-18 United Technologies Corporation Single plane mount system for gas turbine engine
FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
US9637241B2 (en) * 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
US20140084129A1 (en) * 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon
JP6114043B2 (ja) * 2013-01-25 2017-04-12 三菱航空機株式会社 航空機のパイロン、及び、航空機
US10144524B2 (en) * 2013-06-14 2018-12-04 Rohr, Inc. Assembly for mounting a turbine engine to a pylon

Also Published As

Publication number Publication date
WO2013050714A1 (fr) 2013-04-11
RU2014117114A (ru) 2015-11-20
CN103874633A (zh) 2014-06-18
CA2849239A1 (fr) 2013-04-11
FR2981047B1 (fr) 2013-10-25
US20140217234A1 (en) 2014-08-07
FR2981047A1 (fr) 2013-04-12
EP2763897A1 (fr) 2014-08-13

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]