ATE535441T1 - Anordnung zur montage eines motors auf das flugwerk eines flugzeuges - Google Patents

Anordnung zur montage eines motors auf das flugwerk eines flugzeuges

Info

Publication number
ATE535441T1
ATE535441T1 AT08835378T AT08835378T ATE535441T1 AT E535441 T1 ATE535441 T1 AT E535441T1 AT 08835378 T AT08835378 T AT 08835378T AT 08835378 T AT08835378 T AT 08835378T AT E535441 T1 ATE535441 T1 AT E535441T1
Authority
AT
Austria
Prior art keywords
airframe
pylon
arrangement
spars
units
Prior art date
Application number
AT08835378T
Other languages
English (en)
Inventor
Sandoen Raul Carlos Llamas
Original Assignee
Airbus Operations Sl
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 Operations Sl filed Critical Airbus Operations Sl
Application granted granted Critical
Publication of ATE535441T1 publication Critical patent/ATE535441T1/de

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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • 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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Vibration Prevention Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Tires In General (AREA)
AT08835378T 2007-10-03 2008-10-03 Anordnung zur montage eines motors auf das flugwerk eines flugzeuges ATE535441T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200702585A ES2341514B1 (es) 2007-10-03 2007-10-03 Configuracion estructural para el montaje de un motor sobre la estructura de una aeronave.
PCT/EP2008/063274 WO2009043924A1 (en) 2007-10-03 2008-10-03 Arrangement for mounting an engine on the airframe of an aircraft

Publications (1)

Publication Number Publication Date
ATE535441T1 true ATE535441T1 (de) 2011-12-15

Family

ID=40229952

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08835378T ATE535441T1 (de) 2007-10-03 2008-10-03 Anordnung zur montage eines motors auf das flugwerk eines flugzeuges

Country Status (6)

Country Link
US (1) US7726602B2 (de)
EP (1) EP2205486B1 (de)
AT (1) ATE535441T1 (de)
CA (1) CA2701548C (de)
ES (2) ES2341514B1 (de)
WO (1) WO2009043924A1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100001121A1 (en) * 2008-05-30 2010-01-07 Airbus Espana, S.L.. System for tilting a power unit
FR2935954B1 (fr) * 2008-09-18 2011-06-03 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs traversant le fuselage et reliee a celui-ci par au moins une bielle.
FR2935955B1 (fr) * 2008-09-18 2010-10-15 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs reliee au fuselage par au moins un element de blocage sollicite en compression.
FR2935953B1 (fr) * 2008-09-18 2010-10-29 Airbus France Partie arriere d'aeronef comprenant deux semi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef.
FR2939102B1 (fr) * 2008-12-01 2011-01-21 Airbus France Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinale
FR2939101B1 (fr) * 2008-12-01 2010-12-31 Airbus France Structure rigide de mat d'aeronef plaquee contre une extension laterale de fuselage pour sa fixation
FR2943623B1 (fr) * 2009-03-30 2011-04-29 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs montee oscillante sur le fuselage
FR2947528B1 (fr) * 2009-07-03 2011-06-24 Airbus Operations Sas Systeme d'attache d'un moteur a helices
FR2950429B1 (fr) * 2009-09-24 2011-11-18 Airbus Operations Sas Dispositif de mesure d'un torseur des efforts et des moments generes par un ensemble propulsif d'aeronef
ES2391967B1 (es) * 2010-01-14 2013-10-10 Airbus Operations, S.L. Pilón de soporte de motores de aeronaves.
FR2970463B1 (fr) 2011-01-17 2013-02-15 Airbus Operations Sas Dispositif d'eclissage a tenue mecanique amelioree.
FR2976914B1 (fr) * 2011-06-23 2014-12-26 Snecma Structure d'accrochage d'une turbomachine
EP2554472B1 (de) * 2011-08-01 2013-12-11 Eurocopter Deutschland GmbH Lastenschnittstelle, insbesondere Lastenschnittstelle für eine Flugzeugdrucktür
EP2554471B1 (de) * 2011-08-01 2013-10-23 Eurocopter Deutschland GmbH Lastenschnittstelle, insbesondere Lastenschnittstelle einer Flugzeugstruktur
FR2995282B1 (fr) * 2012-09-13 2015-06-19 Snecma Pylone de montage d'un moteur a la structure d'un aeronef
US9845159B2 (en) * 2013-03-07 2017-12-19 United Technologies Corporation Conjoined reverse core flow engine arrangement
JP6266775B2 (ja) 2013-07-26 2018-01-24 エムアールエイ・システムズ・エルエルシー 航空機エンジンパイロン
GB201322077D0 (en) * 2013-12-13 2014-01-29 Rolls Royce Plc Engine mount
FR3014840B1 (fr) 2013-12-17 2017-10-13 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage
FR3014841B1 (fr) 2013-12-17 2017-12-08 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage
FR3015431B1 (fr) 2013-12-19 2017-12-15 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
FR3015433B1 (fr) * 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
FR3041991B1 (fr) * 2015-10-05 2020-05-01 Safran Aircraft Engines Aeronef avec un moyen de propulsion a soufflante deportee
FR3072947B1 (fr) * 2017-10-30 2021-12-17 Airbus Operations Sas Aeronef comprenant au moins un ensemble moteur relie au fuselage de l'aeronef par deux bielles de poussee positionnees au moins partiellement dans une entree d'air de l'ensemble moteur
CN115688500A (zh) * 2021-07-27 2023-02-03 中航西飞民用飞机有限责任公司 一种飞机吊挂结构设计方法
US12221218B2 (en) * 2022-01-20 2025-02-11 Textron Innovations Inc. Engine isolation subframe for aircraft
US12552542B2 (en) 2022-06-08 2026-02-17 General Electric Company Aircraft with a fuselage accommodating an unducted turbine engine
US12030652B2 (en) 2022-06-08 2024-07-09 General Electric Company Aircraft with a fuselage accommodating an unducted turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2863620A (en) * 1952-10-04 1958-12-09 Sud Aviation Jet-propelled aircraft
US4044923A (en) * 1976-05-19 1977-08-30 Glasrock Products, Inc. Foam generating dispenser having a movable and stationary porous element
US5064144A (en) * 1987-05-19 1991-11-12 The Boeing Company Engine mounting assembly
US4854525A (en) * 1987-05-19 1989-08-08 The Boeing Company Engine mounting assembly
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
US4953812A (en) 1987-11-13 1990-09-04 The Boeing Company Aircraft configuration with aft mounted engines and method
US5065959A (en) * 1989-11-21 1991-11-19 The Boeing Company Vibration damping aircraft engine attachment
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
FR2836672B1 (fr) * 2002-03-04 2004-06-04 Airbus France Mat d'accrochage d'un moteur sous une voilure d'aeronef

Also Published As

Publication number Publication date
ES2378182T3 (es) 2012-04-09
US7726602B2 (en) 2010-06-01
EP2205486A1 (de) 2010-07-14
ES2341514B1 (es) 2011-04-18
CA2701548C (en) 2016-05-24
ES2341514A1 (es) 2010-06-21
WO2009043924A1 (en) 2009-04-09
CA2701548A1 (en) 2009-04-09
US20090090811A1 (en) 2009-04-09
EP2205486B1 (de) 2011-11-30

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