FR2676707B1 - Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. - Google Patents

Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.

Info

Publication number
FR2676707B1
FR2676707B1 FR9106198A FR9106198A FR2676707B1 FR 2676707 B1 FR2676707 B1 FR 2676707B1 FR 9106198 A FR9106198 A FR 9106198A FR 9106198 A FR9106198 A FR 9106198A FR 2676707 B1 FR2676707 B1 FR 2676707B1
Authority
FR
France
Prior art keywords
nacelle
turbo
wing
aircraft
flow type
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
FR9106198A
Other languages
English (en)
Other versions
FR2676707A1 (fr
Inventor
Lardellier Alain
Marie
Joseph
Saillot Patrick
William
Roger
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SAS filed Critical SNECMA SAS
Priority to FR9106198A priority Critical patent/FR2676707B1/fr
Priority to US07/886,838 priority patent/US5181675A/en
Publication of FR2676707A1 publication Critical patent/FR2676707A1/fr
Application granted granted Critical
Publication of FR2676707B1 publication Critical patent/FR2676707B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • B64D27/02—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
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9106198A 1991-05-23 1991-05-23 Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. Expired - Fee Related FR2676707B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9106198A FR2676707B1 (fr) 1991-05-23 1991-05-23 Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.
US07/886,838 US5181675A (en) 1991-05-23 1992-05-22 Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9106198A FR2676707B1 (fr) 1991-05-23 1991-05-23 Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.

Publications (2)

Publication Number Publication Date
FR2676707A1 FR2676707A1 (fr) 1992-11-27
FR2676707B1 true FR2676707B1 (fr) 1993-08-13

Family

ID=9413034

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9106198A Expired - Fee Related FR2676707B1 (fr) 1991-05-23 1991-05-23 Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.

Country Status (2)

Country Link
US (1) US5181675A (fr)
FR (1) FR2676707B1 (fr)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
GB2275308B (en) * 1993-02-20 1997-02-26 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5467941A (en) * 1993-12-30 1995-11-21 The Boeing Company Pylon and engine installation for ultra-high by-pass turbo-fan engines
JP3612335B2 (ja) * 1994-12-23 2005-01-19 ユナイテッド テクノロジーズ コーポレイション ガスタービンエンジンの取り付け装置
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
US6189830B1 (en) * 1999-02-26 2001-02-20 The Boeing Company Tuned engine mounting system for jet aircraft
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
GB2359052B (en) * 2000-02-09 2003-09-17 Rolls Royce Plc Engine arrangement
WO2004026689A1 (fr) * 2002-09-17 2004-04-01 Bell Helicopter Textron Inc. Systeme de montage de moteurs decouples en torsion
GB0328671D0 (en) * 2003-12-11 2004-01-14 Rolls Royce Plc Aircraft engine mounting
FR2869589B1 (fr) * 2004-04-28 2007-08-10 Airbus France Sas Dispositif d'attache d'un moteur sur une aile d'un aeronef
FR2873985B1 (fr) * 2004-08-04 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2873986B1 (fr) 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur 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
FR2891251B1 (fr) * 2005-09-28 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
SE535991C2 (sv) * 2011-07-07 2013-03-19 Bae Systems Bofors Ab Rotationsstabiliserad styrbar projektil och förfarande därför
FR2989952B1 (fr) * 2012-04-27 2014-04-18 Aircelle Sa Nacelle de turboreacteur a section aval
US8979020B2 (en) 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
US10144524B2 (en) * 2013-06-14 2018-12-04 Rohr, Inc. Assembly for mounting a turbine engine to a pylon
CN105392700B (zh) 2013-07-26 2018-12-18 Mra***有限责任公司 飞行器发动机吊架
FR3010147B1 (fr) * 2013-08-28 2015-08-21 Snecma Suspension isostatique d'un turboreacteur par double support arriere
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
US10723471B2 (en) 2017-06-14 2020-07-28 General Electric Company Method and system for mounting an aircraft engine
US10597144B2 (en) * 2017-12-01 2020-03-24 Hadie Fotouhie Under the wing-mounted jet engine with pivotal swivel joint to produce directional thrust vectoring thru swivel angle

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3201069A (en) * 1962-05-31 1965-08-17 Haskin Simon Jet-propelled aircraft engine mounting
GB1236917A (en) * 1967-06-14 1971-06-23 Rolls Royce Improvements in or relating to means for supporting a gas turbine engine in an aircraft
US3517897A (en) * 1968-09-11 1970-06-30 Us Air Force Multi-module thrust mount
US3988889A (en) * 1974-02-25 1976-11-02 General Electric Company Cowling arrangement for a turbofan engine
US4055041A (en) * 1974-11-08 1977-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated gas turbine engine-nacelle
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
US4147029A (en) * 1976-01-02 1979-04-03 General Electric Company Long duct mixed flow gas turbine engine
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US4506850A (en) * 1983-01-04 1985-03-26 The Boeing Company Engine installation for aircraft
US4555078A (en) * 1983-12-27 1985-11-26 Societe Belge D'exploitation De La Navigation Aerienne (Sabena) Apparatus for the suspension of an aircraft engine cowling
US4717094A (en) * 1986-05-19 1988-01-05 The Boeing Company Aircraft engine mount system with vibration isolators
US4725019A (en) * 1986-08-11 1988-02-16 The Boeing Company Aircraft engine mount with vertical vibration isolation
FR2606081A1 (fr) * 1986-10-29 1988-05-06 Snecma Moteur de propulsion a turbines de travail contrarotatives
FR2622507B1 (fr) * 1987-10-28 1990-01-26 Snecma
US4917331A (en) * 1988-11-10 1990-04-17 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter

Also Published As

Publication number Publication date
FR2676707A1 (fr) 1992-11-27
US5181675A (en) 1993-01-26

Similar Documents

Publication Publication Date Title
FR2676707B1 (fr) Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.
DE2963215D1 (en) Telescoping seating systems with automatically folding chairs
DE69211557D1 (de) Verkleidungform eines unbemannten luftfahrzeuges
IT8148524A0 (it) Posizionatore idro-pneumatico per il cambio di motori alari di velivoli o simili
FR2670177B1 (fr) Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur.
AU7880287A (en) Axial flow turbine
FR2608680B1 (fr) Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion
DE69104974D1 (de) Rotorverkleidungsleitwerkanschlussebene einer Hubschrauberleitwerkstruktur.
DE59201833D1 (de) Deckband für axialdurchströmte Turbine.
FR2661149B1 (fr) Systeme pour le pilotage d'un avion en tangage.
FR2686855B1 (fr) Actionneur lineaire, notamment pour la manóoeuvre d'une jambe d'atterrisseur d'avion.
FR2603250B1 (fr) Dispositif de commande de la poussee d'un avion
FR2661887B1 (fr) Systeme d'aide au pilotage d'un helicoptere portant une charge, notamment en vol stationnaire.
FR2521280B1 (fr) Structure de support d'aile escamotable, notamment pour missiles
AU2559384A (en) Turbine fluid flow meter
FI821203A0 (fi) Nya piperazino-2-pyrimidin-derivater, foerfarande foer framstaellning daerav och anvaendning daerav som laekemedel eller mellanprodukter foer framstaellning av laekemedel
FR2687123B1 (fr) Train d'atterrissage relevable d'aeronef, notamment pour helicoptere.
FR2605587B1 (fr) Perfectionnements apportes aux helices aeriennes, notamment pour propulseurs d'aeronef
FR2576975B1 (fr) Dispositif de reglage pour groupe moto-propulseur d'avion
FR2605588B1 (fr) Perfectionnements apportes aux helices aeriennes, notamment pour propulseurs d'aeronef
FR2545931B1 (fr) Systeme d'avertissement pour un aeronef atterrissant avec le train d'atterrissage rentre
FR2586130B1 (fr) Reduction du bruit des helices d'un avion
OA04745A (fr) Equipements de pilotage d'avion pour handicapés des membres inférieurs.
FR2698848B1 (fr) Balance de poussée pour un moteur d'avion.
FR2547270B1 (fr) Mecanisme d'extension et de retraction pour un volet de bord d'attaque d'une aile d'avion

Legal Events

Date Code Title Description
CL Concession to grant licences
CD Change of name or company name
TP Transmission of property
CD Change of name or company name
ST Notification of lapse

Effective date: 20110131