FR2698848B1 - Balance of thrust for an aircraft engine. - Google Patents

Balance of thrust for an aircraft engine.

Info

Publication number
FR2698848B1
FR2698848B1 FR9214702A FR9214702A FR2698848B1 FR 2698848 B1 FR2698848 B1 FR 2698848B1 FR 9214702 A FR9214702 A FR 9214702A FR 9214702 A FR9214702 A FR 9214702A FR 2698848 B1 FR2698848 B1 FR 2698848B1
Authority
FR
France
Prior art keywords
thrust
balance
aircraft engine
aircraft
engine
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
FR9214702A
Other languages
French (fr)
Other versions
FR2698848A1 (en
Inventor
Dudley Collard
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.)
Airbus Group SAS
Original Assignee
Airbus Group 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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR9214702A priority Critical patent/FR2698848B1/en
Publication of FR2698848A1 publication Critical patent/FR2698848A1/en
Application granted granted Critical
Publication of FR2698848B1 publication Critical patent/FR2698848B1/en
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
    • B64D27/02—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
FR9214702A 1992-12-07 1992-12-07 Balance of thrust for an aircraft engine. Expired - Fee Related FR2698848B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9214702A FR2698848B1 (en) 1992-12-07 1992-12-07 Balance of thrust for an aircraft engine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9214702A FR2698848B1 (en) 1992-12-07 1992-12-07 Balance of thrust for an aircraft engine.

Publications (2)

Publication Number Publication Date
FR2698848A1 FR2698848A1 (en) 1994-06-10
FR2698848B1 true FR2698848B1 (en) 1995-03-24

Family

ID=9436291

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9214702A Expired - Fee Related FR2698848B1 (en) 1992-12-07 1992-12-07 Balance of thrust for an aircraft engine.

Country Status (1)

Country Link
FR (1) FR2698848B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19713365C1 (en) * 1997-04-01 1998-10-22 Deutsch Zentr Luft & Raumfahrt Engine suspension, in particular for propeller aircraft, with a rod assembly for fastening an engine
FR2867158B1 (en) * 2004-03-04 2007-06-08 Airbus France MOUNTING SYSTEM INTERFERRED BETWEEN AN AIRCRAFT ENGINE AND A RIGID STRUCTURE OF A FIXED HINGING MACHINE UNDER A VESSEL OF THAT AIRCRAFT.
FR2867156B1 (en) * 2004-03-04 2006-06-02 Airbus France MOUNTING SYSTEM INTERFERRED BETWEEN AN AIRCRAFT ENGINE AND A RIGID STRUCTURE OF A FIXED HINGING MACHINE UNDER A VESSEL OF THAT AIRCRAFT.
WO2015010315A1 (en) 2013-07-26 2015-01-29 Mra Systems, Inc. Aircraft engine pylon
US10197128B2 (en) 2017-02-03 2019-02-05 Hutchinson Aerospace & Industry Inc. Hydraulic torque compensation device

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650050A (en) * 1948-06-17 1953-08-25 Niles Bement Pond Co Movable mount for aircraft engines
US3327965A (en) * 1965-09-27 1967-06-27 Douglas Aircraft Inc Flexible engine pylon
US4022018A (en) * 1975-04-29 1977-05-10 General Electric Company Mounting system for a thrust generating engine
US4147029A (en) * 1976-01-02 1979-04-03 General Electric Company Long duct mixed flow gas turbine engine
GB2010969A (en) * 1977-12-22 1979-07-04 Rolls Royce Mounting for Gas Turbine Jet Propulsion Engine
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US5127607A (en) * 1991-07-09 1992-07-07 Lord Corporation Fluid torque-restraint system with optimized fluid expansion

Also Published As

Publication number Publication date
FR2698848A1 (en) 1994-06-10

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
ST Notification of lapse

Effective date: 20110831