FR3021299B1 - Attache moteur pour un aeronef - Google Patents

Attache moteur pour un aeronef

Info

Publication number
FR3021299B1
FR3021299B1 FR1454723A FR1454723A FR3021299B1 FR 3021299 B1 FR3021299 B1 FR 3021299B1 FR 1454723 A FR1454723 A FR 1454723A FR 1454723 A FR1454723 A FR 1454723A FR 3021299 B1 FR3021299 B1 FR 3021299B1
Authority
FR
France
Prior art keywords
aircraft
engine attachment
attachment
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.)
Active
Application number
FR1454723A
Other languages
English (en)
Other versions
FR3021299A1 (fr
Inventor
Jerome Cassagne
Antoine Cousin
Thomas Deforet
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1454723A priority Critical patent/FR3021299B1/fr
Publication of FR3021299A1 publication Critical patent/FR3021299A1/fr
Application granted granted Critical
Publication of FR3021299B1 publication Critical patent/FR3021299B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
    • F16C23/02—Sliding-contact bearings
    • F16C23/04—Sliding-contact bearings self-adjusting
    • F16C23/043—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings
    • F16C23/045—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings for radial load mainly, e.g. radial spherical plain bearings
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
FR1454723A 2014-05-26 2014-05-26 Attache moteur pour un aeronef Active FR3021299B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1454723A FR3021299B1 (fr) 2014-05-26 2014-05-26 Attache moteur pour un aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1454723A FR3021299B1 (fr) 2014-05-26 2014-05-26 Attache moteur pour un aeronef

Publications (2)

Publication Number Publication Date
FR3021299A1 FR3021299A1 (fr) 2015-11-27
FR3021299B1 true FR3021299B1 (fr) 2016-07-01

Family

ID=51298822

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1454723A Active FR3021299B1 (fr) 2014-05-26 2014-05-26 Attache moteur pour un aeronef

Country Status (1)

Country Link
FR (1) FR3021299B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3131734A1 (fr) * 2022-01-07 2023-07-14 Airbus Operations Ensemble propulsif pour aéronef comportant un turboréacteur, un mât et des moyens d’accrochage du turboréacteur au mât

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1160826A (fr) * 1956-11-12 1958-08-11 Snecma Dispositif de suspension de réacteurs
US3141231A (en) * 1961-04-17 1964-07-21 Superior Ball Joint Corp Method of fabricating a ball and socket assembly
FR2755943B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
FR2883256B1 (fr) * 2005-03-18 2008-10-24 Airbus France Sas Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef
US20140084129A1 (en) * 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon

Also Published As

Publication number Publication date
FR3021299A1 (fr) 2015-11-27

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