FR3100529B1 - Ensemble pour un aéronef - Google Patents

Ensemble pour un aéronef Download PDF

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Publication number
FR3100529B1
FR3100529B1 FR1909898A FR1909898A FR3100529B1 FR 3100529 B1 FR3100529 B1 FR 3100529B1 FR 1909898 A FR1909898 A FR 1909898A FR 1909898 A FR1909898 A FR 1909898A FR 3100529 B1 FR3100529 B1 FR 3100529B1
Authority
FR
France
Prior art keywords
turbomachine
aircraft
pylon
fixed
turbine
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
FR1909898A
Other languages
English (en)
Other versions
FR3100529A1 (fr
Inventor
Guillaume Glemarec
Quentin Matthias Emmanuel Garnaud
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1909898A priority Critical patent/FR3100529B1/fr
Publication of FR3100529A1 publication Critical patent/FR3100529A1/fr
Application granted granted Critical
Publication of FR3100529B1 publication Critical patent/FR3100529B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L’invention concerne un ensemble (1) pour un aéronef comportant un pylône (3) destiné à être fixé à l’aéronef et une turbomachine (2) fixée au pylône (3), la turbomachine (2) comportant, d’amont en aval dans le sens du flux de gaz au sein de la turbomachine (2), une soufflante (5), un compresseur (6a, 6b), une chambre de combustion (7) et une turbine (8a, 8b) , la turbomachine (2) comportant un carter d’échappement (18) situé en aval de la turbine (8a), caractérisé en ce que le pylône (3) comporte des moyens de fixation annulaires (23) fixés sur une extrémité aval annulaire du carter d’échappement de la turbomachine (2).
FR1909898A 2019-09-09 2019-09-09 Ensemble pour un aéronef Active FR3100529B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1909898A FR3100529B1 (fr) 2019-09-09 2019-09-09 Ensemble pour un aéronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1909898 2019-09-09
FR1909898A FR3100529B1 (fr) 2019-09-09 2019-09-09 Ensemble pour un aéronef

Publications (2)

Publication Number Publication Date
FR3100529A1 FR3100529A1 (fr) 2021-03-12
FR3100529B1 true FR3100529B1 (fr) 2021-08-27

Family

ID=68425130

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1909898A Active FR3100529B1 (fr) 2019-09-09 2019-09-09 Ensemble pour un aéronef

Country Status (1)

Country Link
FR (1) FR3100529B1 (fr)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2076438A2 (fr) * 2006-10-11 2009-07-08 Aircelle Nacelle pour turboréacteur double flux
FR2948636B1 (fr) 2009-07-31 2012-01-13 Airbus Operations Sas Ensemble moteur pour aeronef dont le mat d'accrochage comprend une enveloppe structurale formant delimitation radiale interne du flux secondaire
GB2492107B (en) * 2011-06-22 2013-09-04 Rolls Royce Plc Mounting assembly

Also Published As

Publication number Publication date
FR3100529A1 (fr) 2021-03-12

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