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FR3010701B1 - Agencement d'un reservoir entre un capot de nacelle et une turbomachine - Google Patents

Agencement d'un reservoir entre un capot de nacelle et une turbomachine

Info

Publication number
FR3010701B1
FR3010701B1 FR1358823A FR1358823A FR3010701B1 FR 3010701 B1 FR3010701 B1 FR 3010701B1 FR 1358823 A FR1358823 A FR 1358823A FR 1358823 A FR1358823 A FR 1358823A FR 3010701 B1 FR3010701 B1 FR 3010701B1
Authority
FR
France
Prior art keywords
turbomachine
tank
arrangement
nacelle hood
nacelle
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
FR1358823A
Other languages
English (en)
Other versions
FR3010701A1 (fr
Inventor
Thierry Kohn
Jeremy Edmond Fert
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 FR1358823A priority Critical patent/FR3010701B1/fr
Priority to CA2862204A priority patent/CA2862204C/fr
Priority to US14/479,820 priority patent/US9611047B2/en
Publication of FR3010701A1 publication Critical patent/FR3010701A1/fr
Application granted granted Critical
Publication of FR3010701B1 publication Critical patent/FR3010701B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • 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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/08—Inspection panels for power plants
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • 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
    • B64D47/00—Equipment not otherwise provided for
    • 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
    • F02C7/06—Arrangements of bearings; Lubricating
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F16N—LUBRICATING
    • F16N19/00—Lubricant containers for use in lubricators or lubrication systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
  • Wind Motors (AREA)
FR1358823A 2013-09-13 2013-09-13 Agencement d'un reservoir entre un capot de nacelle et une turbomachine Active FR3010701B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1358823A FR3010701B1 (fr) 2013-09-13 2013-09-13 Agencement d'un reservoir entre un capot de nacelle et une turbomachine
CA2862204A CA2862204C (fr) 2013-09-13 2014-09-04 Agencement de citerne entre un capot de nacelle et une turbomachine
US14/479,820 US9611047B2 (en) 2013-09-13 2014-09-08 Arrangement for a tank between a nacelle cowling and a turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1358823A FR3010701B1 (fr) 2013-09-13 2013-09-13 Agencement d'un reservoir entre un capot de nacelle et une turbomachine

Publications (2)

Publication Number Publication Date
FR3010701A1 FR3010701A1 (fr) 2015-03-20
FR3010701B1 true FR3010701B1 (fr) 2015-10-09

Family

ID=49667389

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1358823A Active FR3010701B1 (fr) 2013-09-13 2013-09-13 Agencement d'un reservoir entre un capot de nacelle et une turbomachine

Country Status (3)

Country Link
US (1) US9611047B2 (fr)
CA (1) CA2862204C (fr)
FR (1) FR3010701B1 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3001346B1 (fr) * 2013-01-24 2015-02-27 Snecma Dispositif de fixation et de maintien d'au moins un harnais electrique dans une turbomachine
US10634053B2 (en) * 2015-12-21 2020-04-28 United Technologies Corporation Electric windmill pump for gearbox durability
FR3059361B1 (fr) * 2016-11-28 2018-12-07 Safran Aircraft Engines Reservoir d'huile comprenant un dispositif de controle du niveau d'huile
BE1025191B1 (fr) * 2017-05-03 2018-12-06 Safran Aero Boosters S.A. Reservoir a sonde de niveau d’huile pour turbomachine
US20180317723A1 (en) * 2017-05-03 2018-11-08 Hamed Marhi ALDHAFEERI System, apparatus, and method for cleaning a high rise surface
FR3072425B1 (fr) * 2017-10-12 2022-04-22 Safran Aircraft Engines Turbomachine a double flux et son reservoir de lubrifiant
CN107738223B (zh) * 2017-11-13 2023-11-10 山东太古飞机工程有限公司 飞机发动机第一级静子叶片整流罩的拆装辅助工装
GB201804579D0 (en) 2018-03-22 2018-05-09 Rolls Royce Plc Gas turbine engine and oil system thereof
GB201807203D0 (en) 2018-05-02 2018-06-13 Rolls Royce Plc Oil tank filling system
GB201807201D0 (en) 2018-05-02 2018-06-13 Rolls Royce Plc Oil tank filling system
GB201807202D0 (en) 2018-05-02 2018-06-13 Rolls Royce Plc Oil tank filling system
FR3085727A1 (fr) * 2018-09-06 2020-03-13 Airbus Operations Turboreacteur comportant une nacelle equipee d'un systeme inverseur comportant des portes interieures et des volets exterieurs
US11230947B2 (en) * 2019-06-20 2022-01-25 Pratt & Whitney Canada Corp. Gas turbine engine having oil level measurement system
FR3109142B1 (fr) * 2020-04-10 2022-03-04 Safran Nacelles Organe d’obturation amovible pour une partie femelle logée dans une ouverture extérieure d’une nacelle d’aéronef
US12098649B2 (en) 2022-10-25 2024-09-24 General Electric Company Gas turbine engine accessory packaging
US12104539B2 (en) 2022-10-25 2024-10-01 General Electric Company Gas turbine engine
FR3161665A1 (fr) * 2024-04-29 2025-10-31 Safran Aircraft Engines Equipement pour moteur d’aéronef formant une trappe d’accès au moteur

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1933998A (en) * 1930-02-17 1933-11-07 Curtiss Aeroplane & Motor Co Oil cooler
JPS6025887A (ja) * 1983-07-21 1985-02-08 Sanshin Ind Co Ltd 油タンクの注油蓋装置
US5249417A (en) * 1991-09-25 1993-10-05 United Technologies Corporation Method and apparatus to install and remove heavy components
US5610341A (en) * 1996-04-08 1997-03-11 General Electric Company Modular oil monitor
US6039287A (en) * 1996-08-02 2000-03-21 Alliedsignal Inc. Detachable integral aircraft tailcone and power assembly
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle

Also Published As

Publication number Publication date
US9611047B2 (en) 2017-04-04
CA2862204C (fr) 2021-05-18
CA2862204A1 (fr) 2015-03-13
US20150075132A1 (en) 2015-03-19
FR3010701A1 (fr) 2015-03-20

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