FR3082560B1 - Systeme embarque et procede pour le drainage d'un moteur d'aeronef - Google Patents

Systeme embarque et procede pour le drainage d'un moteur d'aeronef Download PDF

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Publication number
FR3082560B1
FR3082560B1 FR1855225A FR1855225A FR3082560B1 FR 3082560 B1 FR3082560 B1 FR 3082560B1 FR 1855225 A FR1855225 A FR 1855225A FR 1855225 A FR1855225 A FR 1855225A FR 3082560 B1 FR3082560 B1 FR 3082560B1
Authority
FR
France
Prior art keywords
board system
tank
draining
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.)
Active
Application number
FR1855225A
Other languages
English (en)
Other versions
FR3082560A1 (fr
Inventor
Almeric Pierre Louis Garnier
Josselin Xavier Coupard
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 FR1855225A priority Critical patent/FR3082560B1/fr
Priority to GB1908594.3A priority patent/GB2575917B/en
Priority to US16/441,790 priority patent/US11655735B2/en
Publication of FR3082560A1 publication Critical patent/FR3082560A1/fr
Application granted granted Critical
Publication of FR3082560B1 publication Critical patent/FR3082560B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/32—Collecting of condensation water; Drainage ; Removing solid particles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F01D25/20—Lubricating arrangements using lubrication pumps
    • 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
    • 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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/602—Drainage
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/98—Lubrication

Landscapes

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

Abstract

L'invention concerne le domaine de la propulsion aéronautique, et plus particulièrement un système embarqué (10) et un procédé pour le drainage d'un moteur d'aéronef. Le système embarqué (10) comporte un réservoir tampon (11) avec un passage d'admission (14) par gravité de fluide provenant du moteur (101) d'aéronef, un réservoir primaire (12), disposé au-dessus du réservoir tampon (11), avec un passage de vidange (17) du fluide provenant du moteur (101) d'aéronef, et un circuit de relevage (13), reliant le réservoir tampon (11) au réservoir primaire (12) pour transférer du réservoir tampon (11) au réservoir primaire (12) le fluide provenant du moteur (101) d'aéronef.
FR1855225A 2018-06-14 2018-06-14 Systeme embarque et procede pour le drainage d'un moteur d'aeronef Active FR3082560B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1855225A FR3082560B1 (fr) 2018-06-14 2018-06-14 Systeme embarque et procede pour le drainage d'un moteur d'aeronef
GB1908594.3A GB2575917B (en) 2018-06-14 2019-06-14 An onboard system and a method for draining an aeroengine
US16/441,790 US11655735B2 (en) 2018-06-14 2019-06-14 Onboard system and a method for draining an aeroengine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1855225 2018-06-14
FR1855225A FR3082560B1 (fr) 2018-06-14 2018-06-14 Systeme embarque et procede pour le drainage d'un moteur d'aeronef

Publications (2)

Publication Number Publication Date
FR3082560A1 FR3082560A1 (fr) 2019-12-20
FR3082560B1 true FR3082560B1 (fr) 2020-08-28

Family

ID=62952155

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1855225A Active FR3082560B1 (fr) 2018-06-14 2018-06-14 Systeme embarque et procede pour le drainage d'un moteur d'aeronef

Country Status (3)

Country Link
US (1) US11655735B2 (fr)
FR (1) FR3082560B1 (fr)
GB (1) GB2575917B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220250758A1 (en) * 2021-02-05 2022-08-11 General Electric Company Remote mount of engine accessories
IT202100003647A1 (it) * 2021-02-17 2022-08-17 Nuovo Pignone Tecnologie Srl Serbatoio di contenimento di allagamento

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2438245A (en) * 1944-03-21 1948-03-23 Bendix Aviat Corp System and means for returning leakage fluid to a main fluid supply
US2949736A (en) * 1952-10-03 1960-08-23 Rolls Royce Expansion joint with fuel drainage collector for ducting of gas turbine power plants
GB1402996A (en) * 1971-10-28 1975-08-13 Plessey Co Ltd Fuel-supply systems for gas-turbine engines
US3841089A (en) * 1973-02-20 1974-10-15 Ltv Aerospace Corp Fuel reclaiming system
US3901025A (en) * 1974-02-01 1975-08-26 Piper Aircraft Corp Aircraft engine fuel system
US5285636A (en) * 1992-10-28 1994-02-15 General Electric Company Diagnostic drain mast for a gas turbine engine
US5289900A (en) * 1992-12-28 1994-03-01 United Technologies Corporation Multi-functional service for lubrication tank
FR2780715B1 (fr) * 1998-07-03 2000-09-29 Joseph Pellerano Dispositif vidangeur realisant l'aspiration de l'huile usagee contenue dans les carters des moteurs thermiques et son transfert automatique, apres chaque vidange, vers une capacite de stockage
US6343465B1 (en) * 1999-06-25 2002-02-05 Norman P. Martinov Aircraft fuel tank explosion reduction safety method
US6571562B2 (en) * 2001-10-08 2003-06-03 Honeywell International Inc. Witness drain valve
US8230974B2 (en) 2009-05-22 2012-07-31 United Technologies Corporation Windmill and zero gravity lubrication system for a gas turbine engine
FR3014134B1 (fr) * 2013-12-04 2015-12-11 Snecma Dispositif de retention de fluides draines pour un ensemble propulsif
FR3015567B1 (fr) * 2013-12-19 2015-12-25 Turbomeca Dispositif de drainage de fluides pour un moteur d'aeronef
US10634053B2 (en) * 2015-12-21 2020-04-28 United Technologies Corporation Electric windmill pump for gearbox durability
US10851688B2 (en) * 2016-04-18 2020-12-01 Pratt & Whitney Canada Corp. Oil leakage recovery system for gas turbine engine
GB201804579D0 (en) * 2018-03-22 2018-05-09 Rolls Royce Plc Gas turbine engine and oil system thereof
JP7152911B2 (ja) * 2018-09-05 2022-10-13 川崎重工業株式会社 航空機用ガスタービンのオイル供給装置

Also Published As

Publication number Publication date
GB2575917A (en) 2020-01-29
GB2575917B (en) 2022-09-28
FR3082560A1 (fr) 2019-12-20
GB201908594D0 (en) 2019-07-31
US11655735B2 (en) 2023-05-23
US20190383175A1 (en) 2019-12-19

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