FR3054856B1 - Turbomachine comportant un systeme de gestion thermique - Google Patents

Turbomachine comportant un systeme de gestion thermique

Info

Publication number
FR3054856B1
FR3054856B1 FR1657541A FR1657541A FR3054856B1 FR 3054856 B1 FR3054856 B1 FR 3054856B1 FR 1657541 A FR1657541 A FR 1657541A FR 1657541 A FR1657541 A FR 1657541A FR 3054856 B1 FR3054856 B1 FR 3054856B1
Authority
FR
France
Prior art keywords
turbomachine
management system
thermal management
thermal
management
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
FR1657541A
Other languages
English (en)
Other versions
FR3054856A1 (fr
Inventor
Jean Michel Rogero
Olivier Verseux
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 FR1657541A priority Critical patent/FR3054856B1/fr
Priority to US15/667,873 priority patent/US20180038280A1/en
Publication of FR3054856A1 publication Critical patent/FR3054856A1/fr
Application granted granted Critical
Publication of FR3054856B1 publication Critical patent/FR3054856B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • F01D25/02—De-icing means for engines having icing phenomena
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
FR1657541A 2016-08-03 2016-08-03 Turbomachine comportant un systeme de gestion thermique Active FR3054856B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1657541A FR3054856B1 (fr) 2016-08-03 2016-08-03 Turbomachine comportant un systeme de gestion thermique
US15/667,873 US20180038280A1 (en) 2016-08-03 2017-08-03 Turbomachine comprising a heat management system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1657541A FR3054856B1 (fr) 2016-08-03 2016-08-03 Turbomachine comportant un systeme de gestion thermique

Publications (2)

Publication Number Publication Date
FR3054856A1 FR3054856A1 (fr) 2018-02-09
FR3054856B1 true FR3054856B1 (fr) 2018-09-07

Family

ID=57121374

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1657541A Active FR3054856B1 (fr) 2016-08-03 2016-08-03 Turbomachine comportant un systeme de gestion thermique

Country Status (2)

Country Link
US (1) US20180038280A1 (fr)
FR (1) FR3054856B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3007738B1 (fr) * 2013-06-28 2015-07-31 Aircelle Sa Dispositif de degivrage et de conditionnement pour aeronef
US10364750B2 (en) * 2017-10-30 2019-07-30 General Electric Company Thermal management system
US11156162B2 (en) * 2018-05-23 2021-10-26 General Electric Company Fluid manifold damper for gas turbine engine
FR3088961A1 (fr) * 2018-11-22 2020-05-29 Airbus Operations (S.A.S.) Turbomachine équipée d’un système de dégivrage de l’entrée d’air.
FR3094749B1 (fr) * 2019-04-03 2021-11-19 Safran Nacelles Système de refroidissement de turboréacteur pour aéronef
FR3094750B1 (fr) * 2019-04-03 2021-11-26 Safran Nacelles Système de refroidissement de turboréacteur pour aéronef
US11326519B2 (en) 2020-02-25 2022-05-10 General Electric Company Frame for a heat engine
US11560843B2 (en) 2020-02-25 2023-01-24 General Electric Company Frame for a heat engine
US11255264B2 (en) 2020-02-25 2022-02-22 General Electric Company Frame for a heat engine
US11795878B2 (en) 2021-02-02 2023-10-24 General Electric Company High-temperature fuel thermal transport bus architecture

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2914365B1 (fr) * 2007-03-28 2012-05-18 Airbus France Systeme de refroidissement et de regulation en temperature d'equipements d'un ensemble propulsif d'aeronef.
FR2987602B1 (fr) * 2012-03-02 2014-02-28 Aircelle Sa Nacelle de turbomoteur equipe d'un echangeur de chaleur
FR3001253B1 (fr) * 2013-01-22 2017-06-23 Snecma Systeme regule de refroidissement d'huile d'un turboreacteur avec degivrage de la nacelle
FR3002978B1 (fr) * 2013-03-07 2016-12-30 Aircelle Sa Nacelle equipee d’un circuit de refroidissement d’huile a echangeur intermediaire
JP6162827B2 (ja) * 2013-04-04 2017-07-12 エル・ピー・ケー・エフ・レーザー・ウント・エレクトロニクス・アクチエンゲゼルシヤフト 基板を分離する方法及び装置
GB201415078D0 (en) * 2014-08-26 2014-10-08 Rolls Royce Plc Gas turbine engine anti-icing system
FR3027624B1 (fr) * 2014-10-27 2019-04-19 Safran Aircraft Engines Circuit de degivrage d'une levre d'entree d'air d'un ensemble propulsif d'aeronef
EP3018304B1 (fr) * 2014-11-06 2020-10-14 United Technologies Corporation Système de gestion thermique pour moteur à turbine à gaz
US9759094B2 (en) * 2015-06-24 2017-09-12 General Electric Company Pump for a turbine engine
US10260419B2 (en) * 2015-07-31 2019-04-16 General Electric Company Cooling system
US20170159564A1 (en) * 2015-12-08 2017-06-08 General Electric Company Thermal management system

Also Published As

Publication number Publication date
US20180038280A1 (en) 2018-02-08
FR3054856A1 (fr) 2018-02-09

Similar Documents

Publication Publication Date Title
FR3054856B1 (fr) Turbomachine comportant un systeme de gestion thermique
GB201818053D0 (en) Thermal management system
GB2542696B (en) Thermal management system
DK3603238T3 (da) Betjeningsunktion med netværksopdeling
GB2548931B (en) Exhaust aftertreatment thermal management controls
IL260284B (en) Thermal management system based on vacuum
FR3023364B1 (fr) Echangeur thermique a double circulation et installation de gestion thermique correspondante
GB2536803B (en) Gas turbine engine fluid heat management system
FI20155989A (fi) Sensoripohjainen kontekstin hallinnointi
GB201616882D0 (en) Turbojet engine with offset fans with a diffrential system
GB2557361B (en) Thermal Management test system
FR3002289B1 (fr) Tuyere a divergent mobile avec systeme de protection thermique
GB2575680B (en) Thermal management system
GB201720667D0 (en) Thermal management device
FR3005099B1 (fr) Structure de turbomachine comportant une bague de ventilation
DK3092443T3 (da) Brændeovnsforbrændingsovervågningssystem
GB2575679B (en) Thermal Management System
FR3019526B1 (fr) Nacelle d'aeronef comportant un systeme d'ecartement destine a maintenir les deux capots ecartes
GB2550288B (en) ATS thermal management system
FR3033394B1 (fr) Circuit de gestion thermique
FR3018543B1 (fr) Installation thermique de combustion
EP3824241C0 (fr) Système de gestion thermique
GB2603082B (en) Thermal management system
IT201700082606A1 (it) Impianto termico
FR3039703B1 (fr) Systeme thermique passif a base de nano-elements

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20180209

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9