FR3054856B1 - Turbomachine comportant un systeme de gestion thermique - Google Patents
Turbomachine comportant un systeme de gestion thermiqueInfo
- 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
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)
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)
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)
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 |
-
2016
- 2016-08-03 FR FR1657541A patent/FR3054856B1/fr active Active
-
2017
- 2017-08-03 US US15/667,873 patent/US20180038280A1/en not_active Abandoned
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 |