FR2915520B1 - Ensemble moteur comprenant un ou plusieurs caloducs pour le refroidissement d'un compresseur haute pression - Google Patents
Ensemble moteur comprenant un ou plusieurs caloducs pour le refroidissement d'un compresseur haute pressionInfo
- Publication number
- FR2915520B1 FR2915520B1 FR0754792A FR0754792A FR2915520B1 FR 2915520 B1 FR2915520 B1 FR 2915520B1 FR 0754792 A FR0754792 A FR 0754792A FR 0754792 A FR0754792 A FR 0754792A FR 2915520 B1 FR2915520 B1 FR 2915520B1
- Authority
- FR
- France
- Prior art keywords
- caloduces
- cooling
- pressure compressor
- engine assembly
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/584—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling or heating the machine
-
- 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
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/5853—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps heat insulation or conduction
-
- 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
- F05D2260/208—Heat transfer, e.g. cooling using heat pipes
-
- 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0754792A FR2915520B1 (fr) | 2007-04-30 | 2007-04-30 | Ensemble moteur comprenant un ou plusieurs caloducs pour le refroidissement d'un compresseur haute pression |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0754792A FR2915520B1 (fr) | 2007-04-30 | 2007-04-30 | Ensemble moteur comprenant un ou plusieurs caloducs pour le refroidissement d'un compresseur haute pression |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2915520A1 FR2915520A1 (fr) | 2008-10-31 |
FR2915520B1 true FR2915520B1 (fr) | 2012-05-25 |
Family
ID=38828665
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0754792A Active FR2915520B1 (fr) | 2007-04-30 | 2007-04-30 | Ensemble moteur comprenant un ou plusieurs caloducs pour le refroidissement d'un compresseur haute pression |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2915520B1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6266775B2 (ja) | 2013-07-26 | 2018-01-24 | エムアールエイ・システムズ・エルエルシー | 航空機エンジンパイロン |
US20160290231A1 (en) * | 2015-04-02 | 2016-10-06 | General Electric Company | Heat pipe intercooling system for a turbomachine |
US10400675B2 (en) * | 2015-12-03 | 2019-09-03 | General Electric Company | Closed loop cooling method and system with heat pipes for a gas turbine engine |
US10830094B2 (en) * | 2016-09-28 | 2020-11-10 | Raytheon Technologies Corporation | Gas turbine engine with graphene heat pipe |
FR3062169B1 (fr) * | 2017-01-20 | 2019-04-19 | Safran Aircraft Engines | Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1516041A (en) * | 1977-02-14 | 1978-06-28 | Secr Defence | Multistage axial flow compressor stators |
JP3365005B2 (ja) * | 1993-10-26 | 2003-01-08 | 石川島播磨重工業株式会社 | タービン静翼の冷却装置 |
AU2001213231A1 (en) * | 2000-11-10 | 2002-05-21 | Marek Kovac | Bypass gas turbine engine and cooling method for working fluid |
US7600382B2 (en) * | 2005-07-20 | 2009-10-13 | Ralls Jr Stephen Alden | Turbine engine with interstage heat transfer |
-
2007
- 2007-04-30 FR FR0754792A patent/FR2915520B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2915520A1 (fr) | 2008-10-31 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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Year of fee payment: 14 |
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Year of fee payment: 15 |
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