FR3092135B1 - Turbomachine, telle qu’un turboreacteur d’avion - Google Patents
Turbomachine, telle qu’un turboreacteur d’avion Download PDFInfo
- Publication number
- FR3092135B1 FR3092135B1 FR1900811A FR1900811A FR3092135B1 FR 3092135 B1 FR3092135 B1 FR 3092135B1 FR 1900811 A FR1900811 A FR 1900811A FR 1900811 A FR1900811 A FR 1900811A FR 3092135 B1 FR3092135 B1 FR 3092135B1
- Authority
- FR
- France
- Prior art keywords
- primary
- turbomachine
- airplane
- turboreactor
- stream
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 238000001816 cooling Methods 0.000 abstract 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- 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
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine 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
- 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
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
L’invention concerne une turbomachine (1), telle qu’un turboréacteur ou un turbopropulseur d’avion, s’étendant selon un axe (X), comportant une veine primaire (2) comprenant au moins un compresseur (4, 5), au moins une chambre de combustion (6) et au moins une turbine (7, 8), et une veine secondaire (3) située radialement à l’extérieur de la veine primaire (2), au moins une canalisation (18), destinée à l’écoulement d’air de refroidissement, ladite canalisation (18) comportant une entrée d’air débouchant dans la veine primaire (2), au niveau du compresseur (4, 5), et une sortie d’air débouchant dans la veine primaire (2), au niveau de la turbine (7, 8). Figure à publier avec l’abrégé : figure 1
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1900811A FR3092135B1 (fr) | 2019-01-29 | 2019-01-29 | Turbomachine, telle qu’un turboreacteur d’avion |
US16/775,412 US20200240641A1 (en) | 2019-01-29 | 2020-01-29 | Turbomachine, such as an aircraft turbojet engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1900811 | 2019-01-29 | ||
FR1900811A FR3092135B1 (fr) | 2019-01-29 | 2019-01-29 | Turbomachine, telle qu’un turboreacteur d’avion |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3092135A1 FR3092135A1 (fr) | 2020-07-31 |
FR3092135B1 true FR3092135B1 (fr) | 2021-10-01 |
Family
ID=67185232
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1900811A Active FR3092135B1 (fr) | 2019-01-29 | 2019-01-29 | Turbomachine, telle qu’un turboreacteur d’avion |
Country Status (2)
Country | Link |
---|---|
US (1) | US20200240641A1 (fr) |
FR (1) | FR3092135B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11732656B2 (en) * | 2021-03-31 | 2023-08-22 | Raytheon Technologies Corporation | Turbine engine with soaring air conduit |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2046797A1 (fr) * | 1990-08-01 | 1992-02-02 | Franklin D. Parsons | Montage d'echangeur de chaleur dans un canal de flux d'une turbine a gaz pour refroidir l'air chaud de prelevement |
FR2670177B1 (fr) | 1990-12-05 | 1993-01-22 | Snecma | Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur. |
US7509797B2 (en) * | 2005-04-29 | 2009-03-31 | General Electric Company | Thrust vectoring missile turbojet |
FR2922589B1 (fr) | 2007-10-22 | 2009-12-04 | Snecma | Controle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine |
FR3018857B1 (fr) * | 2014-03-21 | 2016-05-06 | Snecma | Circuit de refroidissement d'air chaud sous pression d'une turbomachine d'aeronef comportant un echangeur de chaleur pour refroidir l'air |
FR3065030B1 (fr) * | 2017-04-05 | 2021-01-22 | Safran Helicopter Engines | Moteur a combustion interne |
-
2019
- 2019-01-29 FR FR1900811A patent/FR3092135B1/fr active Active
-
2020
- 2020-01-29 US US16/775,412 patent/US20200240641A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US20200240641A1 (en) | 2020-07-30 |
FR3092135A1 (fr) | 2020-07-31 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20200731 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |