FR3017656B1 - Turboreacteur comportant un systeme de prelevement destine a prelever de l'air dans ledit turboreacteur - Google Patents
Turboreacteur comportant un systeme de prelevement destine a prelever de l'air dans ledit turboreacteurInfo
- Publication number
- FR3017656B1 FR3017656B1 FR1451235A FR1451235A FR3017656B1 FR 3017656 B1 FR3017656 B1 FR 3017656B1 FR 1451235 A FR1451235 A FR 1451235A FR 1451235 A FR1451235 A FR 1451235A FR 3017656 B1 FR3017656 B1 FR 3017656B1
- Authority
- FR
- France
- Prior art keywords
- turboreactor
- sampling system
- taking air
- taking
- air
- 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
- 238000005070 sampling Methods 0.000 title 1
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
- 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
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
- B64D13/04—Automatic control of pressure
-
- 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
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the 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
- 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
-
- 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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/115—Heating the by-pass flow by means of indirect heat exchange
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0644—Environmental Control Systems including electric motors or generators
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0648—Environmental Control Systems with energy recovery means, e.g. using turbines
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1451235A FR3017656B1 (fr) | 2014-02-17 | 2014-02-17 | Turboreacteur comportant un systeme de prelevement destine a prelever de l'air dans ledit turboreacteur |
US14/623,037 US9885284B2 (en) | 2014-02-17 | 2015-02-16 | Turbojet comprising a bleeding system for bleeding air in said turbojet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1451235A FR3017656B1 (fr) | 2014-02-17 | 2014-02-17 | Turboreacteur comportant un systeme de prelevement destine a prelever de l'air dans ledit turboreacteur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3017656A1 FR3017656A1 (fr) | 2015-08-21 |
FR3017656B1 true FR3017656B1 (fr) | 2016-03-11 |
Family
ID=50473641
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1451235A Active FR3017656B1 (fr) | 2014-02-17 | 2014-02-17 | Turboreacteur comportant un systeme de prelevement destine a prelever de l'air dans ledit turboreacteur |
Country Status (2)
Country | Link |
---|---|
US (1) | US9885284B2 (fr) |
FR (1) | FR3017656B1 (fr) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10054051B2 (en) * | 2014-04-01 | 2018-08-21 | The Boeing Company | Bleed air systems for use with aircraft and related methods |
US9810158B2 (en) * | 2014-04-01 | 2017-11-07 | The Boeing Company | Bleed air systems for use with aircraft and related methods |
US10100744B2 (en) | 2015-06-19 | 2018-10-16 | The Boeing Company | Aircraft bleed air and engine starter systems and related methods |
US20170067578A1 (en) * | 2015-09-09 | 2017-03-09 | Honeywell International Inc. | Detection of high stage valve leakage by pressure lockup |
US10196928B2 (en) * | 2016-03-02 | 2019-02-05 | General Electric Company | Method and system for piping failure detection in a gas turbine bleeding air system |
DE102016120682A1 (de) * | 2016-10-28 | 2018-05-03 | Rolls-Royce Deutschland Ltd & Co Kg | Zapfluftsystem eines Flugtriebwerks und Verfahren zum Bereitstellen von Zapfluft in einem Flugtriebwerk |
US20180162537A1 (en) * | 2016-12-09 | 2018-06-14 | United Technologies Corporation | Environmental control system air circuit |
US11459906B2 (en) | 2017-05-22 | 2022-10-04 | Raytheon Technologies Corporation | Actively-driven bleed source switching |
US10473037B2 (en) | 2017-05-22 | 2019-11-12 | United Technologies Corporation | Passively-driven bleed source switching |
US11739697B2 (en) | 2017-05-22 | 2023-08-29 | Raytheon Technologies Corporation | Bleed flow safety system |
US10914242B2 (en) * | 2017-11-28 | 2021-02-09 | Raytheon Technologies Corporation | Complex air supply system for gas turbine engine and associated aircraft |
US10954865B2 (en) | 2018-06-19 | 2021-03-23 | The Boeing Company | Pressurized air systems for aircraft and related methods |
US11008949B2 (en) * | 2018-09-25 | 2021-05-18 | Pratt & Whitney Canada Corp. | Multi-source air system and switching valve assembly for a gas turbine engine |
US11465757B2 (en) | 2018-12-06 | 2022-10-11 | The Boeing Company | Systems and methods to produce aircraft cabin supply air |
EP4239172A1 (fr) * | 2020-10-28 | 2023-09-06 | Kawasaki Jukogyo Kabushiki Kaisha | Système d'alimentation en air comprimé |
US11530705B2 (en) * | 2020-11-17 | 2022-12-20 | Hamilton Sundstrand Corporation | Bearing cooling schemes for aircraft fans |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4263786A (en) * | 1979-07-10 | 1981-04-28 | The Boeing Company | Fuel conserving air-conditioning apparatus and method for aircraft |
US5137230A (en) * | 1991-06-04 | 1992-08-11 | General Electric Company | Aircraft gas turbine engine bleed air energy recovery apparatus |
FR2774357B1 (fr) * | 1998-02-05 | 2000-04-07 | Aerospatiale | Systeme d'alimentation en air chaud pour aeronef |
JP3322633B2 (ja) * | 1998-04-20 | 2002-09-09 | 三菱重工業株式会社 | 軸流圧縮機の抽気流量制御システム |
US6189324B1 (en) * | 1999-10-05 | 2001-02-20 | Samuel B. Williams | Environment control unit for turbine engine |
US9062604B2 (en) * | 2011-01-14 | 2015-06-23 | Hamilton Sundstrand Corporation | Low pressure bleed architecture |
US20120185116A1 (en) * | 2011-01-14 | 2012-07-19 | Hamilton Sundstrand Corporation | Integrated bleed and engine controller |
US20130040545A1 (en) * | 2011-08-11 | 2013-02-14 | Hamilton Sundstrand Corporation | Low pressure compressor bleed exit for an aircraft pressurization system |
US9222411B2 (en) * | 2011-12-21 | 2015-12-29 | General Electric Company | Bleed air and hot section component cooling air system and method |
US8967528B2 (en) * | 2012-01-24 | 2015-03-03 | The Boeing Company | Bleed air systems for use with aircrafts and related methods |
US8955794B2 (en) * | 2012-01-24 | 2015-02-17 | The Boeing Company | Bleed air systems for use with aircrafts and related methods |
GB201318572D0 (en) * | 2013-10-21 | 2013-12-04 | Rolls Royce Plc | Pneumatic system for an aircraft |
-
2014
- 2014-02-17 FR FR1451235A patent/FR3017656B1/fr active Active
-
2015
- 2015-02-16 US US14/623,037 patent/US9885284B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20150233291A1 (en) | 2015-08-20 |
US9885284B2 (en) | 2018-02-06 |
FR3017656A1 (fr) | 2015-08-21 |
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