FR2851295B1 - Systeme de prelevement d'air d'un turboreacteur - Google Patents
Systeme de prelevement d'air d'un turboreacteurInfo
- Publication number
- FR2851295B1 FR2851295B1 FR0302016A FR0302016A FR2851295B1 FR 2851295 B1 FR2851295 B1 FR 2851295B1 FR 0302016 A FR0302016 A FR 0302016A FR 0302016 A FR0302016 A FR 0302016A FR 2851295 B1 FR2851295 B1 FR 2851295B1
- Authority
- FR
- France
- Prior art keywords
- collection system
- turbojet engine
- air collection
- air
- turbojet
- 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.)
- Expired - Lifetime
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
- 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
- B64D13/04—Automatic control of pressure
-
- 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
- B64D15/04—Hot gas application
-
- 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
- B64D41/00—Power installations for auxiliary purposes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0302016A FR2851295B1 (fr) | 2003-02-19 | 2003-02-19 | Systeme de prelevement d'air d'un turboreacteur |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0302016A FR2851295B1 (fr) | 2003-02-19 | 2003-02-19 | Systeme de prelevement d'air d'un turboreacteur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2851295A1 FR2851295A1 (fr) | 2004-08-20 |
FR2851295B1 true FR2851295B1 (fr) | 2006-06-23 |
Family
ID=32749684
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0302016A Expired - Lifetime FR2851295B1 (fr) | 2003-02-19 | 2003-02-19 | Systeme de prelevement d'air d'un turboreacteur |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2851295B1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11846237B2 (en) | 2017-01-19 | 2023-12-19 | Rtx Corporation | Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7059136B2 (en) | 2004-08-27 | 2006-06-13 | General Electric Company | Air turbine powered accessory |
US10634051B2 (en) | 2012-01-09 | 2020-04-28 | United Technologies Corporation | Geared turbofan engine with low pressure environmental control system for aircraft |
US8967528B2 (en) * | 2012-01-24 | 2015-03-03 | The Boeing Company | Bleed air systems for use with aircrafts and related methods |
GB201319563D0 (en) * | 2013-11-06 | 2013-12-18 | Rolls Royce Plc | Pneumatic system for an aircraft |
BR102015015377B1 (pt) * | 2014-06-27 | 2022-04-26 | United Technologies Corporation | Conjunto de motor de turbina a gás, e, sistema de controle ambiental de uma aeronave |
US10731560B2 (en) | 2015-02-12 | 2020-08-04 | Raytheon Technologies Corporation | Intercooled cooling air |
US11808210B2 (en) | 2015-02-12 | 2023-11-07 | Rtx Corporation | Intercooled cooling air with heat exchanger packaging |
US10371055B2 (en) | 2015-02-12 | 2019-08-06 | United Technologies Corporation | Intercooled cooling air using cooling compressor as starter |
US9850819B2 (en) | 2015-04-24 | 2017-12-26 | United Technologies Corporation | Intercooled cooling air with dual pass heat exchanger |
US10480419B2 (en) | 2015-04-24 | 2019-11-19 | United Technologies Corporation | Intercooled cooling air with plural heat exchangers |
US10830148B2 (en) | 2015-04-24 | 2020-11-10 | Raytheon Technologies Corporation | Intercooled cooling air with dual pass heat exchanger |
US10221862B2 (en) | 2015-04-24 | 2019-03-05 | United Technologies Corporation | Intercooled cooling air tapped from plural locations |
US10100739B2 (en) | 2015-05-18 | 2018-10-16 | United Technologies Corporation | Cooled cooling air system for a gas turbine engine |
US10794288B2 (en) | 2015-07-07 | 2020-10-06 | Raytheon Technologies Corporation | Cooled cooling air system for a turbofan engine |
US10443508B2 (en) | 2015-12-14 | 2019-10-15 | United Technologies Corporation | Intercooled cooling air with auxiliary compressor control |
US10669940B2 (en) | 2016-09-19 | 2020-06-02 | Raytheon Technologies Corporation | Gas turbine engine with intercooled cooling air and turbine drive |
US10794290B2 (en) | 2016-11-08 | 2020-10-06 | Raytheon Technologies Corporation | Intercooled cooled cooling integrated air cycle machine |
US10550768B2 (en) | 2016-11-08 | 2020-02-04 | United Technologies Corporation | Intercooled cooled cooling integrated air cycle machine |
US10961911B2 (en) | 2017-01-17 | 2021-03-30 | Raytheon Technologies Corporation | Injection cooled cooling air system for a gas turbine engine |
US10577964B2 (en) | 2017-03-31 | 2020-03-03 | United Technologies Corporation | Cooled cooling air for blade air seal through outer chamber |
US10711640B2 (en) | 2017-04-11 | 2020-07-14 | Raytheon Technologies Corporation | Cooled cooling air to blade outer air seal passing through a static vane |
US10738703B2 (en) | 2018-03-22 | 2020-08-11 | Raytheon Technologies Corporation | Intercooled cooling air with combined features |
US10830145B2 (en) | 2018-04-19 | 2020-11-10 | Raytheon Technologies Corporation | Intercooled cooling air fleet management system |
US10808619B2 (en) | 2018-04-19 | 2020-10-20 | Raytheon Technologies Corporation | Intercooled cooling air with advanced cooling system |
US10718233B2 (en) | 2018-06-19 | 2020-07-21 | Raytheon Technologies Corporation | Intercooled cooling air with low temperature bearing compartment air |
US11255268B2 (en) | 2018-07-31 | 2022-02-22 | Raytheon Technologies Corporation | Intercooled cooling air with selective pressure dump |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5137230A (en) | 1991-06-04 | 1992-08-11 | General Electric Company | Aircraft gas turbine engine bleed air energy recovery apparatus |
US5899085A (en) * | 1997-08-01 | 1999-05-04 | Mcdonnell Douglas Corporation | Integrated air conditioning and power unit |
US6305156B1 (en) * | 1999-09-03 | 2001-10-23 | Alliedsignal Inc. | Integrated bleed air and engine starting system |
-
2003
- 2003-02-19 FR FR0302016A patent/FR2851295B1/fr not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11846237B2 (en) | 2017-01-19 | 2023-12-19 | Rtx Corporation | Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox |
Also Published As
Publication number | Publication date |
---|---|
FR2851295A1 (fr) | 2004-08-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2851295B1 (fr) | Systeme de prelevement d'air d'un turboreacteur | |
FR2839119B1 (fr) | Systeme de demarrage de moteur | |
AU2003243627A8 (en) | Microturbine engine system | |
GB2388633B (en) | Engine lubrication system | |
DE60227537D1 (de) | Vollgesteuerter freikolbenmotor | |
FR2863302B1 (fr) | Systeme de fixation d'un distributeur de turbine | |
FR2829541B1 (fr) | Systeme d'embrayage | |
GB0218849D0 (en) | Lubrication system for gas turbine engine | |
ITMI20011010A0 (it) | Procedimento per la diagnosi del funzionamento di un sistema di sfiato di un basamento di un motore endotermico | |
DE60305826D1 (de) | Verbrennungsmotor-Anlassersystem | |
ATA16452002A (de) | Verbrennungsmotor | |
FR2829193B1 (fr) | Systeme de prelevement d'air d'un compresseur | |
FR2848259B1 (fr) | Demarreur de moteur | |
FR2857048B1 (fr) | Verrouillage des capots de nacelle d'un turboreacteur | |
FR2872784B1 (fr) | Systeme de suspension d'un moteur d'aeronef a voilure tournante | |
ITMI20012016A0 (it) | Silenziatore di aspirazione per compressore | |
IL157666A0 (en) | Novel gas turbine engine system | |
AU2003268746A1 (en) | Air scavenging-type two-cycle engine | |
FR2860706B1 (fr) | Systeme de grandissement d'image retinienne | |
EP1553280A4 (fr) | Moteur en v a ouverture etroite | |
DE60221597D1 (de) | Hybrides Brennkraftmachinensystem | |
DE60300869D1 (de) | Brennkraftmaschinengetriebenes System | |
ITTO20020650A0 (it) | Metodo di diagnosi di un impianto di raffreddamento di un motore di un veicolo | |
FR2859761B1 (fr) | Moteur a turbine d'helicoptere | |
DE50313171D1 (de) | Ansaugkanalsystem |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
PLFP | Fee payment |
Year of fee payment: 16 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
PLFP | Fee payment |
Year of fee payment: 18 |
|
PLFP | Fee payment |
Year of fee payment: 19 |
|
PLFP | Fee payment |
Year of fee payment: 20 |