FR2469567A1 - Installation pour un prelevement souple de puissance dans les turbines a gaz d'avions a hautes performances - Google Patents
Installation pour un prelevement souple de puissance dans les turbines a gaz d'avions a hautes performancesInfo
- Publication number
- FR2469567A1 FR2469567A1 FR8024066A FR8024066A FR2469567A1 FR 2469567 A1 FR2469567 A1 FR 2469567A1 FR 8024066 A FR8024066 A FR 8024066A FR 8024066 A FR8024066 A FR 8024066A FR 2469567 A1 FR2469567 A1 FR 2469567A1
- Authority
- FR
- France
- Prior art keywords
- high performance
- gas turbines
- power taking
- flexible power
- performance aircraft
- 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.)
- Granted
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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
INSTALLATION POUR UN PRELEVEMENT SOUPLE OU FLEXIBLE DE PUISSANCE DANS LES TURBINES A GAZ D'AVIONS NON STABLES A HAUTES PERFORMANCES. DES SUPPORTS D'APPAREILS 10, 11 SERVANT AU PRELEVEMENT DE PUISSANCE POUR L'ENTRAINEMENT DU SYSTEME D'ENTRAINEMENT SECONDAIRE, SONT RELIES, D'UNE PART MECANIQUEMENT AU ROTOR HAUTE PRESSION DU PROPULSEUR OU ELECTRIQUEMENT A DES GENERATEURS DE COURANT CONTINU HAUTE TENSION, ET D'AUTRE PART PNEUMATIQUEMENT A UN DISPOSITIF DE PRELEVEMENT D'AIR COMPRIME A PLUSIEURS ETAGES SUR LE COMPRESSEUR DU PROPULSEUR.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2946371A DE2946371C2 (de) | 1979-11-16 | 1979-11-16 | Hilfsantriebsanlage für Flugzeughilfsgeräte |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2469567A1 true FR2469567A1 (fr) | 1981-05-22 |
FR2469567B3 FR2469567B3 (fr) | 1982-07-23 |
Family
ID=6086194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8024066A Granted FR2469567A1 (fr) | 1979-11-16 | 1980-11-12 | Installation pour un prelevement souple de puissance dans les turbines a gaz d'avions a hautes performances |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE2946371C2 (fr) |
FR (1) | FR2469567A1 (fr) |
GB (1) | GB2063188B (fr) |
IT (1) | IT1133799B (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3502578A1 (de) * | 1985-01-26 | 1986-07-31 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Hilfsantrieb fuer ein gasturbinentriebwerk |
DE3515770A1 (de) * | 1985-05-02 | 1986-11-06 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Hilfsantriebsanordnung mit getriebe fuer ein gasturbinentriebwerk |
US7975465B2 (en) | 2003-10-27 | 2011-07-12 | United Technologies Corporation | Hybrid engine accessory power system |
DE102008018101A1 (de) | 2008-04-09 | 2009-10-15 | Rolls-Royce Deutschland Ltd & Co Kg | Strahltriebwerk mit mindestens einem Notantrieb |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2863288A (en) * | 1954-11-19 | 1958-12-09 | Jack & Heintz Inc | Air pressure control means for air turbine drive systems |
BE567824A (fr) * | 1957-05-20 | |||
GB1212109A (en) * | 1968-08-09 | 1970-11-11 | Rolls Royce | Engine assembly |
US3514945A (en) * | 1968-10-04 | 1970-06-02 | Avco Corp | Gas turbine accessory power drive unit |
US4068470A (en) * | 1974-11-08 | 1978-01-17 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Gas turbine engine with convertible accessories |
DE2519152C2 (de) * | 1975-04-30 | 1982-11-25 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Vorrichtung zum Anlassen von Flugzeugtriebwerken und zum Betreiben von Flugzeughilfsgeräten |
-
1979
- 1979-11-16 DE DE2946371A patent/DE2946371C2/de not_active Expired
-
1980
- 1980-11-11 GB GB8036159A patent/GB2063188B/en not_active Expired
- 1980-11-11 IT IT25895/80A patent/IT1133799B/it active
- 1980-11-12 FR FR8024066A patent/FR2469567A1/fr active Granted
Also Published As
Publication number | Publication date |
---|---|
GB2063188B (en) | 1983-09-28 |
GB2063188A (en) | 1981-06-03 |
FR2469567B3 (fr) | 1982-07-23 |
IT8025895A0 (it) | 1980-11-11 |
DE2946371C2 (de) | 1982-07-08 |
DE2946371A1 (de) | 1981-05-27 |
IT1133799B (it) | 1986-07-09 |
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