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
- 238000009434 installation Methods 0.000 abstract 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
- 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)
- Engine Equipment That Uses Special Cycles (AREA)
- Control Of Turbines (AREA)
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 (enExample) | 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 (enExample) |
| FR (1) | FR2469567A1 (enExample) |
| GB (1) | GB2063188B (enExample) |
| IT (1) | IT1133799B (enExample) |
Families Citing this family (6)
| 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 |
| RU2168043C1 (ru) * | 1999-12-10 | 2001-05-27 | Открытое акционерное общество "А.Люлька-Сатурн" | Способ запуска авиационного газотурбинного двигателя |
| US7975465B2 (en) * | 2003-10-27 | 2011-07-12 | United Technologies Corporation | Hybrid engine accessory power system |
| RU2282736C2 (ru) * | 2003-11-14 | 2006-08-27 | Республиканское унитарное предприятие "Головное специальное конструкторско-технологическое бюро гидроаппаратуры с опытно-экспериментальным производством" | Устройство для гидравлического запуска газотурбинного двигателя |
| 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 (enExample) * | 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 |
|---|---|
| FR2469567B3 (enExample) | 1982-07-23 |
| GB2063188B (en) | 1983-09-28 |
| GB2063188A (en) | 1981-06-03 |
| IT1133799B (it) | 1986-07-09 |
| IT8025895A0 (it) | 1980-11-11 |
| DE2946371C2 (de) | 1982-07-08 |
| DE2946371A1 (de) | 1981-05-27 |
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