FR2457380A1 - Turbogenerateur pour voilure tournante d'helicoptere - Google Patents
Turbogenerateur pour voilure tournante d'helicoptereInfo
- Publication number
- FR2457380A1 FR2457380A1 FR7912879A FR7912879A FR2457380A1 FR 2457380 A1 FR2457380 A1 FR 2457380A1 FR 7912879 A FR7912879 A FR 7912879A FR 7912879 A FR7912879 A FR 7912879A FR 2457380 A1 FR2457380 A1 FR 2457380A1
- Authority
- FR
- France
- Prior art keywords
- turbogenerator
- helicopter
- turning wing
- turboreactor
- wing
- 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
- 239000007789 gas Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
- B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
-
- 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
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7912879A FR2457380A1 (fr) | 1979-05-21 | 1979-05-21 | Turbogenerateur pour voilure tournante d'helicoptere |
| US06/230,945 US4404794A (en) | 1979-05-21 | 1980-05-21 | Turbo-generator for a rotary wing helicopter |
| DE8080901071T DE3067675D1 (en) | 1979-05-21 | 1980-05-21 | Turbo-generator for a rotary wing helicopter |
| PCT/FR1980/000083 WO1980002542A1 (fr) | 1979-05-21 | 1980-05-21 | Turbo-generateur pour voilure tournante d'helicoptere |
| EP80901071A EP0029838B1 (fr) | 1979-05-21 | 1980-12-01 | Turbo-generateur pour voilure tournante d'helicoptere |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7912879A FR2457380A1 (fr) | 1979-05-21 | 1979-05-21 | Turbogenerateur pour voilure tournante d'helicoptere |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2457380A1 true FR2457380A1 (fr) | 1980-12-19 |
| FR2457380B3 FR2457380B3 (enExample) | 1982-04-09 |
Family
ID=9225689
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7912879A Granted FR2457380A1 (fr) | 1979-05-21 | 1979-05-21 | Turbogenerateur pour voilure tournante d'helicoptere |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4404794A (enExample) |
| EP (1) | EP0029838B1 (enExample) |
| DE (1) | DE3067675D1 (enExample) |
| FR (1) | FR2457380A1 (enExample) |
| WO (1) | WO1980002542A1 (enExample) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0064936A1 (en) * | 1981-05-04 | 1982-11-17 | Swiss Metalworks Selve Ltd. | High output gas turbine and closely coupled shaft drive load |
| US4899540A (en) * | 1987-08-21 | 1990-02-13 | Donaldson Company, Inc. | Muffler apparatus with filter trap and method of use |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2150670A (en) * | 1938-04-08 | 1939-03-14 | Oliver D H Bentley | Blower |
| US2333053A (en) * | 1940-01-05 | 1943-10-26 | Gen Electric | High temperature elastic fluid turbine |
| US2744722A (en) * | 1951-04-06 | 1956-05-08 | Gen Motors Corp | Turbine bearing support |
| FR1373972A (fr) * | 1963-10-26 | 1964-10-02 | B M W Triebwerkbau Ges M B H | Dispositif de commande du débit d'un groupe d'approvisionnement en air comprimé, notamment du groupe de propulsion d'un hélicoptère à réaction ainsi que le groupe équipé d'un tel dispositif |
| DE1426352A1 (de) * | 1964-06-16 | 1968-12-05 | Licentia Gmbh | Gasturbinenanlage mit Strahltriebwerkeinrichtung und Entspannungsturbine |
| GB1539302A (en) * | 1976-12-11 | 1979-01-31 | Motoren Turbinen Union | Helicopter propulsion systems |
| GB1545365A (en) * | 1977-02-24 | 1979-05-10 | Rolls Royce | Gas turbine engines |
-
1979
- 1979-05-21 FR FR7912879A patent/FR2457380A1/fr active Granted
-
1980
- 1980-05-21 WO PCT/FR1980/000083 patent/WO1980002542A1/fr not_active Ceased
- 1980-05-21 DE DE8080901071T patent/DE3067675D1/de not_active Expired
- 1980-05-21 US US06/230,945 patent/US4404794A/en not_active Expired - Fee Related
- 1980-12-01 EP EP80901071A patent/EP0029838B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| WO1980002542A1 (fr) | 1980-11-27 |
| FR2457380B3 (enExample) | 1982-04-09 |
| EP0029838A1 (fr) | 1981-06-10 |
| EP0029838B1 (fr) | 1984-05-02 |
| US4404794A (en) | 1983-09-20 |
| DE3067675D1 (en) | 1984-06-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| IT7928331A0 (it) | Apparato e metodo per aumentare lapressione all'ingresso del compressore in turbomotori a gas. | |
| IT8023905A0 (it) | Dispositivo per la regolazione dell'aria di sovralimentazione in motori diesel. | |
| IT1151030B (it) | Apparato e metodo per controllare il flusso nel condotto del ventilatore di un turbomotore a gas | |
| GB2049053B (en) | Curved centreline air intake for a gas turbine engine | |
| GB2030657B (en) | Blade for gas turbine engine | |
| IT7926822A0 (it) | Tenuta per l'aria di raffreddamento di turbomotori a gas. | |
| FR2451451B1 (fr) | Rotor aube, a dispositif d'etancheite pour moteur a turbine a gaz | |
| IT1127495B (it) | Perfezionamento nei sistemi di azionamento e di controllo per turbocompressori a gas di scarico | |
| JPS54160911A (en) | Blade for gas turbine engine | |
| ES473820A1 (es) | Perfeccionamientos en turbosoplantes para suministrar aire apresion elevada a un motor de combustion interna. | |
| GB2003988B (en) | Mechanism for operating shut-off members in gas turbine engines | |
| IT1084405B (it) | Dispositivo per regolare la pressione dell'aria di carica in un motore a combustione interna, munito di un turbocompressore a gas di scarico. | |
| IT8020488A0 (it) | Procedimento per attivare e controllare la portata d'aria di by-pass in un motore indotermico sovralimentato e motore endotermico per la realizzazione del procedimento. | |
| GB2033007B (en) | Exhaust turbine driven compressor for ic engines | |
| JPS5372918A (en) | Engine supercharger | |
| JPS54101014A (en) | Winggshaped blade for gas turbine engine | |
| FR2457380A1 (fr) | Turbogenerateur pour voilure tournante d'helicoptere | |
| GB2097863B (en) | Variable air inlet for gas turbine engine | |
| FR2381586A1 (fr) | Installation d'oxycoupage | |
| IT7927795A0 (it) | Dispositivo per il trattamento di aria in motori a combustione. | |
| IT7949090A0 (it) | Ne in motori a turbocompressore dispositivo di regolazione della azionato dai gas di scarico pressione dell'aria di alimentazio | |
| IT1064264B (it) | Valvola di dosatura e di suddivisione del flusso,particolarmente adatta per l'alimentazione di combustibile in turbomotori a gas | |
| IT7949477A0 (it) | Perfezionamento nei motori a turbina a gas | |
| SU582159A1 (ru) | Устройство дл транспортировани грузов по трубопроводу в потоке жидкости или газа | |
| JPS526853A (en) | Constant output electric generating technique and plant by burninc up city trashes |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TP | Transmission of property |