FR1055264A - Improvements to aircraft powertrains - Google Patents
Improvements to aircraft powertrainsInfo
- Publication number
- FR1055264A FR1055264A FR1055264DA FR1055264A FR 1055264 A FR1055264 A FR 1055264A FR 1055264D A FR1055264D A FR 1055264DA FR 1055264 A FR1055264 A FR 1055264A
- Authority
- FR
- France
- Prior art keywords
- powertrains
- aircraft
- aircraft powertrains
- 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
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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- 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
- F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1055264T | 1952-04-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1055264A true FR1055264A (en) | 1954-02-17 |
Family
ID=9596841
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1055264D Expired FR1055264A (en) | 1952-04-28 | 1952-04-28 | Improvements to aircraft powertrains |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1055264A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0580277A1 (en) * | 1992-07-18 | 1994-01-26 | ROLLS-ROYCE plc | Ducted fan gas turbine engine |
FR2698068A1 (en) * | 1992-11-16 | 1994-05-20 | Airbus Ind | Aircraft and other powered aircraft with wings. |
EP1504993A1 (en) * | 2003-08-02 | 2005-02-09 | Airbus Deutschland GmbH | Ram air inlet |
FR3043724A1 (en) * | 2015-11-16 | 2017-05-19 | Snecma | METHOD OF DIMENSIONING A PROPULSIVE ASSEMBLY COMPRISING A MAIN ENGINE AND AN AUXILIARY ENGINE |
EP3594473A1 (en) * | 2018-07-12 | 2020-01-15 | Rolls-Royce plc | Supersonic aircraft propulsion installation |
-
1952
- 1952-04-28 FR FR1055264D patent/FR1055264A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0580277A1 (en) * | 1992-07-18 | 1994-01-26 | ROLLS-ROYCE plc | Ducted fan gas turbine engine |
US5319927A (en) * | 1992-07-18 | 1994-06-14 | Rolls-Royce Plc | Ducted fan gas turbine engine |
FR2698068A1 (en) * | 1992-11-16 | 1994-05-20 | Airbus Ind | Aircraft and other powered aircraft with wings. |
WO1994011248A1 (en) * | 1992-11-16 | 1994-05-26 | Airbus Industrie | Aircraft with at least one set of two engines fitted on each wing |
EP1504993A1 (en) * | 2003-08-02 | 2005-02-09 | Airbus Deutschland GmbH | Ram air inlet |
US7222819B1 (en) | 2003-08-02 | 2007-05-29 | Airbus Deutschland Gmbh | Aircraft ram air inlet with multi-member closure flap |
FR3043724A1 (en) * | 2015-11-16 | 2017-05-19 | Snecma | METHOD OF DIMENSIONING A PROPULSIVE ASSEMBLY COMPRISING A MAIN ENGINE AND AN AUXILIARY ENGINE |
WO2017085405A1 (en) * | 2015-11-16 | 2017-05-26 | Safran Aircraft Engines | Method for rating a propulsion unit comprising a main engine and an auxiliary engine |
US11807376B2 (en) | 2015-11-16 | 2023-11-07 | Safran Aircraft Engines | Method for rating a propulsion unit comprising a main engine and an auxiliary engine |
EP3594473A1 (en) * | 2018-07-12 | 2020-01-15 | Rolls-Royce plc | Supersonic aircraft propulsion installation |
US11383848B2 (en) | 2018-07-12 | 2022-07-12 | Rolls-Royce Plc | Supersonic aircraft propulsion installation |
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