FR1443200A - Powerplant using a gas turbine, for aircraft - Google Patents
Powerplant using a gas turbine, for aircraftInfo
- Publication number
- FR1443200A FR1443200A FR13955A FR13955A FR1443200A FR 1443200 A FR1443200 A FR 1443200A FR 13955 A FR13955 A FR 13955A FR 13955 A FR13955 A FR 13955A FR 1443200 A FR1443200 A FR 1443200A
- Authority
- FR
- France
- Prior art keywords
- powerplant
- aircraft
- gas turbine
- turbine
- gas
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
- B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
- B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR13955A FR1443200A (en) | 1965-04-21 | 1965-04-21 | Powerplant using a gas turbine, for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR13955A FR1443200A (en) | 1965-04-21 | 1965-04-21 | Powerplant using a gas turbine, for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1443200A true FR1443200A (en) | 1966-06-24 |
Family
ID=8576855
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR13955A Expired FR1443200A (en) | 1965-04-21 | 1965-04-21 | Powerplant using a gas turbine, for aircraft |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1443200A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008017567A1 (en) * | 2006-08-11 | 2008-02-14 | Team Smartfish Gmbh | Air inlet for a jet engine |
EP1975064A1 (en) | 2007-03-28 | 2008-10-01 | EADS Deutschland GmbH | Aircraft |
FR2931799A1 (en) * | 2008-05-30 | 2009-12-04 | Airbus France | Aircraft i.e. civil passenger transport aircraft, has reactors located inside envelope surface of theoretical fuselage, where lines of theoretical fuselage correspond to same dimension lines of aircraft fuselage with or without reactors |
CN102202973B (en) * | 2008-10-30 | 2014-12-31 | 斯奈克玛 | Airplane having engines partially encased in the fuselage |
US9266617B2 (en) | 2011-10-24 | 2016-02-23 | Rolls-Royce Plc | Propulsive system |
WO2017013363A1 (en) * | 2015-07-22 | 2017-01-26 | Safran Aircraft Engines | Aircraft comprising a propulsion assembly including a fan on the rear of the fuselage |
EP3333403A1 (en) * | 2016-12-07 | 2018-06-13 | United Technologies Corporation | Boundary layer excitation aft fan gas turbine engine |
-
1965
- 1965-04-21 FR FR13955A patent/FR1443200A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008017567A1 (en) * | 2006-08-11 | 2008-02-14 | Team Smartfish Gmbh | Air inlet for a jet engine |
EP1975064A1 (en) | 2007-03-28 | 2008-10-01 | EADS Deutschland GmbH | Aircraft |
FR2931799A1 (en) * | 2008-05-30 | 2009-12-04 | Airbus France | Aircraft i.e. civil passenger transport aircraft, has reactors located inside envelope surface of theoretical fuselage, where lines of theoretical fuselage correspond to same dimension lines of aircraft fuselage with or without reactors |
US8573531B2 (en) | 2008-05-30 | 2013-11-05 | Airbus Operations Sas | Airplane with rear engines |
CN102202973B (en) * | 2008-10-30 | 2014-12-31 | 斯奈克玛 | Airplane having engines partially encased in the fuselage |
US9266617B2 (en) | 2011-10-24 | 2016-02-23 | Rolls-Royce Plc | Propulsive system |
WO2017013363A1 (en) * | 2015-07-22 | 2017-01-26 | Safran Aircraft Engines | Aircraft comprising a propulsion assembly including a fan on the rear of the fuselage |
FR3039133A1 (en) * | 2015-07-22 | 2017-01-27 | Snecma | AIRCRAFT WITH A PROPULSIVE ASSEMBLY COMPRISING A BLOWER AT THE REAR OF THE FUSELAGE |
US10829232B2 (en) | 2015-07-22 | 2020-11-10 | Safran Aircraft Engines | Aircraft comprising a propulsion assembly including a fan on the rear of the fuselage |
EP3333403A1 (en) * | 2016-12-07 | 2018-06-13 | United Technologies Corporation | Boundary layer excitation aft fan gas turbine engine |
US10823056B2 (en) | 2016-12-07 | 2020-11-03 | Raytheon Technologies Corporation | Boundary layer excitation aft fan gas turbine engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CH466640A (en) | Gas turbine | |
CH452998A (en) | Gas turbine | |
CH448616A (en) | Gas turbine | |
FR89216E (en) | Gas turbine-steam turbine combination | |
FR1443200A (en) | Powerplant using a gas turbine, for aircraft | |
CH460450A (en) | Gas turbine | |
FR1499830A (en) | Gas turbine engine group | |
CH534300A (en) | Gas turbine | |
FR1501477A (en) | Gas turbine rotor | |
FR1499580A (en) | Burner device applicable to gas turbine engines | |
FR1496841A (en) | Gas turbine engine improvements | |
FR1429834A (en) | Improvements made to blades, particularly for gas turbine engines | |
FR1524810A (en) | Gas turbine | |
FR1522468A (en) | Tangential jet gas turbine | |
FR1484643A (en) | Gas turbine | |
FR1447843A (en) | Gas turbine | |
FR1518513A (en) | Gas turbine engine machines | |
FR1420095A (en) | Hand starter for gas turbine | |
FR1536426A (en) | Gas turbine machines | |
CA710536A (en) | Regenerator arrangement for gas turbine powerplants | |
FR1360218A (en) | Gas turbine engine group | |
FR1534901A (en) | Gas turbine | |
FR1523041A (en) | Gas turbine | |
FR1486102A (en) | Safety device for gas turbine | |
FR1431470A (en) | Gas turbine |