FR1372176A - Oscillating Discharge Cone Nozzle for Gas Turbine Jet Engine - Google Patents
Oscillating Discharge Cone Nozzle for Gas Turbine Jet EngineInfo
- Publication number
- FR1372176A FR1372176A FR949987A FR949987A FR1372176A FR 1372176 A FR1372176 A FR 1372176A FR 949987 A FR949987 A FR 949987A FR 949987 A FR949987 A FR 949987A FR 1372176 A FR1372176 A FR 1372176A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- jet engine
- cone nozzle
- discharge cone
- turbine jet
- 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
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
-
- 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
- B64C29/0058—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 vertical jet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3807762A GB948571A (en) | 1962-10-08 | 1962-10-08 | Gas turbine jet propulsion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1372176A true FR1372176A (en) | 1964-09-11 |
Family
ID=10401015
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR949987A Expired FR1372176A (en) | 1962-10-08 | 1963-10-08 | Oscillating Discharge Cone Nozzle for Gas Turbine Jet Engine |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1223626B (en) |
FR (1) | FR1372176A (en) |
GB (1) | GB948571A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4841726A (en) * | 1985-11-19 | 1989-06-27 | Mtu-Munchen Gmbh | Gas turbine jet engine of multi-shaft double-flow construction |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3429509A (en) * | 1967-05-31 | 1969-02-25 | United Aircraft Corp | Cooling scheme for a three bearing swivel nozzle |
GB2379483A (en) * | 2001-09-08 | 2003-03-12 | Rolls Royce Plc | Augmented gas turbine propulsion system |
GB0504272D0 (en) | 2005-03-02 | 2005-04-06 | Rolls Royce Plc | A turbine engine and a method of operating a turbine engine |
US10563613B2 (en) * | 2015-08-31 | 2020-02-18 | Rolls-Royce North American Technologies Inc. | Coanda device for a round exhaust nozzle |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2630673A (en) * | 1950-09-27 | 1953-03-10 | Gen Electric | Cooling means for variable area nozzles |
GB724004A (en) * | 1952-04-29 | 1955-02-16 | Rolls Royce | Improvements in or relating to fuel supply arrangements for gas-turbine engines |
FR1279495A (en) * | 1960-11-10 | 1961-12-22 | Snecma | Jet deflection device for jet aircraft |
-
1962
- 1962-10-08 GB GB3807762A patent/GB948571A/en not_active Expired
-
1963
- 1963-09-27 DE DER36215A patent/DE1223626B/en active Pending
- 1963-10-08 FR FR949987A patent/FR1372176A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4841726A (en) * | 1985-11-19 | 1989-06-27 | Mtu-Munchen Gmbh | Gas turbine jet engine of multi-shaft double-flow construction |
Also Published As
Publication number | Publication date |
---|---|
GB948571A (en) | 1964-02-05 |
DE1223626B (en) | 1966-08-25 |
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