FR1215236A - Adjustable nozzle and jet thruster equipped with such nozzle - Google Patents
Adjustable nozzle and jet thruster equipped with such nozzleInfo
- Publication number
- FR1215236A FR1215236A FR778866A FR778866A FR1215236A FR 1215236 A FR1215236 A FR 1215236A FR 778866 A FR778866 A FR 778866A FR 778866 A FR778866 A FR 778866A FR 1215236 A FR1215236 A FR 1215236A
- Authority
- FR
- France
- Prior art keywords
- nozzle
- adjustable
- jet thruster
- thruster equipped
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR778866A FR1215236A (en) | 1958-11-12 | 1958-11-12 | Adjustable nozzle and jet thruster equipped with such nozzle |
GB37720/59A GB876583A (en) | 1958-11-12 | 1959-11-06 | Adjustable jet propulsion nozzle and jet propulsion engine provided with such nozzle |
DES65748A DE1129775B (en) | 1958-11-12 | 1959-11-07 | Thrust nozzle with adjustable cross-section |
US852070A US3054256A (en) | 1958-11-12 | 1959-11-10 | Adjustable discharge nozzle and jet engine provided with such a nozzle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR778866A FR1215236A (en) | 1958-11-12 | 1958-11-12 | Adjustable nozzle and jet thruster equipped with such nozzle |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1215236A true FR1215236A (en) | 1960-04-15 |
Family
ID=8708187
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR778866A Expired FR1215236A (en) | 1958-11-12 | 1958-11-12 | Adjustable nozzle and jet thruster equipped with such nozzle |
Country Status (4)
Country | Link |
---|---|
US (1) | US3054256A (en) |
DE (1) | DE1129775B (en) |
FR (1) | FR1215236A (en) |
GB (1) | GB876583A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1245646B (en) * | 1961-07-28 | 1967-07-27 | Rolls Royce | Thrust nozzle assembly for jet engines |
US4608822A (en) * | 1980-10-01 | 1986-09-02 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. | System for controlling the valves of a turbo jet shaft engine nozzle |
EP1553092A1 (en) * | 2002-05-08 | 2005-07-13 | Shanghai Institute of Pharmaceutical Industry | Aralkyl formyl-alkyl piperazine derivatives and their uses as cerebral nerve protective agent |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3279194A (en) * | 1962-08-14 | 1966-10-18 | Garrett Corp | Aerothermodynamic duct and control means therefor |
US3316716A (en) * | 1964-07-01 | 1967-05-02 | William J D Escher | Composite powerplant and shroud therefor |
CA961652A (en) * | 1971-12-20 | 1975-01-28 | Richard E. Teagle | Balanced flap converging/diverging nozzle |
DE2845149C2 (en) * | 1978-10-17 | 1982-03-04 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Jet engine, especially for propelling an aircraft |
US5201800A (en) * | 1990-02-26 | 1993-04-13 | General Electric Company | Method for discharging combustion gases from an exhaust nozzle |
US5103639A (en) * | 1990-02-26 | 1992-04-14 | General Electric Company | Exhaust nozzle having variable contour exhaust flap |
US5484105A (en) * | 1994-07-13 | 1996-01-16 | General Electric Company | Cooling system for a divergent section of a nozzle |
US5706650A (en) * | 1995-08-09 | 1998-01-13 | United Technologies Corporation | Vectoring nozzle using injected high pressure air |
DE102008022271A1 (en) * | 2008-05-06 | 2009-11-26 | Opara, Günther | Nozzle i.e. jet-nozzle, for e.g. gas turbine of aircraft, has one-piece tubular body including wall that forms convergent and divergent channel parts by radial contraction of cross-section dimension of nozzle |
DE102017104043A1 (en) * | 2017-02-27 | 2018-08-30 | Rolls-Royce Deutschland Ltd & Co Kg | Convergent-divergent exhaust nozzle for a turbofan engine of a supersonic aircraft and method for reducing the rear resistance behind such a thruster |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2597253A (en) * | 1945-11-13 | 1952-05-20 | Effie B Melchior | Jet-propulsion nozzle |
CA486078A (en) * | 1950-04-27 | 1952-08-26 | W. Kellal George | Exit area control for jet engines |
US2625008A (en) * | 1951-02-28 | 1953-01-13 | Curtiss Wright Corp | Variable flow nozzle |
US2770944A (en) * | 1952-04-26 | 1956-11-20 | United Aircraft Corp | Variable area reaction nozzle movable from convergent to convergent-di-vergent form |
US2858668A (en) * | 1952-09-27 | 1958-11-04 | Curtiss Wright Corp | Control for variable area convergentdivergent exhaust nozzle |
BE531848A (en) * | 1953-09-17 | |||
US2939274A (en) * | 1954-01-04 | 1960-06-07 | North American Aviation Inc | Means for varying a jet engine orifice |
GB782494A (en) * | 1954-03-26 | 1957-09-11 | Rolls Royce | Improvements in or relating to jet propulsion nozzle arrangements |
GB788359A (en) * | 1954-11-26 | 1958-01-02 | Power Jets Res & Dev Ltd | Discharge nozzles for propulsive jets |
GB768014A (en) * | 1955-03-07 | 1957-02-13 | United Aircraft Corp | Improvements in or relating to variable area propulsion nozzles |
US2931169A (en) * | 1956-05-15 | 1960-04-05 | Westinghouse Electric Corp | Variable convergent-divergent exhaust nozzle |
US2910829A (en) * | 1956-08-24 | 1959-11-03 | United Aircraft Corp | Exhaust nozzle interflap seal |
US2932163A (en) * | 1958-05-12 | 1960-04-12 | Orenda Engines Ltd | Means for actuating a variable nozzle |
-
1958
- 1958-11-12 FR FR778866A patent/FR1215236A/en not_active Expired
-
1959
- 1959-11-06 GB GB37720/59A patent/GB876583A/en not_active Expired
- 1959-11-07 DE DES65748A patent/DE1129775B/en active Pending
- 1959-11-10 US US852070A patent/US3054256A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1245646B (en) * | 1961-07-28 | 1967-07-27 | Rolls Royce | Thrust nozzle assembly for jet engines |
US4608822A (en) * | 1980-10-01 | 1986-09-02 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. | System for controlling the valves of a turbo jet shaft engine nozzle |
EP1553092A1 (en) * | 2002-05-08 | 2005-07-13 | Shanghai Institute of Pharmaceutical Industry | Aralkyl formyl-alkyl piperazine derivatives and their uses as cerebral nerve protective agent |
EP1553092A4 (en) * | 2002-05-08 | 2007-06-27 | Shanghai Inst Pharm Industry | Aralkyl formyl-alkyl piperazine derivatives and their uses as cerebral nerve protective agent |
Also Published As
Publication number | Publication date |
---|---|
US3054256A (en) | 1962-09-18 |
GB876583A (en) | 1961-09-06 |
DE1129775B (en) | 1962-05-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR1233323A (en) | Actuator for variable area nozzles of jet airplanes | |
FR1227966A (en) | Propulsion nozzle device for jet propulsion units | |
FR1215236A (en) | Adjustable nozzle and jet thruster equipped with such nozzle | |
FR1182810A (en) | Improvements to adjustable section ejection nozzles | |
FR1246339A (en) | Swiveling ejection nozzle | |
FR1225736A (en) | Adjustable nozzle for jet thruster | |
CH384291A (en) | Jet thruster | |
FR1219639A (en) | Improvements to jet propulsion devices of aerodynes | |
FR1150555A (en) | Improvement in jet thrusters | |
FR1198723A (en) | Convergent-divergent nozzle with continuously variable geometry and neck sections | |
CH401590A (en) | Silent exhaust nozzle for jet thruster | |
CH351801A (en) | Jet thruster | |
FR1215237A (en) | Variable geometry nozzle | |
FR1248777A (en) | Jet mill | |
FR1176983A (en) | Improvements to jet thrusters | |
FR1218561A (en) | Improvements to jet thrusters and more specifically to rockets | |
FR1328385A (en) | Variable orifice section nozzle | |
FR1288602A (en) | Jet thruster | |
FR1183042A (en) | Improvement in the control devices of jet deflection jet aircraft | |
FR1255001A (en) | Improvements to jet thruster ejection nozzles | |
FR1220047A (en) | Improvement in jet thrusters | |
FR1228468A (en) | Variable section nozzle for aircraft turbo-reactors | |
FR74191E (en) | Multi-fit supersonic ejection nozzle | |
FR1269470A (en) | Inlet nozzle for aircraft jet thrusters | |
FR1112620A (en) | Advanced jet thruster |