FR1153561A - New jet propulsion mode for marine vehicles and new jet diverter - Google Patents
New jet propulsion mode for marine vehicles and new jet diverterInfo
- Publication number
- FR1153561A FR1153561A FR1153561DA FR1153561A FR 1153561 A FR1153561 A FR 1153561A FR 1153561D A FR1153561D A FR 1153561DA FR 1153561 A FR1153561 A FR 1153561A
- Authority
- FR
- France
- Prior art keywords
- new jet
- diverter
- propulsion mode
- marine vehicles
- new
- 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
-
- 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
-
- 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
- F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
-
- 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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1153561T | 1956-06-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1153561A true FR1153561A (en) | 1958-03-12 |
Family
ID=9648946
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1153561D Expired FR1153561A (en) | 1956-06-01 | 1956-06-01 | New jet propulsion mode for marine vehicles and new jet diverter |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1153561A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2369428A1 (en) * | 1976-10-29 | 1978-05-26 | Messerschmitt Boelkow Blohm | Rocket outlet nozzle with spoilers - has deflectors with air stream separating jet from one deflector wall |
FR2557925A1 (en) * | 1984-01-05 | 1985-07-12 | Hurel Dubois Avions | IMPROVEMENT TO DOUBLE FLOW REACTION ENGINES EQUIPPED WITH A THRUST INVERTER. |
EP0385834A1 (en) * | 1989-03-01 | 1990-09-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Variable and vectorable nozzle unit for a jet engine |
FR2736390A1 (en) * | 1995-07-05 | 1997-01-10 | Hispano Suiza Sa | PUSH INVERTER OF A SHELL TURBOREACTOR |
-
1956
- 1956-06-01 FR FR1153561D patent/FR1153561A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2369428A1 (en) * | 1976-10-29 | 1978-05-26 | Messerschmitt Boelkow Blohm | Rocket outlet nozzle with spoilers - has deflectors with air stream separating jet from one deflector wall |
FR2557925A1 (en) * | 1984-01-05 | 1985-07-12 | Hurel Dubois Avions | IMPROVEMENT TO DOUBLE FLOW REACTION ENGINES EQUIPPED WITH A THRUST INVERTER. |
EP0150649A1 (en) * | 1984-01-05 | 1985-08-07 | Societe De Construction Des Avions Hurel-Dubois | Dual flux jet engines having a thrust reverser |
EP0385834A1 (en) * | 1989-03-01 | 1990-09-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Variable and vectorable nozzle unit for a jet engine |
FR2643947A1 (en) * | 1989-03-01 | 1990-09-07 | Snecma | AXISYMMETRICAL NOZZLE TURBOREACTOR EJECTION ASSEMBLY WITH VARIABLE SECTION AND PUSH-THROUGH |
US4993638A (en) * | 1989-03-01 | 1991-02-19 | Societe Nationale D'etude Et De Construction De Mateurs D'aviation "S.N.E.C.M.A." | Thrust vectoring nozzle assembly |
FR2736390A1 (en) * | 1995-07-05 | 1997-01-10 | Hispano Suiza Sa | PUSH INVERTER OF A SHELL TURBOREACTOR |
WO1997002419A1 (en) * | 1995-07-05 | 1997-01-23 | Societe Hispano-Suiza | Single-clamshell turbojet thrust reverser |
EP0757170A1 (en) * | 1995-07-05 | 1997-02-05 | Hispano Suiza | Jet engine thrust reverser with a single door |
US5785249A (en) * | 1995-07-05 | 1998-07-28 | Societe Hispano Suiza | Single baffle turbojet engine thrust reverser |
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