BE517529A - Perfectionnements aux tuyeres et propulseurs a reaction - Google Patents
Perfectionnements aux tuyeres et propulseurs a reactionInfo
- Publication number
- BE517529A BE517529A BE517529DA BE517529A BE 517529 A BE517529 A BE 517529A BE 517529D A BE517529D A BE 517529DA BE 517529 A BE517529 A BE 517529A
- Authority
- BE
- Belgium
- Prior art keywords
- vanes
- blades
- nozzle
- jet
- grid
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- 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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
- F02K1/32—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for reversing thrust
-
- 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
- F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DES23082A DE867497C (de) | 1951-05-10 | 1951-05-10 | Reaktionsantriebsvorrichtung |
FR62474T | 1952-02-16 | ||
FR64773T | 1953-11-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE517529A true BE517529A (fr) | 1953-02-28 |
Family
ID=62235375
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE503064D BE503064A (de) | 1951-05-10 | ||
BE517529D BE517529A (fr) | 1951-05-10 | 1953-02-09 | Perfectionnements aux tuyeres et propulseurs a reaction |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE503064D BE503064A (de) | 1951-05-10 |
Country Status (4)
Country | Link |
---|---|
BE (2) | BE517529A (de) |
DE (1) | DE867497C (de) |
FR (3) | FR1020287A (de) |
NL (1) | NL161099C (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2949734A (en) * | 1954-07-27 | 1960-08-23 | Snecma | Removable grate for jet deflection |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1030483A (fr) * | 1951-01-04 | 1953-06-15 | Snecma | Procédé et dispositifs de réglage d'un écoulement et leurs diverses applications |
US2834534A (en) * | 1951-09-27 | 1958-05-13 | Snecma | Centrifugal air compressor control device |
US2797548A (en) * | 1952-02-16 | 1957-07-02 | Snecma | Thrust spoiler for propelling nozzles |
US3024602A (en) * | 1952-04-22 | 1962-03-13 | Snecma | Arrangements for deflecting the jet expelled from a discharge nozzle or from a reaction-propulsion unit |
US3048974A (en) * | 1952-04-23 | 1962-08-14 | Snecma | Jet deflecting device for jet propulsion units |
GB724011A (en) * | 1952-05-30 | 1955-02-16 | Power Jets Res & Dev Ltd | Jet deflectors for aircraft |
US2838909A (en) * | 1952-07-17 | 1958-06-17 | Snecma | Means for the deflection of fluid jets |
US3016699A (en) * | 1952-10-10 | 1962-01-16 | Snecma | Aerodynamically acting jet deflecting device |
DE1017474B (de) * | 1952-12-12 | 1957-10-10 | Snecma | Vorrichtung zum Ablenken des Arbeitsgasstromes eines Strahltriebwerkes |
FR1072523A (fr) * | 1952-12-12 | 1954-09-14 | Snecma | Dispositif de contrôle d'un écoulement de fluide par un éeoulement auxiliaire |
US3020713A (en) * | 1952-12-12 | 1962-02-13 | Snecma | Thrust spoiling device for jet propulsion units |
US2807137A (en) * | 1953-07-15 | 1957-09-24 | Snecma | Jet deflecting device for jet propulsion units |
US3002342A (en) * | 1953-08-12 | 1961-10-03 | Schatzki Erich | Mechanism for controlling relatively high velocity flow of fluids longitudinally through and laterally from ambulant conduit means |
US2960822A (en) * | 1953-09-21 | 1960-11-22 | Snecma | Arrangement for deflecting the jets of reaction propulsion units |
US3013386A (en) * | 1954-06-01 | 1961-12-19 | United Aircraft Corp | Reverse thrust device |
BE537645A (de) * | 1954-06-10 | |||
US2929204A (en) * | 1954-10-01 | 1960-03-22 | Gen Electric | Jet spoiler and reverser |
US2950595A (en) * | 1954-11-01 | 1960-08-30 | Marquardt Corp | Thrust reverser |
DE1027521B (de) * | 1954-12-23 | 1958-04-03 | Armstrong Siddeley Motors Ltd | Strahltriebwerk mit Mitteln zur Schubumkehr |
US2933890A (en) * | 1955-01-20 | 1960-04-26 | Boeing Co | Nozzle closing jet deflectors |
US2791088A (en) * | 1955-03-02 | 1957-05-07 | Gen Electric | Device for thrust spoiling and thrust reversal |
US2886946A (en) * | 1955-04-14 | 1959-05-19 | Canadair Ltd | Thrust reversing device for turbojet engines |
US2957306A (en) * | 1955-06-16 | 1960-10-25 | John S Attinello | Gas jets for controlling entrance and/or exit flow effective diameter |
US2952123A (en) * | 1956-05-25 | 1960-09-13 | Lockheed Aircraft Corp | Directional controls for propulsive jets |
DE1048092B (de) * | 1956-07-03 | 1958-12-31 | Snecma | Verfahren und Vorrichtung zur Regelung des Querschnittes einer Ausstossduese von Strahltriebwerken |
CH351801A (fr) * | 1956-07-03 | 1961-01-31 | Snecma | Propulseur à réaction |
US3020714A (en) * | 1956-07-03 | 1962-02-13 | Snecma | Device for controlling the jet of a reaction propulsion motor |
GB852829A (en) * | 1957-04-03 | 1960-11-02 | Rolls Royce | Improvements in or relating to gas-turbine jet propulsion engines |
US2968149A (en) * | 1957-04-26 | 1961-01-17 | Chance Vought Aircraft Inc | Flight control means |
DE1123919B (de) * | 1957-08-14 | 1962-02-15 | Snecma | Vorrichtung zur Stabilisierung und Steuerung von lotrecht startenden und landenden Luftfahrzeugen |
US3069850A (en) * | 1959-05-18 | 1962-12-25 | United Aircraft Corp | Rocket nozzle with directional control |
DE1147122B (de) * | 1959-06-30 | 1963-04-11 | Rolls Royce | Strahlduese mit Strahlumlenkeinrichtungen |
DE1207216B (de) * | 1959-09-07 | 1965-12-16 | Short Brothers & Harland Ltd | Flugregelanlage fuer lotrecht startende und landende Luftfahrzeuge |
DE1187491B (de) * | 1960-03-07 | 1965-02-18 | Moteuers D Aviat Soc Nat D Etu | Stroemungskanal mit ringfoermigem Querschnitt und seitlichen Strahlumlenkungsoeffnungen |
GB918189A (en) * | 1960-07-01 | 1963-02-13 | Rolls Royce | Jet propulsion nozzle |
US3438384A (en) * | 1960-07-15 | 1969-04-15 | Hyman Hurvitz | Electro-fluid systems |
US3132476A (en) * | 1961-04-27 | 1964-05-12 | Earl W Conrad | Thrust vector control apparatus |
US3144752A (en) * | 1961-10-02 | 1964-08-18 | United Aircraft Corp | Injection thrust vectoring |
US3318532A (en) * | 1964-04-29 | 1967-05-09 | Gen Motors Corp | Gas injection thrust vector control system for rocket engines |
DE1277679B (de) * | 1967-04-28 | 1968-09-12 | Entwicklungsring Sued G M B H | Strahltriebwerk, insbesondere fuer senkrecht startende und landende Flugzeuge, mit schwenkbarer Primaerduese und Zusatzluft ansaugender Sekundaerduese |
US4074568A (en) * | 1976-05-07 | 1978-02-21 | The United States Of America As Represented By The Secretary Of The Air Force | Fluidic oscillating jet for high frequency gust tunnel |
-
0
- NL NL7706571.A patent/NL161099C/xx active
- BE BE503064D patent/BE503064A/xx unknown
-
1950
- 1950-06-16 FR FR1020287D patent/FR1020287A/fr not_active Expired
-
1951
- 1951-05-10 DE DES23082A patent/DE867497C/de not_active Expired
-
1952
- 1952-02-16 FR FR62474D patent/FR62474E/fr not_active Expired
-
1953
- 1953-02-09 BE BE517529D patent/BE517529A/fr unknown
- 1953-11-02 FR FR64773D patent/FR64773E/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2949734A (en) * | 1954-07-27 | 1960-08-23 | Snecma | Removable grate for jet deflection |
Also Published As
Publication number | Publication date |
---|---|
FR64773E (fr) | 1955-12-02 |
BE503064A (de) | 1900-01-01 |
FR62474E (fr) | 1955-06-14 |
DE867497C (de) | 1953-02-19 |
FR1020287A (fr) | 1953-02-04 |
NL161099C (nl) | 1900-01-01 |
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