BE637917A - - Google Patents
Info
- Publication number
- BE637917A BE637917A BE637917DA BE637917A BE 637917 A BE637917 A BE 637917A BE 637917D A BE637917D A BE 637917DA BE 637917 A BE637917 A BE 637917A
- Authority
- BE
- Belgium
Links
Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B17/00—Insulators or insulating bodies characterised by their form
- H01B17/36—Insulators having evacuated or gas-filled spaces
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- 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
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
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- 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
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
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- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US752623A US2483401A (en) | 1947-06-05 | 1947-06-05 | Exhaust nozzle actuating mechanism |
Publications (1)
Publication Number | Publication Date |
---|---|
BE637917A true BE637917A (fr) |
Family
ID=25027087
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE637917D BE637917A (fr) | 1947-06-05 |
Country Status (3)
Country | Link |
---|---|
US (1) | US2483401A (fr) |
BE (1) | BE637917A (fr) |
GB (1) | GB637917A (fr) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2557883A (en) * | 1947-09-17 | 1951-06-19 | Ernest F Miller | Jet propulsion exhaust nozzle apparatus |
US2677233A (en) * | 1949-06-30 | 1954-05-04 | United Aircraft Corp | Exhaust nozzle switch responsive to afterburner pressure ratio |
US2608821A (en) * | 1949-10-08 | 1952-09-02 | Gen Electric | Contrarotating turbojet engine having independent bearing supports for each turbocompressor |
GB685939A (en) * | 1950-05-17 | 1953-01-14 | Rolls Royce | Improvements in or relating to gas-turbine engine structures |
US2712727A (en) * | 1950-05-17 | 1955-07-12 | Rolls Royce | Gas turbine power plants with means for preventing or removing ice formation |
US2674845A (en) * | 1951-05-02 | 1954-04-13 | Walter D Pouchot | Diffuser apparatus with boundary layer control |
US2682147A (en) * | 1951-06-16 | 1954-06-29 | Rohr Aircraft Corp | Adjustable nozzle for exhaust gas |
US2813395A (en) * | 1951-06-29 | 1957-11-19 | United Aircraft Corp | Flap type variable area thrust nozzle having an actuating mechanism including a movable duct |
US2780914A (en) * | 1951-12-20 | 1957-02-12 | Gen Electric | Ambient pressure responsive control for fuel oxidizer and nozzle exhaust area of reaction motors |
US2797548A (en) * | 1952-02-16 | 1957-07-02 | Snecma | Thrust spoiler for propelling nozzles |
US3048974A (en) * | 1952-04-23 | 1962-08-14 | Snecma | Jet deflecting device for jet propulsion units |
BE530004A (fr) * | 1953-06-30 | |||
US2789416A (en) * | 1953-08-26 | 1957-04-23 | Fairchild Engine & Airplane | System for cooling a turbine bearing of a gas turbine power plant |
US2826895A (en) * | 1953-09-03 | 1958-03-18 | Fairchild Engine & Airplane | Bearing cooling system |
US3066480A (en) * | 1954-01-13 | 1962-12-04 | Richard S Buck | Ramjet missile |
GB834907A (en) * | 1956-10-23 | 1960-05-11 | Rolls Royce | Improvements in or relating to jet propulsion nozzles |
US2848867A (en) * | 1956-12-24 | 1958-08-26 | United Aircraft Corp | Ejector-silencer exhaust nozzle |
DE1200067B (de) * | 1957-01-09 | 1965-09-02 | Bertin & Cie | Ausstroemduese |
US2901910A (en) * | 1957-04-22 | 1959-09-01 | Westinghouse Electric Corp | Actuating mechanism |
US3002341A (en) * | 1957-12-31 | 1961-10-03 | Boeing Co | Jet engine noise suppression nozzles |
DE1098294B (de) * | 1958-05-20 | 1961-01-26 | Entwicklungsbau Pirna Veb | Verfahren und Vorrichtung zur Geraeuschminderung eines Gasstrahles, insbesondere eines Abgasstrahles von Brennkraftturbinen- und Brennkraftrueckstoss-Triebwerken |
DE1148820B (de) * | 1960-10-06 | 1963-05-16 | M A N Turbomotoren G M B H | Hubtriebwerk fuer senkrecht startende und landende Flugzeuge |
US3192712A (en) * | 1962-12-31 | 1965-07-06 | Gen Electric | Load balancing arrangement for annular variable area jet exhaust nozzle |
US3425447A (en) * | 1965-12-10 | 1969-02-04 | United States Steel Corp | Gas-duct valve with flexible closure |
US3409622A (en) * | 1967-05-26 | 1968-11-05 | Gen Electric | Ball screw drive for variable area jet nozzle |
US4244294A (en) * | 1978-10-23 | 1981-01-13 | The Garrett Corporation | Stowable nozzle plug and method for air breathing missile |
US4523737A (en) * | 1983-03-21 | 1985-06-18 | Honeywell Inc. | Sleeve valve actuator means |
US6220852B1 (en) * | 1999-03-25 | 2001-04-24 | Hauck Manufacturing Company | Variable exit high velocity burner |
FR3048449B1 (fr) * | 2016-03-02 | 2018-03-02 | Safran Aircraft Engines | Dispositif de protection des canalisations de servitude d'une turbomachine |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2123528A (en) * | 1937-03-06 | 1938-07-12 | Picker X Ray Corp Waite Mfg | X-ray apparatus |
US2383385A (en) * | 1941-11-10 | 1945-08-21 | Heintze Carl Paul | Jet propulsion power plant |
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0
- BE BE637917D patent/BE637917A/xx unknown
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1947
- 1947-06-05 US US752623A patent/US2483401A/en not_active Expired - Lifetime
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1948
- 1948-05-27 GB GB14337/48A patent/GB637917A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US2483401A (en) | 1949-10-04 |
GB637917A (en) | 1950-05-31 |