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
Application number
Priority date (The priority date 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 date listed.)
Publication of BE637917A publication Critical patent/BE637917A/xx

Links

Classifications

    • 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
    • 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
    • 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
    • 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)
BE637917D 1947-06-05 BE637917A (pm)

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 (pm)

Family

ID=25027087

Family Applications (1)

Application Number Title Priority Date Filing Date
BE637917D BE637917A (pm) 1947-06-05

Country Status (3)

Country Link
US (1) US2483401A (pm)
BE (1) BE637917A (pm)
GB (1) GB637917A (pm)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
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 (pm) * 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
CN114991990A (zh) * 2022-05-25 2022-09-02 中国航发沈阳发动机研究所 一种核心机排气喉道面积调节装置

Family Cites Families (2)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
US2483401A (en) 1949-10-04
GB637917A (en) 1950-05-31

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