BE530004A - - Google Patents

Info

Publication number
BE530004A
BE530004A BE530004DA BE530004A BE 530004 A BE530004 A BE 530004A BE 530004D A BE530004D A BE 530004DA BE 530004 A BE530004 A BE 530004A
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 BE530004A publication Critical patent/BE530004A/xx

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
    • F02K1/78—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; Infra-red radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)
BE530004D 1953-06-30 BE530004A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US365005A US2811827A (en) 1953-06-30 1953-06-30 Balanced jet nozzle and cooling means therefor

Publications (1)

Publication Number Publication Date
BE530004A true BE530004A (en)

Family

ID=23437091

Family Applications (1)

Application Number Title Priority Date Filing Date
BE530004D BE530004A (en) 1953-06-30

Country Status (4)

Country Link
US (1) US2811827A (en)
BE (1) BE530004A (en)
FR (1) FR1104307A (en)
GB (1) GB756783A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE977738C (en) * 1957-12-11 1969-03-27 Josef Schaberger & Co G M B H Method for operating a jet engine, in particular for rockets

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2952124A (en) * 1957-07-29 1960-09-13 Boeing Co Plug type noise suppressor and thrust reverser
US3094072A (en) * 1957-12-09 1963-06-18 Arthur R Parilla Aircraft, missiles, missile weapons systems, and space ships
US4044555A (en) * 1958-09-30 1977-08-30 Hayes International Corporation Rear section of jet power plant installations
US3237864A (en) * 1962-12-03 1966-03-01 Gen Electric Low drag variable plug jet exhaust nozzle
US3192712A (en) * 1962-12-31 1965-07-06 Gen Electric Load balancing arrangement for annular variable area jet exhaust nozzle
US3504860A (en) * 1964-07-07 1970-04-07 Us Navy Adjustable spike nozzle for thrust motors
GB1026068A (en) * 1964-11-09 1966-04-14 Rolls Royce Jet nozzle
US3210934A (en) * 1964-11-30 1965-10-12 Gen Motors Corp Jet engine exhaust
GB1035015A (en) * 1965-05-11 1966-07-06 Rolls Royce Improvements in or relating to jet propulsion power plant
DE4225603C1 (en) * 1992-08-03 1993-11-25 Deutsche Aerospace Thruster for a hypersonic combination engine with a cooled central body
US6584766B1 (en) * 2000-03-24 2003-07-01 General Electric Co. Methods and apparatus for minimizing thermal stresses in a centerbody
FR2920194B1 (en) * 2007-08-23 2014-02-21 Airbus France GAS EJECTION CONE FOR AIRCRAFT TURBOJET ENGINE EQUIPPED WITH A DEVICE FOR GENERATING PRIMARY FLOW TURBULENCIES LIMITING JET NOISE
CN110657044B (en) * 2019-08-30 2020-09-25 中国科学院工程热物理研究所 Integrated structure of electric-driven afterburner and area-adjustable tail nozzle
CN113266425B (en) * 2021-05-31 2022-11-01 张龙 Closed fixed annular turbojet steam wheel

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2510506A (en) * 1944-07-15 1950-06-06 Jarvis C Marble Turbojet power plant with controllable primary and secondary outlets
NL70849C (en) * 1945-05-14
US2570629A (en) * 1945-10-05 1951-10-09 Anxionnaz Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles
US2540594A (en) * 1946-08-23 1951-02-06 Lockheed Aircraft Corp Ram jet engine having variable area inlets
US2573982A (en) * 1946-12-14 1951-11-06 Homestead Valve Mfg Co Nozzle
BE637917A (en) * 1947-06-05
US2641104A (en) * 1950-04-18 1953-06-09 United Aircraft Corp Tail cone having radially adjustable wall
US2630673A (en) * 1950-09-27 1953-03-10 Gen Electric Cooling means for variable area nozzles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE977738C (en) * 1957-12-11 1969-03-27 Josef Schaberger & Co G M B H Method for operating a jet engine, in particular for rockets

Also Published As

Publication number Publication date
GB756783A (en) 1956-09-12
US2811827A (en) 1957-11-05
FR1104307A (en) 1955-11-18

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