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BE469592A - - Google Patents

Info

Publication number
BE469592A
BE469592A BE469592DA BE469592A BE 469592 A BE469592 A BE 469592A BE 469592D A BE469592D A BE 469592DA BE 469592 A BE469592 A BE 469592A
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 BE469592A publication Critical patent/BE469592A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0253—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
    • B64D2033/026—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
BE469592D 1945-12-05 BE469592A (tr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3296445A GB614548A (en) 1945-12-05 1945-12-05 Improvements in or relating to air intakes for high speed flight

Publications (1)

Publication Number Publication Date
BE469592A true BE469592A (tr)

Family

ID=10346625

Family Applications (1)

Application Number Title Priority Date Filing Date
BE469592D BE469592A (tr) 1945-12-05

Country Status (2)

Country Link
BE (1) BE469592A (tr)
GB (1) GB614548A (tr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2704645A (en) * 1955-03-22 colvin
US2631425A (en) * 1948-09-11 1953-03-17 Bofors Ab Compression nozzle for ram-jet engines
US2648192A (en) * 1949-09-27 1953-08-11 United Aircraft Corp Variable capacity jet exhaust augmenter
US2975587A (en) * 1949-11-16 1961-03-21 Randolph S Rae Streamlined rings for assuring isentropic compression of supersionic stream through a conventional missile diffuser
US2811828A (en) * 1950-12-02 1957-11-05 United Aircraft Corp Bleed means for confined supersonic flow
US2971724A (en) * 1952-02-19 1961-02-14 Helmut Ph G A R Von Zborowski Annular wing flying machines
US3027712A (en) * 1952-07-16 1962-04-03 Randolph S Rae Means for varying the thrust of a ram-jet
US3005309A (en) * 1952-11-17 1961-10-24 Randolph S Rae Streamlined ring for assuring optimum compression in a ramjet
US2788183A (en) * 1953-02-04 1957-04-09 Curtiss Wright Corp Multi-scoop supersonic inlet
US2861419A (en) * 1953-02-13 1958-11-25 United Aircraft Corp Variable bleed diffuser
US3011307A (en) * 1955-12-15 1961-12-05 Gen Electric Variable throat supersonic diffuser
US3029600A (en) * 1956-07-02 1962-04-17 North American Aviation Inc Variable supersonic inlet and by-pass system
US2969939A (en) * 1956-07-30 1961-01-31 North American Aviation Inc Asymmetrically variable supersonic inlet system
US3080707A (en) * 1956-11-13 1963-03-12 Boeing Co Supersonic air diffuser
US2995892A (en) * 1957-02-27 1961-08-15 Curtiss Wright Corp Supersonic variable inlet
US2971328A (en) * 1958-07-22 1961-02-14 United Aircraft Corp Control system for air inlet bypass
US3208383A (en) * 1963-07-18 1965-09-28 Roland W Larson Ramjet vent
WO1982000048A1 (en) * 1980-06-23 1982-01-07 Co Boeing Supersonic airplane engine configuration
US4477039A (en) * 1982-06-30 1984-10-16 Mcdonnell Douglas Corporation Vented cowl variable geometry inlet for aircraft
GB9025023D0 (en) * 1990-11-16 1991-01-02 Rolls Royce Plc Engine nacelle

Also Published As

Publication number Publication date
GB614548A (en) 1948-12-17

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