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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0253—Arrangements 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—Arrangements 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
BE469592D 1945-12-05 BE469592A (xx)

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 (xx)

Family

ID=10346625

Family Applications (1)

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

Country Status (2)

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

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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