BE682198A - - Google Patents

Info

Publication number
BE682198A
BE682198A BE682198DA BE682198A BE 682198 A BE682198 A BE 682198A BE 682198D A BE682198D A BE 682198DA BE 682198 A BE682198 A BE 682198A
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.)
Filing date
Publication date
Application filed filed Critical
Publication of BE682198A publication Critical patent/BE682198A/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/001Shrouded propellers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K5/00Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
    • F02K5/02Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan the engine being of the reciprocating-piston type

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE682198D 1965-06-09 1966-06-07 BE682198A (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US462694A US3355890A (en) 1965-06-09 1965-06-09 Cruise fan powerplant

Publications (1)

Publication Number Publication Date
BE682198A true BE682198A (en:Method) 1966-11-14

Family

ID=23837430

Family Applications (1)

Application Number Title Priority Date Filing Date
BE682198D BE682198A (en:Method) 1965-06-09 1966-06-07

Country Status (2)

Country Link
US (1) US3355890A (en:Method)
BE (1) BE682198A (en:Method)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2628790A1 (fr) * 1988-03-16 1989-09-22 Snecma Propulseur combine turbofusee aerobie
DE102013213518A1 (de) 2013-07-10 2015-01-15 Rolls-Royce Deutschland Ltd & Co Kg Turbofan-Triebwerk
US10024235B2 (en) * 2014-03-03 2018-07-17 United Technologies Corporation Offset core engine architecture
US9333603B1 (en) 2015-01-28 2016-05-10 United Technologies Corporation Method of assembling gas turbine engine section
US11519289B2 (en) 2019-12-06 2022-12-06 Raytheon Technologies Corporation Systems and methods for hybrid electric turbine engines
US11073107B1 (en) * 2020-01-24 2021-07-27 Raytheon Technologies Corporation Systems and methods for hybrid electric turbine engines

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2505660A (en) * 1950-04-25 Augmentor fob jet propulsion hav
US1929778A (en) * 1930-06-30 1933-10-10 George Crompton Propulsion of aircraft
US2168726A (en) * 1936-03-04 1939-08-08 Whittle Frank Propulsion of aircraft and gas turbines
US2801789A (en) * 1954-11-30 1957-08-06 Power Jets Res & Dev Ltd Blading for gas turbine engines
US3035792A (en) * 1959-12-28 1962-05-22 Gen Electric Thrust augmenting powerplant for aircraft
US3033492A (en) * 1961-04-20 1962-05-08 Gen Electric Cruise lift-fan system
US3212731A (en) * 1963-09-09 1965-10-19 Gen Electric Fan powered aircraft

Also Published As

Publication number Publication date
US3355890A (en) 1967-12-05

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