GB954365A - Jet propulsion engine power plant installation for aircraft - Google Patents

Jet propulsion engine power plant installation for aircraft

Info

Publication number
GB954365A
GB954365A GB21887/60A GB2188760A GB954365A GB 954365 A GB954365 A GB 954365A GB 21887/60 A GB21887/60 A GB 21887/60A GB 2188760 A GB2188760 A GB 2188760A GB 954365 A GB954365 A GB 954365A
Authority
GB
United Kingdom
Prior art keywords
aircraft
power plant
engine power
jet propulsion
propulsion engine
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB21887/60A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Saab AB
Original Assignee
Svenska Aeroplan AB
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 by Svenska Aeroplan AB filed Critical Svenska Aeroplan AB
Publication of GB954365A publication Critical patent/GB954365A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage

Abstract

954,365. Boundary layer control. SVENSKA AEROPLAN A.B. June 22, 1960 [June 27, 1959], No. 21887/60. Heading F2R. [Also in Division B7] In an aircraft (see Division B7) in which the jet engines 10 are mounted on the closure 27 for the cargo space 8, a channel 28 is formed between the jet engine intake 29 and the fuselage to abstract the boundary layer along the fuselage. This passage may be omitted and the intake 39 arranged adjacent the fuselage.
GB21887/60A 1959-06-27 1960-06-22 Jet propulsion engine power plant installation for aircraft Expired GB954365A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE611559 1959-06-27

Publications (1)

Publication Number Publication Date
GB954365A true GB954365A (en) 1964-04-08

Family

ID=20267934

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21887/60A Expired GB954365A (en) 1959-06-27 1960-06-22 Jet propulsion engine power plant installation for aircraft

Country Status (1)

Country Link
GB (1) GB954365A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2703322A1 (en) * 1993-03-27 1994-10-07 Deutsche Aerospace Truncated rear transport aircraft.
JP2016505434A (en) * 2012-11-08 2016-02-25 スネクマ Aircraft propelled by turbojet engine with counter rotating fan

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2703322A1 (en) * 1993-03-27 1994-10-07 Deutsche Aerospace Truncated rear transport aircraft.
JP2016505434A (en) * 2012-11-08 2016-02-25 スネクマ Aircraft propelled by turbojet engine with counter rotating fan
US10435163B2 (en) 2012-11-08 2019-10-08 Safran Aircraft Engines Aircraft propelled by a turbojet engine with contrarotating fans

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