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GB1032274A - Mounting of ducted fan turbine engines in the tail of an aircraft - Google Patents

Mounting of ducted fan turbine engines in the tail of an aircraft

Info

Publication number
GB1032274A
GB1032274A GB6136/63A GB613663A GB1032274A GB 1032274 A GB1032274 A GB 1032274A GB 6136/63 A GB6136/63 A GB 6136/63A GB 613663 A GB613663 A GB 613663A GB 1032274 A GB1032274 A GB 1032274A
Authority
GB
United Kingdom
Prior art keywords
fan
tail
boundary layer
aircraft
turbine engines
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
GB6136/63A
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.)
Messerschmitt AG
Original Assignee
Messerschmitt AG
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 Messerschmitt AG filed Critical Messerschmitt AG
Publication of GB1032274A publication Critical patent/GB1032274A/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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

1,032,274. Boundary layer control. MESSERSCHMITT A.G. Feb. 15, 1963 [March 3, 1962], No. 6136/63. Heading F2R. [Also in Division B7] An aircraft has two tail mounted ducted fan gas turbine engines arranged so that the fan draws air from the fuselage boundary layer and the compressor draws air from outside the boundary layer 3. The fan blades 6 are mounted on a ring surrounding the compressor blades and a wiring chamber 4 with guide vanes 5 is provided in the tail, connecting the two fan intakes, so that the boundary layer air is mixed with other air passing to the fan intake. Afterburners may be fitted in the fan exhaust, the turbine exhaust, or both.
GB6136/63A 1962-03-03 1963-02-15 Mounting of ducted fan turbine engines in the tail of an aircraft Expired GB1032274A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEM52006A DE1256079B (en) 1962-03-03 1962-03-03 Arrangement of dual-circuit engines at the rear of aircraft

Publications (1)

Publication Number Publication Date
GB1032274A true GB1032274A (en) 1966-06-08

Family

ID=7307327

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6136/63A Expired GB1032274A (en) 1962-03-03 1963-02-15 Mounting of ducted fan turbine engines in the tail of an aircraft

Country Status (2)

Country Link
DE (1) DE1256079B (en)
GB (1) GB1032274A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3635308A (en) * 1969-07-03 1972-01-18 Rohr Corp Sound suppression system
US10364021B2 (en) 2016-09-26 2019-07-30 General Electric Company Aircraft having an aft engine and stabilizer root fillet
US10370110B2 (en) 2016-09-21 2019-08-06 General Electric Company Aircraft having an aft engine
US10399670B2 (en) 2016-09-26 2019-09-03 General Electric Company Aircraft having an aft engine and internal flow passages
US10486796B2 (en) 2016-09-26 2019-11-26 General Electric Company Aircraft having an AFT engine and stabilizer with a varying line of maximum thickness

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2755040A (en) * 1951-10-10 1956-07-17 Glenn L Martin Co Air intake system for an aircraft
DE1129833B (en) * 1959-11-24 1962-05-17 Messerschmitt Ag Airplane with an air-breathing jet engine in the fuselage tail

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3635308A (en) * 1969-07-03 1972-01-18 Rohr Corp Sound suppression system
US10370110B2 (en) 2016-09-21 2019-08-06 General Electric Company Aircraft having an aft engine
US11299283B2 (en) 2016-09-21 2022-04-12 General Electric Company Aircraft having an aft engine
US10364021B2 (en) 2016-09-26 2019-07-30 General Electric Company Aircraft having an aft engine and stabilizer root fillet
US10399670B2 (en) 2016-09-26 2019-09-03 General Electric Company Aircraft having an aft engine and internal flow passages
US10486796B2 (en) 2016-09-26 2019-11-26 General Electric Company Aircraft having an AFT engine and stabilizer with a varying line of maximum thickness

Also Published As

Publication number Publication date
DE1256079B (en) 1967-12-07

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