GB883373A - Improvements relating to turbo-jet propulsion units in aircraft - Google Patents

Improvements relating to turbo-jet propulsion units in aircraft

Info

Publication number
GB883373A
GB883373A GB1284/60A GB128460A GB883373A GB 883373 A GB883373 A GB 883373A GB 1284/60 A GB1284/60 A GB 1284/60A GB 128460 A GB128460 A GB 128460A GB 883373 A GB883373 A GB 883373A
Authority
GB
United Kingdom
Prior art keywords
afterburner
nozzle
axis
aircraft
discharges
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
GB1284/60A
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.)
Daimler Benz AG
Original Assignee
Daimler Benz 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 Daimler Benz AG filed Critical Daimler Benz AG
Publication of GB883373A publication Critical patent/GB883373A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

883,373. Direct lift jet propelled aircraft. DAIMLER-BENZ A. G. Jan. 13, 1960 [Jan. 17, 1959], No. 1284/60. Class 4. [Also in. Group XXVI]. An afterburner 12 is pivotable about an axis 24 on a gas turbine unit 11, between a position 12 (shown in full lines) in which it discharges into a supersonic horizontal propulsion nozzle 13, and a position 12<SP>1</SP> (shown in broken lines) in which it discharges in to a subsonic nozzle 14, to provide direct lift for the aircraft in which it is installed. The axis 18 of nozzle 13 is inclined at an angle a to the axis 19 of the afterburner in one extreme position, and the axis 20 of nozzle 14 is inclined at a greater angle b to the axis 19<SP>1</SP> of the afterburner in the other extreme position. In intermediate positions, the afterburner discharges partly into each nozzle, nozzle 14 being divided by deflecting plates 17. Pivot 26 is hollow, and provides a fuel lead for the afterburner fuel injector 22. The afterburner pivots within a fixed casing 21 through which cooling air may flow. Specification 857,899 is referred to.
GB1284/60A 1960-01-06 1960-01-13 Improvements relating to turbo-jet propulsion units in aircraft Expired GB883373A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR814917A FR76840E (en) 1960-01-06 1960-01-06 Gas turbine reactor with downstream burner and thrust nozzle, especially for vertical takeoff and fast takeoff airplanes

Publications (1)

Publication Number Publication Date
GB883373A true GB883373A (en) 1961-11-29

Family

ID=6832004

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1284/60A Expired GB883373A (en) 1960-01-06 1960-01-13 Improvements relating to turbo-jet propulsion units in aircraft

Country Status (2)

Country Link
FR (1) FR76840E (en)
GB (1) GB883373A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2501786A1 (en) * 1981-03-13 1982-09-17 Snecma DEVICE FOR BEARING AND GUIDING AN ORIENTABLE NOZZLE OF A REACTION PROPELLER

Also Published As

Publication number Publication date
FR76840E (en) 1961-12-08

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