GB1093914A - Aircraft jet propulsion engine having an after burner with mechanically controlled jet deflection - Google Patents

Aircraft jet propulsion engine having an after burner with mechanically controlled jet deflection

Info

Publication number
GB1093914A
GB1093914A GB32928/65A GB3292865A GB1093914A GB 1093914 A GB1093914 A GB 1093914A GB 32928/65 A GB32928/65 A GB 32928/65A GB 3292865 A GB3292865 A GB 3292865A GB 1093914 A GB1093914 A GB 1093914A
Authority
GB
United Kingdom
Prior art keywords
burner
deflecting
engine
jet
aircraft
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
GB32928/65A
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.)
HEINKEL AG ERNST
Ernst Heinkel AG
Original Assignee
HEINKEL AG ERNST
Ernst Heinkel 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 HEINKEL AG ERNST, Ernst Heinkel AG filed Critical HEINKEL AG ERNST
Publication of GB1093914A publication Critical patent/GB1093914A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K1/004—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 by using one or more swivable nozzles rotating about their own axis
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Combustion Of Fluid Fuel (AREA)

Abstract

1,093,914. Deflecting propulsive jets. ERNST HEINKEL A.G. Aug. 2, 1965 [Aug. 8, 1964], No. 32928/65. Heading B7G. [Also in Division F1] An aircraft jet propulsion engine having an after-burner with mechanically controlled jet deflecting apparatus has the deflecting surface cooled, when in the deflecting position, by water injected into the after-burner chamber. The engine 1 has a rigidly attached after-burner 2 with a bevelled end wall 3 which co-operates with a cowl member 5 mounted on a fixed pivot 4 and formed with a propulsion nozzle 14. The cowl may be swung forwardly about pivot 4 to partially enclose after-burner 2 whereby nozzle 14 is aligned with engine 1 for forward propulsion of the aircraft in which the engine is installed. When in the deflected position shown the hot gases impinge on surface 8 and deposit an amount of unburnt fuel. To cool the deflecting member and also to cause burning of the unburnt fuel, water is discharged into the after-burner and the deflecting member through fixed nozzles 7. Another arrangement is described in which the deflecting member comprises a plurality of pivoted sections. There is a prior art reference to injection of cooling air into the jet deflecting apparatus.
GB32928/65A 1964-08-08 1965-08-02 Aircraft jet propulsion engine having an after burner with mechanically controlled jet deflection Expired GB1093914A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEH53484A DE1240746B (en) 1964-08-08 1964-08-08 Jet nozzle, especially for the afterburner of an aircraft engine, with mechanically controlled jet deflection

Publications (1)

Publication Number Publication Date
GB1093914A true GB1093914A (en) 1967-12-06

Family

ID=7158359

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32928/65A Expired GB1093914A (en) 1964-08-08 1965-08-02 Aircraft jet propulsion engine having an after burner with mechanically controlled jet deflection

Country Status (3)

Country Link
US (1) US3327480A (en)
DE (1) DE1240746B (en)
GB (1) GB1093914A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4007875A1 (en) 1989-03-14 2010-06-02 British Aerospace Public Ltd. Co. Schubstrahlauslaß

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1260318B (en) * 1965-10-29 1968-02-01 Entwicklungsring Sued G M B H Jet pipe with several pipe sections arranged one behind the other and rotatable against each other
DE1277639B (en) * 1966-01-28 1968-09-12 M A N Turbo G M B H Additional combustion device for heating the gases of a turbine jet engine
US3428257A (en) * 1966-06-03 1969-02-18 Curtiss Wright Corp Thrust vectoring exhaust nozzle with flow guide for minimizing separation of the jet stream
DE1277026B (en) * 1966-07-15 1968-09-05 Entwicklungsring Sued G M B H Aircraft with a jet nozzle
GB1103643A (en) * 1966-07-22 1968-02-21 Rolls Royce Gas turbine engine
US3396538A (en) * 1966-10-03 1968-08-13 United Aircraft Corp Water injection for thrust augmentation
US3393516A (en) * 1966-12-05 1968-07-23 United Aircraft Corp Curved exhaust deflector
US3455266A (en) * 1968-02-23 1969-07-15 Gen Electric Air film drag reduction with viscoelastic additives
GB1381397A (en) * 1971-02-26 1975-01-22 Mtu Muenchen Gmbh Jet pipe arrangement for a jet-propulsion engine
US3899923A (en) * 1971-05-13 1975-08-19 Teller Environmental Systems Test process and apparatus for treatment of jet engine exhaust
US3835643A (en) * 1972-11-21 1974-09-17 Mc Donnell Douglas Corp Nested toroid nozzle apparatus
JPS587519B2 (en) * 1973-04-24 1983-02-10 富士重工業株式会社 I can't wait to see what I can do.
JPS59177762U (en) * 1983-05-14 1984-11-28 鈴木　覚 Turbojet engine afterburner device
US20050138932A1 (en) * 2003-10-22 2005-06-30 Perricone Nicholas V. Aircraft protection method and system
FR2873168B1 (en) * 2004-07-16 2008-10-31 Snecma Moteurs Sa TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER
RU2651947C2 (en) * 2016-05-04 2018-04-24 Борис Никифорович Сушенцев Jet aircraft with shortened or vertical take-off and landing (options)
RU2641393C1 (en) * 2016-06-06 2018-01-17 Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А. Чаплыгина" Vertical take-off and landing aircraft (vtol)
RU2708120C1 (en) * 2019-04-18 2019-12-04 Борис Никифорович Сушенцев Aircraft with short or vertical take-off and landing
US11691726B2 (en) * 2019-06-19 2023-07-04 Darius Sharifzadeh Vertical take-off and landing aircraft

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1070448B (en) *
US2544422A (en) * 1948-05-15 1951-03-06 Daniel And Florence Guggenheim Cooling means for a combustion chamber and nozzle in which solid fuel is burned
US2866313A (en) * 1950-04-14 1958-12-30 Power Jets Res & Dev Ltd Means for cooling turbine-blades by liquid jets
GB723310A (en) * 1951-01-11 1955-02-09 Sydney Albert Powell Improvements in and relating to jet propulsion units
US2702452A (en) * 1951-09-25 1955-02-22 United Aircraft Corp Flameholder construction
US3084508A (en) * 1959-01-17 1963-04-09 Daimler Benz Ag Gas turbine propulsion power plant construction
DE1066428B (en) * 1959-01-17
DE1119126B (en) * 1960-03-18 1961-12-07 Bmw Triebwerkbau Ges M B H Jet engine with a jet deflector

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4007875A1 (en) 1989-03-14 2010-06-02 British Aerospace Public Ltd. Co. Schubstrahlauslaß
US7980508B1 (en) 1989-03-14 2011-07-19 Bae Systems Plc Jet propulsion efflux outlets

Also Published As

Publication number Publication date
DE1240746B (en) 1967-05-18
US3327480A (en) 1967-06-27

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