DE2209748A1 - Umlenkvorrichtung fur die austretenden Gase von Gasturbinentriebwerken - Google Patents

Umlenkvorrichtung fur die austretenden Gase von Gasturbinentriebwerken

Info

Publication number
DE2209748A1
DE2209748A1 DE19722209748 DE2209748A DE2209748A1 DE 2209748 A1 DE2209748 A1 DE 2209748A1 DE 19722209748 DE19722209748 DE 19722209748 DE 2209748 A DE2209748 A DE 2209748A DE 2209748 A1 DE2209748 A1 DE 2209748A1
Authority
DE
Germany
Prior art keywords
doors
deflection
deflection device
openings
air
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.)
Pending
Application number
DE19722209748
Other languages
German (de)
English (en)
Inventor
Alan Avery St Albans Grace Michael Edward Hatfield Hertfordshire Blythe (Großbritannien)
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.)
Hawker Siddeley Aviation Ltd
Original Assignee
Hawker Siddeley Aviation Ltd
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 Hawker Siddeley Aviation Ltd filed Critical Hawker Siddeley Aviation Ltd
Publication of DE2209748A1 publication Critical patent/DE2209748A1/de
Pending 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Air-Flow Control Members (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
DE19722209748 1971-03-01 1972-02-26 Umlenkvorrichtung fur die austretenden Gase von Gasturbinentriebwerken Pending DE2209748A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB569271A GB1388852A (en) 1971-03-01 1971-03-01 Nozzle structure for jet propulsion engines

Publications (1)

Publication Number Publication Date
DE2209748A1 true DE2209748A1 (de) 1972-09-07

Family

ID=9800855

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19722209748 Pending DE2209748A1 (de) 1971-03-01 1972-02-26 Umlenkvorrichtung fur die austretenden Gase von Gasturbinentriebwerken

Country Status (4)

Country Link
US (1) US3806068A (enExample)
DE (1) DE2209748A1 (enExample)
FR (1) FR2128375B1 (enExample)
GB (1) GB1388852A (enExample)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3863867A (en) * 1973-12-26 1975-02-04 Boeing Co Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor
US4358074A (en) * 1979-05-24 1982-11-09 The Boeing Company Propulsion system for V/STOL aircraft
FR2507558B1 (fr) * 1981-06-11 1985-11-15 Do G P Groupe moteur de sustentation et de propulsion d'un vehicule de transport a coussin d'air
US4648571A (en) * 1984-07-19 1987-03-10 Northrop Corporation Transverse thrust lift augmentation system
US5150862A (en) * 1991-01-11 1992-09-29 United Technologies Corporation In-flight reverser
US5161752A (en) * 1991-01-11 1992-11-10 United Technologies Corporation In-flight reverser
GB2346593B (en) * 1999-02-09 2003-01-08 Airship Tech Serv Ltd Airship bow thruster apparatus
US20070221783A1 (en) * 2004-09-17 2007-09-27 Robert Parks Adaptive landing gear
WO2007001373A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences Inbound transition control for a trail-sitting vertical take off and landing aircraft
US7364115B2 (en) * 2004-09-17 2008-04-29 Aurora Flight Sciences Corporation System and method for controlling engine RPM of a ducted fan aircraft
WO2007001372A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences Ducted spinner for engine cooling
WO2007001371A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences Vibration isolation engine mount system and method for ducted fan aircraft
US7441724B2 (en) * 2004-09-17 2008-10-28 Aurora Flight Sciences Corporation System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft
WO2008045082A1 (en) * 2006-10-12 2008-04-17 United Technologies Corporation Reduced take-off field length using variable nozzle
US7883051B2 (en) * 2008-03-27 2011-02-08 Johann Q. Sammy Ducted propulsion vector system
US9394852B2 (en) * 2012-01-31 2016-07-19 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
US8375699B1 (en) 2012-01-31 2013-02-19 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
EP3660279A1 (en) * 2013-03-15 2020-06-03 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
US20170058828A1 (en) * 2015-08-26 2017-03-02 Rohr, Inc. Cascade with varying vane trailing edge thickness

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3068646A (en) * 1959-01-28 1962-12-18 Rolls Royce Improvements in by-pass type gas turbine engines
US3248878A (en) * 1963-09-18 1966-05-03 Gen Electric Thrust deflector and reverser
GB1247691A (en) * 1968-08-08 1971-09-29 Rolls Royce Improvements in or relating to fan ducts for gas turbine ducted fan engines
GB1246136A (en) * 1968-09-14 1971-09-15 Rolls Royce Jet propulsion nozzle
DE1927280A1 (de) * 1969-05-29 1970-12-03 Motoren Turbinen Union Flugzeug,mit einem oder mehreren im Rumpfheck oder in Gondeln angeordneten,mit Schubumkehreinrichtungen ausgeruesteten Turbinenstrahltriebwerken

Also Published As

Publication number Publication date
US3806068A (en) 1974-04-23
FR2128375A1 (enExample) 1972-10-20
GB1388852A (en) 1975-03-26
FR2128375B1 (enExample) 1976-06-11

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Legal Events

Date Code Title Description
OHA Expiration of time for request for examination