BE691769A - - Google Patents

Info

Publication number
BE691769A
BE691769A BE691769DA BE691769A BE 691769 A BE691769 A BE 691769A BE 691769D A BE691769D A BE 691769DA BE 691769 A BE691769 A BE 691769A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE691769A publication Critical patent/BE691769A/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/023Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/12Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/123Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • F02K1/383Introducing air inside the jet with retractable elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
BE691769D 1965-12-29 1966-12-27 BE691769A (US06534493-20030318-C00166.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US517297A US3391898A (en) 1965-12-29 1965-12-29 Actuating mechanism

Publications (1)

Publication Number Publication Date
BE691769A true BE691769A (US06534493-20030318-C00166.png) 1967-05-29

Family

ID=24059220

Family Applications (1)

Application Number Title Priority Date Filing Date
BE691769D BE691769A (US06534493-20030318-C00166.png) 1965-12-29 1966-12-27

Country Status (7)

Country Link
US (1) US3391898A (US06534493-20030318-C00166.png)
BE (1) BE691769A (US06534493-20030318-C00166.png)
DE (1) DE1526883B1 (US06534493-20030318-C00166.png)
FR (1) FR1506194A (US06534493-20030318-C00166.png)
GB (1) GB1167040A (US06534493-20030318-C00166.png)
NL (1) NL6618372A (US06534493-20030318-C00166.png)
SE (1) SE303103B (US06534493-20030318-C00166.png)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3614037A (en) * 1969-09-22 1971-10-19 Boeing Co Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser
GB1526224A (en) * 1975-10-28 1978-09-27 Rolls Royce Gas turbine engine cowls
US8615982B2 (en) * 2011-07-05 2013-12-31 Hamilton Sundstrand Corporation Integrated electric variable area fan nozzle thrust reversal actuation system
FR3012794B1 (fr) * 2013-11-05 2017-03-24 Aircelle Sa Liaison entre un actionneur et un inverseur de poussee d'une nacelle de turboreacteur, comportant des jeux

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US788510A (en) * 1903-04-21 1905-05-02 Crane Co Valve.
US2504006A (en) * 1947-09-05 1950-04-11 Craig L Davis Valve device
DE1193733B (de) * 1961-03-27 1965-05-26 United Aircraft Corp Ejektor-Schubduese zum Flugzeugantrieb
US3057150A (en) * 1961-03-27 1962-10-09 United Aircraft Corp Two dimensional floating blow-in-door and flap ejector

Also Published As

Publication number Publication date
FR1506194A (fr) 1967-12-15
SE303103B (US06534493-20030318-C00166.png) 1968-08-12
GB1167040A (en) 1969-10-15
NL6618372A (US06534493-20030318-C00166.png) 1967-06-30
DE1526883B1 (de) 1971-06-09
US3391898A (en) 1968-07-09

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