GB1167040A - Improvements relating to Door Mechanisms for the Exhaust Nozzles of Jet Propulsion Engines. - Google Patents

Improvements relating to Door Mechanisms for the Exhaust Nozzles of Jet Propulsion Engines.

Info

Publication number
GB1167040A
GB1167040A GB56517/66A GB5651766A GB1167040A GB 1167040 A GB1167040 A GB 1167040A GB 56517/66 A GB56517/66 A GB 56517/66A GB 5651766 A GB5651766 A GB 5651766A GB 1167040 A GB1167040 A GB 1167040A
Authority
GB
United Kingdom
Prior art keywords
door
actuator
cam
locked
jet
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
GB56517/66A
Other languages
English (en)
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.)
RTX Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1167040A publication Critical patent/GB1167040A/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
    • B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/123—Varying 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
    • 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
    • F02K1/38—Introducing air inside the jet
    • F02K1/383—Introducing 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)
GB56517/66A 1965-12-29 1966-12-16 Improvements relating to Door Mechanisms for the Exhaust Nozzles of Jet Propulsion Engines. Expired GB1167040A (en)

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
GB1167040A true GB1167040A (en) 1969-10-15

Family

ID=24059220

Family Applications (1)

Application Number Title Priority Date Filing Date
GB56517/66A Expired GB1167040A (en) 1965-12-29 1966-12-16 Improvements relating to Door Mechanisms for the Exhaust Nozzles of Jet Propulsion Engines.

Country Status (7)

Country Link
US (1) US3391898A (enExample)
BE (1) BE691769A (enExample)
DE (1) DE1526883B1 (enExample)
FR (1) FR1506194A (enExample)
GB (1) GB1167040A (enExample)
NL (1) NL6618372A (enExample)
SE (1) SE303103B (enExample)

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
NL6618372A (enExample) 1967-06-30
US3391898A (en) 1968-07-09
SE303103B (enExample) 1968-08-12
DE1526883B1 (de) 1971-06-09
BE691769A (enExample) 1967-05-29

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees