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GB1473089A - - Google Patents

Info

Publication number
GB1473089A
GB1473089A GB3290773A GB3290773A GB1473089A GB 1473089 A GB1473089 A GB 1473089A GB 3290773 A GB3290773 A GB 3290773A GB 3290773 A GB3290773 A GB 3290773A GB 1473089 A GB1473089 A GB 1473089A
Authority
GB
United Kingdom
Prior art keywords
platform
arm
aircraft
launching
damper
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
GB3290773A
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
Priority to GB3290773A priority Critical patent/GB1473089A/en
Publication of GB1473089A publication Critical patent/GB1473089A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
    • B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Bridges Or Land Bridges (AREA)

Abstract

1473089 Aircraft launching apparatus DEFENCE SECRETARY OF STATE FOR 13 Aug 1974 [10 July 1973] 32907/73 Heading B7G An apparatus for launching aircraft comprises a launching platform 1 pivotally attached to a support arm 4 rotatable in a vertical plane, a linkage 10, 14 to control the inclination of the platform during rotation of the arm, and a jack 7 to rotate the arm and accelerate the platform in a substantially circular arc. An inflated bolster 20 is provided to retard the arm 4, the sudden retardation causing a nosewheel towing link 3 to automatically release the aircraft. A damper 16 is provided to damp rebound motion of the arm. The platform inclinationcontrolling linkage may take the form of a damper (23), Fig. 4 (not shown), acting between the arm 4 and the rear of the platform 1. In an alternative embodiment (not shown), the platform is omitted and the apparatus is directly attached to strong points on the aircraft.
GB3290773A 1974-08-13 1974-08-13 Expired GB1473089A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3290773A GB1473089A (en) 1974-08-13 1974-08-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3290773A GB1473089A (en) 1974-08-13 1974-08-13

Publications (1)

Publication Number Publication Date
GB1473089A true GB1473089A (en) 1977-05-11

Family

ID=10345793

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3290773A Expired GB1473089A (en) 1974-08-13 1974-08-13

Country Status (1)

Country Link
GB (1) GB1473089A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3221140A1 (en) * 1981-06-04 1983-01-13 British Aerospace Public Ltd. Co., London METHOD AND SYSTEM FOR COLLECTING AND / OR STARTING AN AIRCRAFT
RU2344971C1 (en) * 2007-04-05 2009-01-27 Федеральное государственное унитарное предприятие "Научно-производственное объединение им. С.А. Лавочкина" Aircraft catapult takeoff method and aircraft takeoff catapult
RU2373117C1 (en) * 2008-05-16 2009-11-20 Федеральное государственное унитарное предприятие "Научно-производственное объединение им. С.А. Лавочкина" Aircraft take-off accelerator
WO2010031241A1 (en) * 2008-09-19 2010-03-25 Hu Xuanzhe Cold-launch method and apparatus thereof
WO2010113030A3 (en) * 2009-03-31 2011-05-12 Wang Lifeng A carrier-borne aircraft takeoff/landing system and methods of using the same
CN101519124B (en) * 2009-03-31 2012-05-02 王力丰 Take-off device and take-off method for carrier-based aircraft of aircraft carrier
CN109305380A (en) * 2018-09-18 2019-02-05 哈尔滨工程大学 Disc-shaped catapult take-off with adjustment

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3221140A1 (en) * 1981-06-04 1983-01-13 British Aerospace Public Ltd. Co., London METHOD AND SYSTEM FOR COLLECTING AND / OR STARTING AN AIRCRAFT
RU2344971C1 (en) * 2007-04-05 2009-01-27 Федеральное государственное унитарное предприятие "Научно-производственное объединение им. С.А. Лавочкина" Aircraft catapult takeoff method and aircraft takeoff catapult
RU2373117C1 (en) * 2008-05-16 2009-11-20 Федеральное государственное унитарное предприятие "Научно-производственное объединение им. С.А. Лавочкина" Aircraft take-off accelerator
WO2010031241A1 (en) * 2008-09-19 2010-03-25 Hu Xuanzhe Cold-launch method and apparatus thereof
WO2010113030A3 (en) * 2009-03-31 2011-05-12 Wang Lifeng A carrier-borne aircraft takeoff/landing system and methods of using the same
CN101519124B (en) * 2009-03-31 2012-05-02 王力丰 Take-off device and take-off method for carrier-based aircraft of aircraft carrier
CN109305380A (en) * 2018-09-18 2019-02-05 哈尔滨工程大学 Disc-shaped catapult take-off with adjustment

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee