GB1105044A - Improvements in aircraft undercarriages - Google Patents

Improvements in aircraft undercarriages

Info

Publication number
GB1105044A
GB1105044A GB6147/66A GB614766A GB1105044A GB 1105044 A GB1105044 A GB 1105044A GB 6147/66 A GB6147/66 A GB 6147/66A GB 614766 A GB614766 A GB 614766A GB 1105044 A GB1105044 A GB 1105044A
Authority
GB
United Kingdom
Prior art keywords
skid
quadrilateral
feb
aircraft undercarriages
undercarriages
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
GB6147/66A
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.)
RECH ETUDES PROD
Recherches Etudes Production REP SARL
Original Assignee
RECH ETUDES PROD
Recherches Etudes Production REP SARL
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 RECH ETUDES PROD, Recherches Etudes Production REP SARL filed Critical RECH ETUDES PROD
Publication of GB1105044A publication Critical patent/GB1105044A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/52Skis or runners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50Steerable undercarriages; Shimmy-damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)
  • Automatic Assembly (AREA)

Abstract

1,105,044. Aircraft undercarriages. RECHERCHES ETUDES PRODUCTION R.E.P. 11 Feb., 1966 [11 Feb., 1965], No. 6147/66. Heading B7G. A skid-type tail undercarriage has a skid 1 forming part of a quadrilateral 2, 4, 13, 10 which also includes a retraction jack 5, the quadrilateral being connected to a shock absorber 14. A spring box 6 in compression causes the rear edge of the skid to engage the ground first on landing.
GB6147/66A 1965-02-11 1966-02-11 Improvements in aircraft undercarriages Expired GB1105044A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR5173A FR1450451A (en) 1965-02-11 1965-02-11 Tail landing gear, retractable, skid

Publications (1)

Publication Number Publication Date
GB1105044A true GB1105044A (en) 1968-03-06

Family

ID=8570701

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6147/66A Expired GB1105044A (en) 1965-02-11 1966-02-11 Improvements in aircraft undercarriages

Country Status (2)

Country Link
FR (1) FR1450451A (en)
GB (1) GB1105044A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997010145A1 (en) * 1995-09-14 1997-03-20 Sikorsky Aircraft Corporation Energy absorbing landing gear/tail skid including means for indicating the magnitude of impact loads
CN1083785C (en) * 1995-09-14 2002-05-01 西科尔斯基飞机公司 Energy absorbing landing gear/tail skid including means for indicating the magnitude of impact loads
CN106477027A (en) * 2015-08-24 2017-03-08 波音公司 Three position aircraft tailskid mechanisms and actuating method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997010145A1 (en) * 1995-09-14 1997-03-20 Sikorsky Aircraft Corporation Energy absorbing landing gear/tail skid including means for indicating the magnitude of impact loads
US5927646A (en) * 1995-09-14 1999-07-27 Sikorsky Aircraft Corporation Energy absorbing landing gear/tail skid including means for indicating the magnitude of impact loads
CN1083785C (en) * 1995-09-14 2002-05-01 西科尔斯基飞机公司 Energy absorbing landing gear/tail skid including means for indicating the magnitude of impact loads
CN106477027A (en) * 2015-08-24 2017-03-08 波音公司 Three position aircraft tailskid mechanisms and actuating method

Also Published As

Publication number Publication date
FR1450451A (en) 1966-06-24

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