GB581333A - Apparatus for damping swivelling oscillations in caster wheels - Google Patents

Apparatus for damping swivelling oscillations in caster wheels

Info

Publication number
GB581333A
GB581333A GB13336/43A GB1333643A GB581333A GB 581333 A GB581333 A GB 581333A GB 13336/43 A GB13336/43 A GB 13336/43A GB 1333643 A GB1333643 A GB 1333643A GB 581333 A GB581333 A GB 581333A
Authority
GB
United Kingdom
Prior art keywords
wheel
dashpot
pin
collar
arm
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
GB13336/43A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB581333A publication Critical patent/GB581333A/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 
    • B64C25/50Steerable undercarriages; Shimmy-damping
    • B64C25/505Shimmy damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

581,333. Vehicle castor wheels; dashpots. BISHOP, A. E. J. Aug. 17, 1943, No. 13336. Convention date, July 29, 1942. [Classes 108 (ii) and 108 (iii)] Also in Group XXXIII] Swivelling oscillations of a castor wheel, such as a landing wheel of an aircraft undercarriage, are damped by a rotary dashpot on one of the relatively movable elements and comprising a radial arm with an open-ended slot which is engageable by a pin on the other element. The invention is shown as applied to an aircraft landing wheel 12 carried by a telescopic shock absorber leg 14, 15, the movable members being provided with collars 23, 18, connected by pivotal links 22, 20, the collar 18 being integral with the recoil cylinder 15. A bracket 16 on the fork 13 of the wheel stock 14 carries the rotary dashpot 17, of which the open-ended slot 35 in the radial arm 34 is engageable by a downwardly projecting pin 25 carried by the collar 23. The dashpot comprises a rotor 29 with diametral vanes 28, and with upper and lower ports 32, 32a, respectively, the ports being connected by a vertical axial duct 32b fitted with an adjustable control valve. The dashpot is effective only during the period in which the pin 25 is in contact with the arm 34, i.e., for a wheel movement of approximately 30 degrees on either side of the in-line position. Movement of the wheel is limited to 180 degrees in either direction by one of a pair of stops 38 on the dashpot cylinder cover and a stop 42 on the collar 23, which engage recesses 37 in the sides of the arm 34. Modifications are described in which the dashpot is carried by the bearing and the pin by the wheel stock.
GB13336/43A 1942-07-29 1943-08-17 Apparatus for damping swivelling oscillations in caster wheels Expired GB581333A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AU581333X 1942-07-29

Publications (1)

Publication Number Publication Date
GB581333A true GB581333A (en) 1946-10-09

Family

ID=3743475

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13336/43A Expired GB581333A (en) 1942-07-29 1943-08-17 Apparatus for damping swivelling oscillations in caster wheels

Country Status (1)

Country Link
GB (1) GB581333A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2482154A (en) * 2010-07-21 2012-01-25 Ge Aviat Systems Ltd Compact shimmy damper for aircraft landing gear

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2482154A (en) * 2010-07-21 2012-01-25 Ge Aviat Systems Ltd Compact shimmy damper for aircraft landing gear

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