GB438968A - Improvements in or relating to internally sprung wheels for aircraft - Google Patents

Improvements in or relating to internally sprung wheels for aircraft

Info

Publication number
GB438968A
GB438968A GB1625134A GB1625134A GB438968A GB 438968 A GB438968 A GB 438968A GB 1625134 A GB1625134 A GB 1625134A GB 1625134 A GB1625134 A GB 1625134A GB 438968 A GB438968 A GB 438968A
Authority
GB
United Kingdom
Prior art keywords
sleeve
axle
guide
guideway
aircraft
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
GB1625134A
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
Priority to GB1625134A priority Critical patent/GB438968A/en
Publication of GB438968A publication Critical patent/GB438968A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B64C25/62—Spring shock-absorbers; Springs

Landscapes

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

Abstract

438,968. Vehicle wheels. DOWTY, G. H., 17, Lansdown Crescent, Cheltenham. May 31, 1934, No. 16251. [Class 144 (i)] An internally-sprung wheel for aircraft is provided with inner and outer wheel bearings 14, 7 carried by separate halves of a longitudinally-divided sleeve 15 which is slidable against the action of shock-absorbing means over a cylindrical guide 17 rigid with the axle 18. Further, the axle is slidable within the encircling bearing 14 on a slotted guideway 34 arranged at the side of the bearing 14 remote from the sleeve and guide. The telescoping sleeve and guide enclose a shock-absorbing device comprising a spring 25 and dashpot 22. The sleeve guide 17 is formed as a T-head to the axle which moves in a slot in the sleeve. The slot 34 of the guideway is covered by a pair of sliding plates, the outer one 37 of which is fixed to the axle, the other 35 having sliding engagement therewith, its upward and downward movement being limited by stops 36, 38. The brake drum 31 is formed within the thickness of the wheel, the guideway 34 lying within the plane of the brake and being surrounded by the drum.
GB1625134A 1934-05-31 1934-05-31 Improvements in or relating to internally sprung wheels for aircraft Expired GB438968A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1625134A GB438968A (en) 1934-05-31 1934-05-31 Improvements in or relating to internally sprung wheels for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1625134A GB438968A (en) 1934-05-31 1934-05-31 Improvements in or relating to internally sprung wheels for aircraft

Publications (1)

Publication Number Publication Date
GB438968A true GB438968A (en) 1935-11-27

Family

ID=10073932

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1625134A Expired GB438968A (en) 1934-05-31 1934-05-31 Improvements in or relating to internally sprung wheels for aircraft

Country Status (1)

Country Link
GB (1) GB438968A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8714473B2 (en) 2003-04-07 2014-05-06 Airbus Uk Limited Landing gear
US8882043B2 (en) 2003-04-07 2014-11-11 Airbus Uk Limited Landing gear assembly

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8714473B2 (en) 2003-04-07 2014-05-06 Airbus Uk Limited Landing gear
US8746615B2 (en) 2003-04-07 2014-06-10 Airbus Operations Limited Landing gear
US8882043B2 (en) 2003-04-07 2014-11-11 Airbus Uk Limited Landing gear assembly

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