GB637830A - Improved nose or tail wheels of aircraft - Google Patents

Improved nose or tail wheels of aircraft

Info

Publication number
GB637830A
GB637830A GB30076/47A GB3007647A GB637830A GB 637830 A GB637830 A GB 637830A GB 30076/47 A GB30076/47 A GB 30076/47A GB 3007647 A GB3007647 A GB 3007647A GB 637830 A GB637830 A GB 637830A
Authority
GB
United Kingdom
Prior art keywords
wheel
wheels
rim
aircraft
fitted
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
GB30076/47A
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.)
Dunlop Rubber Co Ltd
Original Assignee
Dunlop Rubber Co Ltd
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 Dunlop Rubber Co Ltd filed Critical Dunlop Rubber Co Ltd
Priority to GB30076/47A priority Critical patent/GB637830A/en
Publication of GB637830A publication Critical patent/GB637830A/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 
    • B64C25/50—Steerable undercarriages; Shimmy-damping
    • B64C25/505—Shimmy damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

637,830. Aircraft landing-wheels. DUNLOP RUBBER CO., Ltd., and BUTLER, H. J. Nov. 12, 1947, No. 30076. [Class 4] [Also in Group XXXIV] Twin nose or tail landing-wheels for aircraft rotatably mounted on a fixed axle are coupled together through a shaft rigidly connected to one wheel and a disc which is fast on the shaft and frictionally associated with the other wheel. As shown in Fig. 1, the twin wheels 2, 21 are mounted, through roller bearings 3, 31 on a fixed hollow axle 1. The wheel 2 is fitted with a driving-plate 4 having a sleeve 5 splined on the coned end 6 of a hollow shaft 7 the other end of which is formed with a disc 8. The outer periphery of the latter is clamped, by rings 10, between flanges 11 projecting from the rim of the wheel 2<SP>1</SP>. Friction elements are fitted between the parts 8, 11, 10. In the modification shown in Fig. 3, the friction elements are fitted in a recess 18 bounded by a flange projecting from the rim-part 16 and a backing-plate 19. Axial thrust on the latter is provided by a ring 20 and a sealing-ring 21 housed in an annular recess in the wheel-disc carrying the other rim-part 15, a conduit 22 connecting the recess with the air-chamber of the tyre. Specification 560,795, [Group XXXIV], is referred to.
GB30076/47A 1947-11-12 1947-11-12 Improved nose or tail wheels of aircraft Expired GB637830A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB30076/47A GB637830A (en) 1947-11-12 1947-11-12 Improved nose or tail wheels of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB30076/47A GB637830A (en) 1947-11-12 1947-11-12 Improved nose or tail wheels of aircraft

Publications (1)

Publication Number Publication Date
GB637830A true GB637830A (en) 1950-05-24

Family

ID=10301884

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30076/47A Expired GB637830A (en) 1947-11-12 1947-11-12 Improved nose or tail wheels of aircraft

Country Status (1)

Country Link
GB (1) GB637830A (en)

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