GB515612A - Improvements relating to shock absorber struts particularly for aircraft tail and like wheels - Google Patents

Improvements relating to shock absorber struts particularly for aircraft tail and like wheels

Info

Publication number
GB515612A
GB515612A GB3696/38A GB369638A GB515612A GB 515612 A GB515612 A GB 515612A GB 3696/38 A GB3696/38 A GB 3696/38A GB 369638 A GB369638 A GB 369638A GB 515612 A GB515612 A GB 515612A
Authority
GB
United Kingdom
Prior art keywords
wheels
shock absorber
improvements relating
aircraft tail
tube
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
GB3696/38A
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 GB3696/38A priority Critical patent/GB515612A/en
Publication of GB515612A publication Critical patent/GB515612A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Damping Devices (AREA)
  • Tires In General (AREA)

Abstract

515,612. Stuffing-boxes. DOWTY, G. H. Feb. 5, 1938, No. 3696. [Classes 122 (i) and 122 (v)] [Also in Groups XXXIII and XXXII] A tube 3 rotatable and slidable within a tube 4 carrying a stem 5 is provided with packing means comprising two oppositely arranged U- section leather or rubber washers 12 spaced by a distance piece 13 and forming a seal between the tube and the stem 5.
GB3696/38A 1938-02-05 1938-02-05 Improvements relating to shock absorber struts particularly for aircraft tail and like wheels Expired GB515612A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3696/38A GB515612A (en) 1938-02-05 1938-02-05 Improvements relating to shock absorber struts particularly for aircraft tail and like wheels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3696/38A GB515612A (en) 1938-02-05 1938-02-05 Improvements relating to shock absorber struts particularly for aircraft tail and like wheels

Publications (1)

Publication Number Publication Date
GB515612A true GB515612A (en) 1939-12-11

Family

ID=9763224

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3696/38A Expired GB515612A (en) 1938-02-05 1938-02-05 Improvements relating to shock absorber struts particularly for aircraft tail and like wheels

Country Status (1)

Country Link
GB (1) GB515612A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2462992A (en) * 1944-10-24 1949-03-01 Automotive Prod Co Ltd Centering mechanism for aircraft wheel mountings having castoring or equivalent motion
US2624566A (en) * 1949-03-25 1953-01-06 Peter G Caramelli Adjustable counterseat

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2462992A (en) * 1944-10-24 1949-03-01 Automotive Prod Co Ltd Centering mechanism for aircraft wheel mountings having castoring or equivalent motion
US2624566A (en) * 1949-03-25 1953-01-06 Peter G Caramelli Adjustable counterseat

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