GB523300A - Improvements in or relating to shock absorbers - Google Patents

Improvements in or relating to shock absorbers

Info

Publication number
GB523300A
GB523300A GB37857/38A GB3785738A GB523300A GB 523300 A GB523300 A GB 523300A GB 37857/38 A GB37857/38 A GB 37857/38A GB 3785738 A GB3785738 A GB 3785738A GB 523300 A GB523300 A GB 523300A
Authority
GB
United Kingdom
Prior art keywords
cylinder
spline portion
spline
cylinders
keys
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
GB37857/38A
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.)
Cleveland Pneumatic Tool Co
Original Assignee
Cleveland Pneumatic Tool Co
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 Cleveland Pneumatic Tool Co filed Critical Cleveland Pneumatic Tool Co
Priority to GB37857/38A priority Critical patent/GB523300A/en
Publication of GB523300A publication Critical patent/GB523300A/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 
    • B64C25/58Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60Oleo legs

Landscapes

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

Abstract

523,300. Aircraft undercarriages. STEVENS, A. H. (Cleveland Pneumatic Tool Co.). Dec. 30, 1938, No. 37857. [Class 4] [Also in Group XXXII] A hydraulic shock-absorber for aircraft undercarriages and other purposes comprises a pair of telescoping cylinders provided respectively with an integral spline portion and a separate cooperating spline portion, the separate spline portion being of softer metal than the cylinder provided with the integral spline portion. In the form shown, Figs. 1 and 2, a shockabsorber comprises two telescoping cylinders 10 and 13. A partition 17 in the outer cylinder has a central port 18 and a series of small ports 19 near its periphery. The port 18 is normally closed by means of a valve plate 20 held by coiled springs 21. The portion 11 of the outer cylinder has spline grooves 23 extending throughout its length. The cylinder 13 has a smooth exterior for the greater part of its length but in the thickened portion near the top is provided with key slots in which are fitted keys 32 made from a softer metal than that of the two cylinders. In the lower portion of the cylinder 10 is mounted an oil-tight packing 24. The part 13 carries a ground-wheel 28. In a further modification, Fig. 5, the keys may be provided on a removable sleeve 46 which is held against rotation relative to the inner cylinder by pins 47 and secured by a threaded head 49
GB37857/38A 1938-12-30 1938-12-30 Improvements in or relating to shock absorbers Expired GB523300A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB37857/38A GB523300A (en) 1938-12-30 1938-12-30 Improvements in or relating to shock absorbers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB37857/38A GB523300A (en) 1938-12-30 1938-12-30 Improvements in or relating to shock absorbers

Publications (1)

Publication Number Publication Date
GB523300A true GB523300A (en) 1940-07-11

Family

ID=10399509

Family Applications (1)

Application Number Title Priority Date Filing Date
GB37857/38A Expired GB523300A (en) 1938-12-30 1938-12-30 Improvements in or relating to shock absorbers

Country Status (1)

Country Link
GB (1) GB523300A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1034180C2 (en) * 2007-07-24 2009-01-27 Sonicsampdrill B V Drilling device with rotary vibration drive.
FR3112526A1 (en) * 2020-07-16 2022-01-21 Safran Landing Systems Aircraft lander with steerable wheels, equipped with an integrated alignment cam.

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1034180C2 (en) * 2007-07-24 2009-01-27 Sonicsampdrill B V Drilling device with rotary vibration drive.
WO2009014444A1 (en) * 2007-07-24 2009-01-29 Sonicsampdrill B.V. Drill device having a rotary-vibratory drive
FR3112526A1 (en) * 2020-07-16 2022-01-21 Safran Landing Systems Aircraft lander with steerable wheels, equipped with an integrated alignment cam.

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