GB530342A - Improvements in or relating to roller bearings, particularly for aircraft shock absorbers - Google Patents

Improvements in or relating to roller bearings, particularly for aircraft shock absorbers

Info

Publication number
GB530342A
GB530342A GB1811839A GB1811839A GB530342A GB 530342 A GB530342 A GB 530342A GB 1811839 A GB1811839 A GB 1811839A GB 1811839 A GB1811839 A GB 1811839A GB 530342 A GB530342 A GB 530342A
Authority
GB
United Kingdom
Prior art keywords
rollers
engaging
tubular member
tubular
roller bearings
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
GB1811839A
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.)
RIBBESFORD Co Ltd
Original Assignee
RIBBESFORD 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 RIBBESFORD Co Ltd filed Critical RIBBESFORD Co Ltd
Priority to GB1811839A priority Critical patent/GB530342A/en
Publication of GB530342A publication Critical patent/GB530342A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/04Ball or roller bearings, e.g. with resilient rolling bodies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30Parts of ball or roller bearings
    • F16C33/34Rollers; Needles

Abstract

530,342. Roller bearings. RIBBESFORD CO., Ltd., and ONIONS. J. H. June 21, 1939, No. 18118. [Class 12 (i)] A roller bearing particularly suitable for use in the elbow joints of aircraft shock absorber linkages consists of a number of rollers formed by helically wound wire coils mounted in a tubular race member having means at its ends for retaining the rollers in position. Fig. 1 shows a tubular member 10 mounted on a shaft 12 and formed with curved ends 17 engaging the reduced ends 16 of the wire coil rollers 11. The coils are preferably wound alternately clockwise and anti-clockwise and may be either arranged contiguously or spaced by a cage. The outer surfaces of the rollers are ground to form substantially continuous cylindrical surfaces after being hardened and tempered. The member 10 may alternatively be made of a diameter to fit the outer bearing member 13 and have inwardly turned ends to engage the ends of the rollers. Fig. 4 shows rollers composed of helically wound square-sectioned wire 21 fitted at their ends with pins 20 engaging annular grooves 19 in the flanged ends of the tubular member 10. The outer race is formed by a tubular member 22 having inwardly directed flanges 23 engaging the ends of the rollers. The member 22 is split obliquely at 24 to facilitate assembly. In another construction which may be packed with grease the rollers are enclosed between inner and outer races having abutting edges.
GB1811839A 1939-06-21 1939-06-21 Improvements in or relating to roller bearings, particularly for aircraft shock absorbers Expired GB530342A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1811839A GB530342A (en) 1939-06-21 1939-06-21 Improvements in or relating to roller bearings, particularly for aircraft shock absorbers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1811839A GB530342A (en) 1939-06-21 1939-06-21 Improvements in or relating to roller bearings, particularly for aircraft shock absorbers

Publications (1)

Publication Number Publication Date
GB530342A true GB530342A (en) 1940-12-10

Family

ID=10106950

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1811839A Expired GB530342A (en) 1939-06-21 1939-06-21 Improvements in or relating to roller bearings, particularly for aircraft shock absorbers

Country Status (1)

Country Link
GB (1) GB530342A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001089909A1 (en) * 2000-05-19 2001-11-29 Schwarzbich Joerg Telescopic mechanism

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001089909A1 (en) * 2000-05-19 2001-11-29 Schwarzbich Joerg Telescopic mechanism
US6942417B2 (en) 2000-05-19 2005-09-13 Schwarzbich Joerg Telescopic mechanism

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