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 absorbersInfo
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
- F16C27/04—Ball or roller bearings, e.g. with resilient rolling bodies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/34—Rollers; 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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001089909A1 (en) * | 2000-05-19 | 2001-11-29 | Schwarzbich Joerg | Telescopic mechanism |
-
1939
- 1939-06-21 GB GB1811839A patent/GB530342A/en not_active Expired
Cited By (2)
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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