GB782841A - Improvements in wheels - Google Patents
Improvements in wheelsInfo
- Publication number
- GB782841A GB782841A GB3364654A GB3364654A GB782841A GB 782841 A GB782841 A GB 782841A GB 3364654 A GB3364654 A GB 3364654A GB 3364654 A GB3364654 A GB 3364654A GB 782841 A GB782841 A GB 782841A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flange
- secured
- web
- rim
- hub
- 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
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 238000007789 sealing Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60B—VEHICLE WHEELS; CASTORS; AXLES FOR WHEELS OR CASTORS; INCREASING WHEEL ADHESION
- B60B25/00—Rims built-up of several main parts ; Locking means for the rim parts
- B60B25/04—Rims with dismountable flange rings, seat rings, or lock rings
- B60B25/14—Locking means for flange rings or seat rings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Tires In General (AREA)
Abstract
782,841. Vehicle wheels. DUNLOP RUBBER CO., Ltd. Oct. 11, 1955 [Nov. 20, 1954], No. 33646/54. Class 144 (2). A vehicle wheel comprises a hub 17 with a radial flange 18 to one side of which is secured detachably a generally radial load-supporting body web 3 integral with a rear part 1 having a tyre retaining flange 2, and a separable rim part 8, having the other retaining flange 9, which has a radially inwardly directed rib 11 clamped against the adjacent edge of the rim part 1 by the outer peripheral edge of a separate loadsupporting web 12 detachably secured to the hub flange 18, the rim parts 1, 8 thus being secured together in coaxial relationship. As shown applied to an aircraft wheel, the webs 3 and 12 are oppositely inclined to diverge towards the hub sleeve 17 where they are secured to opposite sides of the flange 18 by bolts 21 having intermediate collars to abut the flange 18 so that the web 12 may be detached without disturbing the web 3. The webs 3 and 12 have also abutting generally radial portions 6 and 14 respectively with aligned holes 7 and 16 to receive clamping bolts 20. Axial alignment of the rim parts 8 and 1 is secured by an axial lip 10 on the part 8 which seats around the part 1 adjacent the edge thereof which abuts the rib 11. A sealing ring may be compressed between the rim parts to permit the use of a tubeless tyre.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3364654A GB782841A (en) | 1954-11-20 | 1954-11-20 | Improvements in wheels |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3364654A GB782841A (en) | 1954-11-20 | 1954-11-20 | Improvements in wheels |
Publications (1)
Publication Number | Publication Date |
---|---|
GB782841A true GB782841A (en) | 1957-09-11 |
Family
ID=10355608
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3364654A Expired GB782841A (en) | 1954-11-20 | 1954-11-20 | Improvements in wheels |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB782841A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2955677A (en) * | 1958-07-08 | 1960-10-11 | Goodrich Co B F | Wheel and brake |
CN106739790A (en) * | 2016-12-20 | 2017-05-31 | 江苏豪然喷射成形合金有限公司 | A kind of heavily loaded aircraft wheel |
CN109910499A (en) * | 2018-09-17 | 2019-06-21 | 华安正兴车轮有限公司 | A kind of two-piece type reflectal wheel |
-
1954
- 1954-11-20 GB GB3364654A patent/GB782841A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2955677A (en) * | 1958-07-08 | 1960-10-11 | Goodrich Co B F | Wheel and brake |
CN106739790A (en) * | 2016-12-20 | 2017-05-31 | 江苏豪然喷射成形合金有限公司 | A kind of heavily loaded aircraft wheel |
CN109910499A (en) * | 2018-09-17 | 2019-06-21 | 华安正兴车轮有限公司 | A kind of two-piece type reflectal wheel |
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