GB282715A - Improvements in airplane tail supporting wheel - Google Patents
Improvements in airplane tail supporting wheelInfo
- Publication number
- GB282715A GB282715A GB27196/27A GB2719627A GB282715A GB 282715 A GB282715 A GB 282715A GB 27196/27 A GB27196/27 A GB 27196/27A GB 2719627 A GB2719627 A GB 2719627A GB 282715 A GB282715 A GB 282715A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- sprocket
- arm
- opposite ends
- machine
- 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
-
- 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)
- Friction Gearing (AREA)
Abstract
282,715. Ford Motor Co., (Assignees of Smith, C. J., and Hicks, H. A.). Dec. 27, 1926, [Convention date]. Land wheels; shock-absorbers, applications of. -The tail is supported by a wheel 32 mounted in a pair of forked arms 19, 23 pivoted to opposite ends of a shaft 18 rotatable in bearings 17 against the action of two pairs of springs 35 connected as shown between triangular plates 37 pivoted respectively on the machine and on opposite ends of a chain engaging a sprocket 33 on the shaft. The arm 23 is telescopic and includes a shock absorber 30 formed of a pile cf rubber rings separated by spacing washers between shoulders on the two parts of the arm, movement in either direction being limited by a pin and slot arrangement. Vertical play of the shaft 18 is prevented by the arrangement of the sprocket 33 and pivot bracket 20 immediately above and below the lower bearing 17. The shaft 18 is inclined forwardly when the machine is on the ground to prevent wabbling.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US282715XA | 1926-12-27 | 1926-12-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB282715A true GB282715A (en) | 1928-08-23 |
Family
ID=21842495
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB27196/27A Expired GB282715A (en) | 1926-12-27 | 1927-10-13 | Improvements in airplane tail supporting wheel |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB282715A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108839791A (en) * | 2018-08-29 | 2018-11-20 | 西安航远数字技术有限公司 | A kind of damping wheel mechanism |
-
1927
- 1927-10-13 GB GB27196/27A patent/GB282715A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108839791A (en) * | 2018-08-29 | 2018-11-20 | 西安航远数字技术有限公司 | A kind of damping wheel mechanism |
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