GB438968A - Improvements in or relating to internally sprung wheels for aircraft - Google Patents
Improvements in or relating to internally sprung wheels for aircraftInfo
- Publication number
- GB438968A GB438968A GB1625134A GB1625134A GB438968A GB 438968 A GB438968 A GB 438968A GB 1625134 A GB1625134 A GB 1625134A GB 1625134 A GB1625134 A GB 1625134A GB 438968 A GB438968 A GB 438968A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sleeve
- axle
- guide
- guideway
- aircraft
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Dampers (AREA)
Abstract
438,968. Vehicle wheels. DOWTY, G. H., 17, Lansdown Crescent, Cheltenham. May 31, 1934, No. 16251. [Class 144 (i)] An internally-sprung wheel for aircraft is provided with inner and outer wheel bearings 14, 7 carried by separate halves of a longitudinally-divided sleeve 15 which is slidable against the action of shock-absorbing means over a cylindrical guide 17 rigid with the axle 18. Further, the axle is slidable within the encircling bearing 14 on a slotted guideway 34 arranged at the side of the bearing 14 remote from the sleeve and guide. The telescoping sleeve and guide enclose a shock-absorbing device comprising a spring 25 and dashpot 22. The sleeve guide 17 is formed as a T-head to the axle which moves in a slot in the sleeve. The slot 34 of the guideway is covered by a pair of sliding plates, the outer one 37 of which is fixed to the axle, the other 35 having sliding engagement therewith, its upward and downward movement being limited by stops 36, 38. The brake drum 31 is formed within the thickness of the wheel, the guideway 34 lying within the plane of the brake and being surrounded by the drum.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1625134A GB438968A (en) | 1934-05-31 | 1934-05-31 | Improvements in or relating to internally sprung wheels for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1625134A GB438968A (en) | 1934-05-31 | 1934-05-31 | Improvements in or relating to internally sprung wheels for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB438968A true GB438968A (en) | 1935-11-27 |
Family
ID=10073932
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1625134A Expired GB438968A (en) | 1934-05-31 | 1934-05-31 | Improvements in or relating to internally sprung wheels for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB438968A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8714473B2 (en) | 2003-04-07 | 2014-05-06 | Airbus Uk Limited | Landing gear |
| US8882043B2 (en) | 2003-04-07 | 2014-11-11 | Airbus Uk Limited | Landing gear assembly |
-
1934
- 1934-05-31 GB GB1625134A patent/GB438968A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8714473B2 (en) | 2003-04-07 | 2014-05-06 | Airbus Uk Limited | Landing gear |
| US8746615B2 (en) | 2003-04-07 | 2014-06-10 | Airbus Operations Limited | Landing gear |
| US8882043B2 (en) | 2003-04-07 | 2014-11-11 | Airbus Uk Limited | Landing gear assembly |
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