GB583963A - Improvements in aircraft landing gear - Google Patents
Improvements in aircraft landing gearInfo
- Publication number
- GB583963A GB583963A GB1517444A GB1517444A GB583963A GB 583963 A GB583963 A GB 583963A GB 1517444 A GB1517444 A GB 1517444A GB 1517444 A GB1517444 A GB 1517444A GB 583963 A GB583963 A GB 583963A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- shock absorber
- intervening layer
- aircraft
- landing gear
- 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
- B64C25/64—Spring shock-absorbers; Springs using rubber or like elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Dampers (AREA)
Abstract
583,963. Shock-absorbers. MILES AIRCRAFT, Ltd., and WOODHOUSE, J. W. Aug. 9, 1944, No. 15174. [Class 108 (iii)] [Also in Group XXXIII] A torsional shock absorber for aircraft undercarriages comprises two members connected by an intervening layer of elastic material, deformable under the landing load with relative movement of partial rotation between the two members. The shock absorber, shown applied to a tail wheel unit in Fig. 2, comprises elliptical inner and outer metal members 1a, 1b, with an intervening layer of natural or synthetic rubber 1c preferably bonded to both members. The outer member may be split at one or more points 10, in order that the rubber may be compressed when the unit is inserted into its housing in the mounting bracket 2. The wheel fork 6 is bolted to the inner member la of the shock absorber. Specification 493,521 is referred to Reference has been directed by the Comptroller to Specification 493,521.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1517444A GB583963A (en) | 1944-08-09 | 1944-08-09 | Improvements in aircraft landing gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1517444A GB583963A (en) | 1944-08-09 | 1944-08-09 | Improvements in aircraft landing gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB583963A true GB583963A (en) | 1947-01-03 |
Family
ID=10054325
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1517444A Expired GB583963A (en) | 1944-08-09 | 1944-08-09 | Improvements in aircraft landing gear |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB583963A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8714473B2 (en) | 2003-04-07 | 2014-05-06 | Airbus Uk Limited | Landing gear |
-
1944
- 1944-08-09 GB GB1517444A patent/GB583963A/en not_active Expired
Cited By (2)
| 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 |
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