GB565758A - Improvements in the manufacture of landing-gear forks for aircraft - Google Patents
Improvements in the manufacture of landing-gear forks for aircraftInfo
- Publication number
- GB565758A GB565758A GB5293/43A GB529343A GB565758A GB 565758 A GB565758 A GB 565758A GB 5293/43 A GB5293/43 A GB 5293/43A GB 529343 A GB529343 A GB 529343A GB 565758 A GB565758 A GB 565758A
- Authority
- GB
- United Kingdom
- Prior art keywords
- welded
- pressings
- bushes
- fork
- wheel
- 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
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/14—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
Abstract
565,758. Landing gear forks for aircraft. RUBERY, OWEN, & CO., Ltd., OWEN, E. W. B., and BUCKLEY, R. O. April 2, 1943, Nos. 5293 and 9401. [Class 4] [Also in Group XXII] Forks for the landing wheels or caterpillar tracks of aeroplanes are made of two sheetmetal pressings or stampings welded together. The retractable fork for a port wheel shown in Figs. 1, 2, comprises two pressings 22, 23 welded along the line 24. Bushes 21 for a retraction pivotal connection and tubes 28, 33 for receiving the casings of the oleo legs are welded into the pressings, the tubes 28 being each held by two spaced straps 29 welded to the pressing 22. Brackets 35 for attachment to a retracting jack are welded to the pressing 22. Electric arc, gas or flash-welding may be employed, the weld zone being heat treated, in the case of flash-welding, to develop the physical properties of the parent metal. The tail-wheel fork shown in Fig.6, formed of pressings 22a, 23a, is provided in addition to the pivot bushes 21a with bushes 37 for the wheel axle. Plates 42 welded to the bridge part of the fork carry bushes 43 for attachment of a retracting oleo-leg or jack and plates 44 welded to the limbs carry towing pins 45. Clips 46 welded to the limbs serve for holding the fork when machining and they may be drilled for pins that pass also transversely through the wheel axle to locate it.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5293/43A GB565758A (en) | 1943-04-02 | 1943-04-02 | Improvements in the manufacture of landing-gear forks for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5293/43A GB565758A (en) | 1943-04-02 | 1943-04-02 | Improvements in the manufacture of landing-gear forks for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB565758A true GB565758A (en) | 1944-11-27 |
Family
ID=9793388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB5293/43A Expired GB565758A (en) | 1943-04-02 | 1943-04-02 | Improvements in the manufacture of landing-gear forks for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB565758A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140346272A1 (en) * | 2011-12-07 | 2014-11-27 | Renesas Electronics Corporation | Aircraft landing gear strut |
-
1943
- 1943-04-02 GB GB5293/43A patent/GB565758A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140346272A1 (en) * | 2011-12-07 | 2014-11-27 | Renesas Electronics Corporation | Aircraft landing gear strut |
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