GB640741A - Improvements in or relating to aircraft undercarriages - Google Patents
Improvements in or relating to aircraft undercarriagesInfo
- Publication number
- GB640741A GB640741A GB657648A GB657648A GB640741A GB 640741 A GB640741 A GB 640741A GB 657648 A GB657648 A GB 657648A GB 657648 A GB657648 A GB 657648A GB 640741 A GB640741 A GB 640741A
- Authority
- GB
- United Kingdom
- Prior art keywords
- leg
- pivoted
- well
- undercarriage
- main leg
- 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
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
-
- 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
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Handcart (AREA)
Abstract
640,741. Retractable undercarriages. FAIREY AVIATION CO., Ltd., COSTIGAN, F. J., and MORRIS, K. W. March 2, 1948, No. 6576. [Class 4] An undercarriage comprises twin wheels each on one of a pair of legs arranged to be retracted about fore-and-aft pivots by swinging laterally in opposite directions and upwardly into a well, a main leg carrying a wheel being arranged to be pivotally secured to the aircraft and a secondary leg carrying a wheel being pivotally secured to the main leg. In the form shown, the main leg 10 and the secondary leg 19 are pivoted together at 18 and carry shock absorbers 15 mounting wheels 14 and 20 respectively. The main leg is pivoted at 11 to the aircraft structure 12 and at 25 to one end of a breakable strut 24 also pivoted to the structure at 26. A radius rod 21 is pivoted to the structure 12 and to the leg 19 at 22. When the strut 24 is broken at 27 the pivot 11 is rotated to retract the undercarriage into the well 13. Fairings 31, 32 (Fig. 5, not shown) are connected by links to the legs 10 and 19 to cover the well 13 when the undercarriage is retracted.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB657648A GB640741A (en) | 1948-03-02 | 1948-03-02 | Improvements in or relating to aircraft undercarriages |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB657648A GB640741A (en) | 1948-03-02 | 1948-03-02 | Improvements in or relating to aircraft undercarriages |
Publications (1)
Publication Number | Publication Date |
---|---|
GB640741A true GB640741A (en) | 1950-07-26 |
Family
ID=9817009
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB657648A Expired GB640741A (en) | 1948-03-02 | 1948-03-02 | Improvements in or relating to aircraft undercarriages |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB640741A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1194711B (en) * | 1961-06-26 | 1965-06-10 | Hawker Siddeley Aviation Ltd | Retractable undercarriage for aircraft |
DE1272736B (en) * | 1966-08-24 | 1968-07-11 | Dornier Gmbh | The aircraft landing gear can be pivoted about an axis extending in the aircraft longitudinal direction |
US3432124A (en) * | 1966-03-07 | 1969-03-11 | Messier Sa | Under-carriage with three wheels arranged on the same shaft |
US5839692A (en) * | 1997-06-13 | 1998-11-24 | The Boeing Company | Splayable aircraft nose landing gear |
-
1948
- 1948-03-02 GB GB657648A patent/GB640741A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1194711B (en) * | 1961-06-26 | 1965-06-10 | Hawker Siddeley Aviation Ltd | Retractable undercarriage for aircraft |
US3432124A (en) * | 1966-03-07 | 1969-03-11 | Messier Sa | Under-carriage with three wheels arranged on the same shaft |
DE1272736B (en) * | 1966-08-24 | 1968-07-11 | Dornier Gmbh | The aircraft landing gear can be pivoted about an axis extending in the aircraft longitudinal direction |
US3485464A (en) * | 1966-08-24 | 1969-12-23 | Dornier Gmbh | Retractable landing gear |
US5839692A (en) * | 1997-06-13 | 1998-11-24 | The Boeing Company | Splayable aircraft nose landing gear |
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