GB556325A - Improvements in and relating to aircraft landing gear - Google Patents
Improvements in and relating to aircraft landing gearInfo
- Publication number
- GB556325A GB556325A GB430142A GB430142A GB556325A GB 556325 A GB556325 A GB 556325A GB 430142 A GB430142 A GB 430142A GB 430142 A GB430142 A GB 430142A GB 556325 A GB556325 A GB 556325A
- Authority
- GB
- United Kingdom
- Prior art keywords
- frame
- struts
- wheels
- members
- landing
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Vehicle Body Suspensions (AREA)
Abstract
556,325. Aircraft undercarriages. GRIFFITHS, E. J. March 31, 1942, No. 4301. [Class 4] A pair of landing wheels 9, 10 for supporting the tail of an aeroplane is carried by a pair of struts 1, 2 connected together by transverse struts 3, 4, 14 braced to form a rigid frame which is supported by members 11, 12 pivoted about a horizontal axis 13 for retracting the landing wheels, the frame being vertically adjustable to two positions in the members 11, 12 to suit landing and take-off conditions. The struts 1, 2 are rotatable in the frame for steering the wheels. A stay 15 connected to one of the cross members of the frame is slidable in a pivoted sleeve 17 to which it can be locked in three positions to support the frame in either of its two extended positions or in its retracted position. The frame is locked to the fuselage in its landing and take-off position by spring loaded bolts 21 engaging blocks 23 on the fuselage and operable by solenoids, the frame being movable by a cable. The stay 15 is locked to the sleeve 17 by a member 19 engaging teeth on the stay and operable by a spring-loaded solenoid. The lower parts of the struts 1, 2 include shock-absorbers 7, 8. The struts 1, 2 have keyways engaged by projections on levers 24 pivoted in the members 11, 12 and connected by a rod 26, Fig. 4, a cable 25 enabling the wheels to be steered by rotating the struts 1, 2 in either of their operative positions. The wheels are retracted into their inoperative position by turning the members 11, 12 about the axis 13.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB430142A GB556325A (en) | 1942-03-31 | 1942-03-31 | Improvements in and relating to aircraft landing gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB430142A GB556325A (en) | 1942-03-31 | 1942-03-31 | Improvements in and relating to aircraft landing gear |
Publications (1)
Publication Number | Publication Date |
---|---|
GB556325A true GB556325A (en) | 1943-09-29 |
Family
ID=9774573
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB430142A Expired GB556325A (en) | 1942-03-31 | 1942-03-31 | Improvements in and relating to aircraft landing gear |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB556325A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2487548A (en) * | 1947-04-11 | 1949-11-08 | Lockheed Aircraft Corp | Main landing gear |
US2740135A (en) * | 1954-10-15 | 1956-04-03 | Charles P Church | Boat with retractable wheels |
CN107117291A (en) * | 2017-04-26 | 2017-09-01 | 浙江大学 | A kind of power-assisted transport foot stool and the unmanned plane with the foot stool |
-
1942
- 1942-03-31 GB GB430142A patent/GB556325A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2487548A (en) * | 1947-04-11 | 1949-11-08 | Lockheed Aircraft Corp | Main landing gear |
US2740135A (en) * | 1954-10-15 | 1956-04-03 | Charles P Church | Boat with retractable wheels |
CN107117291A (en) * | 2017-04-26 | 2017-09-01 | 浙江大学 | A kind of power-assisted transport foot stool and the unmanned plane with the foot stool |
CN107117291B (en) * | 2017-04-26 | 2023-09-15 | 浙江大学 | Helping hand transportation foot rest and have unmanned aerial vehicle of this foot rest |
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