GB538298A - Improvements in or relating to retractable undercarriages for aircraft - Google Patents
Improvements in or relating to retractable undercarriages for aircraftInfo
- Publication number
- GB538298A GB538298A GB777740A GB777740A GB538298A GB 538298 A GB538298 A GB 538298A GB 777740 A GB777740 A GB 777740A GB 777740 A GB777740 A GB 777740A GB 538298 A GB538298 A GB 538298A
- Authority
- GB
- United Kingdom
- Prior art keywords
- strut
- leg
- fore
- aircraft
- extension
- 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
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/26—Control or locking systems therefor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
538,298. Aircraft undercarriages. FAIREY AVIATION CO., Ltd., and COSTIGAN, F. J. April 30, 1940, No. 7777. [Class 4] A retractable undercarriage in which a wheel is adapted to be swung laterally upwards and slightly rearwardly to a position between the spars of an aircraft wing, comprises two jointed struts, pivoted to the oleo-leg and to the aircraft, which lie respectively in a transverse and a fore-and-aft plane when the wheel is lowered, the first mentioned strut being connected with a hydraulic jack whilst the joint of the second mentioned strut is connected by a link to a point on the aircraft offset from said fore- and-aft plane towards the same side as the other jointed strut. An oleo-leg b is pivoted about a transverse pivot upon a tubular member e mounted in bearings so as to be rotatable about a fore-and-aft axis on the aircraft. The leg b is connected by a universal joint g to the lower member h of a jointed strut h, j pivoted about a fore-and-aft axis k. An extension q is separately pivoted about the same axis k with lost motion provided by abutments r, s respectively on the extension q and the upper part j of the strut. A hydraulic jack u is connected between the extension q and a bracket x on the tube e for breaking the strut and raising the leg, the lost motion of the extension q being utilized for withdrawing a locking bolt co-operating with a quadrant n on the part h of the strut. The oleo-leg b is also connected to a bracket on the tubular member e by a jointed strut 13, 14, the cental pivot 17 of the strut being connected by a link 18 and a universal joint 19 to a fixed point on the aircraft wing, offset as shown from the fore-and-aft .member e, so that the leg b is moved rearwardly as it is raised. The extension q is fast upon a short fore-and-aft shaft carrying a spring-urged arm 21 co-operating with a hook 23 on the leg b to secure the leg in its raised position. initial movement of the jack u disengaging the arm from the hook before lowering the leg. A bracket 25 on the locking bolt of the strut h, j actuates a switch 26, when the bolt shoots home, to actuate an indicator showing that the undercarriage is down.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB777740A GB538298A (en) | 1940-04-30 | 1940-04-30 | Improvements in or relating to retractable undercarriages for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB777740A GB538298A (en) | 1940-04-30 | 1940-04-30 | Improvements in or relating to retractable undercarriages for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB538298A true GB538298A (en) | 1941-07-28 |
Family
ID=9839512
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB777740A Expired GB538298A (en) | 1940-04-30 | 1940-04-30 | Improvements in or relating to retractable undercarriages for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB538298A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2444319A (en) * | 1944-12-08 | 1948-06-29 | Curtiss Wright Corp | Airplane landing gear |
GB2234948A (en) * | 1989-08-16 | 1991-02-20 | Dowty Rotol Ltd | An aircraft landing gear arrangement |
EP0451910A1 (en) * | 1990-04-09 | 1991-10-16 | The Boeing Company | Aft cantilevered wing landing gear for heavy airplane with aft center of gravity |
FR3036375A1 (en) * | 2015-11-10 | 2016-11-25 | Airbus Operations Sas | LANDING TRAIN FOR AN AIRCRAFT AND HAVING A LATCHING SYSTEM IN STORAGE POSITION |
EP3492375A1 (en) * | 2017-11-29 | 2019-06-05 | Sikorsky Aircraft Corporation | Retractable landing gear system for a vertical takeoff and landing (vtol) aircraft |
CN114030594A (en) * | 2021-12-17 | 2022-02-11 | 江西洪都航空工业集团有限责任公司 | Strut type undercarriage leg retracting mechanism |
-
1940
- 1940-04-30 GB GB777740A patent/GB538298A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2444319A (en) * | 1944-12-08 | 1948-06-29 | Curtiss Wright Corp | Airplane landing gear |
GB2234948A (en) * | 1989-08-16 | 1991-02-20 | Dowty Rotol Ltd | An aircraft landing gear arrangement |
EP0451910A1 (en) * | 1990-04-09 | 1991-10-16 | The Boeing Company | Aft cantilevered wing landing gear for heavy airplane with aft center of gravity |
FR3036375A1 (en) * | 2015-11-10 | 2016-11-25 | Airbus Operations Sas | LANDING TRAIN FOR AN AIRCRAFT AND HAVING A LATCHING SYSTEM IN STORAGE POSITION |
EP3492375A1 (en) * | 2017-11-29 | 2019-06-05 | Sikorsky Aircraft Corporation | Retractable landing gear system for a vertical takeoff and landing (vtol) aircraft |
US11142304B2 (en) | 2017-11-29 | 2021-10-12 | Sikorsky Aircraft Corporation | Retractable landing gear system for a vertical takeoff and landing (VTOL) aircraft |
CN114030594A (en) * | 2021-12-17 | 2022-02-11 | 江西洪都航空工业集团有限责任公司 | Strut type undercarriage leg retracting mechanism |
CN114030594B (en) * | 2021-12-17 | 2023-08-25 | 江西洪都航空工业集团有限责任公司 | Leg retracting mechanism of strut type landing gear |
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