GB527191A - Improvements relating to retractible undercarriages for aircraft - Google Patents
Improvements relating to retractible undercarriages for aircraftInfo
- Publication number
- GB527191A GB527191A GB1037439A GB1037439A GB527191A GB 527191 A GB527191 A GB 527191A GB 1037439 A GB1037439 A GB 1037439A GB 1037439 A GB1037439 A GB 1037439A GB 527191 A GB527191 A GB 527191A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinder
- wheel
- collar
- aircraft
- undercarriages
- 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)
- Fluid-Damping Devices (AREA)
Abstract
527,191. Retractable undercarriages. BOUL- ,TON PAUL AIRCRAFT, Ltd., and NORTH, J. D. April 3, 1939, No. 10374. [Class 4] In retractable undercarriages of the kind in which the landing wheel is turned through a rightangle about a diameter while it is being swung backwardly and upwardly into a housing such as a recess in an engine nacelle, additional bearing is provided at or near the lower end of the undercarriage leg by a triangular pyramidal, or conical supporting structure hinged at its upper end to the aircraft frame. As shown in Fig. 2, the wheel is carried by a plunger 12 telescopically mounted under elastic and damping restraint in a cylinder 10. Struts 22 are connected to a collar 32 and a horizontal tubular member 20 having journals 40 for pivoting to the framework. The collar 32 and a collar 24 on the member 20 are provided with thrust and journal ball bearings on the cylinder 10. A toothed wheel or sector secured to the cylinder meshes with a similar element mounted on a shaft that passes through one end of the member 20 and is secured to the framework. The cylinder 10 may be locked in the operative position of the wheel by an hydraulicallycontrolled bolt.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1037439A GB527191A (en) | 1939-04-03 | 1939-04-03 | Improvements relating to retractible undercarriages for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1037439A GB527191A (en) | 1939-04-03 | 1939-04-03 | Improvements relating to retractible undercarriages for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB527191A true GB527191A (en) | 1940-10-03 |
Family
ID=9966665
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1037439A Expired GB527191A (en) | 1939-04-03 | 1939-04-03 | Improvements relating to retractible undercarriages for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB527191A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2529377A (en) * | 1947-12-03 | 1950-11-07 | Electro Hydraulics Ltd | Undercarriage suspension for aircraft |
US2667316A (en) * | 1951-04-25 | 1954-01-26 | Bell Aircraft Corp | Retractable aircraft undercarriage |
FR2599103A1 (en) * | 1986-05-20 | 1987-11-27 | Valmet Oy | SUPPORT AND FIXING STRUCTURE FOR A PISTON-CYLINDER OR EQUIVALENT ASSEMBLY |
EP3196117A1 (en) * | 2016-01-14 | 2017-07-26 | Embraer S.A. | Retractable self-aligning aircraft stabilizer strut assembly and aircraft including the same |
GB2551380A (en) * | 2016-06-16 | 2017-12-20 | Airbus Operations Ltd | Aircraft landing gear |
-
1939
- 1939-04-03 GB GB1037439A patent/GB527191A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2529377A (en) * | 1947-12-03 | 1950-11-07 | Electro Hydraulics Ltd | Undercarriage suspension for aircraft |
US2667316A (en) * | 1951-04-25 | 1954-01-26 | Bell Aircraft Corp | Retractable aircraft undercarriage |
FR2599103A1 (en) * | 1986-05-20 | 1987-11-27 | Valmet Oy | SUPPORT AND FIXING STRUCTURE FOR A PISTON-CYLINDER OR EQUIVALENT ASSEMBLY |
EP3196117A1 (en) * | 2016-01-14 | 2017-07-26 | Embraer S.A. | Retractable self-aligning aircraft stabilizer strut assembly and aircraft including the same |
GB2551380A (en) * | 2016-06-16 | 2017-12-20 | Airbus Operations Ltd | Aircraft landing gear |
US11377205B2 (en) | 2016-06-16 | 2022-07-05 | Airbus Operations Limited | Aircraft landing gear |
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