GB429867A - Improvements in or relating to landing gear for aeroplanes - Google Patents
Improvements in or relating to landing gear for aeroplanesInfo
- Publication number
- GB429867A GB429867A GB24886/34A GB2488634A GB429867A GB 429867 A GB429867 A GB 429867A GB 24886/34 A GB24886/34 A GB 24886/34A GB 2488634 A GB2488634 A GB 2488634A GB 429867 A GB429867 A GB 429867A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gear
- strut
- landing
- locking
- absorber
- 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
- B64C25/18—Operating mechanisms
- B64C25/20—Operating mechanisms mechanical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Body Suspensions (AREA)
Abstract
429,867. Aircraft landing-gear. SOC. D'INVENTIONS AERONAUTIQUES ET MECANIQUES S.I.A.M., 1, Route des Alpes, Fribourg, Switzerland. Aug. 29, 1934, Nos. 24886 and 24887. Convention dates, May 24 and June 27. [Class 4] In retractable landing-gear for aeroplanes in which the gear is held in its extended position by a foldable strut, means are provided for transferring the stresses tending to open the strut hinge to a locking-device independent of means for operating the gear, the device being set in a position so that it has to support only very small stresses or is movable against but small resistance. As shown, a shock-absorber A for a wheel R is pivoted to facilitate retraction of the wheel by means of a foldable strut J<1>, J<2> pivoted to the shock-absorber and to the rear wing spar L. An auxiliary arm C on the portion J<2> of the strut co-operates with a hydraulic locking-device V to hold the undercarriage in its operative position. Folding of the strut on release of the locking device, is facilitated by a spring-pressed piston-rod r which urges the arm C downwardly. The landing-gear may be retracted, e.g. by means of a cable. The members J<1> may form a fork. In a modification, an extension of the member J<2> is connected to a hydraulically-operated ram m and moves between plates x a spring- pressed hydraulically-controlled locking-bolt p being provided. The landing-gear may be combined with operating-mechanism described in Specification 425,207.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR429867X | 1934-05-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB429867A true GB429867A (en) | 1935-06-07 |
Family
ID=8899227
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24886/34A Expired GB429867A (en) | 1934-05-24 | 1934-08-29 | Improvements in or relating to landing gear for aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB429867A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE746876C (en) * | 1940-04-13 | 1944-12-27 | Retractable aircraft leg |
-
1934
- 1934-08-29 GB GB24886/34A patent/GB429867A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE746876C (en) * | 1940-04-13 | 1944-12-27 | Retractable aircraft leg |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB429867A (en) | Improvements in or relating to landing gear for aeroplanes | |
US2025743A (en) | Retractable landing gear | |
US2431093A (en) | Retractable landing gear | |
US2505652A (en) | Tail wheel actuated arresting hook | |
US3384331A (en) | Aircraft retractable undercarriage | |
GB651149A (en) | Improvements in or relating to retractable landing gear for aircraft | |
GB1141141A (en) | Improvements in or relating to retractable wheel mountings for aircraft | |
GB860432A (en) | Retractable undercarriages for aircraft | |
GB538298A (en) | Improvements in or relating to retractable undercarriages for aircraft | |
US2014777A (en) | Retractable landing gear | |
US2333981A (en) | Retractable landing gear for aircraft | |
GB458187A (en) | Improvements relating to retractable undercarriages for aircraft | |
GB485414A (en) | Improvements in or relating to self-folding struts for aeroplane landing chassis | |
GB510164A (en) | Improvements in aircraft landing (or alighting) gear | |
GB397964A (en) | Improvements in or relating to aeroplanes | |
US1834254A (en) | Aircraft | |
GB519275A (en) | Improvements in or relating to aeroplane landing gear | |
GB490087A (en) | Improvements in retractable undercarriages for aeroplanes | |
US1983358A (en) | Aircraft landing gear holding device | |
GB613051A (en) | Improvements to retractable landing gears for aircraft | |
GB468092A (en) | Improvements in or relating to retractable undercarriages for aircraft | |
GB456632A (en) | Landing gear for aeroplanes | |
GB534522A (en) | Improvements in retractable landing gear for aircraft | |
US2554009A (en) | Airplane landing gear | |
GB551493A (en) | Improvements in aircraft retractable alighting gear |