GB494961A - Locking aircraft control surfaces - Google Patents
Locking aircraft control surfacesInfo
- Publication number
- GB494961A GB494961A GB12574/37A GB1257437A GB494961A GB 494961 A GB494961 A GB 494961A GB 12574/37 A GB12574/37 A GB 12574/37A GB 1257437 A GB1257437 A GB 1257437A GB 494961 A GB494961 A GB 494961A
- Authority
- GB
- United Kingdom
- Prior art keywords
- locking
- pin
- ground
- control surfaces
- accelerator
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/14—Initiating means actuated personally lockable
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
Abstract
494,961. Locking aircraft control surfaces. FLUGZEUGWERK HALLE GES. May 3, 1937, Nos. 12574, 12575, and 12576. Convention dates, May 2, 1936, Nov. 14, 1936, and Nov. 24, 1936. [Class 4] When aircraft are on the ground the rudders or other control surfaces are locked to prevent accidental movement and damage by means released by the accelerator, retractable undercarriage, tail skid, &c. The locking-means comprises spring pins engaging the rudders and operated by a lever a, Fig. 3, held in locking position by a spring pin l. A wedge face g<1> on the accelerator pedal is adapted to release the pin l and the locking-means when the accelerator is actuated. The wedge face engages a plunger h articulated to a lever i connected by Bowden wire k to the pin l. In Fig. 5, the engagement of the landing wheel with the ground releases a latch n from a slide m on the cable operating the locking-means. The engagement of members n, m during flying prevents the rudder being locked. A similar arrangement is shown operated by a tail skid. In further modifications, special means engage the ground to release the locking device. A locking pin is shown in Fig. 11 and comprises telescopic parts e, e<11> held apart by a spring t. The part e<11> has a head e<1> fitting in a groove v in the rudder.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE494961X | 1936-05-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB494961A true GB494961A (en) | 1938-11-03 |
Family
ID=6544812
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB12574/37A Expired GB494961A (en) | 1936-05-02 | 1937-05-03 | Locking aircraft control surfaces |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB494961A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013126272A1 (en) * | 2012-02-21 | 2013-08-29 | Clean Green Energy LLC | Fluid driven vertical axis turbine |
| US8823199B2 (en) | 2011-11-25 | 2014-09-02 | Rupert Stephen Tull de Salis | Fluid driven turbine |
| GB2514071A (en) * | 2012-02-16 | 2014-11-12 | Cambridge Mechatronics Ltd | Shape memory alloy actuation apparatus |
| CN111976953A (en) * | 2020-07-06 | 2020-11-24 | 西安飞机工业（集团）有限责任公司 | Airplane control surface locking method and locking device |
| CN114593643A (en) * | 2022-01-25 | 2022-06-07 | 北京宇航系统工程研究所 | Double-hinge-rod type air rudder locking, unlocking and buffeting restraining mechanism |
-
1937
- 1937-05-03 GB GB12574/37A patent/GB494961A/en not_active Expired
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8823199B2 (en) | 2011-11-25 | 2014-09-02 | Rupert Stephen Tull de Salis | Fluid driven turbine |
| GB2514071A (en) * | 2012-02-16 | 2014-11-12 | Cambridge Mechatronics Ltd | Shape memory alloy actuation apparatus |
| GB2514071B (en) * | 2012-02-16 | 2015-09-16 | Cambridge Mechatronics Ltd | Shape memory alloy actuation apparatus |
| US9970410B2 (en) | 2012-02-21 | 2018-05-15 | Clean Green Energy LLC | Installation and erection assembly for an elongated structure |
| US8985948B2 (en) | 2012-02-21 | 2015-03-24 | Clean Green Energy LLC | Fluid driven vertical axis turbine |
| GB2513801A (en) * | 2012-02-21 | 2014-11-05 | Clean Green Energy LLC | Fuel Driven Vertical Axis Turbine |
| WO2013126272A1 (en) * | 2012-02-21 | 2013-08-29 | Clean Green Energy LLC | Fluid driven vertical axis turbine |
| GB2513801B (en) * | 2012-02-21 | 2018-11-28 | Clean Green Energy LLC | Fluid driven vertical axis turbine |
| US10808677B2 (en) | 2012-02-21 | 2020-10-20 | Clean Green Energy LLC | Fluid driven vertical axis turbine |
| CN111976953A (en) * | 2020-07-06 | 2020-11-24 | 西安飞机工业（集团）有限责任公司 | Airplane control surface locking method and locking device |
| CN111976953B (en) * | 2020-07-06 | 2022-08-09 | 西安飞机工业（集团）有限责任公司 | Airplane control surface locking method and locking device |
| CN114593643A (en) * | 2022-01-25 | 2022-06-07 | 北京宇航系统工程研究所 | Double-hinge-rod type air rudder locking, unlocking and buffeting restraining mechanism |
| CN114593643B (en) * | 2022-01-25 | 2024-02-09 | 北京宇航系统工程研究所 | Double-hinge rod type air rudder locking and unlocking and buffeting restraining mechanism |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US1869506A (en) | Method of and apparatus for mooring an airplane while in flight to another aircraft | |
| GB1183003A (en) | Improvements in or relating to Latches. | |
| US3618880A (en) | Speed brake system for aircraft spoilers | |
| GB494961A (en) | Locking aircraft control surfaces | |
| GB1057488A (en) | Aircraft and devices for launching same | |
| US2276312A (en) | Landing hook for aircraft | |
| GB1067088A (en) | Aircraft landing gear | |
| US2294467A (en) | Landing gear | |
| US2423501A (en) | Retractable landing gear lock for aircraft | |
| US2505652A (en) | Tail wheel actuated arresting hook | |
| GB548916A (en) | Improvements in and relating to mechanism for releasably locking a pivoted member in one or more positions, particularly applicable to retractable undercarriages for aircraft | |
| US2473792A (en) | Automatic flap retractor | |
| US2553632A (en) | Aircraft arresting gear with releasable hook | |
| GB464384A (en) | Improvements in or relating to tractors having a winch more particularly for trailing ordnance | |
| US2918829A (en) | Non-creep throttle control | |
| GB486936A (en) | Improvements relating to locking means for retractable undercarriages of aircraft | |
| GB1081302A (en) | Improvements to aircraft | |
| GB502240A (en) | Landing hook for aircraft | |
| GB531750A (en) | Improvements relating to retractable undercarriages for aircraft | |
| GB506680A (en) | Improvements relating to aircraft for use in conjunction with launching gear | |
| GB614880A (en) | Improvements in or relating to retractable undercarriages for aircraft | |
| GB609229A (en) | Improvements in or relating to aircraft | |
| GB546588A (en) | Improvements in or relating to aircraft | |
| GB757255A (en) | Improvements in and relating to skid-landing aircraft | |
| GB716465A (en) | Aircraft with quadricycle landing gear |