GB282938A - Improvements in or relating to control mechanism for aircraft - Google Patents
Improvements in or relating to control mechanism for aircraftInfo
- Publication number
- GB282938A GB282938A GB27533/26A GB2753326A GB282938A GB 282938 A GB282938 A GB 282938A GB 27533/26 A GB27533/26 A GB 27533/26A GB 2753326 A GB2753326 A GB 2753326A GB 282938 A GB282938 A GB 282938A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheel
- rod
- arms
- bell
- pivoted
- 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
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0423—Initiating means actuated personally operated by hand yokes or steering wheels for primary flight controls
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
282,938. Camm, S., and Hawker Engineering Co., Ltd., H. G. Nov 3, 1926. Steering, balancing, and regulating altitude.-In control mechanism for aeroplanes comprising a handwheel 2 for controlling the ailerons mounted in a horizontal bearing 10 at the upper end of a pivoted control column 13, a push member 5, 6 for firing a gun, is positioned relatively to the wheel 2 so as to be operable readily by the thumb or fingers without removing the hand from the wheel. As shown, the shaft 1 upon which the wheel 2 is fixed, is made hollow and slidable within it is a rod 3 on the rearwardly-projecting end of which is rotatably mounted a boss 4 carrying two radial arms 5 the outer ends of which are formed as thumb buttons 6 disposed a short distance within the rim 7 of the wheel 2. Guide pins 8 project forwardly from the buttons 6 through holes in the spokes or disc 9 of the wheel so that as the latter is. turned the arms 5 retain their relative position without rotating the rod 3. The forward end of the rod 3 is pivoted to one arm of a bell-crank lever 11 pivoted to a bracket 12 mounted on the column 13, the other arm of the bell-crank lever being connected by a. Bowden wire 14 to the gun mechanism, so that when the rod 3 is pushed forward by pressure on the buttons 6 the gun is fired. A returning spring 16 is provided. For locking or freeing the subsidiary control device, a fork 18, Fig. 3, slidable radially into and out of engagement with a recess 19 in the rod 3, is carried on a rod 21 which slides in a tube 22 mounted on the wheel 2 and terminates in a plate 23 located just within the rim 7 of the wheel so as to be operable conveniently by the fingers. The, rod 21 is held in its in and out positions by a spring-pressed ball 25. If the connection between the end of the shalt 3 and the bell-crank lever 11 comprises a ball and socket joint the arms 5 may be fixed directly to the shaft 3. The guide pins 8 may be dispensed with if in place of the two arms 5 several arms or an annular ring is used.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB27533/26A GB282938A (en) | 1926-11-03 | 1926-11-03 | Improvements in or relating to control mechanism for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB27533/26A GB282938A (en) | 1926-11-03 | 1926-11-03 | Improvements in or relating to control mechanism for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB282938A true GB282938A (en) | 1928-01-05 |
Family
ID=10261124
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB27533/26A Expired GB282938A (en) | 1926-11-03 | 1926-11-03 | Improvements in or relating to control mechanism for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB282938A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107985554A (en) * | 2017-12-05 | 2018-05-04 | 贵州华阳电工有限公司 | Self-resetting turning mechanism |
CN111924090A (en) * | 2020-07-08 | 2020-11-13 | 西安航空制动科技有限公司 | Sliding control device |
CN112407250A (en) * | 2020-11-17 | 2021-02-26 | 中国商用飞机有限责任公司 | Hidden hand wheel device |
-
1926
- 1926-11-03 GB GB27533/26A patent/GB282938A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107985554A (en) * | 2017-12-05 | 2018-05-04 | 贵州华阳电工有限公司 | Self-resetting turning mechanism |
CN107985554B (en) * | 2017-12-05 | 2021-03-09 | 贵州华阳电工有限公司 | Self-resetting turning mechanism |
CN111924090A (en) * | 2020-07-08 | 2020-11-13 | 西安航空制动科技有限公司 | Sliding control device |
CN112407250A (en) * | 2020-11-17 | 2021-02-26 | 中国商用飞机有限责任公司 | Hidden hand wheel device |
CN112407250B (en) * | 2020-11-17 | 2022-02-22 | 中国商用飞机有限责任公司 | Hidden hand wheel device |
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