GB297533A - Improvements in or relating to control devices for aeroplanes and the like - Google Patents
Improvements in or relating to control devices for aeroplanes and the likeInfo
- Publication number
- GB297533A GB297533A GB18616/27A GB1861627A GB297533A GB 297533 A GB297533 A GB 297533A GB 18616/27 A GB18616/27 A GB 18616/27A GB 1861627 A GB1861627 A GB 1861627A GB 297533 A GB297533 A GB 297533A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spindle
- bar
- cross
- head
- post
- 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
- B64C13/044—Initiating means actuated personally operated by feet, e.g. pedals
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
297,533. Frise, L. G., Barnwell, F. S., and Bristol Aeroplane Co., Ltd. July 13, 1927. Steering.-The rudderbar of an aircraft is adjustable towards and away from the pilot's seat on a fixed pivot-post. The pivot post 10 carries a yoke 13 in which are mounted fore-and-aft tubes 16, 17 on which a cross-head 24 is slidably mounted, and a screw-spindle 20 engaging a nut 25 on the cross-head. The cross-head carries the rudder-bar 26 and rotation of the wheel 23 on the spindle 20 by the pilot adjusts the bar as required. The pivot-post carries arms 12 to which the control cables are connected, but the control cables may be directly connected to the bar, turn-buckles being provided therein. The spindle 20 might be dispensed with, the crosshead being locked in a suitable position on the tubes by a locking pin. Suitable heel-rests may be provided.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB18616/27A GB297533A (en) | 1927-07-13 | 1927-07-13 | Improvements in or relating to control devices for aeroplanes and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB18616/27A GB297533A (en) | 1927-07-13 | 1927-07-13 | Improvements in or relating to control devices for aeroplanes and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB297533A true GB297533A (en) | 1928-09-27 |
Family
ID=10115495
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18616/27A Expired GB297533A (en) | 1927-07-13 | 1927-07-13 | Improvements in or relating to control devices for aeroplanes and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB297533A (en) |
-
1927
- 1927-07-13 GB GB18616/27A patent/GB297533A/en not_active Expired
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