GB701384A - Improvements in or relating to aircraft controls - Google Patents
Improvements in or relating to aircraft controlsInfo
- Publication number
- GB701384A GB701384A GB27234/50A GB2723450A GB701384A GB 701384 A GB701384 A GB 701384A GB 27234/50 A GB27234/50 A GB 27234/50A GB 2723450 A GB2723450 A GB 2723450A GB 701384 A GB701384 A GB 701384A
- Authority
- GB
- United Kingdom
- Prior art keywords
- controls
- members
- aircraft
- stop
- rotate
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
- Transmission Devices (AREA)
Abstract
701,384. Aircraft controls. BRISTOL AEROPLANE CO., Ltd. Oct. 31, 1951 [Nov. 7, 1950], No. 27234/50. Class 4 An aircraft control comprises pedals 17 operating the rudder 12, and a hand wheel 14 operating the ailerons 10a and 10b. As shown in Fig. 1, direct manual control is used, but servo assistance may be employed. Either the controls or the adjustable surfaces operate members 20, 21, so that when the aircraft performs a banked turn to port or startboard, members 20, 21 rotate in the same sense. When the controls operate to produce sideslip, members 20, 21 rotate in the opposite sense, and one of rods 24 hinged to member 20, acts as a stop for member 21, preventing the controls from overbalancing, i.e. becoming aerodynamically urged to maximum displacement. Fig. 4 shows an alternative way of producing a stop by means of levers 33, 34 joined by a slotted link 35, and Fig. 3 shows a method where the axes of members 25, 26 are collinear, and a banked turn produces rotations in the opposite sense links 29, 30 being connected by a balance link 31 which co-operates with a slotted member. 32.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB27234/50A GB701384A (en) | 1950-11-07 | 1950-11-07 | Improvements in or relating to aircraft controls |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB27234/50A GB701384A (en) | 1950-11-07 | 1950-11-07 | Improvements in or relating to aircraft controls |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB701384A true GB701384A (en) | 1953-12-23 |
Family
ID=10256287
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB27234/50A Expired GB701384A (en) | 1950-11-07 | 1950-11-07 | Improvements in or relating to aircraft controls |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB701384A (en) |
-
1950
- 1950-11-07 GB GB27234/50A patent/GB701384A/en not_active Expired
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