GB637840A - A pilot's control column for actuating the ailerons and elevator of aeroplanes - Google Patents
A pilot's control column for actuating the ailerons and elevator of aeroplanesInfo
- Publication number
- GB637840A GB637840A GB33448/47A GB3344847A GB637840A GB 637840 A GB637840 A GB 637840A GB 33448/47 A GB33448/47 A GB 33448/47A GB 3344847 A GB3344847 A GB 3344847A GB 637840 A GB637840 A GB 637840A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pivots
- elevator
- lever
- control
- ailerons
- 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
- B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
637,840. Aircraft controls. AVIATION WORKS, NATIONAL CORPORATION, and SLECHTA, J. Dec. 18, 1947, No. 33448. Convention date, Nov. 15, 1946. [Class 4] A pilot's control member 9 for operating the ailerons and elevator of an aircraft comprises two members 1, 4, which are connected to the elevator control-rod 8 and aileron control-rod 7, respectively, and each of which is arranged to move in the fore-and-aft direction. For operation of the elevator, the control member 9 is rotated about pivots 2, and for aileron operation is rotated about perpendicularly disposed pivots 12. Transverse movement of the member 9 is converted into fore-and-aft movement of the lever 4 by a member 14, whose upper end engages a ball-member 13 in the tube 9, and whose lower end is pivotally connected to the lever 4 on an axis which is inclined to that of the pivots 5 by which the lever 4 is connected to the member 1, Fig. 3. In the neutral position of the control member, the point of connection of the lever 4 and link 7 passes through the axis of the pivots 2. Fig. 1 shows an arrangement for dual controls, the handles 17, 18 being carried by an outer tube 10 connected to the inner tube 9 by pivots 12, 21, 20, 22 arranged at the corners of a parallelogram.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CS637840X | 1946-11-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB637840A true GB637840A (en) | 1950-05-24 |
Family
ID=5454174
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB33448/47A Expired GB637840A (en) | 1946-11-15 | 1947-12-18 | A pilot's control column for actuating the ailerons and elevator of aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB637840A (en) |
-
1947
- 1947-12-18 GB GB33448/47A patent/GB637840A/en not_active Expired
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