GB130535A - Improvements in or relating to Power-controls for Aeronautical Machines and the like. - Google Patents
Improvements in or relating to Power-controls for Aeronautical Machines and the like.Info
- Publication number
- GB130535A GB130535A GB2029018A GB2029018A GB130535A GB 130535 A GB130535 A GB 130535A GB 2029018 A GB2029018 A GB 2029018A GB 2029018 A GB2029018 A GB 2029018A GB 130535 A GB130535 A GB 130535A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheel
- power
- arm
- carries
- drum
- 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
- B64C13/24—Transmitting means
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangement And Mounting Of Devices That Control Transmission Of Motive Force (AREA)
Abstract
130,535. Greenly, A. J. July 31, 1918. Relay or power apparatus.-In power control mechanism, a steering-handle, such as the wheel A, drives with lost motion a co-axial drum C, the relative movement causing a fluid pressure valve N to control one of the ports 0' corresponding to the direction in which the wheel has been moved. The drum C, which carries cables D for direct manual control, has an arm E slotted at E<1> to receive one end H<1> of a bell-crank lever pivoted on a pin G' which also .carries two arms H<3>; the other end H<2> of the lever is adjustably secured at J and locked at H<4> to the arms H<3> which operate the valve N. The wheel A carries the pin G' and also a guide-pin L extending between the arms H<3>. The arm E extends between two spring buffers F carried by the wheel A, which also carries a screw R passing through a slot in the arm E to lock the wheel A and drum C together for direct manual control. Should the pilot release the wheel during power operation, the buffers will return the arm E and valve N to a central position and the power will be cut off. The wheel may be mounted on the parts S or S<1> of a control lever rocking about two diameters at right-angles and controlling four power branches T, while this additional control can be rendered inoperative by a locking-ring U. The wheel A may rotate about a vertical axis, while the slot E<1> may be provided in the drum C, which may be replaced by one member in a train of gearing used instead of the cables D.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2029018A GB130535A (en) | 1918-07-31 | 1918-07-31 | Improvements in or relating to Power-controls for Aeronautical Machines and the like. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2029018A GB130535A (en) | 1918-07-31 | 1918-07-31 | Improvements in or relating to Power-controls for Aeronautical Machines and the like. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB130535A true GB130535A (en) | 1919-07-31 |
Family
ID=32348422
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2029018A Expired GB130535A (en) | 1918-07-31 | 1918-07-31 | Improvements in or relating to Power-controls for Aeronautical Machines and the like. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB130535A (en) |
-
1918
- 1918-07-31 GB GB2029018A patent/GB130535A/en not_active Expired
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