GB130430A - Improvements in or relating to Control Mechanism for Aircraft and other purposes. - Google Patents
Improvements in or relating to Control Mechanism for Aircraft and other purposes.Info
- Publication number
- GB130430A GB130430A GB324618A GB324618A GB130430A GB 130430 A GB130430 A GB 130430A GB 324618 A GB324618 A GB 324618A GB 324618 A GB324618 A GB 324618A GB 130430 A GB130430 A GB 130430A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- wheel
- lever
- controls
- aircraft
- 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)
- Mechanical Operated Clutches (AREA)
- Toys (AREA)
- Mechanical Control Devices (AREA)
Abstract
130,430. White, C. Grahame-, and Sidgwick, K. I. Feb. 23, 1918. Steering and balancing.-In a dual control gear for aircraft and other purposes, two wheels G, H, corresponding to the two controls, are loosely mounted on a shaft A at opposite sides of a sleeve B fixed to the shaft, and either wheel may be coupled to the sleeve by pins C, which are normally pressed into engagement with holes in the wheel G by springs D, but may be withdrawn therefrom and moved into engagement with holes in the wheel H, by means of a sliding member E connected to the pins by arms F. The member E is actuated by connexions J, K to a spring L, which may be extended by means of a lever M<1>, so as to overcome the springs D. A lever M<1> is provided adjacent the pilot, and a similar lever is arranged on the same shaft M<2> adjacent the observer, so that either can take over the control, and the shaft A is connected to the elevator controls, similar clutch devices being provided for the aileron and rudder controls, all the clutches being operated from the same levers M<1>. In a modification, the spring L is arranged within the shaft A. Worm gear and hand-wheels may replace the levers M<1>.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB324618A GB130430A (en) | 1918-02-23 | 1918-02-23 | Improvements in or relating to Control Mechanism for Aircraft and other purposes. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB324618A GB130430A (en) | 1918-02-23 | 1918-02-23 | Improvements in or relating to Control Mechanism for Aircraft and other purposes. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB130430A true GB130430A (en) | 1919-08-07 |
Family
ID=32341310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB324618A Expired GB130430A (en) | 1918-02-23 | 1918-02-23 | Improvements in or relating to Control Mechanism for Aircraft and other purposes. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB130430A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2346879A1 (en) * | 1973-09-18 | 1975-03-27 | Waechtler Maximilian Dr | Multichannel direction finder - reception channels are designed for greatest possible dynamic range |
-
1918
- 1918-02-23 GB GB324618A patent/GB130430A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2346879A1 (en) * | 1973-09-18 | 1975-03-27 | Waechtler Maximilian Dr | Multichannel direction finder - reception channels are designed for greatest possible dynamic range |
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