SU18076A1 - Device for self-compensation of depth rudders or ailerons - Google Patents
Device for self-compensation of depth rudders or aileronsInfo
- Publication number
- SU18076A1 SU18076A1 SU41460A SU41460A SU18076A1 SU 18076 A1 SU18076 A1 SU 18076A1 SU 41460 A SU41460 A SU 41460A SU 41460 A SU41460 A SU 41460A SU 18076 A1 SU18076 A1 SU 18076A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- ailerons
- compensation
- self
- depth
- depth rudders
- Prior art date
Links
Description
При управлении летательными аппаратами , т.-е. при отклонении элеронов или рулей высоты происходит большое давление на ручку пилота. Насто щее изобретение имеет уменьшить давление на ручку пилота.When controlling the aircraft, i.e. when deflecting ailerons or elevators, there is a lot of pressure on the pilot's handle. The present invention has to reduce the pressure on the pilot's handle.
Изобретение видно из прилагаемого при сем схематического чертежа, и состоит в том, что ось вращени одной половины обычной формы рул глубины или элерона сдвинута относительно оси другой половины и расположена в плоскости рул между кромками атаки и обтекани .The invention can be seen from the schematic drawing attached herewith, and consists in the fact that the axis of rotation of one half of the usual shape of the depth or aileron roll is shifted relative to the axis of the other half and is located in the plane of the steering wheel between the attack and flow edges.
Цифрами О-О, 1-Г обозначены оси рулевой Высоты или элеронов 2 и 3,The numbers OO, 1-D designate the axis of the steering height or ailerons 2 and 3,
плоскости рул высот или элеронов, 5-ручка пилота, б-ось вращени , 7 н 9-т ги, 8 и 10-опоры дл закреплени т ги, стрелками 11 и 11 обозначено действие аэродинамической силы.elevator or aileron planes, 5-handle pilot, b-axis of rotation, 7 n 9-ton gi, 8 and 10-pylons for securing thrust, arrows 11 and 11 indicate the effect of aerodynamic force.
Предмет патента.The subject of the patent.
Устройство дл самокомпенсацйи рулей глубины «ли элеронов, отличающеес тем, что ось вращени одной половины обычной формы рул глубины или элерона сдвинута относительно оси другой половины и расположена в плоскости рул между кромками атаки и обтекани . 7A device for self-compensation of aileron depth rudders, characterized in that the axis of rotation of one half of a conventional depth or aileron shape is shifted relative to the axis of the other half and located in the plane of the rudder between the attack and flow edges. 7
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU41460A SU18076A1 (en) | 1929-02-23 | 1929-02-23 | Device for self-compensation of depth rudders or ailerons |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU41460A SU18076A1 (en) | 1929-02-23 | 1929-02-23 | Device for self-compensation of depth rudders or ailerons |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU18076A1 true SU18076A1 (en) | 1930-09-30 |
Family
ID=48337996
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU41460A SU18076A1 (en) | 1929-02-23 | 1929-02-23 | Device for self-compensation of depth rudders or ailerons |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU18076A1 (en) |
-
1929
- 1929-02-23 SU SU41460A patent/SU18076A1/en active
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