SU756760A1 - DEVICE FOR MANAGING THE SPEED OF THE AIRCRAFT - Google Patents
DEVICE FOR MANAGING THE SPEED OF THE AIRCRAFTInfo
- Publication number
- SU756760A1 SU756760A1 SU2722475/23A SU2722475A SU756760A1 SU 756760 A1 SU756760 A1 SU 756760A1 SU 2722475/23 A SU2722475/23 A SU 2722475/23A SU 2722475 A SU2722475 A SU 2722475A SU 756760 A1 SU756760 A1 SU 756760A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- unit
- speed
- sensor
- engine throttle
- angle
- Prior art date
Links
Landscapes
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
Устройство для управления скоростью летательного аппарата, содержащее датчики угла тангажа и атаки, руль высоты и тормозные щитки с исполнительными приводами, входы которых соединены с выходами переключателя, а также дроссель двигателя с исполнительным приводом, первый вход которого соединен с рукой управления скоростью полета, а второй через блок усилителей - с датчиком скорости полета, отличающееся тем, что, с целью повышения точности и быстродействия в него введены датчик вертикальной перегрузки, блок изодрома, блок определения угла траектории, входы которого соединены с датчиками угла тангажа и угла атаки, а выход через блок усилителей - с исполнительным приводом дросселя двигателя, последовательно соединенные блок нелинейности, вход которого соединен с датчиком угла атаки и блок умножения, другой вход которого соединен с датчиком вертикальной перегрузки, а выход через блок усилителей - с исполнительным приводом дросселя двигателя, а также связанный с дросселем двигателя датчик отклонения дросселя, выход которого через блок изодрома соединен со входом переключателя.A device for controlling the speed of an aircraft, comprising pitch and attack sensors, an elevator and brake flaps with executive drives, the inputs of which are connected to the switch outputs, as well as an engine throttle with an executive drive, the first input of which is connected to the speed control hand, and the second through an amplifier unit - with a flight speed sensor, characterized in that, in order to increase accuracy and speed, a vertical overload sensor, an isodrome unit, an angle detection unit are introduced into it trajectories, the inputs of which are connected to the sensors of pitch angle and angle of attack, and the output through the amplifier unit - with the engine throttle actuator, are connected in series to the nonlinearity unit, the input of which is connected to the angle of attack sensor and the multiplication unit, the other input of which is connected to the vertical overload sensor, and the output through the amplifier unit - with the executive drive of the engine throttle, as well as the throttle deflection sensor connected to the engine throttle, the output of which is connected to the switch via the isodrome unit for
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU2722475/23A SU756760A1 (en) | 1979-02-06 | 1979-02-06 | DEVICE FOR MANAGING THE SPEED OF THE AIRCRAFT |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU2722475/23A SU756760A1 (en) | 1979-02-06 | 1979-02-06 | DEVICE FOR MANAGING THE SPEED OF THE AIRCRAFT |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU756760A1 true SU756760A1 (en) | 2004-09-27 |
Family
ID=60523300
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU2722475/23A SU756760A1 (en) | 1979-02-06 | 1979-02-06 | DEVICE FOR MANAGING THE SPEED OF THE AIRCRAFT |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU756760A1 (en) |
-
1979
- 1979-02-06 SU SU2722475/23A patent/SU756760A1/en active
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