SU788594A1 - DEVICE MANAGEMENT STABILIZER AIRPLANE - Google Patents

DEVICE MANAGEMENT STABILIZER AIRPLANE

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Publication number
SU788594A1
SU788594A1 SU2820348/23A SU2820348A SU788594A1 SU 788594 A1 SU788594 A1 SU 788594A1 SU 2820348/23 A SU2820348/23 A SU 2820348/23A SU 2820348 A SU2820348 A SU 2820348A SU 788594 A1 SU788594 A1 SU 788594A1
Authority
SU
USSR - Soviet Union
Prior art keywords
input
switches
servo
demodulator
adder
Prior art date
Application number
SU2820348/23A
Other languages
Russian (ru)
Inventor
Л.Р. Львов
Original Assignee
Л.Р. Львов
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Л.Р. Львов filed Critical Л.Р. Львов
Priority to SU2820348/23A priority Critical patent/SU788594A1/en
Application granted granted Critical
Publication of SU788594A1 publication Critical patent/SU788594A1/en

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Abstract

Устройство управления стабилизатором самолета, содержащее ручку управления, соединенную с механизмом загрузки и подключенную через кинематическое звено к сервоприводу, выход которого связан с рулями высоты, снабженными датчиком положения рулей, а также датчик угла атаки, фильтр верхних частот и демодулятор, отличающееся тем, что, с целью повышения надежности работы устройства, в него дополнительно введены источник опорного сигнала, нелинейное звено, два выключателя и сумматор, при этом вход нелинейного звена подключен к датчику угла атаки, а его выходы - ко входу сервопривода и к управляющим входам выключателей, сигнальный вход первого выключателя соединен с источником опорного сигнала, а второго - через демодулятор и фильтр верхних частот - с датчиком положения рулей, выходы выключателей подключены ко входам сумматора, а его выход - ко входу сервопривода.An aircraft stabilizer control device comprising a control knob connected to a loading mechanism and connected via a kinematic link to a servo drive, the output of which is connected to elevators equipped with rudder position sensors, as well as an angle of attack sensor, a high-pass filter and a demodulator, characterized in that in order to improve the reliability of the device, a reference signal source, a nonlinear link, two switches and an adder are added to it, while the nonlinear link input is connected to the angle sensor at Aki, and its outputs - to the input of the servo and to the control inputs of the switches, the signal input of the first switch is connected to the source of the reference signal, and the second through a demodulator and high pass filter - with the rudder position sensor, the outputs of the switches are connected to the inputs of the adder, and its output - to the servo input.

SU2820348/23A 1979-09-28 1979-09-28 DEVICE MANAGEMENT STABILIZER AIRPLANE SU788594A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2820348/23A SU788594A1 (en) 1979-09-28 1979-09-28 DEVICE MANAGEMENT STABILIZER AIRPLANE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2820348/23A SU788594A1 (en) 1979-09-28 1979-09-28 DEVICE MANAGEMENT STABILIZER AIRPLANE

Publications (1)

Publication Number Publication Date
SU788594A1 true SU788594A1 (en) 2005-04-20

Family

ID=60517003

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2820348/23A SU788594A1 (en) 1979-09-28 1979-09-28 DEVICE MANAGEMENT STABILIZER AIRPLANE

Country Status (1)

Country Link
SU (1) SU788594A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2460670C2 (en) * 2007-03-15 2012-09-10 Эрбус Оперейшнс Гмбх Method and device to control shift of movable stabiliser on aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2460670C2 (en) * 2007-03-15 2012-09-10 Эрбус Оперейшнс Гмбх Method and device to control shift of movable stabiliser on aircraft

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