SU1144311A1 - THE DEVICE OF MANAGEMENT OF POWER INSTALLATION OF THE PLANE WITH VERTICAL TAKEOFF AND LANDING - Google Patents

THE DEVICE OF MANAGEMENT OF POWER INSTALLATION OF THE PLANE WITH VERTICAL TAKEOFF AND LANDING

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Publication number
SU1144311A1
SU1144311A1 SU3706553/23A SU3706553A SU1144311A1 SU 1144311 A1 SU1144311 A1 SU 1144311A1 SU 3706553/23 A SU3706553/23 A SU 3706553/23A SU 3706553 A SU3706553 A SU 3706553A SU 1144311 A1 SU1144311 A1 SU 1144311A1
Authority
SU
USSR - Soviet Union
Prior art keywords
output
adder
input
unit
speed sensor
Prior art date
Application number
SU3706553/23A
Other languages
Russian (ru)
Inventor
О.В. Шолохов
Р.Н. Новиков
В.А. Шиянов
Original Assignee
О.В. Шолохов
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 О.В. Шолохов filed Critical О.В. Шолохов
Priority to SU3706553/23A priority Critical patent/SU1144311A1/en
Application granted granted Critical
Publication of SU1144311A1 publication Critical patent/SU1144311A1/en

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  • Control Of Multiple Motors (AREA)

Abstract

Устройство управления силовой установкой самолета с вертикальным взлетом и посадкой, включающей подъемные и подъемно-маршевые двигатели, содержащее ручку управления двигателями, связанную с задатчиком скоростей вращения, первый выход которого связан с первым входом первого сумматора, а второй выход - с первым входом второго сумматора, датчик скорости вращения подъемного двигателя, выход которого соединен с вторым входом первого сумматора, датчик скорости вращения подъемно-маршевого двигателя, выход которого соединен с вторым входом второго сумматора, выход первого сумматора соединен с входом топливодозирующего блока подъемного двигателя, а выход второго сумматора - с входом топливодозирующего блока подъемно-маршевого двигателя, отличающееся тем, что, с целью повышения точности синхронизации двигателей на переходных режимах, в нее введены два дифференциатора, причем вход первого дифференциатора соединен с выходом датчика скорости вращения подъемного двигателя, вход второго дифференциатора соединен с выходом датчика скорости вращения подъемно-маршевого двигателя, а выходы дифференциаторов соединены с третьим и четвертым входами первого сумматора.The control unit of the power plant of the aircraft with vertical takeoff and landing, including lifting and mainboard engines, contains an engine control knob associated with the unit of rotational speeds, the first output of which is connected to the first input of the first adder, and the second output - to the first input of the second adder, the speed sensor of the lift motor, the output of which is connected to the second input of the first adder, the speed sensor of the lift-main engine, the output of which is connected to the second input to The second adder, the output of the first adder is connected to the input of the lifting unit's toplide-dosing unit, and the output of the second adder is connected to the entrance of the top-diving throttle-sustainer unit, characterized in that, in order to improve the synchronization accuracy of the motors in transient conditions, the input of the first differentiator is connected to the output of the rotational speed sensor of the lifting motor; the input of the second differentiator is connected to the output of the rotational speed sensor of the main propulsion engine And differentiators are connected to the outputs of the third and fourth inputs of the first adder.

SU3706553/23A 1983-11-29 1983-11-29 THE DEVICE OF MANAGEMENT OF POWER INSTALLATION OF THE PLANE WITH VERTICAL TAKEOFF AND LANDING SU1144311A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3706553/23A SU1144311A1 (en) 1983-11-29 1983-11-29 THE DEVICE OF MANAGEMENT OF POWER INSTALLATION OF THE PLANE WITH VERTICAL TAKEOFF AND LANDING

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3706553/23A SU1144311A1 (en) 1983-11-29 1983-11-29 THE DEVICE OF MANAGEMENT OF POWER INSTALLATION OF THE PLANE WITH VERTICAL TAKEOFF AND LANDING

Publications (1)

Publication Number Publication Date
SU1144311A1 true SU1144311A1 (en) 2004-08-10

Family

ID=60539010

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3706553/23A SU1144311A1 (en) 1983-11-29 1983-11-29 THE DEVICE OF MANAGEMENT OF POWER INSTALLATION OF THE PLANE WITH VERTICAL TAKEOFF AND LANDING

Country Status (1)

Country Link
SU (1) SU1144311A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2672440C2 (en) * 2014-04-15 2018-11-14 Сафран Эйркрафт Энджинз Method for synchronising aircraft engines with dual intermediate state

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2672440C2 (en) * 2014-04-15 2018-11-14 Сафран Эйркрафт Энджинз Method for synchronising aircraft engines with dual intermediate state

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