SU739859A1 - BRAKING SYSTEM OF THE PLANE - Google Patents

BRAKING SYSTEM OF THE PLANE

Info

Publication number
SU739859A1
SU739859A1 SU2705235/23A SU2705235A SU739859A1 SU 739859 A1 SU739859 A1 SU 739859A1 SU 2705235/23 A SU2705235/23 A SU 2705235/23A SU 2705235 A SU2705235 A SU 2705235A SU 739859 A1 SU739859 A1 SU 739859A1
Authority
SU
USSR - Soviet Union
Prior art keywords
wheel
aircraft
electro
braking
speed
Prior art date
Application number
SU2705235/23A
Other languages
Russian (ru)
Inventor
О.А. Артемов
Original Assignee
О.А. Артемов
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.А. Артемов filed Critical О.А. Артемов
Priority to SU2705235/23A priority Critical patent/SU739859A1/en
Application granted granted Critical
Publication of SU739859A1 publication Critical patent/SU739859A1/en

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  • Regulating Braking Force (AREA)

Abstract

Система торможения самолета, содержащая соединенные с колесом тормоз, электрогидравлический клапан, вычислитель скорости вращения колеса, датчики скорости и ускорения самолета, отличающаяся тем, что, с целью усиления тормозного эффекта, она имеет блок задаваемого скольжения, датчик нагрузки и самотормозящий редуктор с вращающим приводом, при этом датчик нагрузки через электрогидравлический клапан связан с тормозом, а выходы датчиков ускорения и скорости самолета и блока задаваемого скольжения связаны с входами вычислителя скорости вращения колеса, выход которого подключен к входу вращающего привода.The braking system of the aircraft, which contains a brake connected to the wheel, an electro-hydraulic valve, a calculator of the wheel rotation speed, an airplane speed and acceleration sensors, characterized in that, in order to enhance the braking effect, it has a settable slip unit, a load sensor and a self-braking gearbox with a rotating drive, at the same time, the load sensor is connected to the brake via an electro-hydraulic valve, and the outputs of the acceleration sensors and speeds of the aircraft and the settable slip unit are connected to the inputs of the speed calculator in ascheniya wheel whose output is connected to the input drive torque.

SU2705235/23A 1978-12-26 1978-12-26 BRAKING SYSTEM OF THE PLANE SU739859A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2705235/23A SU739859A1 (en) 1978-12-26 1978-12-26 BRAKING SYSTEM OF THE PLANE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2705235/23A SU739859A1 (en) 1978-12-26 1978-12-26 BRAKING SYSTEM OF THE PLANE

Publications (1)

Publication Number Publication Date
SU739859A1 true SU739859A1 (en) 2004-11-10

Family

ID=60521297

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2705235/23A SU739859A1 (en) 1978-12-26 1978-12-26 BRAKING SYSTEM OF THE PLANE

Country Status (1)

Country Link
SU (1) SU739859A1 (en)

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