SU474208A1 - DEVICE FOR MANUAL CONTROL OF AIRPLANE - Google Patents

DEVICE FOR MANUAL CONTROL OF AIRPLANE

Info

Publication number
SU474208A1
SU474208A1 SU1981464/23A SU1981464A SU474208A1 SU 474208 A1 SU474208 A1 SU 474208A1 SU 1981464/23 A SU1981464/23 A SU 1981464/23A SU 1981464 A SU1981464 A SU 1981464A SU 474208 A1 SU474208 A1 SU 474208A1
Authority
SU
USSR - Soviet Union
Prior art keywords
lever
control
manual control
airplane
gear ratio
Prior art date
Application number
SU1981464/23A
Other languages
Russian (ru)
Inventor
В.А. Барденков
В.В. Смирнов
Original Assignee
В.А. Барденков
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 В.А. Барденков filed Critical В.А. Барденков
Priority to SU1981464/23A priority Critical patent/SU474208A1/en
Application granted granted Critical
Publication of SU474208A1 publication Critical patent/SU474208A1/en

Links

Abstract

Устройство для ручного управления самолетом, включающее рычаг управления, механическую проводку, соединяющую рычаг управления с гидроусилителем, связанным с управляющей поверхностью, механизм загрузки рычага управления, создающий усилие на рычаге в зависимости от режимов полета, и автомат изменения передаточного числа, отличающееся тем, что, с целью повышения надежности, упрощение конструкции и эксплуатации, автомат изменения передаточного числа выполнен в виде упругого элемента, например пружины, включенного в проводку между рычагом управления и механизмом загрузки.A device for manual control of the aircraft, including a control lever, mechanical wiring connecting the control lever with a hydraulic booster connected to the control surface, a mechanism for loading the control lever that generates a force on the lever depending on flight modes, and an automatic gear ratio change, characterized in that in order to increase reliability, simplify the design and operation, the automatic change of the gear ratio is made in the form of an elastic element, such as a spring, included in the wiring between the lever management and loading mechanism.

SU1981464/23A 1973-12-27 1973-12-27 DEVICE FOR MANUAL CONTROL OF AIRPLANE SU474208A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1981464/23A SU474208A1 (en) 1973-12-27 1973-12-27 DEVICE FOR MANUAL CONTROL OF AIRPLANE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1981464/23A SU474208A1 (en) 1973-12-27 1973-12-27 DEVICE FOR MANUAL CONTROL OF AIRPLANE

Publications (1)

Publication Number Publication Date
SU474208A1 true SU474208A1 (en) 2004-11-20

Family

ID=60520619

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1981464/23A SU474208A1 (en) 1973-12-27 1973-12-27 DEVICE FOR MANUAL CONTROL OF AIRPLANE

Country Status (1)

Country Link
SU (1) SU474208A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2505456C1 (en) * 2012-09-05 2014-01-27 Николай Евгеньевич Староверов Aircraft variable manual control (versions)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2505456C1 (en) * 2012-09-05 2014-01-27 Николай Евгеньевич Староверов Aircraft variable manual control (versions)

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