SU660357A1 - DRIVE OF BRAKE CONTROL OF WHEELS OF THE AIRCRAFT - Google Patents

DRIVE OF BRAKE CONTROL OF WHEELS OF THE AIRCRAFT

Info

Publication number
SU660357A1
SU660357A1 SU2546986/23A SU2546986A SU660357A1 SU 660357 A1 SU660357 A1 SU 660357A1 SU 2546986/23 A SU2546986/23 A SU 2546986/23A SU 2546986 A SU2546986 A SU 2546986A SU 660357 A1 SU660357 A1 SU 660357A1
Authority
SU
USSR - Soviet Union
Prior art keywords
drive
axis
aircraft
control
wheels
Prior art date
Application number
SU2546986/23A
Other languages
Russian (ru)
Inventor
А.С. Михеев
А.Я. Козырев
Original Assignee
А.С. Михеев
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 А.С. Михеев filed Critical А.С. Михеев
Priority to SU2546986/23A priority Critical patent/SU660357A1/en
Application granted granted Critical
Publication of SU660357A1 publication Critical patent/SU660357A1/en

Links

Abstract

Привод управления тормозами колес летательного аппарата, содержащий рычаг торможения, расположенный на рукоятке управления, кардан и проводку управления с тягами, отличающийся тем, что, с целью повышения надежности и стабильности работы привода путем замены тросовой проводки на жесткую, в него введены основная и дополнительная качалки, связанные между собой промежуточным звеном, ось крепления которого к основной качалке совмещена с осью вращения рукоятки управления, а ось крепления дополнительной качалки к тяге управления совмещена с осью вращения кардана.Drive control wheels brakes of the aircraft, containing the brake lever, located on the control handle, cardan and control wiring with rods, characterized in that, in order to improve the reliability and stability of the drive by replacing the cable wiring to hard, it introduced the main and additional rocking , interconnected by an intermediate link, the axis of attachment of which to the main rocking chair is combined with the axis of rotation of the control handle, and the axis of attachment of the additional rocking chair to the control rod is combined with cardan axis of rotation.

SU2546986/23A 1977-11-25 1977-11-25 DRIVE OF BRAKE CONTROL OF WHEELS OF THE AIRCRAFT SU660357A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2546986/23A SU660357A1 (en) 1977-11-25 1977-11-25 DRIVE OF BRAKE CONTROL OF WHEELS OF THE AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2546986/23A SU660357A1 (en) 1977-11-25 1977-11-25 DRIVE OF BRAKE CONTROL OF WHEELS OF THE AIRCRAFT

Publications (1)

Publication Number Publication Date
SU660357A1 true SU660357A1 (en) 2005-04-27

Family

ID=60520938

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2546986/23A SU660357A1 (en) 1977-11-25 1977-11-25 DRIVE OF BRAKE CONTROL OF WHEELS OF THE AIRCRAFT

Country Status (1)

Country Link
SU (1) SU660357A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2710993C1 (en) * 2019-04-26 2020-01-14 Акционерное общество "Московский вертолетный завод им. М.Л. Миля" Helicopter chassis wheel braking device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2710993C1 (en) * 2019-04-26 2020-01-14 Акционерное общество "Московский вертолетный завод им. М.Л. Миля" Helicopter chassis wheel braking device

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