SU1338264A1 - DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER - Google Patents

DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER

Info

Publication number
SU1338264A1
SU1338264A1 SU3962577/23A SU3962577A SU1338264A1 SU 1338264 A1 SU1338264 A1 SU 1338264A1 SU 3962577/23 A SU3962577/23 A SU 3962577/23A SU 3962577 A SU3962577 A SU 3962577A SU 1338264 A1 SU1338264 A1 SU 1338264A1
Authority
SU
USSR - Soviet Union
Prior art keywords
axes
sensors
rocking chair
main
control system
Prior art date
Application number
SU3962577/23A
Other languages
Russian (ru)
Inventor
В.И. Долгов
Original Assignee
В.И. Долгов
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.И. Долгов filed Critical В.И. Долгов
Priority to SU3962577/23A priority Critical patent/SU1338264A1/en
Application granted granted Critical
Publication of SU1338264A1 publication Critical patent/SU1338264A1/en

Links

Abstract

1. Устройство сигнализации положения стабилизатора летательного аппарата, содержащее основную качалку, соединенную с осями датчиков системы управления, закрепленных на кронштейне, одно плечо которой кинематически связано со стабилизатором, а другое через тягу и дополнительную качалку - с другими датчиками системы управления, закрепленными на этом же кронштейне, отличающееся тем, что, с целью уменьшения габаритов и массы, а также повышения технологичности обслуживания, кронштейн выполнен П-образным, а датчики установлены на его параллельных сторонах попарно, а также соосно между собой и осями вращения качалок, размещенных между ними, причем основная качалка снабжена механизмами регулировки углов установки осей датчиков, размещенными по внутренней полости основной качалки и взаимодействующими с осями соответствующих датчиков.2. Устройство по п.1, отличающееся тем, что механизмы регулировки углов установки осей датчиков системы управления выполнены в виде двух независимых червячных передач, расположенных вдоль оси вращения основной качалки и направленных, перпендикулярно к ней, при этом оси червячных колес связаны с осью основной качалки посредством фрикционной передачи.1. The device for signaling the position of the stabilizer of the aircraft, containing the main rocking chair connected to the axes of the sensors of the control system mounted on a bracket, one arm of which is kinematically connected to the stabilizer, and the other through traction and an additional rocking chair to other sensors of the control system attached to the same bracket, characterized in that, in order to reduce dimensions and weight, as well as improve the manufacturability of the service, the bracket is U-shaped, and the sensors are installed on its parallel The two sides are in pairs, as well as coaxially between themselves and the axes of rotation of the rockers placed between them, the main rocker being equipped with mechanisms for adjusting the angles of the sensor axes located along the internal cavity of the main rocker and interacting with the axes of the respective sensors.2. The device according to claim 1, characterized in that the mechanisms for adjusting the angles of installation of the axes of the sensors of the control system are made in the form of two independent worm gears located along the axis of rotation of the main rocking chair and directed perpendicular to it, while the axes of the worm wheels are connected to the axis of the main rocking chair by friction transmission.

SU3962577/23A 1985-10-14 1985-10-14 DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER SU1338264A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3962577/23A SU1338264A1 (en) 1985-10-14 1985-10-14 DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3962577/23A SU1338264A1 (en) 1985-10-14 1985-10-14 DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER

Publications (1)

Publication Number Publication Date
SU1338264A1 true SU1338264A1 (en) 2005-02-20

Family

ID=60534884

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3962577/23A SU1338264A1 (en) 1985-10-14 1985-10-14 DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER

Country Status (1)

Country Link
SU (1) SU1338264A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2673755C1 (en) * 2015-10-21 2018-11-29 Сафран Электроникс Энд Дифенс Aircraft flight control device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2673755C1 (en) * 2015-10-21 2018-11-29 Сафран Электроникс Энд Дифенс Aircraft flight control device

Similar Documents

Publication Publication Date Title
FR2828167B1 (en) DEVICE FOR HANGING AN ENGINE ON AN AIRCRAFT
MX150053A (en) IMPROVEMENTS IN CONTROL SYSTEM FOR LOCOMOTIVE WITH MULTIPLE UNIT
EP0319177A3 (en) Constant natural frequency, mechanical spring seat suspension
KR870000522A (en) Spring pendulum type copper reducer
SU1338264A1 (en) DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER
SE8007701L (en) DEVICE Vibration Seat Device
ES295825U (en) Elastic suspension with high angular rigidity.
IT8605175A0 (en) FREE WHEEL DEVICE DISENGAGEABLE IN THE DIRECTION OF MOTION TRANSMISSION.
FR2547079B1 (en) ADJUSTABLE VEHICLE SEAT POWERED BY BOWDEN CONTROLS
SE8107011L (en) VIBRATIONSDEMPARE
SU1230092A1 (en) DEVICE FOR REMOTE CONTROL OF THE STEERING SURFACES OF THE AIRCRAFT
ES8206801A1 (en) Cam control.
SE9001716L (en) WHEEL SUSPENSION BY VEHICLE
DE3854318D1 (en) Seat device.
SE7906787L (en) BIKE VEHICLE WITH DRIVING DEVICE IN BOGGI
BR8707995A (en) DOSING CONTROL VALVE WITH POLARIZED CONTROL PISTON BY SPRING
SU1369166A1 (en) AIRPLANE ENGINE MANAGEMENT SYSTEM
SU1338265A1 (en) DEVICE FOR DISCONNECTING A STEERING MACHINE
SU592877A1 (en) Accompanying shaft wing actuating device
FR2581207B3 (en) VEHICLE SPOTLIGHT ADJUSTMENT CONTROL DEVICE
KR880010868A (en) Chamfering device of gear teeth
UA8160A1 (en) Boiler support of railway tank
SU1074002A1 (en) DEVICE FOR DISCONNECTING THE EXECUTIVE MECHANISM FROM THE MECHANICAL WIRING OF THE MANAGEMENT OF THE AIRCRAFT
JPS6457319A (en) Solar light reflecting device
IT1195862B (en) SIGNALING AND SUCCESSNESS SYSTEM FOR THE SPACING OF THE TRAINS AND FOR THE ADJUSTMENT OF THE TRAVEL OF THEMSELVES, ABSOLUTELY INSENSITIVE TO THE INTERFERENCES OF THE ELECTRONIC TRACTION DRIVES