RU93008976A - DEVICE FOR CONNECTING A SENSOR'S SHAFT WITH A ROTARY ELEMENT OF EXECUTIVE MECHANISM - Google Patents

DEVICE FOR CONNECTING A SENSOR'S SHAFT WITH A ROTARY ELEMENT OF EXECUTIVE MECHANISM

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Publication number
RU93008976A
RU93008976A RU93008976/23A RU93008976A RU93008976A RU 93008976 A RU93008976 A RU 93008976A RU 93008976/23 A RU93008976/23 A RU 93008976/23A RU 93008976 A RU93008976 A RU 93008976A RU 93008976 A RU93008976 A RU 93008976A
Authority
RU
Russia
Prior art keywords
rotary element
sensor
shaft
executive mechanism
sensor shaft
Prior art date
Application number
RU93008976/23A
Other languages
Russian (ru)
Other versions
RU2068798C1 (en
Inventor
Н.В. Мухин
Е.И. Смирнов
Original Assignee
Авиационный комплекс им.С.В.Ильюшина
Filing date
Publication date
Application filed by Авиационный комплекс им.С.В.Ильюшина filed Critical Авиационный комплекс им.С.В.Ильюшина
Priority to RU93008976A priority Critical patent/RU2068798C1/en
Priority claimed from RU93008976A external-priority patent/RU2068798C1/en
Publication of RU93008976A publication Critical patent/RU93008976A/en
Application granted granted Critical
Publication of RU2068798C1 publication Critical patent/RU2068798C1/en

Links

Claims (1)

Изобретение позволяет повысить надежность работы устройства. Это обеспечивается повышением точности передаваемого сигнала с поворотного элемента исполнительного механизма на вал датчика системы управления опорой шасси самолета. Для этого механизм передачи движения от поворотного элемента к валу датчика выполнен в виде упругой крестообразной пластины, концы которой попарно отогнуты в противоположные стороны и направлены навстречу один другому.The invention improves the reliability of the device. This is achieved by increasing the accuracy of the transmitted signal from the rotary element of the actuator to the sensor shaft of the aircraft landing gear control system. For this purpose, the mechanism for transferring motion from the rotating element to the sensor shaft is made in the form of an elastic cruciform plate, the ends of which are bent in pairs in opposite directions and directed towards each other.
RU93008976A 1993-02-17 1993-02-17 Device for connection of sensor shaft with swivel member of actuating mechanism RU2068798C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93008976A RU2068798C1 (en) 1993-02-17 1993-02-17 Device for connection of sensor shaft with swivel member of actuating mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93008976A RU2068798C1 (en) 1993-02-17 1993-02-17 Device for connection of sensor shaft with swivel member of actuating mechanism

Publications (2)

Publication Number Publication Date
RU93008976A true RU93008976A (en) 1995-01-09
RU2068798C1 RU2068798C1 (en) 1996-11-10

Family

ID=20137447

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93008976A RU2068798C1 (en) 1993-02-17 1993-02-17 Device for connection of sensor shaft with swivel member of actuating mechanism

Country Status (1)

Country Link
RU (1) RU2068798C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005059369B4 (en) 2005-12-13 2012-06-14 Airbus Operations Gmbh Method and device for automatically relieving a high-lift surface system, in particular a landing flap system, of an aircraft

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