AIRCRAFT CONTROL MULTICHANNEL COMPONENT Russian patent published in 2015 - IPC B64C13/06 

Abstract RU 2559188 C1

FIELD: aircraft engineering.

SUBSTANCE: proposed component consists of the support arranged at bank control actuator support whereat secured is the position adjustment master. Two-axis spinning mechanism is fitted at the latter to read off the signals to be converted into control effects in heading and pitching, the handle being coupled therewith. Two-axis spinning mechanism is composed of rectangular frame whereto connected is the handle lower adjustment element intended for setting the different distances from wrist joint centre to axis of operator hand handle grip axis. Handle is provided with three push-buttons at side surface. Note here that handle top surface has the propeller common pitch control slide.

EFFECT: higher efficiency and safety.

8 cl, 10 dwg, 1 tbl

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RU 2 559 188 C1

Authors

Chuntul Aleksandr Vasil'Evich

Taratonov Il'Ja Aleksandrovich

Dates

2015-08-10Published

2014-03-25Filed