LANDING GEAR FRONT LEG WHEEL TURN CONTROL SYSTEM Russian patent published in 1995 - IPC

Abstract RU 2042575 C1

FIELD: aeronautical engineering. SUBSTANCE: landing gear front leg wheel turn control system has control rod whose one end is hinged to flying vehicle control system through double-arm bell crank, actuating hydraulic cylinder of control surface mechanism connected with one end of feedback coupling rod through bell crank, hydraulic system with pipe lines and distributing electrically-actuated valve, limit switch mechanism and distributing dampening unit. EFFECT: enhanced reliability. 3 dwg

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RU 2 042 575 C1

Authors

Sokolov V.I.

Dates

1995-08-27—Published

1992-07-07—Filed