AIRCRAFT MANUAL CONTROL SYSTEM Russian patent published in 1997 - IPC

Abstract RU 2089447 C1

FIELD: flying vehicle control systems. SUBSTANCE: mechanical linkage connecting the electric drive with trimmer contains bell crank whose one end is articulated on fixed surface of wing or tail unit and other end is made in form of adjusting mechanism engageable with trimmer rod which is adjustable in length. EFFECT: extended functional capabilities of aircraft manual control system; change of loading characteristics of control levers. 3 dwg

Similar patents RU2089447C1

Title Year Author Number
MANUAL CONTROL SYSTEM OF TRAINER AEROPLANE 1993
RU2093419C1
LANDING GEAR FRONT LEG WHEEL TURN CONTROL SYSTEM 1992
  • Sokolov V.I.
RU2042575C1
AIRCRAFT STEERING COLUMN 2007
  • Aleksandrov Viktor Konstantinovich
RU2356793C1
AEROBATIC PLANE 1992
  • Zhidovetskij K.M.
RU2005662C1
THREE-DIMENSIONAL BOTTOM STATION FOR MANUAL CONTROL OF AIRCRAFT 2014
  • Jakovlev Vladimir Vasilevich
RU2579250C2
AIRPLANE CONTROL SYSTEM 0
  • Zhidovetskij Kazimir Mikhajlovich
SU1762751A3
THREE-CORDINATE MANUAL AIRCRAFT CONTROL STATION 2016
  • Yakovlev Vladimir Vasilevich
RU2647220C2
LANDING GEAR UP LOCAL 1992
  • Sokolov V.I.
RU2076827C1
ULTRA LOW MASS AIRPLANE 2005
  • Kljujkin Stanislav Anatol'Evich
  • Bekhter Jurij Anatol'Evich
  • Bessmertnyj Vladimir Aleksandrovich
  • Zinchenko Grigorij Ivanovich
RU2336200C2
THREE-COORDINATE POST FOR DOUBLED MANUAL AIRCRAFT CONTROL 2014
  • Jakovlev Vladimir Vasilevich
RU2579417C2

RU 2 089 447 C1

Authors

Dates

1997-09-10Published

1994-09-26Filed