MANUAL CONTROL SYSTEM OF TRAINER AEROPLANE Russian patent published in 1997 - IPC

Abstract RU 2093419 C1

FIELD: control systems of flying vehicles. SUBSTANCE: manual control system includes control sticks of instructor pilot and student pilot provided in longitudinal control channel and rigidly interconnected; these control sticks are kinematically linked with variable gearing mechanism, elevator hydraulic drive, spring-type loading mechanism and trimming effect mechanism which is electrically connected with trimming buttons found in each control stick. Manual control system is additionally provided with stability and controllability characteristics reprogramming computer, electrohydraulic loading mechanism containing electric drive for shifting the control sticks, force sensors fitted on these sticks and monitoring and control unit whose input is electrically connected with force sensors, trimming buttons and computer of stability and controllability characteristics reprogramming and its output is connected with electrohydraulic drive and trimming effect mechanism; besides that, system is provided with second electrohydraulic drive which is electrically connected with reprogramming computer and is kinematically linked with spring centering its outlet rod and differentiating bell crank arranged between variable gearing mechanism and elevator hydraulic drive. Control stick of instructor pilot is provided with two selector switches having two make-before-break contact pairs each. One selector switch is connected with force sensor and trimming button of trainer pilot control stick; second selector switch is connected with hydraulic valves of respective electrohydraulic drives and its own trimming button. EFFECT: extended functional capabilities. 2 cl, 2 dwg

Similar patents RU2093419C1

Title Year Author Number
AIRCRAFT MANUAL CONTROL SYSTEM 1994
RU2089447C1
LANDING GEAR FRONT LEG WHEEL TURN CONTROL SYSTEM 1992
  • Sokolov V.I.
RU2042575C1
COMPLEX NAVIGATIONAL SYSTEM 1992
  • Eremin A.V.
  • Kukolevskij O.I.
  • Budnik V.K.
  • Borisov I.V.
RU2077028C1
METHOD OF CONTROL OF AIRCRAFT 2003
  • Krjukov S.P.
  • Kazakov V.V.
  • Golovanov N.A.
  • Kuznetsov A.G.
  • Kalik A.A.
  • Demchenko O.F.
  • Popovich K.F.
  • Shkolin V.P.
  • Mitrichenko A.N.
  • Kodola V.G.
RU2235042C1
LIGHT MULTI-MISSION AIRCRAFT 2003
  • Demchenko O.F.
  • Popovich K.F.
  • Shkolin V.P.
  • Mitrichenko A.N.
  • Krjukov S.P.
  • Kazakov V.V.
  • Golovanov N.A.
  • Kuznetsov A.G.
  • Kodola V.G.
RU2235044C1
AIRCRAFT CONTROL SYSTEM 2003
  • Krjukov S.P.
  • Kazakov V.V.
  • Golovanov N.A.
  • Kuznetsov A.G.
  • Kalik A.A.
  • Kirjushkin A.P.
  • Demchenko O.F.
  • Popovich K.F.
  • Shkolin V.P.
  • Mitrichenko A.N.
  • Kodola V.G.
RU2235043C1
INTEGRATED ON-BOARD EQUIPMENT COMPLEX FOR LIGHT COMBAT TRAINER 2002
  • Efanov A.G.
  • Demchenko O.F.
  • Pjaternev S.V.
  • Popovich K.F.
  • Shkolin V.P.
  • Nikitin V.N.
  • Sorokin V.F.
  • Kodola V.G.
RU2203200C1
AIRCRAFT TRAINING COMPLEX 2004
  • Demchenko O.F.
  • Dolzhenkov N.N.
  • Popovich K.F.
  • Shkolin V.P.
  • Gurtovoj A.I.
  • Sorokin V.F.
  • Kodola V.G.
RU2250511C1
INTEGRATED COMPLEX OF ON-BOARD EQUIPMENT WITH MULTIPLEX INFORMATION EXCHANGE SYSTEM 2001
  • Demchenko O.F.
  • Dolzhenkov N.N.
  • Popovich K.F.
  • Shkolin V.P.
  • Kodola V.G.
  • Nikitin V.N.
  • Sorokin V.F.
RU2174485C1
AIRCRAFT SEMI-AUTOMATIC LONGITUDINAL CONTROL SYSTEM 2006
  • Bondarets Anatolij Jakovlevich
  • Nikitin Aleksandr Igorevich
RU2316450C1

RU 2 093 419 C1

Authors

Dates

1997-10-20Published

1993-05-25Filed