DYNAMIC STAND Russian patent published in 2006 - IPC G09B9/08 

Abstract RU 2285959 C2

FIELD: automatic adjustment technologies, namely, a dynamic stand - aviation training machine, working as part of complex for semi-natural modeling of flight conditions during training of airplane crews.

SUBSTANCE: dynamic stand contains a platform, carrying useful load, hydraulic power source and hydraulic drives, each one of which has electric control input and consists of serially connected sensitive element, adder, power amplifier, hydraulic amplifier and force hydraulic cylinder. Electric control input is connected to second input of adder, output of hydraulic power source is connected to second input of hydraulic amplifier, while input of sensitive element is connected to platform. Additionally provided are computing device, commutation device, emergency electric power source and, connected serially, device for controlling position of hydraulic cylinders and device for locking the platform. In each hydraulic drive between adder and power amplifier a controllable key is mounted, controlling input of which is connected to electric drive of emergency control, while second input is connected to output of commutation device, matching the hydraulic drive. Controlling input of commutation device is connected to output of device for controlling position of hydraulic cylinders, inputs, in accordance to number of hydraulic cylinders - to outputs of computing device and additionally one input - to output of device for platform locking. Controlling input of platform locking device is connected to electric emergency control input. Output of sensitive element of each hydraulic drive is connected to appropriate inputs of device for controlling position of hydraulic cylinders and computing device, while one additional input of computing device is connected to output of emergency electric power source.

EFFECT: increased safety of crew in training.

2 dwg

Similar patents RU2285959C2

Title Year Author Number
DYNAMIC MULTI-LEVEL STAND 2006
  • Pinishin Vladimir Nikolaevich
  • Shvetsov Petr Evgen'Evich
RU2321073C1
DYNAMIC MULTI-LEVEL STAND 2004
  • Adesskij L.K.
  • Novoselov B.V.
  • Smirnov B.A.
  • Fedorov V.S.
  • Timakov V.M.
  • Pinishin V.N.
RU2259597C1
DYNAMIC AIRCRAFT SIMULATOR BENCH 2011
  • Timakov Vladimir Mikhajlovich
  • Proshkin Viktor Nikolaevich
  • Proshin Ivan Aleksandrovich
  • Magomedova Madina Asadullaevna
RU2486600C1
DYNAMIC MULTIPLE-STAGE BOARD 1996
  • Zhukov D.A.
  • Smirnov B.A.
  • Timakov V.M.
  • Fedorov V.S.
RU2129305C1
FLIGHT SIMULATOR 2009
  • Pinishin Vladimir Nikolaevich
  • Pinishina Lidija Nikolaevna
RU2398286C1
POSITIVE CONTROL HYDRAULIC DRIVE 2006
  • Grigor'Ev Vladimir Vasil'Evich
  • Kornakovskij Aleksandr Evgen'Evich
  • Petrov Jurij Arkad'Evich
  • Samokhin Aleksandr Petrovich
  • Shulakov Valentin Ivanovich
RU2322618C1
AIRCRAFT HYDRAULIC SYSTEM 2010
  • Krivoj Sergej Grigor'Evich
  • Panin Sergej Anatol'Evich
  • Kubasov Aleksej Viktorovich
  • Pimenov Aleksandr Viktorovich
RU2455197C1
MOVING SYSTEM OF VEHICLE SIMULATOR 1990
  • Tikhomirov B.S.
  • Osipov M.V.
  • Proshkin V.N.
SU1828295A1
DEVICE FOR SYNCHRONOUS MOVEMENT OF WORKING MEMBER HYDRAULIC CYLINDERS 1997
  • Stojalov V.V.
RU2119597C1
PHYSICAL MODEL OF SPATIAL SYSTEM OF ACTIVE VIBRATION INSULATION AND GUIDANCE 2001
  • Frolov K.V.
  • Sajapin S.N.
  • Sinev A.V.
  • Galushkin A.I.
  • Jakemenko G.V.
RU2224295C2

RU 2 285 959 C2

Authors

Pinishin Vladimir Nikolaevich

Shvetsov Petr Evgen'Evich

Dates

2006-10-20Published

2005-02-01Filed