FIELD: transport.
SUBSTANCE: invention relates to aerodynamics. Proposed method consists in automatic reduction of load on control surfaces generating higher lift in case sticking originates. Proposed device has, at least, one surface generating high lift driven by local mechanical final control element in response to control signal generated by control device is set to predefined position by central drive coupled via rotary shaft with said local mechanical final control element to transmit torque generated by central drive to rotary shaft. If signal designating origination of sticking in control surfaces, then torque transmitted to rotary shaft by central drive is automatically reduced to preset lower level to fix the position of control surfaces generating higher lift.
EFFECT: automatic reduction of load.
20 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR LIMITATION OF POWER LOAD IN DRIVE SYSTEMS FOR SYSTEMS OF AIRCRAFT LIFTING FORCE INCREASE | 2004 |
|
RU2360844C2 |
SET OF FLAPS ON WING OF FIXED-WING AIRCRAFT | 2004 |
|
RU2346851C2 |
AIRCRAFT WITH LIFT INCREASING SYSTEM | 2010 |
|
RU2494931C2 |
SYSTEM TO DRIVE, AT LEAST, AIRCRAFT ONE CONTROLLED FLAP AND METHOD OF SYSTEM TESTING | 2008 |
|
RU2485012C2 |
AEROSTAT TRAJECTORY CONTROL SYSTEM | 1999 |
|
RU2238217C2 |
HIGH-SPEED TURBOFAN COMBINED HELICOPTER | 2016 |
|
RU2629475C1 |
HIGH-ALTITUDE SOLAR AND WIND POWER PLANT | 2014 |
|
RU2563048C1 |
WING FLAP LIFT INCREASING REGULATOR | 2007 |
|
RU2446987C2 |
HOVERCRAFT | 2013 |
|
RU2547665C1 |
METHOD OF FORMING THE SYSTEM OF FORCES OF FLYING VEHICLE AND FLYING VEHICLE-GROUND-AIR-AMPHIBIAN FOR REALIZATION OF THIS METHOD | 2006 |
|
RU2317220C1 |
Authors
Dates
2011-04-10—Published
2006-12-08—Filed