DEVICE FOR MEASURING AERODROME COATINGS SURFACE PROFILE SLOPES Russian patent published in 2016 - IPC E01C23/07 

Abstract RU 2592930 C1

FIELD: construction.

SUBSTANCE: invention relates to construction and operation of aerodromes. In device containing transport wheeled module with platform, gyroscopic platform turn angle relative to the horizontal plane with longitudinal and transverse angle sensors meter, longitudinal and transverse level sensors, longitudinal and transverse moment sensors, multi-channel electronic control unit including channels lengthwise, crosswise correction of gyroscopic meter and output information forming channel, wherein input of longitudinal correction channel is connected to output of longitudinal horizon sensor, and output of longitudinal correction channel is to input of longitudinal torque sensor, input of crosswise correction channel is to output of cross horizon sensor, and output of crosswise correction channel is to input of the cross torque sensor, inputs of output information forming channel are connected to outputs of gyroscopic meter sensors, according to invention transport wheeled module with platform is made in form of independent single-axis wheeled module resting on two coaxial rims, controlled by driving motors installed on platform, device is equipped with wheels rotation angular speed sensors, wheel rotation angular acceleration sensors, devices for measuring height of two extreme points of platform bracket longitudinal axis above surface profile, driving motors control channel in control and computing unit, outputs of wheel rotation angular speed sensors are connected to additional inputs of longitudinal correction channel, outputs of wheel rotation angular velocity transducers are connected to additional inputs of crosswise correction channel, outputs of altitude meters are to additional inputs of output information forming channel, output of gyroscopic meter cross angle sensor is additionally connected to input of driving motors control channel, outputs of driving motors control channel are to control windings of these motors.

EFFECT: technical result is increase of accuracy of measuring slopes surface profile aerodrome (pavement) coating, reduced labour intensity at measurement of these slopes.

1 cl, 3 dwg

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RU 2 592 930 C1

Authors

Chernomorskij Aleksandr Isaevich

Maksimov Vladimir Nikolaevich

Kuris Eduard Davydovich

Lelkov Konstantin Sergeevich

Dates

2016-07-27Published

2015-06-18Filed