Electric direction indicator EUP-53
Replenishment date: 05.04.2008
Content: apiisk.zip (704.66 KB)
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Description
An electric direction indicator is a gyroscopic direction indicator in which the gyroscope rotor is driven by electrical energy.
The EUP-53 direction indicator is intended for correct execution of the aircraft turn around the vertical axis with a lateral roll of up to 45˚ at a flight speed of 500 km / h.
The principle of operation of EUP-53 is based on the use of the property of a gyroscope with two degrees of freedom to combine the axis of its own rotation with the axis of forced rotation.
The EUP-53 direction indicator is intended for correct execution of the aircraft turn around the vertical axis with a lateral roll of up to 45˚ at a flight speed of 500 km / h.
The principle of operation of EUP-53 is based on the use of the property of a gyroscope with two degrees of freedom to combine the axis of its own rotation with the axis of forced rotation.