It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation.
Features:
accuracy: error of the compass is no more than 2.5°
It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation.
Features:
accuracy: error of the compass is no more than 2.5°
It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation.
Features:
accuracy: error of the compass is no more than 2.5°
It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation.
Features:
accuracy: error of the compass is no more than 2.5°
It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation.
Features:
accuracy: error of the compass is no more than 2.5°
It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation.
Features:
accuracy: error of the compass is no more than 2.5°
It is used in a small aircraft to determine and indicate magnetic heading of the aircraft. Dial is soaked in kerosene and sealed completely. It has a simple structure and a reliable operation.
Features:
accuracy: error of the compass is no more than 2.5°
The heading indicator (also known as the directional gyro, or DG; sometimes also called the gyrocompass, though usually not in aviation applications) displays the aircraft’s heading with respect to geographical north. Principle of operation is a spinning gyroscope, and is therefore subject to drift errors (called precession) which must be periodically corrected by calibrating the instrument to the magnetic compass.
Features:
operating voltage: 14 ± 10% V DC
ambient temperature: -40 – +50 °C
ambient relative humidity: no more than 95%
vibration strength: 1.5g
working range: indicating heading angle within the range of 360°
accuracy: the drift error is not more than 4°/10 min
operating current is not more than 0.72A
rated Rotating speed is 22000 turns per min: it warns when power-off the rotating speed is below 70% of the rate rotating speed
the insulating resistance between the power and case is not less than 20M?
The heading indicator (also known as the directional gyro, or DG; sometimes also called the gyrocompass, though usually not in aviation applications) displays the aircraft’s heading with respect to geographical north. Principle of operation is a spinning gyroscope, and is therefore subject to drift errors (called precession) which must be periodically corrected by calibrating the instrument to the magnetic compass.
Features:
ambient temperature: -30 – +50 °C
ambient relative humidity: no more than 95%
anti-vibration tensity: 1.5g
height: 40000feet
driving power: 15 ~18K Pa for vacuum or air pressure
pressure for starting: 7KPa
working range: indicating heading angle within the range of 360°
accuracy: the drift error is not more than 4°/10 min
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