Nose Wheel actuator test stand.
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Main instrumentation includes speed control potentiometer, digital torque, frequency and flow meters.
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Functions
The test stand is designed for carrying out test and maintenance procedures on Nose Wheel Steering Actuators.
An oscillating drive system along with a load system simulates the most severe environment of aircraft operation.
Consists of a primary hydraulic system to supply pressure to the actuator and a secondary system to provide hydraulic fluid and control for the rotary load system.
The primary hydraulic system requires an external source of hydraulic pressure.
Specifications
- Oscillation drive system consists of a 1.5 HP motor and drive motor controller.
- Electrical service: 220 V, single phase, 50 Hz, 5KVA
Manufacturer
JA STALEY
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valid for helicopters:
all
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