IRKUT MC-21 FLAP ACTUATOR TEST RIG
The test rig allows for a number of actuators with differing drive geometry to be located on the rig , the input drive is simulated for speed and torque via a hydraulic servo motor and the output profiled load is applied via a closed loop servo controlled hydraulic actuator . Comar have supplied the total package simulating aircraft mounting, kinematics, loading and environmental conditions, including the integrated electronic control system.
PRODUCTION ACCEPTANCE (PAT) TEST RIG FOR INTER STAGE BLEED VALVES FOR PRATT & WHITNEY PW150 ENGINES
Current tests were taking over 6 hours / unit this was successfully reduced by more than 50% by introducing an electronic control system , dedicated instrumentation and an automated high pressure pneumatic system operating up to 400psi and a 1000 slpm.
MRO THRUST REVERSER ACTUATOR TEST RIG: BOEING 737-700.
Comar provide a test rig that carried out all of the tests in the aircraft CMM using a computer controlled hydraulic system for the unit supplies and control , with monitoring and logging of locks , LVDT,s , velocities and strokes
