SALES NEWS
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.
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.
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
AZIPULL TORQUE TEST RIG
The test stand had to cater for a variety of units of different sizes and torques with driveline speeds of 1-2rpm 0-70 kNm input torque and output torques of 0-200 kNm. We manufactured and assembled in the UK completing FAT Tests then shipped to Norway and recommisioned. See our you tube page for a time lapse video of the rig being assembled.
