We conducted a feasibility study containing concept design (predicting the state(temperature,flow rate) of seperate altitude-exhaust gas based on the thrust 30,000 lbf class engine, determining the air condition (temperature, pressure) supplied to seperate altitude engine, determing the exhaust gas cooling
F404-GE-102 Engine Test Cell (Korea Air Force)
This is the US GE’s F404 ground test equipment for gas turbine engines, an engine stand that can measure the actual engine thrust. It consists of engine test bed, fuel supplier, preserving oil supplier, intercom equipment, equipment integration control device,
PT6A-67 Engine Performance Tests equipment in medium altitude
A medium altitude test equipment is designed to predict whether the performance output of the engine applied to UAVs can be ensured in the medium altitude. It uses an existing high altitude environmental testing equipment. We delivered an engine thrust measurement bed, a
PT6A-67 Engine performance ground-test facility
This is an engine power performance test equipment on the ground in the early stages for the research and development of UAV (MUAV). In the propeller mounted condition, it consists of engine thrust measurement Bed considering the air flow, fuel
PT6A-62 engine test cell (Korea Air Force)
This is a Pratt Whitney Canada’s turboprop gas turbine engine ground test cell, equipment to check the performance of the engine equipped with a propeller. It consists of an engine fixing stand, a fuel supply device, scavenging oil cooling devices,