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CM14

INTERNAL COMBUSTION ENGINES - CM14 Axial Flow Gas Turbine

The new CM14 is a complete aeronautical axial flow gas turbine engine, and a great tool for those teaching and studying in areas such as engine systems and thermodynamics.

The engine itself is a small compact Olympus HP E-start turbine engine, comprising a single stage radial compressor, annular combustion chamber, and a low mass, high performance axial flow turbine. Full instrumentation is included as standard, allowing the measurment of a wide range of variables such as temperature, pressure, air and fuel flow, shaft speed and thrust.

The CM14 connects to a PC via a single USB interface, allowing for easy installation into a test cell or soundproof enclosure. The included software runs on the user's PC, and features powerful educational tools together with sophisticated graph plotting and data logging capability.

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