Innovative compressor inlet invention which increases compressor flow range with use of an inlet duct that pre-swirls inlet flow of turbocharger compressor.

Innovative compressor inlet invention which increases compressor flow range with use of an inlet duct that pre-swirls inlet flow of turbocharger compressor.
A novel, high efficiency low pressure ratio turbine developed by engineers at Imperial College London to capture a significant portion of residual exhaust energy with negligible effect on engine base performance.
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