This paper reports on the development of the Low Speed Turbocharger (LST), a single shaft turbocharger capable of pressure ratios in excess of 5/1. Key decisions regarding the fundamental design concept are discussed as well as compressor design, analysis methodology and performance results; turbine design challenges and resulting tested performance; rotor-dynamics analysis and bearing system design.
Development of an Ultra-High Pressure Ratio Turbocharger
Sae Technical Papers
SAE 2005 World Congress & Exhibition ; 2005
2005-04-11
Conference paper
English
Development of an ultra-high pressure ratio turbocharger
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