The basic aerodynamic design criteria and methodology used in the design of the variable geometry turbine are presented along with gas stand test results.A microprocessor controller was designed and tested with the engine and VPT. Both the development of the controller and the exploration of the optimum relationship between the VPT turbo and the engine are presented along with steady-state engine data.
Schwitzer Variable Geometry Turbo and microprocessor Control Design and Evaluation
Sae Technical Papers
SAE International Congress and Exposition ; 1987
01.02.1987
Aufsatz (Konferenz)
Englisch
Schwitzer Variable Geometry Turbo and Microprocessor Control Design and Evaluation
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