Turbocharger Map Reduction for Control-Oriented Modeling

Author:

Stricker Karla1,Kocher Lyle1,Koeberlein Ed1,Van Alstine D. G.2,Shaver Gregory M.3

Affiliation:

1. Cummins, Inc., Box 3005, Columbus, IN 47202

2. Caterpillar, 100 North East Adams Street, Peoria, IL 61629

3. School of Mechanical Engineering, Purdue University, 585 Purdue Mall, West Lafayette, IN 47907

Abstract

Models of the gas exchange process in modern diesel engines typically use manufacturer-provided maps to describe mass flows through, and efficiencies of, the turbine and compressor based on pressure ratios across the turbine and compressor, as well as the turbocharger shaft speed, and in the case of variable-geometry turbochargers, the nozzle position. These look-up maps require multiple interpolations to produce the necessary information for turbocharger performance, and are undesirable when modeling for estimation and control. There have been several previous efforts to reduce dependence on maps with general success, yet many of these approaches remain complex and are not easily integrated into engine control systems. The focus of this paper is the reduction of turbomachinery maps to analytical functions that are amenable to estimator and control design, and have been validated against manufacturer-provided turbomachinery data.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Reference40 articles.

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4. Improved Model to Determine Turbine and Compressor Boundary Conditions With the Method of Characteristics;Int. J. Mech. Sci.,2006

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