2013 American Control Conference 2013
DOI: 10.1109/acc.2013.6580648
|View full text |Cite
|
Sign up to set email alerts
|

Control oriented modeling of a radial turbine for a turbocharged gasoline engine

Abstract: This paper presents a control oriented model for predicting turbine major variables in a turbocharged spark ignition engine. The turbine is simulated as a two-nozzle chamber where the pressure ratio over the two nozzles is not the same. A convex nonlinear estimation algorithm is formulated to determine the relation between these pressure ratios. The new model is experimentally validated with transient and steady state data collected from a 1.7 liter gasoline engine. The results show the new model can predict t… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
4
0

Year Published

2013
2013
2021
2021

Publication Types

Select...
5
1

Relationship

1
5

Authors

Journals

citations
Cited by 9 publications
(4 citation statements)
references
References 23 publications
0
4
0
Order By: Relevance
“…Performance of the designed observer is tested using measured data from a turbocharged 4-cylinder port fuel injected gasoline engine detailed in [13]. Experimental validation of the designed observer is done by applying different step inputs to the engine torque and engine speed using a test procedure shown in Fig.…”
Section: Resultsmentioning
confidence: 99%
“…Performance of the designed observer is tested using measured data from a turbocharged 4-cylinder port fuel injected gasoline engine detailed in [13]. Experimental validation of the designed observer is done by applying different step inputs to the engine torque and engine speed using a test procedure shown in Fig.…”
Section: Resultsmentioning
confidence: 99%
“…(2) Single-nozzle partial empirical model Jensen et al [18] modeled the mass flow rate of the turbine with the flow equation of an adiabatic nozzle, _ m ffiffiffiffiffiffiffi T 00 p P 00 ¼ (24) where p' crit is the critical pressure ratio of an adiabatic nozzle (for air, p' crit ¼ 0.528). To account for the choked flow condition, the effective nozzle area should be expressed as,…”
Section: Review Of Turbine Mass Flow Modelsmentioning
confidence: 99%
“…Similar with Payri's model, Serrano et al [23] deduced a more accurate equation of the intermediate pressure between the stator and the rotor and expanded this model to variable geometry turbines. Eriksson [16] and Salehi et al [24] proposed other simplified expressions of the pressure ratio across the stator. Fang et al [2,25] proposed partial empirical models to predict the mass flow rate and efficiency of inward radial turbines using the Taylor expansion and regression analysis.…”
Section: Introductionmentioning
confidence: 99%
“…In order to design a controller for regulating speed of diesel engine, the nonlinear model was linearized and represented in a state-space form [9]. Reference [10] presented a controloriented model for predicting major turbine variables in a turbocharged spark ignition engine. In the model, the turbine was simulated as a two-nozzle chamber.…”
Section: Introductionmentioning
confidence: 99%