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The Use of Neural Nets for Matching Fixed or Variable Geometry Compressors With Diesel Engines
- Source :
- Journal of Engineering for Gas Turbines and Power. 125:572-579
- Publication Year :
- 2003
- Publisher :
- ASME International, 2003.
-
Abstract
- A technique which uses trained neural nets to model the compressor in the context of a turbocharged diesel engine simulation is introduced. This technique replaces the usual interpolation of compressor maps with the evaluation of a smooth mathematical function. Following presentation of the methodology, the proposed neural net technique is validated against data from a truck type, 6-cylinder 14-liter diesel engine. Furthermore, with the introduction of an additional parameter, the proposed neural net can be trained to simulate an entire family of compressors. As a demonstration, a family of compressors of different sizes is represented with a single neural net model which is subsequently used for matching calculations with intercooled and nonintercooled engine configurations at different speeds. This novel approach readily allows for evaluation of various options within a wide range of possible compressor configurations prior to prototype production. It can also be used to represent the variable geometry machine regardless of the method used to vary compressor characteristics. Hence, it is a powerful design tool for selection of the best compressor for a given diesel engine system and for broader system optimization studies.
- Subjects :
- Engineering
Artificial neural network
business.industry
Mechanical Engineering
Energy Engineering and Power Technology
Aerospace Engineering
Control engineering
Context (language use)
Diesel engine
Automotive engineering
Fuel Technology
Nuclear Energy and Engineering
Internal combustion engine
Spark-ignition engine
Turbomachinery
business
Gas compressor
Turbocharger
Subjects
Details
- ISSN :
- 15288919 and 07424795
- Volume :
- 125
- Database :
- OpenAIRE
- Journal :
- Journal of Engineering for Gas Turbines and Power
- Accession number :
- edsair.doi...........63c0497b5fc7f494b53503391eb45dc4