Determination of performance and parameters for turboprop and turboshaft engine for modification through change of gas temperature before turbine
 
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Publication date: 2006-11-01
 
 
Combustion Engines 2006,127(4), 34-43
 
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ABSTRACT
The article presents the analysis of a commonly used performance modification method for turboprop and turboshaft engines with a free power turbine. The description of analytical and numerical methods of evaluation for a change of parameters and geometry of turbine assemblies are presented. There are also given the basic methods of changing throat area of turbine nozzle guide vanes and its influence on engine performance. The calculation methods are verified by experimental tests run by WSK “PZL-Rzeszów” S.A.
 
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Exhaust emissions from the PZL W-3 Sokol helicopter based on the measurements of the concentrations of exhaust components in the exhaust gases during a pre-flight test
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eISSN:2658-1442
ISSN:2300-9896
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