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Curved blade is a widely used 3d-blade-method for compressor performance improvement.
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Pierre (1982) developed general correlations of compressor performance for a wide range of open piston compressors based on a vast amount of data provided by the most important open compressors manufacturers at that time.
A mathematical model has been developed for calculating the compressor performance and for validating the results with experimental data.
The model was then linked with an optimization algorithm to search for a combination of some six design dimensions and seven sets of design constraints, for an optimum compressor performance with minimum mechanical losses.
This is the main reason for the variation of the compressor performance resulted from the stator clocking effects.
For instance, the relation between DR-1(Enhancing compressor performance) and PC-1 at the level I (1/3 hp Hermetic compressor) is strong and hence value 9 is assigned in the corresponding cell of the matrix.
The variation of the compressor performance due to the clocking effect is less pronounced for the compressor with compound-lean stators than with the baseline.
A semi-hermetic reciprocating compressor was developed for application in CO2 refrigeration, and a test system was incorporated into the compressor performance test rig, with a focus on investigating the dynamics of the discharge valves.
The results of the study suggested that for a given compressor swept volume, a proper combination of the compressor design dimensions can lead to significant compressor performance.
Compressor performance is a function of the type of compressor.
This chapter examines the effects that multistage compressor configurations have on the overall compressor performance curve.
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