Curved blade is a widely used 3d-blade-method for compressor performance improvement.
(1) optimization methods, (2) stochastic optimization combined with blade parameterization methods and the design of experiment methods, (3) gradient-based optimization methods for compressors and turbines and (4) data mining techniques for Pareto Fronts.
The proposed approach is, to our best knowledge, the first automated method for reciprocating compressor valve fault detection that can handle varying load conditions.
The paper gives the extension of the Schmidt-Kuhlmann method for reciprocating compressor pipeline systems having a tree-structure, consisting of receivers and pipes with an optional number of branchings.
Oil atomization is an effective enhanced heat transfer method for single screw compressor, which can make the compression process of single screw compressor be close to the isothermal process, then the working efficiency can be improved.
The present investigation aims to find a proper classification method for eigenmodes of compressor airfoils.
Finally, an optimal design method for the rotary compressor oriented to proposed end-plate gas injection with check valve is raised.
The objective of this work is to suggest a method for optimizing the compressor and turbine components in hybrid SOFC GT (Solid Oxide Fuel Cell – Gas Turbine) applications.
In this paper, the design for the mixed flow compressor is based on the results of a S2 through flow aerodynamic design program and a general arbitrary curved blade design method for axial, centrifugal/mixed compressors.
Because of the limitations of isobaric ratio designs of two-stage compressors, this paper presents a new method for mathematically modeling the compressor's transient thermal processes.
The difficulties, due to a lack of information about the performance of compressors, demand predictive and modern approximation methods to be used for compressor modelling.
