The compressor of composite gear teeth is a new type of rotor compressor withpartial built-in compression process. Analysis of its thermodynamic process indicates that thebuilt-in process is incomplete. The thermodyna...The compressor of composite gear teeth is a new type of rotor compressor withpartial built-in compression process. Analysis of its thermodynamic process indicates that thebuilt-in process is incomplete. The thermodynamic process of the compressor of composite gear teethcan be considered as five processes; the suction process, the isometric process, the compressionprocess, the pressure-balance process at high pressure and low pressure gas, and discharge process.Here, it is necessary to explain further the pressure-balance process. The pressure-balance processis isometric process. It is found that the isometric process of gas in chamber A whose capacity is83 percent of total work volume can be eliminated basically through extending the discharge port toconnect early the discharge port with the chamber B. By the above-mentioned method, the loss ofenergy will be reduced.展开更多
Considering the essential and influential role of centrifugal compressors in a wide range of industries makes most of engineers research and study on design and optimization of centrifugal compressors. Centrifugal com...Considering the essential and influential role of centrifugal compressors in a wide range of industries makes most of engineers research and study on design and optimization of centrifugal compressors. Centrifugal compressors are the key to part ofoil, gas and petrochemical industries as well as gas pipeline transports. Since complete 3D design of the compressor consumes a considerable amount of time, most of active companies in the field, are profoundly interested in obtaining a design outline before taking any further steps in designing the entire machine. In this paper, a numerical algorithm, named ACDA （adapted compressor design algorithm） for fast and accurate preliminary design of centrifugal compressor is presented. The design procedure is obtained under real gas behavior, using an appropriate equation of state. Starting from impeller inlet, the procedure is continued on by resulting in numerical calculation for other sections including impeller exit, volute and exit diffuser. Clearly, in any step suitable correction factors are employed in order to conclude in precise numerical results. Finally, the achieved design result is compared with available reference data.展开更多
文摘The compressor of composite gear teeth is a new type of rotor compressor withpartial built-in compression process. Analysis of its thermodynamic process indicates that thebuilt-in process is incomplete. The thermodynamic process of the compressor of composite gear teethcan be considered as five processes; the suction process, the isometric process, the compressionprocess, the pressure-balance process at high pressure and low pressure gas, and discharge process.Here, it is necessary to explain further the pressure-balance process. The pressure-balance processis isometric process. It is found that the isometric process of gas in chamber A whose capacity is83 percent of total work volume can be eliminated basically through extending the discharge port toconnect early the discharge port with the chamber B. By the above-mentioned method, the loss ofenergy will be reduced.
文摘Considering the essential and influential role of centrifugal compressors in a wide range of industries makes most of engineers research and study on design and optimization of centrifugal compressors. Centrifugal compressors are the key to part ofoil, gas and petrochemical industries as well as gas pipeline transports. Since complete 3D design of the compressor consumes a considerable amount of time, most of active companies in the field, are profoundly interested in obtaining a design outline before taking any further steps in designing the entire machine. In this paper, a numerical algorithm, named ACDA （adapted compressor design algorithm） for fast and accurate preliminary design of centrifugal compressor is presented. The design procedure is obtained under real gas behavior, using an appropriate equation of state. Starting from impeller inlet, the procedure is continued on by resulting in numerical calculation for other sections including impeller exit, volute and exit diffuser. Clearly, in any step suitable correction factors are employed in order to conclude in precise numerical results. Finally, the achieved design result is compared with available reference data.
