Pipeline compressor model level of 0.022 in flow coefficient and impeller designing method

A pipeline compressor and flow coefficient technology, applied in the field of compressors, to achieve high efficiency, reduce bearing span, and reduce operating speed

Inactive Publication Date: 2017-05-24
SHENYANG TURBO MASCH CORP +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] In order to solve the above-mentioned problems existing in the existing pipeline model stage 9, the purpose of the present invention is to provide a pipeline compressor model stage with a flow coefficient of 0.022 and its impeller design method, so that the efficiency of the pipeline compressor product unit can be significantly improved, and the work of the unit can be reduced. consumption

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  • Pipeline compressor model level of 0.022 in flow coefficient and impeller designing method
  • Pipeline compressor model level of 0.022 in flow coefficient and impeller designing method
  • Pipeline compressor model level of 0.022 in flow coefficient and impeller designing method

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Embodiment Construction

[0039] see figure 1 , a pipeline compressor model stage with a flow coefficient of 0.022 provided by the embodiment of the present invention is suitable for the modular design of pipeline compressors and other light medium compressor products, including impeller 1, vaneless diffuser 2, bend 3 and Recirculator 4, wherein impeller 1 is located at the inlet position of model stage nine, vaneless diffuser 2 is provided at the outlet of impeller 1, and recirculator 4 is located at the outlet position of model stage nine, vaneless diffuser 2 and recirculator 4 They are connected by 3 bends. The machine Mach number M that can be used by this model level u2 =0.35~0.65, design point flow coefficient Φ 1 =0.022, the design point energy head coefficient τ=0.588, the variable efficiency η under the design flow coefficient working condition at each Mach number pel =0.812~0.817, the applicable flow range is 60%-150% of the design point. Specific performance curves such as Figures 17-1...

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Abstract

The invention provides a pipeline compressor model level of 0.022 in flow coefficient. The pipeline compressor model level comprises an impeller, a vaneless diffuser, a bend and a backflow device. The impeller is positioned at an inlet of a ninth model level, the vaneless diffuser is arranged at an outlet of the impeller, the backflow device is positioned at an outlet of the ninth model level, and the vaneless diffuser is communicated with the backflow device through the bend; machine mach number Mu2 of the ninth model level is 0.35-0.6, design point flow coefficient phi 1 is 0.022, design point energy head coefficient t is 0.588, polytropic efficiency npcl in design flow coefficient working condition under each mach number is 0.812-0.817, and applied flow range is 60-150% of a design point. The invention further provides a design method of the impeller with the model level. The ninth model level is high in efficiency and energy head coefficient, large in rub ratio and small in span; by adopting the model level, a light-medium compressor is enabled to have high running efficiency and wide working condition range, working rotation speed of a rotor can be lowered, bearing span can be reduced, and stability of the rotor can be improved.

Description

technical field [0001] The invention relates to the technical field of compressors, in particular to a model stage and impeller design method of a pipeline compressor with a flow coefficient of 0.022. Background technique [0002] The pipeline compressor is the key equipment of the national key project of the West-to-East Gas Transmission Project. During its research and development process, the design of the model stage 9 is very critical, and the development of new products depends on the corresponding model stage 9. [0003] The existing pipeline model stage 9 has disadvantages such as small hub ratio, large axial span, and low efficiency. Therefore, in the process of product design, the diameter of the shaft is small and the shaft is long, and the critical speed of the product, the stability of the rotor and the stiffness of the shaft There are big problems in other aspects, which bring great difficulties to product design. In addition, the performance of the unit is lo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F04D29/28F04D29/30F04D29/44G06F17/50
CPCF04D29/284F04D29/30F04D29/441G06F30/17
Inventor 卢傅安韩亮孙博孙昊强孙云莹李云程健庞佳璇伊洪丽
Owner SHENYANG TURBO MASCH CORP
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