An inert gas closed circulation radial impeller mechanical performance test device

A closed cycle, inert gas technology, applied in the direction of safety devices, mechanical equipment, non-variable pumps, etc., can solve the problems that the influence factors cannot be considered, and the accuracy of the aerodynamic characteristics of the impeller machinery cannot be guaranteed, so as to reduce the cost of performance tests , Ease of large-scale promotion and utilization, and the effect of reducing construction costs

Active Publication Date: 2022-07-05
BEIJING POWER MACHINERY INST
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AI Technical Summary

Problems solved by technology

Both theoretical analysis and numerical simulation have their own limitations, and cannot consider all the influencing factors in the actual operating environment, and the existing loss model is established based on the air working fluid, and the aerodynamic characteristics of the turbomachinery obtained through the two cannot guarantee its accuracy sex

Method used

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  • An inert gas closed circulation radial impeller mechanical performance test device
  • An inert gas closed circulation radial impeller mechanical performance test device
  • An inert gas closed circulation radial impeller mechanical performance test device

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Embodiment Construction

[0027] refer to figure 1 As shown, the inert gas closed-cycle radial impeller mechanical performance test device based on the turbocharger structure of the present invention includes an inert gas storage tank, an intake pressure regulating valve, a vacuum pump, a surge tank, a centrifugal compressor, and an anti-surge valve. , throttle valve 1, bypass valve 2, regenerator, heater, centripetal turbine, throttle valve 2, throttle valve 3, bypass valve 1, motor, temperature and pressure probe, etc. When performing centrifugal compressor performance test, centrifugal compressor tester, anti-surge valve, throttle valve 1, bypass valve 1, regenerator, heater, centripetal turbine and vacuum pump, surge tank, temperature and pressure probe The needles are connected in turn to form a closed loop; when the performance test of the centrifugal turbine is carried out, the centrifugal compressor, the anti-surge valve, the throttle valve 1, the bypass valve 2, the regenerator, the heater, th...

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Abstract

The invention discloses a mechanical performance test device of an inert gas closed-cycle radial impeller based on a turbocharger structure, comprising: an inert gas storage tank, a pressure stabilizer box, a turbocharger, a tester, a motor, and a cooler , heater, regenerator, throttle valve, anti-surge valve, bypass valve, temperature and pressure probe, vacuum pump. Take the turbocharger as the basic structure, replace its original centripetal turbine or centrifugal compressor with the tester, and use the centrifugal compressor of the turbocharger as the power consumption device, or use the centrifugal compressor of the turbocharger as the power consumption device. Turbine as power plant. The tester, heater, regenerator and cooler form a closed loop with inert gas as the working fluid through pipelines and valves, and the closed loop utilization of inert gas is realized by cooperatively controlling multiple test equipment. The invention has the remarkable features of ingenious and reasonable structure design, resource saving and the like, and is easy to popularize and apply on a large scale.

Description

technical field [0001] The invention belongs to the technical field of engine performance testing, and relates to a radial impeller mechanical performance testing device, in particular to an inert gas closed-circulation radial impeller mechanical performance testing device based on a turbocharger structure. Background technique [0002] At present, a variety of inert gases, including helium, argon, xenon and their mixtures, are used as substitutes for air, and are increasingly widely used in various closed and semi-closed Brayton cycle systems. As one of the key components of the energy conversion system, the inert gas turbomachine usually works under various working conditions, and its aerodynamic performance directly affects the efficiency of the entire system. Therefore, it is very necessary to obtain the aerodynamic characteristic data of the turbomachinery under all working conditions for the safe and reliable operation of the system. Theoretical analysis and numerical...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F04D27/00F01D21/00
CPCF04D27/001F01D21/003
Inventor 秦勇王大磊郑振江张希马同玲王正
Owner BEIJING POWER MACHINERY INST
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