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Turbine compressor test system

A turbo compressor and test system technology, applied in the field of compressors, can solve the problems of not being able to test the force performance of the blades, not being able to measure the performance, etc., to achieve the effect of reducing power consumption and strengthening the effect of airflow excitation

Inactive Publication Date: 2013-02-20
HEFEI GENERAL MACHINERY RES INST
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  • Abstract
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AI Technical Summary

Problems solved by technology

Conventional test systems and methods cannot measure the performance of compressors under abrupt operating conditions
[0004] The invention patent application with the publication number CN 101251411A discloses a natural frequency measuring device, which uses a vibrator to vibrate the measuring blade, and measures the natural frequency of the blade through an eddy current sensor installed on the blade. Mechanical performance on the blade under sudden change conditions

Method used

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  • Turbine compressor test system
  • Turbine compressor test system
  • Turbine compressor test system

Examples

Experimental program
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Effect test

Embodiment Construction

[0026] see figure 1 , the turbocompressor test system in this embodiment is set to:

[0027] The rotational output of the motor 1 is transmitted to the main shaft 182 of the turbocompressor 18 through the gearbox 2 and the torque sensor 3 to form a test host.

[0028] The intake disturbance unit is set at the air inlet of the turbocompressor 18, and the intake disturbance unit is to arrange an inlet pressure temperature sensor 5, an intake disturbance device 4, a flow rate sensor, etc. meter 7 and intake valve 8; an exhaust disturbance unit is arranged at the exhaust port of the turbocompressor 18, and the exhaust disturbance unit is provided with outlet pressure and temperature sensors sequentially on the exhaust pipeline from the exhaust port of the turbocompressor 17. Outlet disturbing device 15, safety valve 14, main regulating valve 12 and exhaust valve 10, auxiliary regulating valve 13 is arranged in parallel on main regulating valve 12, parallel outlet of main regulati...

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Abstract

The invention discloses a turbine compressor test system. The turbine compressor test system is characterized in that rotation output of a motor is driven to a turbine compressor main shaft of a turbine compressor through a transmission case and a torque sensor so as to form a test main engine, an air inlet disturbance unit, an exhaust disturbance unit, an airflow actuating device and a measure and control unit are respectively arranged aiming at the test main engine. The turbine compressor test system provided by the invention can test properties of the turbine compressor under various working conditions such as different air inlet condition saltations, air inlet distortion and exhaust conditional mutation, simulate the excitation of airflow to blades under different work conditions through an experimental method, and measure the parameters including stress and vibration frequency of the blades under situations with different excitation of airflow.

Description

technical field [0001] The invention belongs to the technical field of compressors, and in particular relates to a turbo-compressor testing system and testing method. Background technique [0002] Turbocompressor is the core equipment in important industrial fields such as petrochemical, metallurgy and coal chemical industry, and its performance directly affects the performance and reliability of these large devices. Traditional turbocompressor test systems usually aim at a certain stable working condition, and test parameters such as flow rate, power, suction and discharge pressure, and temperature of the turbocompressor under this working condition on a standard turbocompressor test platform, and These parameters serve as the basis for evaluating and designing compressors. [0003] With the change of crude oil quality and the application of more and more new processes, the process parameters of compressors in the refining and chemical industry have gradually changed, whic...

Claims

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Application Information

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IPC IPC(8): F04D27/00
Inventor 李连生赵远扬杨启超肖军李新宏
Owner HEFEI GENERAL MACHINERY RES INST
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