Continuous supersonic sand erosion test table and test method thereof

A supersonic, test-bed technology, applied in the direction of testing wear resistance, measuring devices, instruments, etc., can solve the problems of high cost, hidden dangers to the safety of test personnel, and inability to achieve supersonic speed, and achieve the effect of low cost and continuous supply.

Inactive Publication Date: 2017-07-14
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
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AI Technical Summary

Problems solved by technology

This method has some disadvantages: first, the device cannot realize continuous erosion
The test device needs to re-place the material and re-inflate the shock tube every time the erosion test is carried out. It belongs to the intermittent test device and cannot achieve the purpose of the test and research of continuous feeding erosion.
Second, the safety and test efficiency of the device are not high
Due to the dispersion of the performance of the aluminum film material, if the aluminum film is not breaking, it will bring safety hazards to the test personnel; because the device uses intermittent work, it takes a certain amount of time to place the materials and materials for each test. Inflating the shock tube affects the test efficiency and increases the labor burden of the test personnel
Thirdly, it is very difficult for the device to make the sand particles reach the supersonic state
The disadvantage of this method is that: the ejected high-temperature flame will inevitably affect the test piece eroded by sand particles; the high-temperature flame continuously acting on the metal test piece will greatly reduce its structural strength, making Sand particles are more likely to cause damage to the surface of the eroded material, so that it cannot reflect the erosion resistance of the material
This method has some deficiencies: first, the device cannot realize supersonic erosion of sand grains
The device does not use a Laval tube to accelerate the gas-sand two-phase flow, but uses an ordinary flat nozzle; according to the relevant knowledge of fluid mechanics, when the air velocity is infinitely close to the speed of sound, the gas flow per unit area reaches the maximum; For straight pipes, the congestion effect has already been formed at this time, and the gas flow in the downstream of the pipe is absolutely impossible to be smaller than that in the upstream, so no matter how much pressure the airflow in the straight pipe has, it cannot achieve supersonic speed.
Second, if a compressor is used as a supersonic gas source, the cost will be too high

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  • Continuous supersonic sand erosion test table and test method thereof
  • Continuous supersonic sand erosion test table and test method thereof
  • Continuous supersonic sand erosion test table and test method thereof

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Embodiment Construction

[0037] Attached below figure 1 , attached figure 2 , attached image 3 , attached Figure 4 And attached Figure 5 The specific embodiment of the present invention will be further described.

[0038] figure 1 It is a general structure diagram of the present invention. The right side of the gas cylinder group 1 composed of 5 high-pressure cylinders is the pressure regulator tank 2, the right side of the pressure regulator tank 2 is the pressure control valve 3, the right side of the pressure control valve 3 is the solenoid valve 4, and the solenoid valve 4 is Control the switch of the main air flow, the main air is respectively connected to the sand supply device 5 and the sand blasting device 6, and the sand supply device 5 and the sand blasting device 6 are fixed on the test table 16; the right side of the sand blasting device 6 is the test piece fixture 8, and the test Fixture 8 is fixed in test chamber 9, and the lower side of test chamber 9 is connected with transla...

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Abstract

The invention discloses a continuous supersonic sand erosion test table and a test method thereof. The test table comprises a gas source device, a screw sand supply device, a sand blasting device, a test chamber, an exhaust tube and a cyclone separator. The gas supply device obtains high pressure gas flow through a high pressure gas storage tank, the screw sand supply device adopts a pressure container as a sand storage container, a motor drives a screw to rotate at a uniform speed, and the gas outlet of a feeding cylinder is provided with a gas flowing hole for assisting sand falling in order to avoid sand grain obstruction; and high quality gas flow is obtained from the Laval tube outlet of the sandblasting device to make the sand grains move along the axis in order to reduce sand grain and tube wall collision. The sand grains can be accelerated to a supersonic state only through room-temperature drying gas; the sand supply device has a good sealing property, can balance the pressure of the sand supply device in a high pressure environment, and has a good sand supply precision; and a gas source used in the invention has a low price and stable performances.

Description

technical field [0001] The invention relates to the field of fine particle transportation and powder transportation under pressure environment, and also relates to the field of sandblasting test. Background technique [0002] So far, according to published literature, there is no equipment that can continuously spray sand particles to a designated target at supersonic speed through normal temperature gas. To achieve the goal of cold-state continuous supersonic erosion, several interlocking technical problems are faced: first, how to accelerate sand particles to a supersonic state through normal temperature gas. To make the sand particles reach the supersonic state, the high-pressure gas (the pressure value is usually set above 3MPa) should be fully mixed with the sand particles in a low-speed environment, and then the gas-sand two-phase flow with a certain pressure should pass through the Laval structure tube. (Shock tube) accelerated to the supersonic state required for th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/56
CPCG01N3/565
Inventor 颜诚陈伟赵振华
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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