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Low-temperature hydraulic impact test method

A technology of hydraulic shock and test method, applied in shock test, machine/structural component test, measurement device, etc., can solve the problems of not being able to truly respond to test results, not directly controlling pressure signals, increasing pulse width, etc. Realize the effect of impact resistance test, simple and convenient operation, and reduced requirements

Active Publication Date: 2016-03-23
TIANJIN AEROSPACE RELIA TECH
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] Considering that the traditional vibration shock table cooperates with the controller to use acceleration as feedback, and does not directly control the pressure signal, and because only the impact test is performed, the cost is relatively high
[0004] In addition, the circuit of the detection system generally cannot directly withstand low temperature, and will fail in a low temperature environment. Moreover, when there is a large amount of gas in the sensor, the detected peak is much smaller than the actual one, and the pulse width is relatively increased, which cannot be true. The results of the reaction test

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Embodiment Construction

[0041] In order to enable those skilled in the art to better understand the technical solutions in the present invention, the following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described The embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0042] Participate figure 1 And combine figure 2 , image 3 As shown, the low-temperature hydraulic impact test system involved in this embodiment can be used to test the anti-fluid medium impact performance of a pressure accumulator on a pipeline. The bracket 3 is vertically fixed on the iron stack 7 of the impact t...

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Abstract

The invention discloses a low-temperature hydraulic impact test method. The method is used for testing a strength characteristic of an accumulator bearing a lot of hydraulic impact under a low temperature condition and the method is realized mainly based on a low-temperature hydraulic impact test system. The system is mainly formed by a falling impact bench, a support, a corrugated pipe pressure chamber, a thermal insulation system, a pressure monitoring unit and the like. The pressure chamber is divided into an external cavity and an internal cavity by one corrugated pipe. An external cavity portion of the pressure chamber is connected to a glass steel shaft. The external cavity is directly immersed into the thermal insulation system which is filled with liquid nitrogen. The internal cavity is filled with the liquid nitrogen and is connected to the accumulator. In the invention, the impact bench is cooperated with the corrugated pipe so that impact under a low temperature medium is realized; through a simple method, a gasification phenomenon of the liquid nitrogen in a pipeline is effectively solved; a real condition is simulated and a low-temperature impact resistance test of the accumulator can be effectively realized; through setting work parameters of an impact bench height, internal contracting brake time and the like, a pressure impact amplitude is accurately set so that different test demands are satisfied.

Description

Technical field [0001] The invention particularly relates to a low-temperature hydraulic shock test method, the pressure medium of which is liquid nitrogen, which can be used to truly simulate the pressure shock in a rocket fuel transportation pipeline and to assess the shock resistance performance of the pressure accumulator on the pipeline. Background technique [0002] In the pressure shock test in the simulated rocket fuel pipeline, the simulated medium is liquid nitrogen, which is used to truly assess the shock resistance of the pressure accumulator. Because liquid nitrogen is very easy to vaporize under the normal test environment and cannot be maintained in liquid nitrogen Therefore, how to maintain liquid nitrogen as a pressure medium is a difficult problem. [0003] Considering that the traditional vibration shock table and the control instrument all use acceleration as feedback, and do not directly control the pressure signal, and because only the impact test is performed...

Claims

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Application Information

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IPC IPC(8): G01M7/08
CPCG01M7/08
Inventor 朱正邦李杰祝济之
Owner TIANJIN AEROSPACE RELIA TECH
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