Method used for stripping influence of background noise in sealed cabin noise testing process

A background noise and airtight chamber technology, applied in the measurement of ultrasonic/sonic/infrasonic waves, measuring devices, instruments, etc., can solve the problems of analyzing background noise and affecting the accuracy of the actual measurement results, and achieve the effect of improving the accuracy

Inactive Publication Date: 2018-12-21
BEIJING SPACE TECH RES & TEST CENT
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, when my country's manned spacecraft conducts noise tests in sealed cabins on the ground, the requirement for background noise is generally to "keep the scene quiet", and the influence of background noise on the measured results has not been analyzed from the mechanism, which in turn affects the accuracy of the measured results.

Method used

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  • Method used for stripping influence of background noise in sealed cabin noise testing process
  • Method used for stripping influence of background noise in sealed cabin noise testing process
  • Method used for stripping influence of background noise in sealed cabin noise testing process

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Embodiment approach

[0040] Such as figure 1 As shown, according to an embodiment of the present invention, a method for stripping the influence of background noise when testing the noise of the sealed cabin of the present invention includes:

[0041] S1. Select test points for testing noise in the airtight cabin, and install noise testing instruments;

[0042] S2. Obtain the background noise level L of the load in the airtight cabin in the shutdown state through the noise testing instrument p' , energize the airtight cabin and obtain the measured noise level L of the load in the airtight cabin in working condition p∑ , and define the real noise level after the load in the airtight compartment is in working condition and the effect of background noise is removed as L p ;

[0043] S3. According to the background noise level L p' with the measured noise level L p∑ Obtain the first noise difference, and according to the measured noise level L p∑ with the real noise level L p Obtain a second no...

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Abstract

The invention relates to a method used for stripping influence of a background noise in a sealed cabin noise testing process, comprising the following steps: S1, selecting a test point used for testing a noise in a sealed cabin, and mounting a noise test instrument; S2, acquiring a background noise level Lp' when a load in the sealed cabin is in a shutdown state by virtue of the noise test instrument, electrifying the sealed cabin and acquiring the actually measured noise level LpSigma when the load in the sealed cabin is in an operating state, and defining a real noise level when the load inthe sealed cabin is in the operating state and after the influence of the background noise is stripped as Lp; S3, obtaining a first noise difference value according to the background noise level Lp' and the actually measured noise level LpSigma, and obtaining a second noise difference value according to the actually measured noise level LpSigma and the real noise level Lp; and S4, acquiring a correction curve of the actually measured noise level LpSigma according to the first noise different value and the second noise difference value. The method provided by the invention realizes precise stripping on the background noise and obtains a more accurate real noise test result.

Description

technical field [0001] The invention relates to a method for stripping the influence of background noise when testing the noise of a sealed cabin, in particular to a method for stripping the influence of background noise when testing the noise of a sealed cabin for a manned spacecraft. Background technique [0002] When a manned spacecraft is in orbit for a long time, it is exposed to the poor noise environment in the airtight cabin, which will have adverse effects on the work, life, physiology and psychology of the astronauts. The harsh noise environment will even affect the safety of the mission. Users generally require that the noise level index in the airtight cabin of a manned spacecraft be limited within a certain range. Before the manned spacecraft is launched into orbit, it is necessary to conduct effective test verification on the noise level in the airtight cabin during the ground development period. During the test, the background noise at the test site directly ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01H17/00
CPCG01H17/00
Inventor 彭华康黄震邵立民高旭俞进
Owner BEIJING SPACE TECH RES & TEST CENT
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