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A Method for Determining Continuous Vibration Transfer Spectrum of Rocket Sled Test

A technology of vibration transmission and determination method, which is applied to instruments, measuring devices, and measuring ultrasonic/sonic/infrasonic waves, etc. It can solve problems such as inability to realize continuous frequency band analysis, high noise, and lack of direct acquisition methods for high-frequency vibration information.

Active Publication Date: 2019-03-12
BEIJING INST OF AEROSPACE CONTROL DEVICES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there is a lack of direct acquisition methods for high-frequency vibration information;
[0010] (2) Only periodic power spectrum analysis is carried out for vibration information at all levels, which is characterized by large noise and lack of effective noise reduction processing methods;
[0011] (3) It only qualitatively analyzes the magnitude of vibration at all levels, whether there is a resonance peak, etc., and cannot analyze the vibration transfer characteristics from the skid to the vibration damping platform, from the vibration damping platform to the product under test, and from the skid to the product under test;
[0012] (4) Vibration transfer can only achieve discrete frequency points, but not continuous frequency segment analysis, therefore, the resolution is low

Method used

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  • A Method for Determining Continuous Vibration Transfer Spectrum of Rocket Sled Test
  • A Method for Determining Continuous Vibration Transfer Spectrum of Rocket Sled Test
  • A Method for Determining Continuous Vibration Transfer Spectrum of Rocket Sled Test

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Experimental program
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Effect test

Embodiment 1

[0124] Taking the tested product as an example, the effectiveness of the power spectrum amplitude correction method proposed by the present invention is verified.

[0125] The setting conditions are as follows: In the rocket sled test, the sampling frequency of the sensor is 9.6kHz, and the vibration power spectrum of the tested product based on the periodic spectrum is as follows: figure 2 As shown, the initial power spectrum based on the AR model is as image 3 It can be seen that there is a slight difference in magnitude between the two. Adopt the method of the present invention, the power spectrum amplitude correction coefficient is c=0.723, after this value is substituted into the correction formula, the accurate power spectrum of the tested product based on the AR model is as follows: Figure 4 shown. Compare image 3 with Figure 4 As can be seen, Figure 4 The power spectrum curve of image 3 The power spectrum curve of the power spectrum moves down as a whole, ...

Embodiment 2

[0127] From the rocket sled test, the continuous vibration transfer spectrum between stages is calculated according to the vibration information of multiple sensors to realize the analysis of vibration transfer characteristics.

[0128] The setting conditions are as follows: In the rocket sled test, a multi-stage installation method is adopted, that is, the tested product is installed on the vibration-damping plate, and then the vibration-damping plate is installed on the sled through the vibration isolator. The sensor sampling frequency is 9.6kHz. During the process from start to stop, the heading sensor installed on the skid, the heading sensor installed on the vibration-damping plate, and the heading sensor installed on the inertial platform (the product under test) respectively collect and record the corresponding acceleration value information, and the vibration is obtained through a high-pass filter. data, and further get the power spectral density.

[0129] The vibrati...

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Abstract

The present invention provides a continuous vibration transmission spectrum determination method of a rocket sled test, belonging to the mechanical environment test technology field. The method comprises the following steps: (1) measuring the acceleration magnitude sequences aIx(k) and aIy(k) of a device X and a device Y at running through a sensor; (2) taking the aIx(k) and aIy(k) as input quantity, and obtaining the vibration value sequences adx(k) and ady(k) after the high-pass filtering; (3) solving the continuous functions Px(f) and Py(f) of the vibration power spectrums of the adx(k) and ady(k) based on an AR model; (4) correcting the amplitudes of the continuous functions Px(f) and Py(f) of the vibration power spectrums, and obtaining P'x(f) and P'y(f); and (5) calculating the continuous vibration transmission spectrums from the device X to the device Y. The continuous vibration transmission spectrum determination method of the rocket sled test can directly obtain the high-frequency vibration information and effectively remove the noise so as to realize the quantization description of each-grade vibration transmission characteristic which is continuously changed with the frequency, and the precision is high.

Description

technical field [0001] The invention relates to a method for determining the continuous vibration transfer spectrum of a rocket sled test, belonging to the technical field of mechanical environmental tests. Background technique [0002] The rocket sled is a sled that uses a rocket engine as a thrust to run at high speed on the track. Since the rocket sled can generate a large overload during operation, different types of products are installed on the sled to carry out the rocket sled test. [0003] During the rocket sled test, there are two installation methods for the tested product according to the test requirements. The first method is that the tested product is directly installed on the sled; the second method is that the tested product is installed on the vibration-damping plate, and the The vibrating plate is mounted on the skid through metal shock absorbers. The vibration and impact signals of the sled and the product under test (including the damping plate in the s...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01H17/00
CPCG01H17/00
Inventor 魏宗康董小燕魏珍虹
Owner BEIJING INST OF AEROSPACE CONTROL DEVICES
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