Equivalent method for on-board initiating explosive device explosion shock spectra

A technology of explosive shock and pyrotechnics, which is applied to the equivalent field of explosive shock spectrum of pyrotechnics on the planet, can solve the problems of lack of engineering analysis methods, shock-sensitive device hazards, and high cost, and achieve the effect of simple test methods

Active Publication Date: 2017-05-10
AEROSPACE DONGFANGHONG SATELLITE
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Problems solved by technology

[0002] In order to achieve specific functions, mechanical products such as star and arrow belts, solar wings on the star, antennas, and outriggers need to be unlocked with explosive device devices, and use the load generated by the combustion and explosion of the charge to realize their functions. When the device explodes, it will produce high-level, broadband, and short-term complex oscillating explosive shock loads, which usually propagate in the form of high-frequency stress waves in the structure, which will cause microelectronic chips and component solder joints in spacecraft electronic products. , crystal oscillator, electromagnetic relay, etc., which will affect the on-orbit performance of the product
[0003] Due to the lack of accurate and effective engineering analysis methods for the stress and deformation of products under the impact of explosion and impact environment of pyrotechnics, in the design of products, the adaptability under the impact of explosion separation and impact environment can only be considered qualitatively
At present, the electronic equipment with a large shock response in the explosive shock test of pyrotechnic products on the planet needs to be assessed and evaluated for the shock environment, but it is very expensive to use pyrotechnic devices to simulate the explosive shock environment. According to the standards MIL-HDBK-340A, NASA- STD-7003 and GJB 1027A carry out identification tests on products, and the test methods generally adopt the classic shock response spectrum method
However, for products with relatively large impacts near pyrotechnics, the shock spectrum shows that the low-frequency magnitude is low, and some high-frequency frequency peaks are high. It is difficult for pendulums, electric vibration tables and bubble shock tables on the ground to simulate the shock response of this spectrum.
If the shock test is carried out according to the peak value actually measured, due to the limitation of the test equipment, it is difficult to achieve, and it will also cause the shock to pass the test and cause harm to the shock-sensitive devices. Therefore, the shock response of explosive explosives is equivalent to the shock spectrum of the general test specification. relationships matter

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  • Equivalent method for on-board initiating explosive device explosion shock spectra
  • Equivalent method for on-board initiating explosive device explosion shock spectra
  • Equivalent method for on-board initiating explosive device explosion shock spectra

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Embodiment Construction

[0035] The basic train of thought of the present invention is: the equivalent method of proposing a kind of pyrotechnic product explosion shock spectrum on the star is as follows: (1) obtain the explosive shock time-domain acceleration spectrum value of the device pyrotechnic product on the star, convert into shock response spectrum; (2) ) using the shock response spectrum to obtain the vibration displacement at different frequency points, such as Figure 5 (3) Accumulative summation of the vibration displacement at each frequency point; (4) According to the impact acceleration spectrum value imposed on the satellite by the satellite general ground impact test, according to steps (2) and (3), the ground general The cumulative sum of the displacements of the shock response spectrum; (5) according to steps (3) and (4), determine the displacement ratio of the shock response spectrum of the on-board equipment and the general shock response spectrum conditions on the ground. (6) Us...

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Abstract

An equivalent method for on-board initiating explosive device explosion shock spectra includes the steps: (1) acquiring on-board equipment initiating explosive device explosion shock time domain acceleration spectrum values and converting the spectrum values into shock response spectra; (2) acquiring vibration displacement for obtaining different frequency points by the aid of the shock response spectra; (3) accumulating and summing the vibration displacement of each frequency point; (4) acquiring displacement cumulative sum of the ground universal shock response spectra according to on-board applied shock acceleration spectrum values in satellite universal ground impact test and according to the steps (2) and (3); (5) determining the displacement ratio of the shock response spectra of on-board equipment to ground universal shock response spectrum conditions according to the steps (3) and (4); (6) acquiring the shock response spectra equivalent to on-board equipment initiating explosive device explosion shock by the aid of the obtained ratio and universal shock response spectra of on-board equipment ground impact tests.

Description

technical field [0001] The invention relates to an equivalent method for the explosion shock spectrum of pyrotechnics on a planet, which is suitable for a ground shock platform to truly simulate the explosion and shock environment of pyrotechnics on a planet, and to assess and evaluate the influence of the shock environment on products on the planet. Background technique [0002] In order to achieve specific functions, mechanical products such as star and arrow belts, solar wings on the star, antennas, and outriggers need to be unlocked with explosive device devices, and use the load generated by the combustion and explosion of the charge to realize their functions. When the device explodes, it will produce high-level, broadband, and short-term complex oscillating explosive shock loads, which usually propagate in the form of high-frequency stress waves in the structure, which will cause microelectronic chips and component solder joints in spacecraft electronic products. , cr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/313
CPCG01N3/313G01N2203/0039
Inventor 扈勇强杨新峰邹轶群
Owner AEROSPACE DONGFANGHONG SATELLITE
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