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Vibration test system and test method for full missile vibration in rotating state of rotating missile

A technology of vibration test and rotation state, applied in vibration test, machine/structural component test, wave/particle radiation, etc., can solve the problems of insufficient reliability and environmental adaptability assessment of rotating missiles, and achieve the balance of gravity Effect

Pending Publication Date: 2022-07-12
SHANGHAI SPACE PRECISION MACHINERY RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the present invention provides a vibration test system and test method for full-bomb vibration under the rotating state of the rotating missile, and solves the problems that the reliability and environmental adaptability assessment of the rotating missile is not sufficient for the missile vibration environment test under the non-rotating state.

Method used

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  • Vibration test system and test method for full missile vibration in rotating state of rotating missile
  • Vibration test system and test method for full missile vibration in rotating state of rotating missile
  • Vibration test system and test method for full missile vibration in rotating state of rotating missile

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Embodiment 1

[0047] The present invention provides a vibration test system for full-bullet vibration under the rotating state of a rotating missile, such as Figure 1-6 As shown, it includes a vibration device 100 , a fixing device 200 and a rotating device 300 . The fixing device 200 fixes the rotating missile 17 on the vibration device 100 , and the end of the rotating missile 17 is connected to the rotating device 300 ; the rotating missile 17 realizes vibration excitation through the vibration device 100 The application of the rotating missile 17 through the fixing device 200 realizes the balance of the gravity of the missile, and the rotating missile 17 realizes the application of the rotating motion through the rotating device 300 .

[0048] The fixing device 200 includes a missile hoisting ring 9, a rubber rope 10 and a gantry 11. The missile hoisting ring 9 is evenly connected to the rotating missile 17 to drive the rotating missile to maintain gravity balance. like Figure 4 As s...

Embodiment 2

[0055] The present invention also provides a test method for the vibration test system of the full-elastic vibration under the rotating state of the rotating missile, which specifically includes the following steps:

[0056] Step 1: use three-dimensional design software, dynamic analysis software, and system simulation software to establish the mapping of the entire test system in the virtual digital space, and conduct virtual experiments in the virtual digital space;

[0057] Step 2: In the virtual digital space, continuously adjust the position of the excitation point and the suspension position, and select the optimal position of the excitation point, suspension position, and vibration control point according to the virtual test results, and obtain the dynamic transfer characteristics of the missile. parameter;

[0058] Step 3: Design the vibration fixture 7, the missile suspension ring 9 and the rotating fixture 12 according to the selected optimal excitation point positio...

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Abstract

The invention provides a vibration test system and test method for full-missile vibration in a rotating state of a rotating missile, and relates to the technical field of missile mechanical environment tests, the vibration test system comprises a vibration device, a fixing device and a rotating device, the fixing device fixes the rotating missile on the vibration device, and the tail end of the rotating missile is connected with the rotating device; the rotating missile achieves application of vibration excitation through the vibration device, achieves balance of missile gravity through the fixing device and achieves application of rotating motion through the rotating device. According to the invention, the vibration dynamics environment experienced by the rotating missile in the flight process can be simulated more truly, and the reliability and vibration environment adaptability of the rotating missile can be fully examined. A non-contact laser sensor is adopted, measurement and control of vibration of the whole missile in the rotating state of the missile are achieved, and the problem that a traditional sensor cannot measure vibration under rotating motion is solved.

Description

technical field [0001] The invention relates to the technical field of missile mechanics environmental test, in particular to a vibration test system and a test method for full missile vibration under the rotating state of a rotating missile. Background technique [0002] As a kind of missile suitable for short-range, low altitude and fast response, the rotating missile has the advantages of simple structure, flexible operation and low cost. It is often used in terminal defense systems. Compared with ordinary missiles, the biggest feature of rotating missiles is that The projectile performs periodic rotational motion, and the frequency is generally between 10 and 20 Hz, so the aerodynamic force generated by the air rudder also performs periodic motion. In the case of only one pair of rudder surfaces, the control force in the 360° direction can also be generated, so the rotating missile can achieve single-channel control through a pair of rudders. However, the rotating state...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M7/02G01H9/00
CPCG01M7/02G01M7/022G01M7/027G01H9/00Y02T90/00
Inventor 汤杰陈洋利云云盛鹏王肇喜管耀耀傅烨沈晨晨
Owner SHANGHAI SPACE PRECISION MACHINERY RES INST
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