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System and method for online measurement of vibration of solid rocket engine

A solid engine and measurement module technology, which is applied in the direction of measuring devices, ultrasonic/sonic/infrasonic measurement, internal combustion engine testing, etc., can solve the problems of charge accumulation effect, small charge, poor DC response, etc.

Active Publication Date: 2017-01-04
内蒙航天动力机械测试所
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, piezoelectric accelerometers also have some disadvantages. First, due to the small amount of charge generated, the generated signal is very weak and the output impedance is high, and the output DC response is poor. It is necessary to use a high input impedance circuit or a charge amplifier to overcome this problem. Defects; secondly, it is seriously disturbed by the electric field, and there is a charge accumulation effect. For continuous high-frequency shocks and charge accumulation effects, the piezoelectric accelerometer cannot respond continuously, and the output is saturated; again, due to the leakage phenomenon on the edge of the crystal, charge leakage will occur. Therefore it cannot be used for steady-state, static measurements

Method used

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  • System and method for online measurement of vibration of solid rocket engine
  • System and method for online measurement of vibration of solid rocket engine
  • System and method for online measurement of vibration of solid rocket engine

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Embodiment Construction

[0020] Now according to figure 1 Take radial vibration measurement as an example to illustrate. Place two vertical rods 1 on the left and right sides of the solid motor that has been connected. A crossbar 2 is added to the top of the pole 1, and a dark box 4 is fixed on the crossbar 2. A light box 5 and a linear array CCD sensor 7 are installed in the dark box 4. There is a light-emitting diode array 3 in the light box 5, and the light-emitting diode array 3 consists of Light emitting diodes with a wavelength of 550nm are arranged, and different luminous brightness can be obtained by adjusting the current of the light emitting diodes. There is a vertical slit on the front of the light box 5, and the effect of the slit is to change the light emitted by the LED array 3 into linearly polarized light. The linear array CCD sensor 7 is composed of a series of pixels arranged linearly, the direction of the pixels is consistent with the direction of the slit of the light box 5, and ...

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PUM

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Abstract

The invention discloses a system and method for online measurement of vibration of a solid rocket engine, and relates to the field of machining manufacture and optical measurement. The system performs measurement by employing a measuring module formed by a camera obscura and a blocking piece, the inner part of the camera obscura includes a light emitting diode array, a lamp box, and a linear array CCD sensor, different light-emitting brightnesses can be obtained through adjustment of the current of the light emitting diodes, the front surface of the lamp box is provided with a vertical slit, light emitted by the light emitting diode array can be changed to linearly polarized light through the vertical slit, the linear array CCD sensor is used for receiving the light emitted by the lamp box, and the goal of online measurement is finally achieved by optical signals received by the linear array CCD sensor. According to the system and method, inevitable defects of many conventional piezoelectric accelerometers are overcome, the measuring precision is radically improved, and the measuring efficiency is improved.

Description

technical field [0001] The invention relates to a solid rocket motor testing technology, in particular to a system and method for on-line measuring the vibration of a solid rocket motor, and belongs to the fields of mechanical processing and optical measurement. Background technique [0002] The system composed of the engine and the test frame will vibrate under the impact of the engine ignition and shutdown and the unstable combustion during the whole working process. When the vibration is severe, the structural strength of the engine and test equipment may decrease, cracks may occur in the propellant, and the equipment on the bomb may fail. This not only directly affects the working performance of the engine, but may even lead to the failure of the engine test and missile flight, so the vibration measurement in the engine test is very necessary. [0003] The vibration generated during the working process of the engine is basically random vibration. The amplitude and phas...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01H9/00G01M15/12
CPCY02T90/00
Inventor 郭东升蒋韫韬张海旺江晓瑞郭畅张昱
Owner 内蒙航天动力机械测试所
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