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Real-time regression detection system and method for solid rocket propellant burning surface

A solid rocket, real-time detection technology, used in measurement devices, material analysis using sonic/ultrasonic/infrasonic waves, instruments, etc., can solve problems such as large measurement errors and uneven combustion surfaces, to reduce detection errors and improve detection. The effect of precision

Pending Publication Date: 2017-09-08
UNIV OF SHANGHAI FOR SCI & TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the effective information used in this method is reflected waves, it is easily affected by the unevenness of the burning surface, and the measurement error is large

Method used

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  • Real-time regression detection system and method for solid rocket propellant burning surface
  • Real-time regression detection system and method for solid rocket propellant burning surface
  • Real-time regression detection system and method for solid rocket propellant burning surface

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Embodiment Construction

[0021] The specific implementation manners of the present invention will be described below in conjunction with the accompanying drawings.

[0022] figure 1 It is a structural schematic diagram of the real-time detection system for the solid rocket propellant combustion surface retreat in this embodiment.

[0023] Such as figure 1 As shown, the solid rocket propellant combustion surface retreat real-time detection system 100 adopts the working mode of non-contact measurement of ultrasonic transducer. It includes a signal generation unit 11 , a pre-amplification unit 12 , a non-destructive testing unit 13 , a post-amplification unit 14 , a signal conditioning unit 15 , a data acquisition unit 16 and a processing control unit 17 .

[0024] The signal generating unit 11 is used for generating an ultrasonic signal as an original pulse signal; the preamplifying unit 12 is used for amplifying the ultrasonic signal.

[0025] The non-destructive testing unit 13 is arranged near the...

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Abstract

The invention provides a real-time regression detection system and method for a solid rocket propellant burning surface. The real-time regression detection system comprises a signal generation unit used for generating an ultrasonic signal serving as an original pulse signal, a pre-amplification unit used for amplifying the ultrasonic signal, a nondestructive detection unit in contact with the housing of a solid rocket engine, a post-amplification unit used for amplifying a transmission signal, a signal conditioning unit used for converting the transmission signal into a digital signal, and a processing control unit used for processing the digital signal to obtain displacement of the propellant burning surface and the burning rate of a propellant and controlling the signal generation unit, the pre-amplification unit, the nondestructive detection unit, the post-amplification unit and the signal conditioning unit to work, wherein the nondestructive detection unit comprises a plurality of ultrasonic transducer groups arranged at certain intervals, and each ultrasonic transducer group is provided with a transmitting transducer for transmitting the amplified ultrasonic signal and a receiving transducer for receiving the transmission signal penetrating the housing.

Description

technical field [0001] The invention belongs to the field of propellant testing of solid rocket motors, in particular to a real-time detection system for the retreat of the burning surface of the solid rocket propellant and a method for determining the displacement of the burning surface of the propellant in real time and dynamically obtaining the burning speed of the propellant. Background technique [0002] Solid rocket motor is a rocket power device using solid propellant. It has the advantages of simple structure, good maneuverability, high reliability and easy maintenance. It is more and more widely used in rocket weapon systems and plays a huge role in the aerospace field. role. [0003] The reliability of solid rocket motor combustion will directly affect the safety of the entire rocket system. Therefore, it is necessary to use reliable nondestructive testing methods to measure the combustion state of the fuel and the retreat of the combustion surface in real time. B...

Claims

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Application Information

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IPC IPC(8): G01N29/024G01N29/32
CPCG01N29/024G01N29/32G01N2291/011
Inventor 杨斌苏明旭顾建飞杨敬贤潘科玮陈晓龙徐秋丽王伟
Owner UNIV OF SHANGHAI FOR SCI & TECH
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