Solid engine adhesion interface loaded state monitoring device

A solid-state engine and detection device technology, applied in the direction of internal combustion engine testing, etc., to achieve the effects of easy installation, full life cycle measurability, high accuracy and stability

Pending Publication Date: 2017-08-15
NAVAL AERONAUTICAL & ASTRONAUTICAL UNIV PLA
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  • Application Information

AI Technical Summary

Problems solved by technology

So far, embedded sensors have only been used in simulated monitoring and detection engines, and have not been used in real-installe

Method used

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  • Solid engine adhesion interface loaded state monitoring device
  • Solid engine adhesion interface loaded state monitoring device
  • Solid engine adhesion interface loaded state monitoring device

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Experimental program
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Embodiment Construction

[0028] 1. Solid engine and its monitoring and detection system

[0029] The structure of the solid engine is mainly composed of an ignition device, a combustion chamber, and a nozzle. The combustion chamber is the core component of the solid engine, and the bonding interfaces of the engine are the weak parts of the combustion chamber. Therefore, the monitoring of the health status of the bonding interface is an important part of the health monitoring of the engine structure. According to the causes, characteristics and failure mode analysis results of the debonding of the engine bonding interface, the target quantity of the solid engine structure health monitoring is determined to be the stress and temperature of the grain bonding interface.

[0030] The solid engine structural health monitoring system is mainly composed of hardware-solid engine bonding interface loading state monitoring device and software. The hardware part includes the sensor network and the corresponding...

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Abstract

The invention discloses a solid engine adhesion interface loaded state monitoring device, which comprises stress-temperature sensors arranged on the inner wall of a solid engine, a stress transmitter which is arranged outside the solid engine and connected with the stress-temperature sensor by means of lead wires, and a data acquisition device and an excitation power supply which are connected with the stress transmitter. Different from the prior art, the solid engine adhesion interface loaded state monitoring device is characterized that the number of the stress-temperature sensors is nine, the stress-temperature sensors are of a plane membrane cylindrical structure, the diameter of each sensor is less than or equal to phi 15 mm, the thickness thereof is less than or equal to 3 mm, the lead wires are insulated flat connecting lines with a width of 3 mm and a thickness of about 0.1 mm; and the solid engine adhesion interface loaded state monitoring device is embedded in a thermal insulation layer/lining interface of a solid rocket engine. Compared with the prior art, the solid engine adhesion interface loaded state monitoring device is easy to install, does not affect a powder charge stress field, has high precision and stability, and can monitor the required data information comprehensively, has low influence on strength property, storage property and operating property of an engine adhesion interface after being embedded, and does not cause destructive impact on the structure of the engine.

Description

technical field [0001] The invention relates to the technical field of detection of rocket solid motors, in particular to a monitoring and detection device for the loading state of the bonding interface of the solid motor. Background technique [0002] Due to its simple structure, convenient use and maintenance, high reliability, stable storage performance, high mobility and good economy, solid rocket motors are the most popular among the more than 100 kinds of missiles currently in service and under development in various countries. Accounted for more than 80%. After more than 40 years of development, most of the first-stage or second-stage engines of the missiles currently in service in my country use them as propulsion power devices. Because solid rocket motors are stored for a long time and used once, the industrial sector has uniformly given its storage and service life when delivering solid rocket motors to troops. However, in the actual use of the army, due to the d...

Claims

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Application Information

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IPC IPC(8): G01M15/05
CPCG01M15/05
Inventor 张波董可海唐岩辉张春龙裴立冠张旭东王永帅于畅吴昊
Owner NAVAL AERONAUTICAL & ASTRONAUTICAL UNIV PLA
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