Operation state monitoring and emergency stop method for distributed supersonic air flow generation device

A technology for generating devices and operating states, which is applied to jet propulsion devices, gas turbine devices, measuring devices, etc., to achieve the effects of easy inspection, high operating efficiency, and reduced operating load

Active Publication Date: 2021-03-26
XIAN AEROSPACE PROPULSION TESTING TECHN INST
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem of the operation monitoring of the supersonic air flow generating device in the prior art, and provide an efficient and reliable real-time monitoring and emergency stop method for the operation state of the supersonic air flow generating device, so as to prevent the risk from occurring at the beginning Rapid emergency stop control of supersonic air flow generating device

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  • Operation state monitoring and emergency stop method for distributed supersonic air flow generation device

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Embodiment Construction

[0034] Below in conjunction with accompanying drawing, further describe the present invention in detail through embodiment.

[0035] A distributed supersonic air flow generating device operating state monitoring and emergency stop method in this embodiment is implemented based on a distributed measurement lower computer cluster and a measurement upper computer. The measurement lower computer cluster and the measurement upper computer transmit data through the ring optical fiber Ethernet network.

[0036] According to the user's input, the criterion setting is completed on the measurement host computer in advance.

[0037] This operation is carried out on the measurement host computer, including selection of characterization parameters and setting of criteria. To select characterization parameters, it is first necessary to determine the parts that can accurately reflect the operating status of the device, and deploy measurement sensors for these parts, generally including the ...

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Abstract

The invention provides an operation state monitoring and emergency stop method for a distributed supersonic air flow generation device. The method is implemented based on a distributed measurement lower computer cluster and a measurement upper computer, and comprises the following steps that: 1) state characterization parameters are sampled; 2) the parameters are screened; 3) each measurement lower computer unit discriminates corresponding characterization parameter data after parameter screening according to an obtained criterion table; 4) when a certain condition is satisfied, the measurement lower computer unit sends early warning signals of the characterization parameters to the measurement upper computer; and 5) the measurement upper computer conducts early warning summarizing, and sends an emergency stop instruction to a control host when a certain condition is satisfied, so that the supersonic air flow generation device executes an emergency stop program. According to the method, only the criterion table needs to be set and issued on the measurement upper computer, so that the workload is small; and excessive network resources are not occupied, data congestion is avoided, and the risk that equipment is damaged due to the fact that early warning is not conducted in time is reduced.

Description

technical field [0001] The invention belongs to the technical field of ramjet tests, and in particular relates to a method for monitoring the running state of a distributed supersonic air flow generating device and an emergency stop method. Background technique [0002] The supersonic air flow generation device continuously heats the continuous supersonic air flow through liquid oxygen and alcohol combustion to generate a continuous supersonic high-temperature air flow, providing a supersonic high-temperature air flow simulation environment for the ramjet test. The supersonic air flow generating device has risks such as leakage of three high-pressure component pipeline media (liquid oxygen, alcohol, air) and device damage during operation, and it cannot be found in the supersonic air flow generating device through human visual observation. In the early stage of the risk, timely response confirmation and emergency shutdown of the device. [0003] At present, the fault diagno...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K7/10F02C7/00G01M15/04
CPCF02K7/10F02C7/00G01M15/042
Inventor 董冬唐云龙麻军德徐峰安成琳赵恒曹一凡
Owner XIAN AEROSPACE PROPULSION TESTING TECHN INST
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