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A Distributed Supersonic Airflow Generator Operation Status Monitoring and Emergency Stop Method

A technology for generating devices and operating states, which is applied to jet propulsion devices, gas turbine devices, measuring devices, etc., to reduce operating load, reduce the risk of equipment damage, and facilitate inspection

Active Publication Date: 2022-03-11
XIAN AEROSPACE PROPULSION TESTING TECHN INST
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  • Abstract
  • Description
  • Claims
  • Application Information

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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

Method used

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  • A Distributed Supersonic Airflow Generator Operation Status Monitoring and Emergency Stop Method

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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 proposes a distributed supersonic air flow generating device operating state monitoring and emergency stop method. The method is realized based on a distributed measurement slave computer cluster and a measurement host computer, including: step 1) sampling of state representation parameters; step 2) parameter screening; step 3) each measurement slave unit checks the parameter The screened corresponding characterization parameter data is discriminated; step 4) when certain conditions are met, the measurement slave unit sends an early warning signal of the characterization parameter to the measurement host computer; step 5) the measurement host computer makes an early warning summary; The control host sends an "emergency stop" command to make the supersonic air flow generating device execute an emergency stop procedure. The present invention only needs to set and release the criterion table on the measurement host computer, and the workload is small; it does not occupy too many network resources, avoids data congestion, and reduces the risk of equipment damage due to untimely early warning.

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 Patents(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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