Real-time vibration alarm system for helicopter health monitoring

An alarm system and helicopter technology, applied in the field of avionics, can solve the problems of unbalanced computing load, low integration, high false alarm rate, etc., and achieve the effect of balancing computing load, ensuring flight safety, and improving integration and reliability

Pending Publication Date: 2022-02-01
SHAANXI QIANSHAN AVIONICS
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the development of vibration monitoring technology and flight parameter acquisition and recording technology, health monitoring technology and flight parameter acquisition and recording technology have been widely used in helicopter health monitoring, but the current vibration warning system of helicopters has low integration and unbalanced computing load And only supports offline monitoring, high false alarm rate and other deficiencies

Method used

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  • Real-time vibration alarm system for helicopter health monitoring

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Embodiment Construction

[0027] The present invention will be further described below in conjunction with specific embodiments, and the advantages and characteristics of the present invention will become clearer along with the description. However, these embodiments are only exemplary and do not constitute any limitation to the scope of the present invention. Those skilled in the art should understand that the details and forms of the technical solutions of the present invention can be modified or replaced without departing from the spirit and scope of the present invention, but these modifications and replacements all fall within the protection scope of the present invention.

[0028] In the description of this embodiment, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. are based on the orientatio...

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Abstract

The invention provides a real-time vibration alarm system for helicopter health monitoring, which comprises a vibration monitoring subsystem. The vibration monitoring subsystem comprises a monitoring processor, a vibration alarm assembly and a plurality of first vibration sensors, and the first vibration sensors collect first vibration signals of a helicopter in real time and send the first vibration signals to the monitoring processor. The vibration monitoring subsystem is bidirectionally connected with a flight parameter recording subsystem through a bus, the flight parameter recording subsystem comprises a flight parameter acquisition recorder and a plurality of second vibration sensors, and the second vibration sensors acquire second vibration signals of the helicopter in real time and send the second vibration signals to the monitoring processor. The monitoring processor forms and outputs an alarm signal based on the first vibration signal, the second vibration signal and a vibration alarm judgment condition, and the vibration alarm assembly executes the alarm signal and feeds back an alarm execution result to the monitoring processor. The alarm system has the advantages of high integration level, high reliability, low false alarm rate and the like, and can ensure the flight safety of the helicopter.

Description

technical field [0001] The invention belongs to the field of avionics and relates to the design technology of a real-time vibration warning system, in particular to a real-time vibration warning system for helicopter health monitoring. Background technique [0002] With the development of vibration monitoring technology and flight parameter acquisition and recording technology, health monitoring technology and flight parameter acquisition and recording technology have been widely used in helicopter health monitoring, but the current vibration warning system of helicopters has low integration and unbalanced computing load And only supports offline monitoring, high false alarm rate and other deficiencies. [0003] Therefore, it is necessary to improve the vibration warning system for helicopter health monitoring. Contents of the invention [0004] The purpose of the present invention is to design a real-time vibration alarm system for helicopter health monitoring, which use...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/00B64D47/02
CPCB64D45/00B64D47/02B64D2045/0085B64D2045/0065
Inventor 周鹏甲李伟杰肖方可贾瑞雪代方远白皓张珣王科许中冲吴雷于悦
Owner SHAANXI QIANSHAN AVIONICS
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