The invention relates to an aircraft tire pressure abnormity monitoring method and system. The method comprises the following steps: acquiring a current external temperature value, an actual wheel pressure value and a first wheel pressure key parameter; judging whether the actual wheel pressure value meets a first preset condition or not by utilizing a preset tire pressure abnormity alarm message model; if so, generating and sending a first tire pressure abnormity alarm message; judging whether the current first wheel pressure key parameter and the current second wheel pressure key parameter meet a second preset condition or not by utilizing a preset tire pressure abnormity alarm message model; if so, generating a second tire pressure abnormity alarm message and sending the second tire pressure abnormity alarm message; the first tire pressure abnormity alarm message and the second tire pressure abnormity alarm message are received and analyzed, the current external temperature value is received and utilized to correct and filter the analyzed alarm messages, and effective messages are obtained; and displaying and sending the effective message. Compared with the prior art, the method has the advantages of quickly and accurately predicting the tire pressure abnormity of the aircraft in advance, predicting the tire pressure in advance and the like.
本发明涉及一种飞机轮胎压力异常监控方法及系统。该方法获取当前的外界温度值、实际轮压值和第一轮压关键参数;利用预设的轮胎压力异常报警报文模型判断实际轮压值是否符合第一预设条件:若为是,则生成第一轮胎压力异常报警报文并发送;利用预设的轮胎压力异常报警报文模型判断当前的第一轮压关键参数和第二轮压关键参数是否符合第二预设条件:若为是,则生成第二轮胎压力异常报警报文并发送;接收并解析第一、第二轮胎压力异常报警报文,接收并利用当前的外界温度值修正并过滤解析后报警报文,得到有效报文;显示并发送有效报文。与现有技术相比,本发明具有快速、准确地提前预知飞机轮胎压力异常,提前预测轮胎压力等优点。
Aircraft tire pressure abnormity monitoring method and system
一种飞机轮胎压力异常监控方法及系统
25.03.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B60C VEHICLE TYRES , Fahrzeugreifen |
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