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Aircraft tire management method and aircraft tire management device

机译:飞机轮胎管理方法及飞机轮胎管理装置

摘要

In order to adjust the tire internal pressure on landing to an appropriate internal pressure, the internal pressure and temperature of the tires when housed inside the aircraft in flight, the temperature and atmospheric pressure around the aircraft, and the altitudes and air temperatures at the takeoff and landing sites of the aircraft are obtained, and a target internal pressure at takeoff is calculated from information relating to the altitude and air temperature at the takeoff airport, after which an in-flight tire internal pressure whereby the tire internal pressure becomes a target internal pressure on landing is calculated from the temperature and atmospheric pressure around the tires of the aircraft, the air temperature and atmospheric pressure at the landing airport, and information relating to a load anticipated to act on the tires on landing, and subsequently the in-flight tire internal pressure is adjusted so that the obtained internal pressure of the tires housed inside the aircraft becomes the calculated in-flight tire internal pressure.
机译:为了将着陆时的轮胎内部压力调整到适当的内部压力,在飞行中将其容纳在飞机内部时轮胎的内部压力和温度,飞机周围的温度和大气压力以及起飞时的海拔和空气温度获得飞机的起降点,并根据与起飞机场的高度和空气温度有关的信息计算起飞时的目标内部压力,此后,飞行中的轮胎内部压力使轮胎内部压力成为目标内部压力。着陆压力是根据飞机轮胎周围的温度和大气压力,着陆机场的气温和大气压力以及与预计会在着陆轮胎上以及随后在飞行中作用于轮胎的负荷有关的信息来计算的调节轮胎内部压力,以便获得容纳在轮胎内部的轮胎的内部压力。飞机将成为计算出的飞行中轮胎内部压力。

著录项

  • 公开/公告号US10759234B2

    专利类型

  • 公开/公告日2020-09-01

    原文格式PDF

  • 申请/专利权人 BRIDGESTONE CORPORATION;

    申请/专利号US201716094550

  • 发明设计人 YOSHINOBU SHOYAMA;

    申请日2017-04-17

  • 分类号B60C23;B60C23/04;B60C19;B60C23/20;B60S5/04;B64C25/36;B60C23/10;

  • 国家 US

  • 入库时间 2022-08-21 11:29:54

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