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    • 11. 发明公开
    • AIRCRAFT TYRE PRESSURE MONITORING SYSTEM
    • SYSTEM ZURFLUGZEUGREIFENDRUCKÜBERWACHUNG
    • EP3150408A1
    • 2017-04-05
    • EP16190837.1
    • 2016-09-27
    • Airbus Operations Limited
    • BILL, Andrew
    • B60C23/04
    • B60C23/0405B60C23/0474B60C23/0476B60C23/0484B60C23/0486B64D45/00B64F5/60G07C5/006
    • A method of operating a monitoring system to provide pressure warnings associated with a tyre of an aircraft. The monitoring system comprises a flight deck display (15) on a flight deck (16) of the aircraft and a processor (12). When the aircraft is stationary, the processor (12) operates in a maintenance mode (24) in which the processor (12) receives a first pressure measurement indicating a pressure of the tyre; compares the first pressure measurement with a maintenance mode low pressure threshold, and causes the flight deck display to display a low pressure warning associated with the tyre if the first pressure measurement is below the maintenance mode low pressure threshold. When the aircraft is in motion, the processor (12) operates in a flight mode (26) in which the processor (12) receives a second pressure measurement indicating a pressure of the tyre, compares the second pressure measurement with an abnormal pressure threshold which is lower than the maintenance mode low pressure threshold, and causes the flight deck display (15) to display an abnormal pressure warning associated with the tyre if the second pressure measurement is below the abnormal pressure threshold. When the processor (12) is in the flight mode (26), if the second pressure measurement is between the maintenance mode low pressure threshold and the abnormal pressure threshold, then the processor (12) does not cause the flight deck display (15) to display a low pressure warning associated with the tyre, so the flight crew is not distracted.
    • 一种操作监视系统以提供与飞行器的轮胎相关联的压力警告的方法。 监视系统包括在飞行器的飞行甲板(16)上的飞行甲板显示器(15)和处理器(12)。 当飞机静止时,处理器(12)在其中处理器(12)接收指示轮胎的压力的第一压力测量的维护模式(24)中操作; 将第一压力测量与维护模式低压阈值进行比较,并且如果第一压力测量低于维护模式低压阈值,则使驾驶舱显示器显示与轮胎相关联的低压警告。 当飞行器运动时,处理器(12)以飞行模式(26)操作,其中处理器(12)接收指示轮胎压力的第二压力测量值,将第二压力测量值与异常压力阈值进行比较 低于维护模式低压阈值,并且如果第二压力测量值低于异常压力阈值,则导致驾驶舱显示器(15)显示与轮胎相关联的异常压力警告。 当处理器(12)处于飞行模式(26)时,如果第二压力测量处于维护模式低压阈值和异常压力阈值之间,则处理器(12)不引起飞行甲板显示(15) 显示与轮胎相关的低压警告,所以飞行机组人员不会分心。
    • 12. 发明公开
    • METHOD OF CHECKING THE PRESSURE OF AN AIRCRAFT TYRE
    • VERFAHREN ZUR KONTROLLE DES DRUCKES EINES FLUGZEUGREIFENS
    • EP3069903A1
    • 2016-09-21
    • EP16161277.5
    • 2016-03-18
    • Airbus Operations Limited
    • BILL, Andrew
    • B60C23/04
    • B60C23/0476B60C23/04B60C23/0422B60C23/0479B60C2200/02B64C25/36
    • A method of checking the pressure of a tyre of an aircraft. A pressure reading is taken from the tyre with a pressure sensor and wirelessly transmitted to a hand-held device. The hand-held device receives the pressure reading, an aircraft ID which uniquely identifies the aircraft, and a tyre ID. The device then retrieves from a memory a reference pressure level associated in the memory with the aircraft ID and the tyre ID; compares either the pressure reading, or an adjusted pressure based on the pressure reading, with the reference pressure level; and displays a warning if the pressure reading, or the adjusted pressure based on the pressure reading, is below the reference pressure level.
    • 一种检查飞机轮胎压力的方法。 用压力传感器从轮胎中取出压力读数,并将其无线传送到手持式装置。 手持装置接收压力读数,唯一地识别飞机的飞行器ID和轮胎ID。 然后,设备从存储器检索与存储器相关联的与飞行器ID和轮胎ID的参考压力水平; 将压力读数或基于压力读数的调节压力与参考压力水平进行比较; 并且如果压力读数或基于压力读数的调节压力低于参考压力水平,则显示警告。
    • 18. 发明公开
    • TIRE STATE SENSING DEVICE AND TIRE STATE MONITORING DEVICE
    • REIFENZUSTANDMESSVORRICHTUNG UND REIFENZUSTANDBERBERCHSVORRICHTUNG
    • EP3132953A4
    • 2017-08-02
    • EP15834664
    • 2015-06-26
    • TAIHEIYO KOGYO KK
    • TSUJITA YASUHISA
    • B60C23/04
    • B60C23/0416B60C23/0437B60C23/0462B60C23/0476B60C23/0483B60C23/0488B60C23/0489
    • A tire condition detecting apparatus includes a condition detecting section, a transmission section, and a transmission-side control section. The condition detecting section detects the condition of the corresponding tire. The transmission section is configured to transmit a signal that contains information related to the condition of the tire to a receiver, which includes a reception-side control section. The reception-side control section identifies the position of the wheel assembly in which the tire condition detecting apparatus is provided based on the received signal strength indication (RSSI) of the signal. The transmission-side control section causes the transmission section to transmit the signal. The transmission-side control section is configured to cause a position detecting signal and an instruction signal to be transmitted from the transmission section to the receiver. The position detecting signal is configured to cause the reception-side control section to identify the position of the tire condition detecting apparatus. The instruction signal is transmitted before the position detecting signal is transmitted and instructs the reception-side control section to start obtaining the RSSI.
    • 轮胎状态检测设备包括状态检测部分,变速器部分和变速器侧控制部分。 条件检测部分检测相应轮胎的状况。 发送部分被配置为将包含与轮胎的状况有关的信息的信号发送到包括接收侧控制部分的接收器。 接收侧控制部分基于信号的接收信号强度指示(RSSI)来识别轮胎状态检测设备所在的轮组件的位置。 发送侧控制部分使发送部分发送信号。 发送侧控制部分被配置为使位置检测信号和指令信号从发送部分发送到接收器。 位置检测信号被配置为使接收侧控制部分识别轮胎状态检测设备的位置。 指示信号在发送位置检测信号之前被发送,并指示接收侧控制部分开始获取RSSI。
    • 19. 发明公开
    • TIRE STATE SENSING DEVICE AND TIRE STATE MONITORING DEVICE
    • REIFENZUSTANDMORRICHTUNG UNDREIFENZUSTANDÜBERWACHUNGSVORRICHTUNG
    • EP3132953A1
    • 2017-02-22
    • EP15834664.3
    • 2015-06-26
    • Pacific Industrial Co., Ltd.
    • TSUJITA, Yasuhisa
    • B60C23/04
    • B60C23/0416B60C23/0437B60C23/0462B60C23/0476B60C23/0483B60C23/0488B60C23/0489
    • A tire condition detecting apparatus includes a condition detecting section, a transmission section, and a transmission-side control section. The condition detecting section detects the condition of the corresponding tire. The transmission section is configured to transmit a signal that contains information related to the condition of the tire to a receiver, which includes a reception-side control section. The reception-side control section identifies the position of the wheel assembly in which the tire condition detecting apparatus is provided based on the received signal strength indication (RSSI) of the signal. The transmission-side control section causes the transmission section to transmit the signal. The transmission-side control section is configured to cause a position detecting signal and an instruction signal to be transmitted from the transmission section to the receiver. The position detecting signal is configured to cause the reception-side control section to identify the position of the tire condition detecting apparatus. The instruction signal is transmitted before the position detecting signal is transmitted and instructs the reception-side control section to start obtaining the RSSI.
    • 轮胎状况检测装置包括条件检测部,发送部和发送侧控制部。 条件检测部检测相应轮胎的状况。 发送部被配置为将包含与轮胎的状况有关的信息的信号发送到包括接收侧控制部的接收机。 接收侧控制部根据信号的接收信号强度指示(RSSI)来识别提供了轮胎状况检测装置的车轮组件的位置。 发送侧控制部使发送部发送信号。 发送侧控制部被配置为使得位置检测信号和指示信号从发送部分发送到接收器。 位置检测信号被配置为使得接收侧控制部分识别轮胎状态检测装置的位置。 在发送位置检测信号之前发送指示信号,指示接收侧控制部开始获取RSSI。
    • 20. 发明公开
    • METHOD OF MONITORING THE PRESSURE OF AN AIRCRAFT TYRE
    • VERFAHREN ZURÜBERWACHUNGDES DRUCKS EINES FLUGZEUGREIFENS
    • EP3069904A1
    • 2016-09-21
    • EP16161289.0
    • 2016-03-18
    • Airbus Operations Limited
    • Bill, Andrew
    • B60C23/04
    • B60C23/0476B60C23/0408B60C23/0474B60C23/0486B60C2200/02G01K11/00G01L17/00G01M17/02
    • A method of monitoring the pressure of a tyre of an aircraft, the method comprising: taking two or more pressure readings from the tyre at different times; calculating an estimated deflation rate based on the pressure readings; and calculating a time for the tyre to deflate to a reference pressure level based on the estimated deflation rate. Two or more temperature readings are each associated with one of the pressure readings, and the estimated deflation rate is calculated by normalising each pressure reading based on its associated temperature reading and a common reference temperature to obtain a temperature-normalised pressure reading, and calculating the estimated deflation rate based on the temperature-normalised pressure readings. The estimated deflation rate is compared with a threshold, and a warning provided if the estimated deflation rate exceeds the threshold.
    • 一种监测飞行器轮胎压力的方法,该方法包括:在不同时间从轮胎取两个或多个压力读数; 基于压力读数计算估计的通货膨胀率; 以及基于所估计的通气量计算轮胎缩短到基准压力水平的时间。 两个或更多个温度读数各自与压力读数之一相关联,并且通过根据其相关联的温度读数和公共参考温度归一化每个压力读数来计算估计的放气速率,以获得温度归一化压力读数,并且计算 基于温度归一化压力读数的估计通气率。 将估计的通缩率与阈值进行比较,如果估计的通风速率超过阈值,则提供警告。