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    • 2. 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。
    • 3. 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。