System and method for monitoring health of airfoils
    1.
    发明授权
    System and method for monitoring health of airfoils 有权
    用于监测机翼健康的系统和方法

    公开(公告)号:US09404386B2

    公开(公告)日:2016-08-02

    申请号:US14089995

    申请日:2013-11-26

    CPC classification number: F01D21/003 F01D5/005 G01M5/0016 G01M5/0033

    Abstract: A method comprising the steps of determining normalized delta times of arrival corresponding to a plurality of blades based upon actual times of arrival corresponding to the plurality of blades, and determining static deflections of the plurality of blades by removing effects of one or more common factors from the normalized delta times of arrival corresponding to the plurality of blades.

    Abstract translation: 一种方法,包括以下步骤:基于与所述多个刀片相对应的实际到达时间来确定对应于多个刀片的归一化的到达时间的到达次数,以及通过从一个或多个刀片的一个或多个常见因素中除去多个刀片的影响来确定所述多个刀片的静态偏转 对应于多个叶片的归一化的到达时间。

    ESTIMATION OF CYLINDER CONDITIONS USING A KNOCK SENSOR

    公开(公告)号:US20190128200A1

    公开(公告)日:2019-05-02

    申请号:US15797555

    申请日:2017-10-30

    Abstract: A reciprocating engine system includes a cylinder, a piston disposed within the cylinder, a knock sensor disposed proximate to the cylinder and configured to detect vibrations of the cylinder, piston, or both, a crankshaft sensor configured to sense a crank angle of a crankshaft, and a controller communicatively coupled to the knock sensor and the crankshaft sensor. The controller is configured to receive a raw knock signal from the knock sensor and a crank angle signal from the crankshaft sensor corresponding to vibrations of the cylinder, piston, or both relative to the crank angle of the crankshaft, convert the raw knock signal into a digital value signal, and at least one of a crank angle for a start of combustion, a peak firing pressure, a percentage of fuel mass fraction burn, or a combination thereof, based on the digital value signal and the crank angle.

    SYSTEM AND METHOD FOR MONITORING HEALTH OF AIRFOILS
    8.
    发明申请
    SYSTEM AND METHOD FOR MONITORING HEALTH OF AIRFOILS 有权
    用于监测航空器健康的系统和方法

    公开(公告)号:US20150226081A1

    公开(公告)日:2015-08-13

    申请号:US14089995

    申请日:2013-11-26

    CPC classification number: F01D21/003 F01D5/005 G01M5/0016 G01M5/0033

    Abstract: A method comprising the steps of determining normalized delta times of arrival corresponding to a plurality of blades based upon actual times of arrival corresponding to the plurality of blades, and determining static deflections of the plurality of blades by removing effects of one or more common factors from the normalized delta times of arrival corresponding to the plurality of blades.

    Abstract translation: 一种方法,包括以下步骤:基于与所述多个刀片相对应的实际到达时间来确定对应于多个刀片的归一化的到达时间的到达次数,以及通过从一个或多个刀片的一个或多个常见因素中除去多个刀片的影响来确定所述多个刀片的静态偏转 对应于多个叶片的归一化的到达时间。

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