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    • 1. 发明申请
    • DATA COLLECTION AND REPORTING SYSTEM AND METHOD
    • 数据采集​​与报告系统及方法
    • WO2017003626A1
    • 2017-01-05
    • PCT/US2016/035134
    • 2016-06-01
    • SIEMENS ENERGY, INC.
    • BANCALARI, AlejandroDEASCANIS, JoshuaHATCHER JR., CliffordRUHGE, Forrest R.
    • G06F11/30G06F1/16G06Q50/10G06Q10/06
    • G06F3/16G06F1/163G06Q10/20G06Q50/06G10L25/48Y02P90/82
    • A wearable device (102) is provided that is configured to carry out an inspection of a gas turbine or other type of system (148). The device may include a processor (104), a data store (110), at least one output device (112), and at least one input device (118). The processor in the wearable device is responsive to inputs through the at least one input device and set of tasks (142) stored in the data store corresponding to an inspection (140) of the system to provide outputs (220, 234) through the at least one output device that prompt a user to gather data (150) associated with the system being inspected using the wearable device while the wearable device is mounted to the user without the user holding the wearable device with the hand of the user. Also, the processor in the wearable device is configured to generate and output an inspection report (152) responsive to the set of tasks and the data gathered using the wearable device.
    • 提供了一种可佩戴装置(102),其被配置为执行燃气轮机或其他类型的系统(148)的检查。 该设备可以包括处理器(104),数据存储(110),至少一个输出设备(112)和至少一个输入设备(118)。 可佩戴装置中的处理器响应于通过至少一个输入装置的输入和对应于系统的检查(140)的存储在数据存储器中的一组任务(142),以提供输出(220,234) 至少一个输出装置,其提示用户使用所述可穿戴装置收集与被检查的系统相关联的数据(150),同时所述可穿戴装置安装到所述用户,而所述用户不用用户的手握住所述可佩戴装置。 此外,可穿戴设备中的处理器被配置为响应于该组任务和使用可穿戴设备收集的数据来产生和输出检查报告(152)。
    • 6. 发明申请
    • IN-SITU BLADE-MOUNTED TIP GAP MEASUREMENT FOR TURBINES
    • 用于涡轮机的现场叶片安装螺纹间隙测量
    • WO2015050658A1
    • 2015-04-09
    • PCT/US2014/053636
    • 2014-09-02
    • SIEMENS ENERGY, INC.
    • RUHGE, Forrest R.HATCHER, JR., Clifford
    • F01D21/00G01B7/14G01B11/14
    • G01B21/16F01D21/003F05D2270/80F05D2270/821G01B11/14G01M15/02G01N21/8803
    • Turbine blade tip (28) clearance is measured in a fully assembled turbine casing by mounting a contact or non-contact displacement probe (40) on a turbine blade (26) that generates data indicative of probe distance from the turbine casing (22) that circumferentially surrounds the blade. Variations in probe distance data are recorded as the blade circumferentially sweeps the turbine casing when the turbine is operated in turning gear mode. Blade rotational position data are collected by a rotational position sensor (60). A data processing system (70, 80, 34) correlates the distance and rotational position data with localized blade tip gap at angular positions about the turbine casing circumference. An optical camera inspection system may be coupled to a turbine blade to obtain visual inspection information within the turbine casing. This method and apparatus provide an accurate and cost effective solution for accessing turbine casing deformation impact on blade tip clearance and rotor/casing alignment.
    • 在完全组装的涡轮机壳体中通过将接触或非接触位移探头(40)安装在涡轮机叶片(26)上来测量涡轮叶片尖端(28)间隙,涡轮叶片(26)产生指示与涡轮机壳体(22)的探测距离的数据, 周向地围绕叶片。 记录探头距离数据的变化,当涡轮机在转向齿轮模式下操作时刀片周向地扫掠涡轮机壳体。 叶片旋转位置数据由旋转位置传感器(60)收集。 数据处理系统(70,80,44)将距离和旋转位置数据与局部的叶片尖端间隙关联在围绕涡轮壳体圆周的角位置处。 光学照相机检查系统可以联接到涡轮机叶片以获得涡轮机壳体内的视觉检查信息。 该方法和装置提供了准确和成本有效的解决方案,用于访问涡轮机壳体变形对叶片顶端间隙和转子/壳体对准的影响。