公开(公告)号：US20090078053A1

公开(公告)日：2009-03-26

申请号：US11861582

申请日：2007-09-26

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: G01H11/00

CPC classification number: G01H1/006

Abstract: A method and apparatus for monitoring vibrations in a blade structure of a turbine including generating signals from a probe located adjacent to a radial outer edge of the blade structure to provide signals corresponding to vibrations at predetermined locations along the tips of the blades. A leading edge of a blade tip is detected during a blade tracking operation, and a known location along the length of the blade tips is monitored during a vibration measurement operation. The measurement operation may be performed simultaneously with the tracking operation to provide measurements as the axial location of the blades change during transitional modes of operation of the turbine.

Abstract translation: 一种用于监测涡轮机叶片结构中的振动的方法和装置，包括从位于叶片结构的径向外边缘附近的探头产生信号，以提供对应于沿叶片尖端的预定位置的振动的信号。 在叶片跟踪操作期间检测叶片尖端的前缘，并且在振动测量操作期间监测沿叶片尖端的长度的已知位置。 测量操作可以与跟踪操作同时进行，以在叶片的轴向位置在涡轮机的过渡操作模式期间改变时提供测量值。

公开(公告)号：US20090078052A1

公开(公告)日：2009-03-26

申请号：US11923748

申请日：2007-10-25

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: G01H1/06

CPC classification number: G01H1/003 ,  G01H1/08

Abstract: A method of matching sensors in a multi-probe blade vibration monitor for a turbine. The method includes providing at least two probes mounted in a casing of the turbine adjacent to a rotating blade structure of the turbine. Targets are provided on radially outer portions of the blade structure. Each of the probes includes a sensor generating signals corresponding to target passing events, and a set of synchronous harmonics of the rotational speed of the rotor are produced for each sensor. The position of the sensors is adjusted such that the sets of harmonics of the sensors are substantially matched, indicating that the positions of the sensors are matched.

Abstract translation: 一种用于涡轮机的多探针叶片振动监测器中匹配传感器的方法。 该方法包括提供安装在涡轮机壳体中的至少两个探针，其与涡轮机的旋转叶片结构相邻。 靶设置在叶片结构的径向外部。 每个探头包括产生对应于目标通过事件的信号的传感器，并且为每个传感器产生一组转子的转速的同步谐波。 调整传感器的位置，使得传感器的谐波组合基本匹配，表明传感器的位置匹配。

公开(公告)号：US07230205B2

公开(公告)日：2007-06-12

申请号：US11093126

申请日：2005-03-29

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: H05B1/00

CPC classification number: H05B1/0213

Abstract: In some instances, ice can form on the surface of a compressor airfoil. If the ice dislodges, it can impact and damage other compressor components. Aspects of the invention relate to systems for detecting the presence of ice or water on a compressor vane during engine operation. A ceramic insulating coating can be deposited on a portion of the surface of the vane. A heater and a thermocouple can be provided near the outermost surface of the coating such that the thermocouple can sense heat from the heater. The heater and the thermocouple can be provided within the coating. The presence of water film and/or ice on the coating surface can be detected by taking a thermocouple measurement following a heater pulse. The presence of a water film or ice results in a delay in the temperature rise detected by the thermocouple.

Abstract translation: 在某些情况下，冰可以形成在压缩机翼面的表面上。 如果冰块移动，它可能会影响和损坏其他压缩机组件。 本发明的方面涉及用于在发动机操作期间检测压缩机叶片上的冰或水的存在的系统。 陶瓷绝缘涂层可以沉积在叶片表面的一部分上。 可以在涂层的最外表面附近提供加热器和热电偶，使得热电偶可以感测来自加热器的热量。 加热器和热电偶可以在涂层内提供。 可以通过在加热器脉冲之后进行热电偶测量来检测涂层表面上的水膜和/或冰的存在。 水膜或冰的存在导致热电偶检测到的温度上升延迟。

公开(公告)号：US20060237416A1

公开(公告)日：2006-10-26

申请号：US11093126

申请日：2005-03-29

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: H05B11/00 ,  H05B1/00 ,  H05B3/00

CPC classification number: H05B1/0213

Abstract: In some instances, ice can form on the surface of a compressor airfoil. If the ice dislodges, it can impact and damage other compressor components. Aspects of the invention relate to systems for detecting the presence of ice or water on a compressor vane during engine operation. A ceramic insulating coating can be deposited on a portion of the surface of the vane. A heater and a thermocouple can be provided near the outermost surface of the coating such that the thermocouple can sense heat from the heater. The heater and the thermocouple can be provided within the coating. The presence of water film and/or ice on the coating surface can be detected by taking a thermocouple measurement following a heater pulse. The presence of a water film or ice results in a delay in the temperature rise detected by the thermocouple.

Abstract translation: 在某些情况下，冰可以形成在压缩机翼面的表面上。 如果冰块移动，它可能会影响和损坏其他压缩机组件。 本发明的方面涉及用于在发动机操作期间检测压缩机叶片上的冰或水的存在的系统。 陶瓷绝缘涂层可以沉积在叶片表面的一部分上。 可以在涂层的最外表面附近提供加热器和热电偶，使得热电偶可以感测来自加热器的热量。 加热器和热电偶可以在涂层内提供。 可以通过在加热器脉冲之后进行热电偶测量来检测涂层表面上的水膜和/或冰的存在。 水膜或冰的存在导致热电偶检测到的温度上升延迟。

公开(公告)号：US07123031B2

公开(公告)日：2006-10-17

申请号：US11018771

申请日：2004-12-20

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: G01R27/08 ,  G01N27/00

CPC classification number: G01B7/18 ,  G01N2203/0664

Abstract: Aspects of the invention relate to a system for assessing the condition of a thermal barrier coating on a turbine vane during engine operation. According to embodiments of the invention, one or more wires can be passed along the airfoil portion of the vane. The wires can extend over, within, or beneath the thermal coating. An electrical current can be passed along the wires, and electrical resistance can be measured across the wires. Thus, if a portion of the thermal coating becomes damaged, then the wires located in that area may break. A disconnect in the wires can lead to an increase in resistance across the wires, which can alert an operator to a problem. Some assessment systems can provide a general indication of the magnitude of damage and whether the damage is spreading.

公开(公告)号：US6094989A

公开(公告)日：2000-08-01

申请号：US138187

申请日：1998-08-21

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: G01N29/07 ,  G01N29/14 ,  G01N29/46 ,  G01N29/00

CPC classification number: G01N29/14 ,  G01N29/07 ,  G01N29/46 ,  G01N2291/015 ,  G01N2291/2693

Abstract: Non-synchronous vibrations in blades on a rotating wheel, such as a turbine wheel, are measured using Fourier analysis adjusted to correct for uneven sampling produced by a pair of probes spaced from each other about the wheel by a probe angle (PA) other than 180.degree.. The Fourier transform matrix is phase shifted by an amount which is a function of the PA which is other than 180.degree., and the harmonic in which the mode of non-synchronous vibration is expected to be found. A scaling factor in the form of an inverse correction factor is applied to the frequency spectra produced by the phase shifted Fourier transform matrix to generate an output representative of the frequency and amplitude of the true excitation frequency which can be presented on a display.

Abstract translation: 使用傅立叶分析来测量旋转轮上的叶片（例如涡轮机轮）中的非同步振动，以校正由围绕车轮相互间隔的一对探针产生的不均匀采样，除了除了 180度。 傅里叶变换矩阵相位移是除了180度以外的PA的函数的量以及期望发现非同步振动模式的谐波。 将逆校正因子形式的缩放因子应用于由相移傅立叶变换矩阵产生的频谱，以产生表示可以在显示器上呈现的真实激发频率的频率和幅度的输出。

公开(公告)号：US5152309A

公开(公告)日：1992-10-06

申请号：US706912

申请日：1991-05-29

Applicant: Michael Twerdochlib ,  David E. Bateman

Inventor： Michael Twerdochlib ,  David E. Bateman

IPC: G01F1/00 ,  G05D7/06

CPC classification number: G05D7/0635 ,  Y10T137/0357 ,  Y10T137/7759 ,  Y10T137/7761

Abstract: The present invention provides a valve control apparatus which can be programmed to deliver a desired flow of gas. A valve 22 is connected to a stepper motor 28 which is controlled by a computer 32 to open or close the valve in steps within a gas flow line 24 to deliver a desired rate of flow. A flowmeter 30 is provided along the gas flow line 24 for measuring the flow and inputting this flow to the computer 32. The computer 32 calculates rate of flow information obtained from the flowmeter 30 and controls the stepper motor 28 to open or close the valve 22 as necessary in accordance with the received rate of flow information and a desired rate of flow preprogrammed into the computer 32. As a result, a precise desired rate of flow can be obtained. Also, position indicators 34 may be added to the valve 22 to indicate when the valve 22 is completely open or completely closed. The valve 22 may be provided with a return spring 36 to automatically close the valve 22 in the event of a power loss. The computer 32 may be programmed to detect a significant increase in the rate of gas flow being closing the valve 22 accordingly. Additionally, a pressure switch 38 may be provided along the gas flow line 24 to cause the valve 22 to close upon a pressure change. Finally, temperature 40 and pressure 42 sensors may be added along the gas flow line so that the computer 32 can calculate and maintain a specific mass flow of gas.

Abstract translation: 本发明提供了一种阀控制装置，其可编程为输送期望的气体流。 阀门22连接到步进马达28，步进马达28由计算机32控制，以在气体流动管线24内逐步打开或关闭阀门，以输送所需的流量。 沿着气体流路24设置流量计30，用于测量流量并将该流量输入到计算机32.计算机32计算从流量计30获得的流量信息，并控制步进马达28打开或关闭阀22 根据所接收的流量信息和预编程到计算机32中的期望流量，根据需要，可以获得精确的期望流量。 此外，位置指示器34可以被添加到阀22以指示阀22何时完全打开或完全关闭。 阀22可以设置有复位弹簧36，以在功率损失的情况下自动关闭阀22。 计算机32可以被编程为检测相应地关闭阀门22的气体流量的显着增加。 另外，压力开关38可以沿着气体流动管线24设置，以使得阀22在压力变化时闭合。 最后，温度40和压力42传感器可以沿着气体流动管线被添加，使得计算机32可以计算和维持气体的特定质量流量。

公开(公告)号：US5033305A

公开(公告)日：1991-07-23

申请号：US462506

申请日：1990-01-08

Applicant: Paul F. Rozelle ,  Michael Twerdochlib

Inventor： Paul F. Rozelle ,  Michael Twerdochlib

IPC: G01H1/10 ,  G01H1/00 ,  G01M15/04 ,  G01M99/00 ,  G07C3/00

CPC classification number: G01M15/046 ,  G01H1/003 ,  G07C3/00 ,  F02D2200/1015

Abstract: The movement of a rotating part of a machine is monitored by deriving a signal representing the motion of the rotating part, at least temporarily storing the derived signal, and analyzing the stored signal, with temporary storage being performed only on portions of the signal derived during spaced time intervals during each revolution of the rotating part.

Abstract translation: 通过导出表示旋转部分的运动的信号来监测机器的旋转部分的运动，至少暂时存储导出的信号，并且分析所存储的信号，其中暂时存储仅在所导致的信号的部分上被执行 在旋转部件的每转期间间隔时间间隔。

公开(公告)号：US5031459A

公开(公告)日：1991-07-16

申请号：US349029

申请日：1989-05-08

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: G01B21/22 ,  F01D21/00 ,  G01H1/10

CPC classification number: G01H1/10

Abstract: A shaft torsion monitor comprises a plurality of sensors for sensing the angular position of various portions of the shaft under dynamic conditions and for producing sets of data representative of the sensed angular positions. A memory is provided for periodically storing one of the sets of data representative of the angular position of the various portions of the shaft in the absence of torsion. Circuitry is provided for subtracting the stored set of data from each of the other sets of data to eliminate the effects of noise. The resulting data is analyzed to determine the torsion experienced by the shaft.

Abstract translation: 轴扭转监视器包括多个传感器，用于在动态条件下感测轴的各个部分的角位置并且用于产生表示所感测的角位置的数据组。 提供存储器，用于在不存在扭转的情况下周期性地存储表示轴的各个部分的角位置的数据组之一。 提供电路，用于从每个其他数据集中减去存储的数据集，以消除噪声的影响。 分析得到的数据以确定轴经受的扭转。

公开(公告)号：US4987555A

公开(公告)日：1991-01-22

申请号：US277833

申请日：1988-11-30

Applicant: Michael Twerdochlib

Inventor： Michael Twerdochlib

IPC: G01B7/14

CPC classification number: G01B7/14

Abstract: A system for monitoring the clearance between a plurality of turbine blade shroud segments connected to form a turbine blade shroud and the stationary portion of the turbine comprises a sensor responsive to eddy currents generated in each of the shroud segments for producing input signals representative of the clearance between each shroud segment and the stationary portion of the turbine. Indicia are carried by the turbine blade shroud for causing the sensor to produce a known displacement signal. A processor is responsive to the input signals and the displacement signal for producing output signals indicative of the clearance between each shroud segment and the stationary portion of the turbine. The output signals have a predetermined relationship to the known displacement signal.

Abstract translation: 用于监测连接以形成涡轮机叶片护罩的多个涡轮机叶片护罩段与涡轮机的固定部分之间的间隙的系统包括响应于在每个护罩段中产生的涡流的传感器，用于产生代表间隙的输入信号 在每个护罩段和涡轮机的固定部分之间。 标记由涡轮机叶片护罩承载，以使传感器产生已知的位移信号。 处理器响应于输入信号和位移信号，用于产生指示每个护罩区段和涡轮机的静止部分之间的间隙的输出信号。 输出信号与已知的位移信号具有预定的关系。