Eddy current sensor capable of sensing through a conductive barrier

• US 7,023,205 B1
• Filed: 08/01/2001
• Issued: 04/04/2006
• Est. Priority Date: 08/01/2000
• Status: Expired due to Fees

• Current Assignee: General Dynamics Advanced Information Systems Incorporated (General Dynamics Corporation)
• Original Assignee: General Dynamics Advanced Information Systems Incorporated (General Dynamics Corporation)
• Inventors: Krupp, Roy S.
• Primary Examiner(s): PATIDAR, JAY M
• Application Number:
  US09/920,427
• Time in Patent Office: 1,707 Days
• Field of Search: 324/207.15, 324/207.25, 324/239, 324/173, 324/174, 324/228, 324234-243, 738/617.8
• US Class Current: 324/239
• CPC Class Codes: G01N 27/72 by investigating magnetic variables

Abstract

An eddy current sensor that can be mounted on the outside of a casing for a turbine or other rotating machinery to measure characteristics of nearby, moving, electrically conductive objects through the casing. Monodirectional and omnidirectional sensors are provided. High-strength uniaxial permanent magnets generate static magnetic fields. A signal voltage is produced on a wound coil in response to a variable magnetic field caused by eddy currents in the conductive object as the conductive object passes through the stationary magnetic field. The present invention sensors are also directed to measuring characteristics of turbine blades through jet engine casings.

Claims

1. An eddy current sensor for measuring characteristics of a nearby, moving, electrically conductive object with an intervening barrier of material between the sensors and the object, the sensor comprising:

a uniaxial permanent magnet for generating a stationary magnetic field, the magnet being mounted proximate and external to the barrier and sized and shaped so that the stationary magnetic field penetrates through the barrier and can be intersected by the moving conductive object; and

a coil wound around the magnet so that a signal voltage can be produced on the coil in response to a variable magnetic field caused by eddy currents in the conductive object as the conductive object passes through the stationary magnetic field;

wherein the magnet includes a first dimension along a longitudinal central major axis generally parallel to the proximate surface of the barrier, a second dimension along a second minor axis, and third dimension along a third minor axis, the first dimension being the greatest, and wherein the magnet is magnetized along one of the second minor axis and the third minor axis, whereby the sensor is monodirectional.

2. The eddy current sensor as recited in claim 1, wherein the magnet is generally rectangular in cross-section.

3. An eddy current sensor for measuring characteristics of moving turbine blades of a jet engine having a casing, through which the sensor measures the blade characteristics, the sensor comprising:

a uniaxial permanent magnet for generating a stationary magnetic field, the magnet being mounted proximate and external to the casing and sized so that the stationary magnetic field penetrates through the casing and can be intersected by a portion of the blade, wherein the magnet includes a generally rectangular cross-section, a first dimension along a longitudinal central major axis generally parallel to the proximate surface of the casing, a second dimension along a second minor axis, and third dimension along a third minor axis, the first dimension being the greatest, and the magnet is magnetized substantially along one of the second minor axis and the third minor axis; and

a coil wound around the magnet so that a signal voltage can be produced on the coil in response to a variable magnetic field caused by eddy currents in the blade as the blade passes through the stationary magnetic field,

whereby the sensor is substantially monodirectional.

4. The eddy current sensor as recited in claim 3, wherein the magnet material is selected from the group consisting of Neodymium-Iron-Boron, Samarium-Cobalt, and Aluminum-Nickel-Cobalt.

5. A method of measuring characteristics of moving turbine blades of a jet engine having a casing, through which blade characteristics are sensed, comprising the steps of:

generating a stationary magnetic field by using a substantially uniaxial permanent magnet, the magnet being mounted proximate and external to the casing and sized so that the stationary magnetic field penetrates through the casing and can be intersected by a portion of the blade, the magnet includes a generally rectangular cross-section, a first dimension along a longitudinal central major axis generally parallel to the proximate surface of the casing, a second dimension along a second minor axis, and third dimension along a third minor axis, the first dimension being the greatest, and the magnet being magnetized substantially along one of the second minor axis and the third minor axis;

producing a signal voltage on a coil wound around the magnet in response to a variable magnetic field caused by eddy currents in the blade as the blade passes through the stationary magnetic field; and

measuring the signal voltage.