Non-destructive evaluation methods for determining a thickness of a coating layer on a turbine engine component

Patent metadata

Field	Value
Publication number	US-2015000405-A1
Application number	US-201313928538-A
Country	US
Kind code	A1
Filing date	Jun 27, 2013
Priority date	Jun 27, 2013
Publication date	Jan 1, 2015
Grant date	—

Abstract

A method of non-destructively evaluating a thickness of a coating layer on a turbine engine component includes directing an acoustic wave into the turbine engine component, the acoustic wave including a frequency and a wavelength, receiving a return time-domain signal reflected from the turbine engine component, and transforming the time-domain signal into a frequency-domain signal. The method further includes subtracting a baseline signal from the frequency-domain signal and determining a local minimum frequency of the baseline-subtracted frequency-domain signal. Still further, the method includes calculating the thickness of the coating layer based on the determined local minimum frequency. Additional evaluation methods including ones based on resistivity, terahertz, and microwave are further disclosed.

First claim

What is claimed is:

1 . A method of non-destructively evaluating a thickness of a coating layer on a turbine engine component, the method comprising:
directing an acoustic wave into the turbine engine component, the acoustic wave comprising a frequency and a wavelength; receiving a return time-domain signal reflected from the turbine engine component; transforming the time-domain signal into a frequency-domain signal; subtracting a baseline signal from the frequency-domain signal; determining a local minimum frequency of the baseline-subtracted frequency-domain signal; and calculating the thickness of the coating layer based on the determined local minimum frequency.

2 . The method of claim 1 , wherein directing the acoustic wave comprises directing an ultrasonic acoustic wave.

3 . The method of claim 2 , wherein directing the ultrasonic wave is performed using an ultrasonic transducer.

4 . The method of claim 2 , wherein receiving the return time-domain signal is performed using an ultrasonic transducer.

5 . The method of claim 1 , wherein calculating the thickness of the coating layer comprises calculating the thickness of a coating layer having a thickness of 50 microns or less.

6 . The method of claim 1 , wherein calculating the thickness of the coating layer comprises calculating the thickness of a coating layer disposed over a bond coat, which in turn is disposed on the turbine engine component.

7 . The method of claim 1 , wherein the baseline signal is determined from an uncoated turbine engine component.

8 . A method of non-destructively evaluating a thickness of a coating layer on a turbine engine component, the method comprising:
placing first and second probes on an outer surface of the coating layer, wherein the first and second probes are separated by a first distance, and wherein the first and second probes are configured to generate an electrical current in the coating layer; placing third a fourth probes on the outer surface of the coating layer in a location that is between the first and second probes, wherein the third and fourth probes are separated by a second distance that is less than the first distance, and wherein the third and fourth probes are configured to measure an electrical resistivity in the coating layer; generating an electrical current in the coating layer using the first and second probes; measuring the electrical resistivity of the coating layer using the third and fourth probes; and calculating the thickness of the coating layer based on the measured electrical resistivity.

9 . The method of claim 8 , wherein the first, second, third, and fourth probes are placed on the coating layer in a substantially linear fashion.

10 . The method of claim 8 , wherein the first, second, third, and fourth probes are configured to make ohmic contact with the coating layer.

11 . The method of claim 8 , wherein generating the electrical current comprises generating an electrical current that is about 1 μA or less for desired ohmic contact as an example.

12 . The method of claim 11 , measuring the electrical resistivity comprises ensuring that desired generated voltage is about 100 mV or less.

13 . The method of claim 11 , wherein the thickness of the coating layer is less than half of either the first or second distances.

14 . The method of claim 8 , wherein calculating the thickness of the coating layer comprises calculating the thickness of a coating layer disposed over a bond coat, which in turn is disposed on the turbine engine component.

Assignees

• Honeywell Int Inc

Inventors

• Singh Surendra
• Ohm Jim Michael
• Vensel Frederick William
• Krantz Richard Lee

Classifications

• G01B21/08

  for measuring thickness · CPC title

• G01B15/02

  for measuring thickness · CPC title

• G01B11/0633

  using one or more discrete wavelengths · CPC title

• G01B7/06

  for measuring thickness {(measuring during the manufacture of coatings C23C14/54)} · CPC title

• G01B17/025 Primary

  for measuring thickness of coating · CPC title