Methods for effluent based condition assessment

Patent metadata

Field	Value
Publication number	US-10906670-B2
Application number	US-201716306929-A
Country	US
Kind code	B2
Filing date	May 23, 2017
Priority date	Jun 29, 2016
Publication date	Feb 2, 2021
Grant date	Feb 2, 2021

Abstract

A method for determining a condition of a second component of an engine is disclosed wherein the engine includes at least a first component and the second component. The method includes determining a concentration value of a chemical species in an effluent obtained from washing at least a portion of the first component of the engine, inputting the concentration value of the chemical species in a condition assessment model to update the condition assessment model, and estimating the condition of the second component based on an output of the updated condition assessment model. The effluent used herein includes a wash fluid and the chemical species. The second component is different from the first component and the condition assessment model is a representative of a condition of the second component of the engine.

First claim

What we claim is:

1. A method for determining a condition of a second component of an engine, wherein the engine comprises at least a first component and the second component, wherein the first component and the second components are components of an aviation engine, the method comprising:
determining a concentration value of a chemical species in an effluent obtained from washing at least a portion of the first component of the engine, wherein the effluent comprises a wash fluid and the chemical species, and wherein the concentration value is indicative of environmental conditions the aviation engine has encountered;
inputting the concentration value of the chemical species in a condition assessment model, to update the condition assessment model, wherein the condition assessment model is representative of a condition of the second component of the engine and wherein the second component is different from the first component; and
estimating the condition of the second component based on an output of the updated condition assessment model.

2. The method of claim 1 , further comprising washing at least the portion of the first component of the engine using the wash fluid to form the effluent.

3. The method of claim 1 , wherein the wash fluid comprises water.

4. The method of claim 1 , comprising determining concentration value of the chemical species dissolved in the wash fluid.

5. The method of claim 1 , comprising determining concentration value of the chemical species suspended in the wash fluid.

6. The method of claim 1 , wherein the chemical species comprises an organic species, an inorganic species, an ionic species, or combinations thereof.

7. The method of claim 1 , wherein the chemical species comprises sulfur, chlorine, calcium, sodium, potassium, aluminum, magnesium, cobalt, nickel, iron, phosphorous, chromium, manganese, or combinations thereof.

8. The method of claim 1 , wherein determining the concentration value of the chemical species comprises using X-ray diffraction, scanning electron microscopy, energy dispersive and wavelength dispersive spectroscopy, inductively coupled plasma mass spectroscopy, atomic emission spectroscopy, mass spectrometry, ion chromatography, or combinations thereof.

9. The method of claim 1 , comprising determining concentration values of at least two chemical species in the effluent.

10. The method of claim 9 , comprising inputting the condition assessment model with a ratio of the concentration values of the at least two chemical species in the effluent.

11. The method of claim 1 , wherein the condition assessment model comprises a crack propagation model, an oxidation model, a corrosion model, a wear model, or combinations thereof.

12. The method of claim 1 , wherein the first component and the second component are components of an aviation engine.

13. The method of claim 1 , wherein the first component and the second component comprise an engine compressor, a compressor blade, a compressor casing, a combustor, a turbine blade, a turbine shroud, a turbine blade underplatform, a turbine disk, a turbine casing, or combinations thereof.

14. The method of claim 1 , further comprising inputting the concentration value of the chemical species into an engine efficiency model, wherein the engine efficiency model is representative of an efficiency of the engine.

15. The method of claim 1 , further comprising modifying the wash fluid based on the concentration value of the chemical species, updated condition assessment model, or a combination thereof.

16. The method of claim 1 , further comprising repeating the steps of determining the concentration value of the chemical species in an effluent, inputting the concentration value of the chemical species in a condition assessment model, and estimating the condition of the second component of the engine, at specific wash intervals.

17. The method of claim 16 , further comprising modifying the specific wash intervals based on the concentration value the chemical species, updated condition assessment model, or a combination thereof.

18. A method for determining corrosion of a hot-section component of an aviation engine, comprising:
determining a concentration value of a chemical species in an effluent obtained from washing at least a portion of a compressor of the aviation engine, wherein the effluent comprises a wash fluid and the chemical species;
inputting the concentration value of the chemical species in a corrosion model of the hot-section component of the aviation engine to update the corrosion model, wherein the corrosion model is representative of a corrosion in the hot-section component of the aviation engine; and
estimating presence of the corrosion, an amount of the corrosion, or both of the hot-section component of the aviation engine.

19. The method of claim 18 , further comprising washing at least the portion of the compressor using the wash fluid comprising water to form the effluent.

Assignees

• Gen Electric

Inventors

• Sachdeva Deepika
• Reddy Raji
• Parayalil Chithra
• Kaushik Anshul
• Shanmukh Saratchandra
• Rajagopalan Venkatesh

Classifications

• F01D25/002 Primary

  Cleaning of turbomachines · CPC title

• F05D2230/72

  Maintenance · CPC title

• F05D2260/81

  Modelling or simulation · CPC title

• B64F5/60 Primary

  Testing or inspecting aircraft components or systems · CPC title

• F05D2260/80

  Diagnostics · CPC title