The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 18, 2017

Filed:

Jun. 08, 2015
Applicant:

Siemens Energy, Inc., Orlando, FL (US);

Inventors:

Joshua DeAscanis, Oviedo, FL (US);

Clifford Hatcher, Jr., Orlando, FL (US);

David Letter, Deland, FL (US);

Assignee:

Siemens Energy, Inc., Orlando, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 15/14 (2006.01); G01N 21/954 (2006.01); F01D 21/00 (2006.01); G02B 23/24 (2006.01); G01M 15/02 (2006.01);
U.S. Cl.
CPC ...
G01M 15/14 (2013.01); F01D 21/003 (2013.01); G01N 21/954 (2013.01); G02B 23/2484 (2013.01); G02B 23/2492 (2013.01); G01M 15/02 (2013.01);
Abstract

Internal components of power generation machines, such as gas or steam turbines, are inspected with a laser profilometer inspection system that is inserted and positioned within the turbine, for example through an inspection port that is in communication with an open inter-row spacing volume between an opposing turbine vane and turbine blade row. Component surface profile scans are performed to determine relative profile heights along a two-dimensional scan line generated by the profilometer. Three-dimensional profile information is obtained by translating the scan line across the surface. Real time profile information is gathered without physical contact, which is helpful for extracting off-line engineering information about component surface conditions, including surface spallation, perforation, and gaps between components. The system is capable of determining blade tip gap between a turbine blade tip and its opposing abradable surface in the turbine casing.


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