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. 16, 2019

Filed:

Sep. 17, 2013
Applicant:

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

Inventors:

Xuefei Guan, Princeton, NJ (US);

Jingdan Zhang, Plainsboro, NJ (US);

Shaohua Kevin Zhou, Plainsboro, NJ (US);

Nancy H. Ulerich, Longwood, FL (US);

Nam Eung Kim, Jupiter, FL (US);

Nikolai R. Tevs, Daytona Beach Shores, FL (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01L 5/00 (2006.01); G01M 5/00 (2006.01); G01M 15/14 (2006.01); G06F 19/00 (2018.01); G01N 3/56 (2006.01); G01D 21/00 (2006.01); G01H 17/00 (2006.01); G06F 17/40 (2006.01);
U.S. Cl.
CPC ...
G01L 5/00 (2013.01); G01M 5/0016 (2013.01); G01M 5/0041 (2013.01); G01M 15/14 (2013.01); G01D 21/00 (2013.01); G01H 17/00 (2013.01); G01N 3/56 (2013.01); G06F 17/40 (2013.01); G06F 19/00 (2013.01);
Abstract

A method dynamically reconstructing a stress and strain field of a turbine blade includes providing a set of response measurements from at least one location on a turbine blade, band-pass filtering the set of response measurements based on an upper frequency limit and a lower frequency limit, determining an upper envelope and a lower envelope of the set of response measurements from local minima and local maxima of the set of response measurements, calculating a candidate intrinsic mode function (IMF) from the upper envelope and the lower envelope of the set of response measurements, providing an N×N mode shape matrix for the turbine blade, where N is the number of degrees of freedom of the turbine blade, when the candidate IMF is an actual IMF, and calculating a response for another location on the turbine blade from the actual IMF and mode shapes in the mode shape matrix.


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