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:
Dec. 06, 2016

Filed:

Oct. 02, 2013
Applicants:

Forrest R. Ruhge, Orlando, FL (US);

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

Inventors:

Forrest R. Ruhge, Orlando, FL (US);

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

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01B 21/16 (2006.01); G01B 11/14 (2006.01); G01M 15/02 (2006.01); G01N 21/88 (2006.01); F01D 21/00 (2006.01);
U.S. Cl.
CPC ...
G01B 21/16 (2013.01); F01D 21/003 (2013.01); G01B 11/14 (2013.01); G01M 15/02 (2013.01); G01N 21/8803 (2013.01); F05D 2270/80 (2013.01); F05D 2270/821 (2013.01);
Abstract

Turbine blade tip clearance is measured in a fully assembled turbine casing by mounting a contact or non-contact displacement probe on a turbine blade that generates data indicative of probe distance from the turbine casing that circumferentially surrounds the blade. Variations in probe distance data are recorded as the blade circumferentially sweeps the turbine casing when the turbine is operated in turning gear mode. Blade rotational position data are collected by a rotational position sensor. A data processing system correlates the distance and rotational position data with localized blade tip gap at angular positions about the turbine casing circumference. An optical camera inspection system may be coupled to a turbine blade to obtain visual inspection information within the turbine casing. This method and apparatus provide an accurate and cost effective solution for accessing turbine casing deformation impact on blade tip clearance and rotor/casing alignment.


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