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:
Aug. 07, 2018

Filed:

Feb. 06, 2015
Applicant:

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

Inventors:

Joshua DeAscanis, Oviedo, FL (US);

David Letter, Deland, FL (US);

Alejandro Bancalari, Casselberry, FL (US);

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

Assignee:

SIEMENS ENERGY, INC., Orlando, FL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); H04N 7/18 (2006.01); G01M 15/14 (2006.01); H04N 5/33 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); G01M 15/14 (2013.01); H04N 5/33 (2013.01); H04N 7/183 (2013.01); F05D 2220/32 (2013.01); F05D 2260/83 (2013.01);
Abstract

A robotically articulated inspection scope () inserted into a pilot fuel nozzle port () of a turbine engine () for in-situ measurement of gaps () between tips of turbine blades (A) and the surrounding shroud (). A non-contact gap measuring device () on a distal end () of the scope may be navigated through a combustor () and transition duct () into a position proximate a blade tip gap. The scope may be controlled via computer () via a robotic drive () affixed to the pilot fuel nozzle port. Multiple scopes may be used to measure gaps (A-D) at multiple azimuths of the turbine simultaneously. The turbine disk () may be rotated on its operating turning gear to sequentially measure each blade at each azimuth. The computer may memorize an interactively navigated path for subsequent automated positioning.


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