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:
Nov. 12, 2019

Filed:

Feb. 13, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Mohamed Sakami, West Chester, OH (US);

Nirm Velumylum Nirmalan, Liberty Township, OH (US);

Jeremy Clyde Bailey, Liberty Township, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01J 5/06 (2006.01); G01J 5/00 (2006.01); G02B 23/24 (2006.01); G02B 7/02 (2006.01); F02D 41/14 (2006.01); G01N 21/954 (2006.01); H04N 5/225 (2006.01); G01N 25/72 (2006.01); G01M 15/14 (2006.01); G01N 21/15 (2006.01);
U.S. Cl.
CPC ...
G01J 5/061 (2013.01); F02D 41/1451 (2013.01); G01J 5/0088 (2013.01); G01N 21/954 (2013.01); G02B 7/028 (2013.01); G02B 23/243 (2013.01); G02B 23/2492 (2013.01); H04N 5/2254 (2013.01); G01J 2005/0077 (2013.01); G01M 15/14 (2013.01); G01N 25/72 (2013.01); G01N 2021/151 (2013.01); G01N 2021/9542 (2013.01); H04N 2005/2255 (2013.01);
Abstract

An apparatus for insertion through an opening in an outer casing of a gas turbine engine and inspection of internal turbine components at elevated temperatures having an optical sight tube configured to optically communicate with an interior of gas turbine engine via a distal end disposed at the interior and a proximal end disposed exterior of the internal turbine components and defined by a first longitudinal wall, at least one lens at the distal end of the optical sight tube adjacent to the longitudinal wall; and at least one longitudinal cooling groove in the longitudinal wall for flowing a cooling medium from a location external to the turbine to cool the optical sight tube at a location at least adjacent the distal end.


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