MICRO THERMAL IMAGING SYSTEM FOR TURBINE ENGINE

Title:

MICRO THERMAL IMAGING SYSTEM FOR TURBINE ENGINE

Document Type and Number:

Japanese Patent JP2017201164

Kind Code:

A

Abstract:

PROBLEM TO BE SOLVED: To provide a micro thermal imaging system for consistently measuring temperatures of internal components for a gas turbine engine.SOLUTION: A turbine engine also includes a plurality of internal components (124, 125, 236, 238, 240, 246) coupled to one of a compressor section, a combustor section, a turbine section 108 and a drive shaft 115. The turbine engine also includes at least one micro infrared sensor coupled to at least one of the plurality of internal components. The micro infrared sensor (270) is configured to detect a surface temperature of the plurality of internal components (124, 125, 236, 238, 240, 246).SELECTED DRAWING: Figure 2

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Inventors:

WANG GUANGHUA
TODD GALLET WETZEL
JASON EDWARD DEES

Application Number:

JP2017080170A

Publication Date:

November 09, 2017

Filing Date:

April 14, 2017

Export Citation:

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Assignee:

GENERAL ELECTRIC CO GE

International Classes:

F02C7/00; F01D25/00; F02C9/00; G01J5/00; G01J5/48

Domestic Patent References:

JP2015524036A	2015-08-20
JP2015102094A	2015-06-04
JP2011179493A	2011-09-15

Attorney, Agent or Firm:

Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka

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