MICRO THERMAL IMAGING SYSTEM FOR TURBINE ENGINES

A turbine engine includes a compressor section, a combustor section fluidly coupled to the compressor section, a turbine section fluidly coupled to the combustor section, and a drive shaft coupled to the turbine section and the compressor section. The turbine engine also includes a plurality of inte...

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Bibliographische Detailangaben
Hauptverfasser:	DEES, JASON EDWARD, WANG, GUANGHUA, WETZEL, TODD GARRETT
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COLORIMETRY COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT,POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED,VISIBLE OR ULTRA-VIOLET LIGHT MEASURING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS RADIATION PYROMETRY STEAM ENGINES TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS
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Beschreibung
Zusammenfassung:	A turbine engine includes a compressor section, a combustor section fluidly coupled to the compressor section, a turbine section fluidly coupled to the combustor section, and a drive shaft coupled to the turbine section and the compressor section. The turbine engine also includes a plurality of internal components coupled to one of the compressor section, the combustor section, the turbine section, and the drive shaft. 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 is configured to detect a surface temperature of the plurality of internal components.