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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