SENSOR ASSEMBLY FOR USE WITH TURBOMACHINE AND METHODS FOR ASSEMBLING THE SAME

PROBLEM TO BE SOLVED: To provide a sensor assembly for use with a turbomachine.SOLUTION: The sensor assembly includes a detection device 302 configured to measure at least one parameter of components of the turbomachine and a cover configured to fix the detection device to the components of the turb...

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Bibliographische Detailangaben
Hauptverfasser:	BRUCE KEVIN LEON, YATES SHAWN CARROL, POTH III LEISSNER FERDINAND, SCHLEIF KURT KRAMER, WILSON DEREK RAY
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MEASURING MEASURING QUANTITY OF HEAT MEASURING TEMPERATURE MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TESTING THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a sensor assembly for use with a turbomachine.SOLUTION: The sensor assembly includes a detection device 302 configured to measure at least one parameter of components of the turbomachine and a cover configured to fix the detection device to the components of the turbomachine. The cover includes: a first portion 306 formed therein and including a cavity 308 that dimensioned to accepting the detection device; and a second portion 311 extending from the first portion and detachably coupled with a surface of the components of the turbomachine.