PROBE HOLDER FOR TURBINE ENGINE SENSOR

PROBLEM TO BE SOLVED: To provide a probe holder for a turbine engine sensor.SOLUTION: A turbine 10 includes: a component having a body that can rotate around a rotor center line 122 and is formed to define a cavity approaching in a radial direction in a target measuring point 20 specified in a radia...

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Bibliographische Detailangaben
Hauptverfasser:	HART ANDREW CLIFFORD, PAK JONG YOUN, SCHLEIF KURT KRAMER, BROWN GREGORY QUENTIN, CASANOVA FERNANDO JORGE, JONES ROBERT DAVID, CHOI SEUNG-WOO, CUMMINS JOSEF S, CARUSO PHILIP MICHAEL, FERSLEW MATTHEW RYAN
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 HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC ORINFRASONIC WAVES MEASURING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES TESTING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a probe holder for a turbine engine sensor.SOLUTION: A turbine 10 includes: a component having a body that can rotate around a rotor center line 122 and is formed to define a cavity approaching in a radial direction in a target measuring point 20 specified in a radial direction distance from the rotor center line 122; a sensor 25 that measures a state in the target measuring point 20; a communication system 30 that can transmit a state measurement value to a non-rotation recording system 75 from the sensor 25; and a probe holder 90 that can be inserted into the cavity for securing the sensor 25 so that the sensor approaches the target measuring point 20.