Title :
In-line oil debris monitor for aircraft engine condition assessment
Author :
Miller, Jerry L. ; Kitaljevich, Duka
Author_Institution :
Pratt & Whitney, East Hartford, CT, USA
Abstract :
The development of an in-line, full flow oil debris sensor for aircraft engine condition assessment is described. First used on the F22 fighter, this sensor is the only “all-metals” debris detector in production. The sensor is based on an inductive measurement technique which enables the system to detect, count and classify wear metal particles by size and type (ferromagnetic and nonferromagnetic) above a minimum particle size threshold. In flight, the measured count values are compared to preset levels to provide prognostic health information on the oil-wetted components of the engine. This paper describes the sensor design requirements, principle of operation, electronic design and mechanical design features. The results of a test program established to correlate the oil borne debris measurements to component degradation characteristics and data from actual engine bearing failures, are also presented
Keywords :
aerospace engines; aircraft testing; condition monitoring; gas turbines; particle size measurement; aircraft engine; all-metals debris detector; component degradation characteristics; electronic design; engine bearing failures; engine condition assessment; in-line oil debris monitor; inductive measurement technique; measured count values; mechanical design; oil-wetted components; particle size threshold; prognostic health information; sensor design requirements; wear metal particles; Aircraft propulsion; Condition monitoring; Detectors; Engines; Measurement techniques; Petroleum; Production; Sensor phenomena and characterization; Sensor systems; Wearable sensors;
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-5846-5
DOI :
10.1109/AERO.2000.877882