1988
DOI: 10.1109/20.92278
|View full text |Cite
|
Sign up to set email alerts
|

Incipient failure prediction of rotating electrical machinery by eddy current on-line monitoring method

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2012
2012
2018
2018

Publication Types

Select...
1
1

Relationship

0
2

Authors

Journals

citations
Cited by 2 publications
(3 citation statements)
references
References 1 publication
0
3
0
Order By: Relevance
“…Significant work has been done in the field of high temperature eddy current sensor development and its application in turbine blade health monitoring and disk monitoring (Barranger, 1984; Chari et al , 1988; Cartz, 1995; Tietze, 1990). Significant progress in the development of commercial high temperature eddy current sensors has been made by Hood Technology, General Dynamics Advanced Information Systems, JENTEK Sensors, and Qinetiq, among others.…”
Section: Required Specifications For a Sensing Technology Applicable To High‐temperature Zones In A Propulsion Systemmentioning
confidence: 99%
See 1 more Smart Citation
“…Significant work has been done in the field of high temperature eddy current sensor development and its application in turbine blade health monitoring and disk monitoring (Barranger, 1984; Chari et al , 1988; Cartz, 1995; Tietze, 1990). Significant progress in the development of commercial high temperature eddy current sensors has been made by Hood Technology, General Dynamics Advanced Information Systems, JENTEK Sensors, and Qinetiq, among others.…”
Section: Required Specifications For a Sensing Technology Applicable To High‐temperature Zones In A Propulsion Systemmentioning
confidence: 99%
“…The state of the art for harsh environment, high‐temperature sensors have improved considerably over the past few years (McCarty and Thompson, 1980; Gauthier, 1981; Forth and Staroselsky, 2001; Hudak et al , 2004; Wrbanek et al , 2004; Gregory et al , 2002; Hulse et al , 1985; Auciello, 1999; Elshabini‐Riad and Barlow, 1998; Lei et al , 1997; Metev, 1998; Dharan, 1986; Barranger, 1984; Chari et al , 1988; Cartz, 1995; Tietze, 1990; Sayir et al , 2006). Existing fatigue and life prediction studies for high‐temperature zones (1,000‐1,400°C in propulsion systems and higher for missile systems) depend on the strain/stress values computed from indirect measurements of temperature, flow velocity, pressure, and so on.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, robust and simple fault identification methods are essential to detect unexpected motor faults. Costly and complicated conventional techniques [3] usually involve the use of sensors fitted in the machine measuring and sensing temperature or vibration as well as professionally analysed data [1,4].…”
Section: Introductionmentioning
confidence: 99%