Gear tooth crack signals and their detection via the FM4 measure in application for a helicopter HUMS (health usage and management system)^Ω

Author

Hochmann, David ; Bechhoefer, Eric

Author_Institution

Goodrich Corporation

Volume

fYear

2003

fDate

March 8-15, 2003

Firstpage

3313

Lastpage

3326

Keywords

Analytical models; Condition monitoring; Damping; Equations; Fault detection; Gears; Helicopters; Signal detection; Steady-state; Teeth;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace Conference, 2003. Proceedings. 2003 IEEE

ISSN

1095-323X

Print_ISBN

0-7803-7651-X

Type

DOI

10.1109/AERO.2003.1234175

Filename

1234175

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