Mechanical and propulsion systems prognostics: U.S. navy strategy and demonstration

JOM

Volumn 56, Issue 3, 2004, Pages 21-27

  Hardman, William ^a  

^a NAVAL AIR WARFARE CENTER AIRCRAFT DIVISION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COST EFFECTIVENESS; FAILURE (MECHANICAL); LIFE CYCLE; MECHANICAL DRIVES; MILITARY AIRCRAFT; MONITORING; PERFORMANCE; VIBRATIONS (MECHANICAL);

AIRCRAFT LIFE CYCLE; HEALTH MONITORING; POWER DRIVE SYSTEM MONITORING; PROGNOSTICS; PROPULSION SYSTEMS PROGNOSTICS;

PROPULSION;

EID: 1942453835     PISSN: 10474838     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11837-004-0028-3     Document Type: Article

References (2)

1. W. Hardman, A. Hess, and C. Neubert, "SH-60 Helicopter Integrated Diagnostic System (HIDS) Program Experience and Results of Seeded Fault Testing" (Paper presented at the American Helicopter Society 54th Annual Forum, Washington, D.C., 20-22 May 1998).
2. B. Pregger, H-60 IGB Pinion Gear Fatigue Crack Analysis, Report Number MA-1145 (U.S. Navy publication, 5 October 2001).