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NASA NTRS · Conference Paper

Helicopter propulsion system reliability and engine monitoring assessments

Published 2019-06-21 From Legacy CDMS 1 author

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The major short life, unreliable, and high maintenance engine and power components and subsystems in current civil helicopters were identified. Categories included both reciprocating and turbine engines, single and multiple engine configurations, single and tandem trotor vehicles, and light, medium, and heavy helicopters. The major focus was on the following parameters: accident rate data; maintenance rate data; and direct operator input.

Author

  • Murphy, J. A. Textron Bell Helicopter

Citation: Murphy, J. A. (2019). Helicopter propulsion system reliability and engine monitoring assessments. Legacy CDMS. NASA NTRS ID 19810022671. https://ntrs.nasa.gov/citations/19810022671 ↗