Share Email Print

Proceedings Paper

CH-46 Sea Knight flight test results for the Rotor Acoustic Monitoring System (RAMS)
Author(s): Fred Malver; Jeffrey N. Schoess; Jerry Kooyman; Ron Jiracek; John Volk
Format Member Price Non-Member Price
PDF $17.00 $21.00

Paper Abstract

From August 28 to September 18, 1997, Honeywell's Rotor Acoustic Monitoring System was successfully flight-tested at Patuxent River Naval Base. This flight-test was the culmination of an ambitious, 40-month, proof-of-concept effort to demonstrate the feasibility of detecting crack propagation in helicopter rotor components. During the three weeks of flight-testing, the system was operated on 12 flights plus one ground test and accumulated more than 16 hours of flight data recorder data and about 25 Gbyte of digital data from eight on-rotor acoustic sensors. The flight-test showed that rotor head acoustic monitoring could be uniquely valuable not only for rotor crack and fault detection but also for monitoring the general health of the entire rotor assembly. This paper presents preliminary results from that flight-test.

Paper Details

Date Published: 27 July 1998
PDF: 12 pages
Proc. SPIE 3329, Smart Structures and Materials 1998: Smart Structures and Integrated Systems, (27 July 1998); doi: 10.1117/12.316921
Show Author Affiliations
Fred Malver, Honeywell Technology Ctr. (United States)
Jeffrey N. Schoess, Honeywell Technology Ctr. (United States)
Jerry Kooyman, Honeywell Technology Ctr. (United States)
Ron Jiracek, Honeywell Technology Ctr. (United States)
John Volk, Honeywell Technology Ctr. (United States)

Published in SPIE Proceedings Vol. 3329:
Smart Structures and Materials 1998: Smart Structures and Integrated Systems
Mark E. Regelbrugge, Editor(s)

© SPIE. Terms of Use
Back to Top
Sign in to read the full article
Create a free SPIE account to get access to
premium articles and original research
Forgot your username?