Oil Debris Detection System (ODDS)
Abstract
A flight test evaluation was conducted to investigate condition monitoring/diagnostic techniques. Using the UH-1 aircraft as a test bed, a diagnostic oil monitoring system was designed, incorporating high-efficiency, 3- micron filters and full-flow burn-off chip detectors in the engine and transmission, with burn-off detectors in the 42-and 90-degree gearboxes. A test program was structured to establish the feasibility and utility of the improved ODDS for use in the Army helicopter engines, transmissions and gearboxes. The results of the program have shown that the ODDS is a highly effective diagnostic system for monitoring the condition of gears and bearings in all Army helicopters. It has demonstrated reliable detection of failures while eliminating no-fault removals.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1984
- Accession Number
- ADB083462
Entities
People
- W. A. Hudgins
Organizations
- United States Army Aviation and Missile Command