Hydraulic Diagnostic Monitoring System.
Abstract
Task I encompassed the design, development and procurement of hardware, sensors, and microprocessors for two diagnostic monitoring systems. The first system was installed on the F-14 Hydraulic Flight Simulator on Task II of the program. Task II included the installation of one system on the F-14A Hydraulic Simulator for system component reliability demonstrations. The task also covered simulated component failures and diagnostic system reaction. In Task III, the Diagnostic System was integrated into A6E B/N 155628. The system was debugged and a 12 month flight test schedule. This report covers Task III. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 02, 1981
- Accession Number
- ADA100730
Entities
People
- John J. Duzich
Organizations
- Grumman