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)
Hydraulic Diagnostic Monitoring System
1981
303 pages
Report
Keine Angabe
Englisch
Aircraft , Hydraulic & Pneumatic Equipment , Job Training & Career Development , Hydraulic equipment , Monitors , Diagnostic equipment , Microprocessors , Onboard , Detectors , Failure , Monitoring , Aircraft equipment , Test sets , Fiber optics transmission lines , Analog signals , Pneumatic devices , Hydraulic fluids , Display systems , Attack bombers , Flight testing , Aircraft maintenance , HYCOS(Hydraulic Diagnostic Monitoring System) , A-6 aircraft , NTISDODXA
Hydraulic diagnostic monitoring system
Tema Archiv | 1981
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