DocumentCode
3093638
Title
F-111/TF30 engine monitoring system: a fusion of past, present, and future technology
Author
Somers, Richard D.
fYear
1989
fDate
22-26 May 1989
Firstpage
2062
Abstract
The extension of present-day engine-monitoring technology to older aircraft and demonstration of future diagnostic technologies are discussed. A development program for F-111/TF30 engine monitoring is described. The system design utilizes standard parts and technology insertion upgrades such as MIL-STD-1750A computer designs for existing complex devices. A design agent approach was used to realize the logistics goal of providing an Air-Force-owned design which could be purchased from multiple sources. An internal research and development program to investigate neural-network applications to expert-system diagnostics is described. A competitive associative network was used to implement the troubleshooting diagnostics for TF30 engine start problems and to examine its application potential
Keywords
aerospace engines; aerospace testing; aircraft; expert systems; F-111/TF30 engine monitoring system; MIL-STD-1750A computer designs; aircraft; expert-system diagnostics; logistics; neural-network applications; technology insertion upgrades; troubleshooting diagnostics; Cities and towns; Contracts; Engines; Instruments; Monitoring; Neural networks; Project management;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location
Dayton, OH
Type
conf
DOI
10.1109/NAECON.1989.40504
Filename
40504
Link To Document