DocumentCode :
1855306
Title :
Advanced-aircraft integrated-diagnostics system-concept evaluation
Author :
Gaffney, Kevin S. ; Morones, Paul
Author_Institution :
Lockheed Fort Worth Co., Fort Worth, TX, USA
fYear :
1994
fDate :
24-27Jan 1994
Firstpage :
20
Lastpage :
25
Abstract :
An integrated diagnostics system engineering process was utilized to develop an effective diagnostic/health monitoring system which meets user´s needs. Weighing results from reliability, maintainability, and system safety trade studies, a comprehensive aircraft diagnostic/health monitoring system was defined which decreases aircraft turnaround time and increases safety while minimally impacting system reliability. The approach of considering reliability, maintainability, and system safety requirements as the customer´s requirements in a quality function deployment (QFD) analysis can be employed in the design and development of other products which require the amalgamation of complicated and conflicting design requirements
Keywords :
aerospace computing; aircraft; maintenance engineering; reliability; safety systems; advanced-aircraft integrated-diagnostics system-concept evaluation; aircraft diagnostic/health monitoring system; maintainability; quality function deployment analysis; reliability; system safety requirements; Aerospace engineering; Air safety; Aircraft propulsion; Health and safety; Maintenance engineering; Monitoring; Product safety; Quality function deployment; Reliability engineering; Systems engineering and theory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium, 1994. Proceedings., Annual
Conference_Location :
Anaheim, CA
Print_ISBN :
0-7803-1786-6
Type :
conf
DOI :
10.1109/RAMS.1994.291073
Filename :
291073
Link To Document :
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