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