DocumentCode
3373912
Title
R&M in conceptual aircraft design
Author
Sherrieb, Harold ; Stracener, Jerrell T.
Author_Institution
LTV Aerosp. & Defense Co., Dallas, TX, USA
fYear
1992
fDate
1992
Firstpage
245
Lastpage
254
Abstract
Effectiveness of R&M (reliability and maintainability) in conceptual aircraft design is dependent on successful integration of R&M into the design process. The R&M process must not only integrate R&M tasks, but must also be integrated with other design and engineering functions. Once the process has been established, automation and tools required to support the process can be defined. An element often taken for granted is the skill requirements to effectively and efficiently perform the R&M tasks during conceptual design. The process, automation, and tools all support the R&M engineer, they do not replace him. The authors address the need for R&M in conceptual aircraft design. They provide a status in terms of approaches and technology and their effectiveness. A view of what is needed for R&M to become an effective member of the design team is presented. A process is presented by which the R&M engineer can interact the conceptual design process. Recommendations for realizing this vision are set forth
Keywords
CAD; aerospace computing; concurrent engineering; maintenance engineering; reliability; R and M; conceptual aircraft design; concurrent engineering; design process; design team; engineering functions; reliability and maintainability; skill requirements; Aerospace engineering; Aircraft propulsion; Automation; Costs; Design engineering; Environmental economics; History; Process design; Product development; Reliability engineering;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability and Maintainability Computer-Aided Engineering in Concurrent Engineering, 1990 and 1991., Combined Proceedings of the 1990 and 1991 Leesburg Workshops on
Conference_Location
Leesburg, VA ; Ellicott City, MD
Type
conf
DOI
10.1109/RMCAE.1992.245539
Filename
245539
Link To Document