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Analytical Method to Evaluate Failure Potential During High-Risk Component DevelopmentCommunicating failure mode information during design and manufacturing is a crucial task for failure prevention. Most processes use Failure Modes and Effects types of analyses, as well as prior knowledge and experience, to determine the potential modes of failures a product might encounter during its lifetime. When new products are being considered and designed, this knowledge and information is expanded upon to help designers extrapolate based on their similarity with existing products and the potential design tradeoffs. This paper makes use of similarities and tradeoffs that exist between different failure modes based on the functionality of each component/product. In this light, a function-failure method is developed to help the design of new products with solutions for functions that eliminate or reduce the potential of a failure mode. The method is applied to a simplified rotating machinery example in this paper, and is proposed as a means to account for helicopter failure modes during design and production, addressing stringent safety and performance requirements for NASA applications.
Document ID
20020087935
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Tumer, Irem Y.
(NASA Ames Research Center Moffett Field, CA United States)
Stone, Robert B.
(Missouri Univ. Rolla, MO United States)
Clancy, Daniel
Date Acquired
September 7, 2013
Publication Date
June 25, 2001
Subject Category
Quality Assurance And Reliability
Report/Patent Number
DETC2001/DFM-21173
Report Number: DETC2001/DFM-21173
Meeting Information
Meeting: 2001 ASME Design Engineering Technical Conference
Location: Pittsburgh, PA
Country: United States
Start Date: September 9, 2001
End Date: September 12, 2001
Sponsors: American Society of Mechanical Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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