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Integration Methodology For Oil-Free Shaft Support Systems: Four Steps to SuccessCommercial applications for Oil-Free turbomachinery are slowly becoming a reality. Micro-turbine generators, highspeed electric motors, and electrically driven centrifugal blowers are a few examples of products available in today's commercial marketplace. Gas foil bearing technology makes most of these applications possible. A significant volume of component level research has led to recent acceptance of gas foil bearings in several specialized applications, including those mentioned above. Component tests identifying such characteristics as load carrying capacity, power loss, thermal behavior, rotordynamic coefficients, etc. all help the engineer design foil bearing machines, but the development process can be just as important. As the technology gains momentum and acceptance in a wider array of machinery, the complexity and variety of applications will grow beyond the current class of machines. Following a robust integration methodology will help improve the probability of successful development of future Oil-Free turbomachinery. This paper describes a previously successful four-step integration methodology used in the development of several Oil-Free turbomachines. Proper application of the methods put forward here enable successful design of Oil-Free turbomachinery. In addition when significant design changes or unique machinery are developed, this four-step process must be considered.
Document ID
20100040419
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Howard, Samuel A.
(NASA Glenn Research Center Cleveland, OH, United States)
DellaCorte, Christopher
(NASA Glenn Research Center Cleveland, OH, United States)
Bruckner, Robert J.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2010
Subject Category
Mechanical Engineering
Report/Patent Number
E-17456
NASA/TM-2010-216827
Report Number: E-17456
Report Number: NASA/TM-2010-216827
Meeting Information
Meeting: 8th International Conference on Rotor Dynamics
Location: Seoul
Country: Korea, Republic of
Start Date: September 12, 2010
End Date: September 15, 2010
Sponsors: International Federation for the Promotion of Mechanism
Funding Number(s)
WBS: WBS 877868.02.07.03.01.01.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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