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Small Scale High Speed TurbomachineryA small scale, high speed turbomachine is described, as well as a process for manufacturing the turbomachine. The turbomachine is manufactured by diffusion bonding stacked sheets of metal foil, each of which has been pre-formed to correspond to a cross section of the turbomachine structure. The turbomachines include rotating elements as well as static structures. Using this process, turbomachines may be manufactured with rotating elements that have outer diameters of less than four inches in size, and/or blading heights of less than 0.1 inches. The rotating elements of the turbomachines are capable of rotating at speeds in excess of 150 feet per second. In addition, cooling features may be added internally to blading to facilitate cooling in high temperature operations.
Document ID
20180004301
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
London, Adam P.
Droppers, Lloyd J.
Lehman, Matthew K.
Mehra, Amitav
Date Acquired
August 9, 2018
Publication Date
June 26, 2018
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-10,006,291
Patent Application Number: US-Patent-Appl-SN-14/616,048
Funding Number(s)
CONTRACT_GRANT: NNX10CA89C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-10,006,291
Patent Application
US-Patent-Appl-SN-14/616,048
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