COMPOSITE BOUNDARY LAYER TURBINE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20130039742A1
SERIAL NO

13508245

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A turbine includes a plurality of stacked disks, each disk comprising an opening in the center of the disk, which forms a central flow chamber. The turbine further includes a first disk that is coupled to a bottom of the plurality of stacked disks. The first disk does not have an opening in the center like the stacked disks. There is a plurality of disk spacers positioned between one or more of the plurality of stacked disks, thereby creating flow channels between the disks. The flow channels extend from an outside perimeter of the stacked disks to the central flow chamber. A tapered armature is coupled to the first disk and positioned within the central flow chamber, and a fluid collection unit is in communication with the outside perimeter of the stacked disks.

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Patent Owner(s)

Patent OwnerAddress
NP TECHNOLOGIESMINNEAPOLIS MN

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Holt, Drew Minneapolis, US 1 4
Wilson, Erich A Provo, US 13 118

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