Bracket/spacer optimization in bladeless turbines, compressors and pumps
OwnerErich A. Wilsoninventor
Life of this patent
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Abstract
A bracket/spacer design in a bladeless turbine, compressor or pump comprising of a hub for axial mounting and one or more arms connected to the hub. This bracket/spacer configuration contributes in part or completely to form one or more fluid flow chambers along with coinciding geometry of the neighboring disk or disks facilitating the entrance or exit of fluid for the purpose of extracting or infusing energy into or from the fluid. Furthermore, this invention includes a precise description of non-constant angular and axial geometry of the bracket/spacer arm or arms.
Claims5
A one piece bracket and/or spacer attached to a single disk or disks, said single disk or disks comprises a generally planar geometry, said bracket and/or spacer comprising a rotational axis said bracket and/or spacer comprises an axial geometry which is generally flat, tapered or contoured such that it completely spans the axial distance between two disks or acts as an inlet/outlet structure when adjacent to said single disk, is used with gaseous or liquid working fluid and implemented as a component of a disk assembly creating a distance between disks or shapes said inlet/outlet structure at the end of said disk assembly of a bladeless compressor, pump or turbine further comprising:
- geometry and function independent of attachment to a neighboring disk;
- and
- comprising a hub at or around the axis of rotation extending outward away from the axis of rotation and initially contouring in a non-linear fashion along flow chambers of the neighboring disk or disks, and defining multiple separate flow chambers between each two neighboring disks.
Dependencies are inferred from the claim text.