Inertial pneumatic wave energy device
US-2023383722-A1 · Nov 30, 2023 · US
US9765753B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9765753-B2 |
| Application number | US-201314070855-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 4, 2013 |
| Priority date | Jul 26, 2006 |
| Publication date | Sep 19, 2017 |
| Grant date | Sep 19, 2017 |
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A turbine arrangement for a bi-directional reversing flow is provided. The turbine arrangement may include a rotor rotatably mounted to rotate about an axis of the turbine arrangement, and the rotor may have a plurality of rotor blades disposed circumferentially thereabout. A first set of guide vanes may be circumferentially disposed about the axis for directing the bi-directional reversing flow to and from the rotor blades via a first flow passaged defined by a first duct. A second set of guide vanes may be axially spaced from the first set of guide vanes and circumferentially disposed about the axis for directing the bi-directional reversing flow to and from the rotor blades via a second flow passage defined by a second duct. The guide vanes may be disposed at a greater radius than the rotor blades, such that the guide vanes are radially offset from the rotor blades.
Opening claim text (preview).
We claim: 1. A bi-directional flow impulse type turbine arrangement for use with a bi-directional reversing flow through the turbine arrangement, the turbine arrangement having an axis and comprising: a rotor rotatably mounted to rotate about the axis and having a plurality of rotor blades disposed circumferentially around the rotor, a first set of guide vanes circumferentially disposed about the axis for directing the bi-directional reversing flow to and from the rotor blades via a first flow passage defined by a first duct; and a second set of guide vanes axially spaced from the first set of guide vanes and circumferentially disposed about the axis for directing the bi-directional reversing flow to and from the rotor blades via a second flow passage defined by a second duct, wherein the first and second sets of guide vanes are disposed at a greater radius than the rotor blades, such that an entirety of each of the first and second sets of guide vanes is disposed radially outward from each blade tip of the rotor blades. 2. The turbine arrangement of claim 1 , wherein the height of the first and second flow passages is constant along the length of the respective first and second ducts. 3. An oscillating water column power generator comprising: a housing defining a chamber for a fluid which is periodically compressed and expanded by the oscillating water column, the housing having an outlet for directing a bi-directional reversing flow of the fluid periodically compressed and expanded by the oscillating water column from the housing; a turbine arrangement of any preceding claim connected to the outlet and driven by the bi-directional reversing flow of the fluid from the outlet; and a generator connected to and driven by the rotor of the turbine arrangement.
of impulse type · CPC title
Means for influencing boundary layers or secondary circulations (for compressors F04D29/68) · CPC title
Shape, i.e. outer, aerodynamic form (F01D5/148 - F01D5/20 take precedence; blade construction F01D5/147) · CPC title
of impulse type · CPC title
to control boundary layer · CPC title
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