Multiple-blade wind machine with shrouded rotors
10066597 ยท 2018-09-04
Assignee
Inventors
Cpc classification
F05B2240/33
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/2211
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/0204
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
F03D1/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A horizontal-shaft wind machine having improved low wind speed performance and greater overall efficiency consists of multiple rotors, wherein each successive rotor is larger in diameter than the previous rotor moving from the most windward rotor to the most leeward rotor. Each rotor may be coupled to a shroud/diffuser that is displaced axially downwind from the rotor.
Claims
1. A wind machine (10) adapted to extract work from the wind comprising: a first rotor shaft (14) having a substantially horizontal axis of rotation; a bearing support (70) capable of aligning the axis of rotation (20) of the first rotor shaft (14) with the wind direction whereby the first rotor shaft has an upwind end (72) and a downwind end (74); a first rotor assembly (28) rotatable about the first rotor shaft, the first rotor assembly comprising a hub (36) attached to the upwind end (72) of the first rotor shaft (14), the rotor assembly (28) further comprising a first plurality of sails (54) attached to the hub (36), the first plurality of sails extending substantially radially outward substantially equidistant from the hub (36) to define an outer diameter (d) of the rotor assembly (28); the first rotor assembly having an upwind face and a downwind face; and a first shroud (32) comprising a substantially annular body having an upwind leading edge (52), a downwind trailing edge (76) and an inside diameter (D), the inside diameter (D) of the first shroud (32) having a dimension that is larger than the outer diameter (d) of the first rotor assembly (28), the first shroud being mounted for rotation with the first rotor shaft (14), the upwind leading edge of the first shroud being offset axially downwind from the downwind face of the first rotor assembly, whereby an axial and radial gap is formed between the first rotor assembly and the first shroud.
2. The wind machine of claim 1, further comprising a second rotor shaft (78) mounted for rotation coaxially with the first rotor shaft (14), the second rotor shaft having an upwind end (72) and a downwind end (74); a second rotor assembly (30) attached to the second rotor shaft (78), the second rotor assembly (30) comprising a second (80) attached to the upwind end (72) of the second rotor shaft (78), the second rotor assembly (30) further comprising a second plurality of sails (82) attached to the second hub (80), the second plurality of sails (82) extending substantially radially outward substantially equidistant from the hub to define an outer diameter (d.sub.2) of the second rotor assembly (30), the second rotor assembly having an upwind face and a downwind face; and a second shroud (34) comprising a substantially annular body having an upwind leading edge (84), a downwind trailing edge (86) and an inside diameter (D.sub.2), the inside diameter (D.sub.2) of the second shroud having a dimension that is larger than the outer diameter (d.sub.2) of the second rotor assembly, the second shroud (32) being mounted for rotation with the second rotor shaft, the upwind leading edge of the second shroud being offset axially downwind from the downwind face of the second rotor assembly, whereby an axial and radial gap is formed between the second rotor assembly and the second shroud.
3. The wind machine of claim 2, wherein: the outer diameter of the second rotor assembly (d.sub.2) is larger than the outer diameter (d) of the first rotor assembly; and the second rotor assembly (30) is displaced axially downwind from the first rotor assembly (28).
Description
BRIEF DESCRIPTION OF THE DRAWING
(1) The present invention will be better understood from a reading of the following detailed description, taken in conjunction with the accompanying drawing figures in which like references designate like elements and, in which:
(2)
(3)
DETAILED DESCRIPTION
(4) The drawing figures are intended to illustrate the general manner of construction and are not necessarily to scale. In the detailed description and in the drawing figures specific illustrative examples are shown and herein described in detail. It should be understood, however, that the drawing figures and detailed description are not intended to limit the invention to the particular form disclosed, but are merely illustrative and intended to teach one of ordinary skill how to make and/or use the invention claimed herein and for setting forth the best mode for carrying out the invention.
(5) With reference to
(6) With particular reference to
(7) A plurality of sails 54 are mounted to wheel arms 38 and/or support bands 46, 48 and 50 so as to extend in a windward (72) direction forward of wheel arms 38. Sails 54 are attached substantially equidistant from shaft 14 to create a substantially rotationally balanced circular rotor having an outer diameter (d). Each of the plurality of sails 54 has a root 56, a tip 58, a leading edge 60, and a trailing edge 62. Sails 54 may be of any conventional construction, for example fabric, sheet metal, or ultraviolet-resistant plastic, but in the illustrative embodiment are formed of galvanized steel sheet.
(8) In addition to providing support for wheel arms 38, support band 46 provides a mounting point for shroud 32 which is mounted to wheel arms 38. Shroud 32 comprises a generally cylindrical section 64 having an inside diameter (D) a tapered conical section 66 and a brim 68 which cooperate to act as a diffuser to form a low-pressure region immediately behind rotor 28. Shroud 32 is supported so that the leading-edge 52 of shroud 32 is displaced in a downwind (76) direction relative to the trailing edges 62 of sails 54 so that there is a gap g between the leading-edge 52 of shroud 32 and the trailing edges 56 of sails 54. The gap g may be optimized for various wind conditions to maximize the energy captured by rotor 30, which would otherwise be lost due to side flow. As shown in
(9) Although certain illustrative embodiments and methods have been disclosed herein, it will be apparent from the foregoing disclosure to those skilled in the art that variations and modifications of such embodiments and methods may be made without departing from the invention. For example, although the illustrative embodiment of
(10) Wind machine 10 may be used for AC or DC electric power generation, pumping water, or any other task performed by wind machines and therefore the invention is not intended to be limited to the manner in which the power is transmitted to the ultimate load. Accordingly, it is intended that the invention should be limited only to the extent required by the appended claims and the rules and principles of applicable law. Additionally, as used herein, unless otherwise specifically defined, the terms substantially or generally when used with mathematical concepts or measurements mean within 10 degrees of angle or within 10 percent of the measurement, whichever is greater. As used herein, a step of providing a structural element recited in a method claim means and includes obtaining, fabricating, purchasing, acquiring or otherwise gaining access to the structural element for performing the steps of the method. As used herein, the claim terms are to be given their broadest reasonable meaning unless a clear disavowal of that meaning appears in the record in substantially the following form (As used herein the term .sub. is defined to mean .sub.)