Wind turbine blade with uncoupled trailing edge
11078883 · 2021-08-03
Inventors
Cpc classification
F01D5/147
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0658
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/18
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
F03D1/0691
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F03D1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A blade for a wind turbine has a hollow or exoskeleton blade body. The blade body has a leading edge and a trailing edge along a span thereof. The blade body includes a first blade portion and a second blade portion wherein the first blade portion and the second blade portion are integrated with one another along at least 90% of the leading edge, and are in uncoupled contact at the trailing edge. The uncoupled contact permits the first blade portion and second blade portion to experience relative movement at the trailing edge when the blade body twists.
Claims
1. A blade for a wind turbine, comprising an exoskeleton blade body having a leading edge and a trailing edge along a span of said blade body, said blade body having a first blade portion and a second blade portion wherein said first blade portion and said second blade portion are integrated with one another along at least 90% of said leading edge, and wherein said first blade portion and said second blade portion are in unbonded and non-integrated contact at said trailing edge for supporting relative movement between said first blade portion and said second blade portion all along said span of said blade body at said trailing edge when said blade body twists wherein, when oscillating torsional loads are generated as said blade body undergoes cyclic twisting, said unbonded and non-integrated contact causes said oscillating torsional loads to be directed through said leading edge and not through said trailing edge.
2. The blade as in claim 1, further comprising a hollow mounting support integrated with a root of said blade body, said hollow mounting support having a first support portion extending from said first blade portion and having a second support portion extending from said second blade portion, wherein said first support portion and said second support portion are integrated where extending from said leading edge, and wherein said first support portion and said second support portion are in contact with one another where extending from said trailing edge for supporting sliding movement there between when said blade body twists.
3. The blade as in claim 2, further comprising a rigid support disposed in at least a portion of said hollow mounting support, said rigid support and said hollow mounting support adapted to be coupled to a hub of a wind turbine wherein said first support portion and said second support portion remain in said contact with one another where extending from said trailing edge for supporting sliding movement there between when said blade body twists.
4. The blade as in claim 1, wherein said first blade portion and said second blade portion are integrated with one another along 100% of said leading edge.
5. The blade as in claim 1, wherein said at least 90% of said leading edge is a first contiguous region of said leading edge extending from a root of said blade body, wherein a second contiguous region of said leading edge extends from said first contiguous region to a tip of said blade body, and wherein said first blade portion and said second blade portion are in contact with one another at said second contiguous region and at said tip of said blade body for supporting sliding movement there between when said blade body twists.
6. A blade for a wind turbine, comprising a hollow blade-shaped body having a root and a tip, said blade-shaped body having a leading edge and a trailing edge wherein said leading edge and said trailing edge extend from said root to said tip, said blade-shaped body having a first blade portion and a second blade portion wherein said first blade portion and said second blade portion are integrated at said leading edge and are in unbonded and non-integrated contact at said trailing edge for supporting relative movement between said first blade portion and said second blade portion all along said span of said blade body along all of said trailing edge when said blade body twists wherein, when oscillating torsional loads are generated as said blade body undergoes cyclic twisting, said unbonded and non-integrated contact causes said oscillating torsional loads to be directed through said leading edge and not through said trailing edge.
7. The blade as in claim 6, further comprising a hollow mounting support integrated with and extending from said root, said hollow mounting support having a first support portion extending from said first blade portion and having a second support portion extending from said second blade portion, wherein said first support portion and said second support portion are integrated where extending from said leading edge, and wherein said first support portion and said second support portion are in contact with one another where extending from said trailing edge for supporting sliding movement there between when said blade body twists.
8. The blade as in claim 7, further comprising a rigid support disposed in at least a portion of said hollow mounting support, said rigid support and said hollow mounting support adapted to be coupled to a hub of a wind turbine wherein said first support portion and said second support portion remain in said contact with one another where extending from said trailing edge.
9. The blade as in claim 6, wherein said first blade portion and said second blade portion are in contact with one another at said tip of said blade body for supporting sliding movement there between when said blade body twists.
10. A blade for a wind turbine, comprising a hollow blade-shaped body having a root and a tip, said blade-shaped body having a leading edge and a trailing edge wherein said leading edge and said trailing edge extend from said root to said tip, said blade-shaped body having a first blade portion and a second blade portion wherein said first blade portion and said second blade portion are integrated with one another along at least 90% of said leading edge and are in an unbonded and non-integrated contact relationship at said trailing edge, said blade-shaped body adapted to be coupled to a hub of a wind turbine wherein said first body portion and said second body portion remain in said unbonded and non-integrated contact relationship at said trailing edge for supporting relative movement between said first blade portion and said second blade portion all along said span of said blade body along all of said trailing edge when said blade body twists wherein, when oscillating torsional loads are generated as said blade body undergoes cyclic twisting, said unbonded and non-integrated contact relationship causes said oscillating torsional loads to be directed through said leading edge and not through said trailing edge.
11. The blade as in claim 10, wherein said blade-shaped body includes a hollow mounting support integrated with and extending from said root, said hollow mounting support having a first support portion extending from said first blade portion and having a second support portion extending from said second blade portion, wherein said first support portion and said second support portion are integrated where extending from said leading edge and wherein said first support portion and said second support portion are in contact with one another where extending from said trailing edge for supporting sliding movement there between when said blade body twists.
12. The blade as in claim 11, further comprising a rigid support disposed in at least a portion of said hollow mounting support, said rigid support and said hollow mounting support adapted to be coupled to a hub of a wind turbine wherein said first support portion and said second support portion remain in said contact with one another where extending from said trailing edge.
13. The blade as in claim 10, wherein said first blade portion and said second blade portion are integrated with one another along 100% of said leading edge.
14. The blade as in claim 10, wherein said at least 90% of said leading edge is a first contiguous region of said leading edge extending from said root of said blade body, wherein a second contiguous region of said leading edge extends from said first contiguous region to said tip of said blade body, and wherein said first blade portion and said second blade portion are in contact with one another at said second contiguous region and at said tip of said blade body for supporting sliding movement there between when said blade body twists.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Other objects, features and advantages of the present invention will become apparent upon reference to the following description of the preferred embodiments and to the drawings, wherein corresponding reference characters indicate corresponding parts throughout the several views of the drawings and wherein:
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DETAILED DESCRIPTION OF THE INVENTION
(15) Referring now to the drawings and more particularly to
(16) In accordance with the present invention, blade 10 is defined by a hollow-body construction. That is, blade 10 is an exoskeleton structure that can be manufactured, for example, as a composite structure made using well-known material lay-up and curing fabrication techniques. For example, a blade of the present invention could be fabricated using low cost materials like fiberglass. The blade's outer skin could be fabricated by draping fiberglass material over a lay-up tool in the region that will ultimately become the blade's leading edge 16 with the fiberglass material then extending to cover the entire lay-up tool to thereby define portions 20 and 22 up to what will ultimately become the blade's trailing edge 18. The process is repeated from root 12 to tip 14 of the blade. Additional load bearing composite material in the form of, for example, rectangular plies can be draped during the lay-up process at the portion of the blade that will ultimately become leading edge 16.
(17) Regardless of the fabrication technique used to construct blade 10, its exoskeleton or hollow body will cause portions 20 and 22 to be in contact with one another at trailing edge 18. However, unlike conventional blades, portions and 22 are not coupled, joined, bonded or integrated with one another at trailing edge 18. That is, portions 20 and 22 are in an uncoupled contact relationship with one another at trailing edge 18. As a result, when blade 10 experiences torsional loads that cause blade 10 to twist along its span, portions 20 and 22 can experience relative movement there between along trailing edge 18 (i.e., along the span of blade 10) as indicated by opposing arrows 24 and 26, respectively. It is to be understood that the directions of relative movement 24 and 26 are dependent on whether blade 10 twists into portion 20 or into portion 22.
(18) Blade 10 with its uncoupled trailing edge 18 prevents torsional (or twist) movement-based shear loads from being transferred through the blade's trailing edge 18. Instead, the uncoupled contact trailing edge 18 redirects all of the torsional or twist energy through the leading edge as a “spring” load. The exoskeleton or hollow-body blade 10 simplifies the uncoupling contact at trailing edge 18 while also maximizing the blades ability to redirect and distribute the torsional loads by allowing portions 20 and 22 to slide or slip relative to one another across the entire span of trailing edge 18 from root 12 to tip 14 regardless of which way blade 10 is twisting. Accordingly, the relative movement of portions 20 and 22 is easily accomplished and repeated during a blade's cyclic motion experienced as the blade rotates around a hub to which it is coupled.
(19) The uncoupled contact between portions 20 and 22 permitting the above-described movements 24/26 can be realized in a variety of ways without departing from the scope of the present invention. By way of non-limiting and illustrative examples,
(20) Referring now to
(21) Another embodiment of the present invention is illustrated in
(22) In general, open channel 220 can wrap around at tip 14 and extend to a point along the blade's leading edge that is up to 10% of the entire span length of the blade. Said another way, a blade's leading edge must have its blade portions 20 and 22 integrated with one another along at least 90% of the blade's span length beginning at the blade's root. This is illustrated in the embodiment shown in
(23) Blades constructed in accordance with the present invention must be connected to a rotating hub. To facilitate such a connection, a mounting support can serve as a link between a blade's root and a rotating hub. An embodiment of such a mounting support is illustrated in
(24) In the illustrated embodiment, the open channel configuration of uncoupled contact transitions from being constructed using the high pressure side of mounting support 30 (i.e., open channel 400 constructed as a continuation of portion 40) to using the low pressure side of blade 10 (i.e., open channel 220 constructed as a continuation blade portion 22). The advantage of this construction is that it allows the high pressure portion of the blade (i.e., blade portion 20) to move inboard without interacting with the low pressure portion of the blade (i.e., blade portion 22) at the blade's root.
(25) Referring now to the cross-sectional view presented in
(26) Referring now to
(27) The advantages of the present invention are numerous. The uncoupled contact at the blade's trailing edge reduces torsional loads normally transmitted into a blade's trailing edge as it undergoes cyclic twist during rotation. More specifically, the blade's unique construction redirects the oscillating load path (generated during blade rotation) entirely through the lead edge from the high pressure portion of the blade to the low pressure portion of the blade and back again. By directing the load path through the blade's leading edge and not through the blade's trailing edge, the blade will act more like a spring than a confined box that is shaped like a conventional wing having high and low pressure surfaces coupled along its trailing edge. Instead of fatigue stress loads traveling through the blade, the loads translate to harmless oscillating inboard-to-outboard or side-to-side motion as the trailing edge slide in a channel the length of the trailing edge. The blade's design lends itself to solid, co-cure lay-up techniques that require no bonded components or adhesives. The blade and its operations advantages are achieved totally autonomously using gravity-induced, cyclic oscillating blade pitch mode. The hollow or exoskeleton design provides a lighter blade that requires no interior core elements. The blade's cyclic oscillating blade pitch mode means the falling-blade portion of the rotation cycle is in a streamline state to reduce the blade's noise signature.
(28) Although the invention has been described relative to a specific embodiment thereof, there are numerous variations and modifications that will be readily apparent to those skilled in the art in light of the above teachings. It is therefore to be understood that, within the scope of the appended claims, the invention may be practiced other than as specifically described.