Integral ring gear and torque arm for a wind turbine gearbox
US-2019136962-A1 · May 9, 2019 · US
US11660671B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11660671-B2 |
| Application number | US-201917253212-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 21, 2019 |
| Priority date | Jun 21, 2018 |
| Publication date | May 30, 2023 |
| Grant date | May 30, 2023 |
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A method for manufacturing a planet gear or a sun gear of a gearbox of a wind turbine includes forming a base of the planet gear via at least one of casting or forging. The base of the planet gear includes an inner circumferential surface and an outer circumferential surface. Therefore, at least one of the inner circumferential surface or the outer circumferential surface of the planet gear includes a plurality of net or near-net gear teeth. The method also includes applying a coating material to at least a portion of the base of the gear and at least a portion of the plurality of gear teeth of the gear via an additive manufacturing process so as to increase a hardness of the portions of the base and the plurality of gear teeth that includes the coating material.
Opening claim text (preview).
What is claimed is: 1. A method for manufacturing a gear of a gearbox of a wind turbine, the gear comprising at least one of a planet gear or a sun gear, the method comprising: forming a base of the gear via at least one of casting or forging, the base of the gear comprising an inner circumferential surface and an outer circumferential surface, the outer circumferential surface of the gear comprising a plurality of gear teeth; applying a coating material to at least a portion of the base of the gear and at least a portion of the plurality of gear teeth of the gear via an additive manufacturing process so as to increase a hardness of the portions of the base and the plurality of gear teeth that includes the coating material; and wherein the coating material comprises at least one of boron nitride, aluminum oxide, silicon carbide, tungsten carbide, or a nickel-based alloy; and machining the plurality of gear teeth after applying the coating material. 2. The method of claim 1 , further comprising forming a journal bearing on the other of the inner circumferential surface or the outer circumferential surface opposite the plurality of gear teeth via the additive manufacturing process. 3. The method of claim 1 , further comprising forming the base with one or more voids through a thickness thereof defined between the inner circumferential surface and the outer circumferential surface so as to minimize a weight of the gear. 4. The method of claim 1 , wherein the additive manufacturing process comprises at least one of cold spraying, thermal spray, laser cladding, binder jetting, material jetting, directed energy deposition; or powder bed fusion. 5. The method of claim 1 , wherein applying the coating material to at least a portion of the base of the gear and at least a portion of the plurality of gear teeth of the gear via the additive manufacturing process further comprises applying the coating material to at least one side of the plurality of gear teeth, a root of the gear teeth, or a tip of the gear teeth. 6. The method of claim 1 , wherein applying the coating material to at least a portion of the base of the gear and at least a portion of the plurality of gear teeth of the gear via the additive manufacturing process further comprises applying the coating material with varying thicknesses on the base or ole each of the gear teeth depending on a location of the gear within the wind turbine. 7. The method of claim 1 , further comprising forming the base of the gear from at least one of steel, cast steel, iron, or ductile iron. 8. The method of claim 1 , wherein the machining the plurality of gear teeth further comprises at least one of hobbing or grinding the plurality of gear teeth after applying the coating material. 9. A method for manufacturing a planetary carrier for supporting a plurality of planet gears of a gearbox of a wind turbine, the method comprising: forming a base of the planetary carrier via at least one of casting or forging, the base of the planetary carrier comprising an upwind end and downwind end; applying a coating material to the base and at least one of the upwind end or the downwind end to form a journal bearing thereon via an additive manufacturing process; and machining the base and the at least one the upwind end or the downwind end after applying the coating material. 10. The method of claim 9 , wherein the additive manufacturing process comprises at least one of cold spraying, thermal spray, laser cladding, binder jetting, material jetting, directed energy deposition, or powder bed fusion. 11. The method of claim 9 , wherein the coating material comprises at least one of boron nitride, aluminum oxide, silicon carbide, tungsten carbide, or a nickel-based alloy. 12. The method of claim 9 , further comprising forming the base of the planetary carrier from at least one of steel, cast steel, iron, or ductile iron.
by spraying molten metal, i.e. spray sintering, spray casting · CPC title
by casting · CPC title
Coatings or solid lubricants, e.g. anti-seize layers or pastes · CPC title
Materials specially adapted for additive manufacturing · CPC title
of the epicyclical, planetary or differential type · CPC title
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