US2012051898A1PendingUtilityA1
Wind turbine component having a lightweight structure
Est. expiryAug 5, 2031(~5.1 yrs left)· nominal 20-yr term from priority
F05B 2280/105F05B 2280/10302F05B 2260/96F05B 2280/10304F03D 15/00F05B 2280/1021F05B 2280/101Y02E10/72F05B 2280/1025F05B 2280/6012B22D 25/005F03D 80/00B22D 19/00
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Claims
Abstract
A wind turbine component having a lightweight structure is provided and includes a metallic matrix defining a cavity, metallic foam enclosed within the cavity and a solidification metallurgical bond formed at an entire interface between the metallic matrix and the metallic foam.
Claims
exact text as granted — not AI-modified1 . A wind turbine component configured to have a lightweight structure, the wind turbine component comprising:
a metallic matrix defining a cavity; metallic foam enclosed within the cavity; and a solidification metallurgical bond formed at an entire interface between the metallic matrix and the metallic foam.
2 . The wind turbine component according to claim 1 , for use as a wind turbine casing, gearbox housing or bedplate.
3 . The wind turbine component according to claim 1 , for use as a multi-ton component of wind turbine.
4 . The wind turbine component according to claim 1 , for use as a cast housing torque arm of a gearbox.
5 . The wind turbine component according to claim 1 , wherein the metallic matrix comprises at least one or more of aluminum, magnesium, iron, nickel, titanium, cobalt, copper, chromium and alloys thereof
6 . The wind turbine component according to claim 1 , wherein the metallic foam comprises at least one or more of aluminum, magnesium, iron, nickel, titanium, cobalt, copper, chromium and alloys thereof.
7 . The wind turbine component according to claim 1 , wherein the solidification metallurgical bond comprises an interface region in which eutectic precipitates are formed.
8 . A method to form a wind turbine component configured to have a lightweight structure, the method comprising:
shaping a mold cavity between metallic foam and an exterior mold; filling a molten metallic matrix into the mold cavity to enclose the metallic foam; and, as the molten metallic matrix cools, forming a solidification metallurgical bond at an entire interface between the metallic matrix and the metallic foam.
9 . The method according to claim 8 , further comprising controlling a distribution of metallic material in the metallic foam.
10 . The method according to claim 8 , wherein the shaping comprises at least one or more of cleaning a surface of the metallic foam and pre-heating the metallic foam.
11 . The method according to claim 8 , further comprising forming a sacrificial layer about a surface of the metallic foam.
12 . The method according to claim 8 , further comprising defining core regions in the mold cavity.
13 . The method according to claim 8 , further comprising conducting a heat treatment to improve the solidification metallurgical bond.
14 . The method according to claim 8 , wherein the shaping comprises:
building an expendable foam pattern in the mold cavity; coating a surface of the expendable foam pattern; and burning out the expendable foam pattern around preformed metallic foam inserts during the filling.
15 . A method to form a wind turbine component configured to have a lightweight structure, the method comprising:
shaping a mold cavity within a metallic matrix having an opening; filling the mold cavity with molten metallic material and a foaming agent; closing the opening such that the metallic matrix encloses the mold cavity; and, as the molten metallic material cools and foams within the mold cavity, forming a solidification metallurgical bond at an entire interface between the metallic matrix and the metallic foam.
16 . The method according to claim 15 , further comprising controlling a distribution of the metallic material in the mold cavity.
17 . The method according to claim 15 , wherein the shaping comprises at least one or more of cleaning a surface of the metallic matrix and pre-heating the metallic matrix.
18 . The method according to claim 15 , further comprising forming a sacrificial layer about a surface of the metallic matrix.
19 . The method according to claim 15 , further comprising defining core regions in the mold cavity.
20 . The method according to claim 15 , further comprising conducting a heat treatment to improve the solidification metallurgical bond.Cited by (0)
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