US2009288742A1PendingUtilityA1
Method for increasing the fatigue strength of a predominantly steel mechanical part of a wind turbine and/or for reducing the tendency to form what are called "white etching cracks" or "brittle flakes" in such steel mechanical parts
Est. expiryMay 20, 2028(~1.9 yrs left)· nominal 20-yr term from priority
F16C 33/62F16C 2361/61C21D 1/09C21D 9/36C21D 9/40F16C 2300/14F16C 33/36
51
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Claims
Abstract
Method for increasing the fatigue strength of a mechanical part of a wind turbine and/or for reducing the tendency to form what are called “white etching cracks” or “brittle flakes” in such a bearing, which includes making one or several of the bearing rings and/or roller elements concerned of the bearing at least partly of a hardened steel having a carbon content between 0.4 and 0.8 percent by weight.
Claims
exact text as granted — not AI-modified1 . Method for increasing the fatigue strength of the predominantly steel mechanical part ( 1 ) of a wind turbine and/or for reducing the tendency to form what are called “white etching cracks” or “brittle flakes” in such steel mechanical part ( 1 ), which comprises making the mechanical part at least partly out of a hardened steel having a carbon content between 0.4 and 0.8 percent by weight.
2 . Method according to claim 1 , characterised in that it is applied to a part of the gearbox of a wind turbine.
3 . Method according to claim 1 , characterised in that the above-mentioned elements of the mechanical part ( 1 ) which are made of hardened steel are hardened by means of full-hardening.
4 . Method according to claim 3 , characterised in that the above-mentioned elements of the mechanical part ( 1 ) which are made of hardened steel are entirely full-hardened.
5 . Method according to claim 1 , characterised in that the above-mentioned elements of the mechanical part ( 1 ) which are made of hardened steel are hardened by means of induction hardening.
6 . Method according to claim 1 , characterised in that the above-mentioned elements of the mechanical part ( 1 ) which are made of hardened steel are hardened by means of laser hardening.
7 . Method according to claim 1 , characterised in that, when cooling the steel so as to harden it, the variation in temperature as a function of time is controlled such that a predominantly martensitic metal matrix is obtained with little or no carbide formation.
8 . Method according to claim 1 , characterised in that, when cooling the steel so as to harden it, the variation in temperature as a function of time is controlled such that a predominantly bainitic metal matrix is obtained with little or no carbide formation.
9 . Method according to claim 7 , characterised in that a hardened steel is used with a martensite content, bainite content respectively, of more than 80 percent by weight.
10 . Method according to claim 7 , characterised in that the formation of carbides is restricted to less than 2% carbides measured as a portion of the surface.
11 . Method according to claim 1 , characterised in that the hardened steel is alloyed with one of the following elements or a combination thereof: Cr, Mn, Si, Mo, V.
12 . Method according to claim 1 , characterised in that it is applied to a bearing, in particular to one or several of the bearing rings ( 2 , 3 ) and/or roller elements ( 4 ) of the bearing ( 1 ) concerned.
13 . Method according to claim 2 , characterised in that the above-mentioned elements of the mechanical part ( 1 ) which are made of hardened steel are hardened by means of full-hardening.
14 . Method according to claim 8 , characterised in that a hardened steel is used with a martensite content, bainite content respectively, of more than 80 percent by weight.
15 . Method according to claim 8 , characterised in that the formation of carbides is restricted to less than 2% carbides measured as a portion of the surface.Cited by (0)
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