US2014086755A1PendingUtilityA1
Turbocharger and component therefor
Est. expiryJun 7, 2031(~4.9 yrs left)· nominal 20-yr term from priority
C22C 38/04C22C 38/28F05D 2300/13C22C 38/02C22C 38/26C22C 38/38C22C 38/001C22C 38/22F02C 6/12F01D 25/24C22C 38/24F02B 37/00F01D 5/12
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Claims
Abstract
A component for turbocharger applications, in particular in diesel engines, which has an iron-based alloy having a ferritic base structure which has a carbide and nitride structure.
Claims
exact text as granted — not AI-modified1 . A component for turbocharger applications, in particular in diesel engines, comprising an iron-based alloy having a ferritic base structure comprising a carbide and nitride structure.
2 . The component for turbocharger applications as claimed in claim 1 , comprising at least one of the elements selected from: W, Ti and Nb.
3 . The component for turbocharger applications as claimed in claim 1 , comprising at least one of the elements selected from: C, W, Cr, Mn, Ti, V, Nb and Si.
4 . The component for turbocharger applications as claimed in claim 1 , comprising substantially the following elements:
C: 0.1 to 0.5% by weight, in particular 0.25 to 0.4% by weight, Cr: 15 to 22% by weight, in particular 18 to 20% by weight, Mn: ≦1.3% by weight, in particular ≦1% by weight, Si: 0.8 to 2.1% by weight, in particular 1 to 1.8% by weight, Nb: 0.4 to 1.3% by weight, in particular 0.6 to 1.1% by weight, Ti: 0.2 to 0.6% by weight, in particular 0.3 to 0.5% by weight, W: 1.8 to 3.0% by weight, in particular 2 to 2.7% by weight, V: 0.3 to 1.0% by weight, in particular 0.5 to 0.8% by weight, N: ≦3% by weight, in particular ≦2% by weight, and Fe: ad 100% by weight.
5 . The component for turbocharger applications as claimed in claim 1 , wherein it is substantially free of sigma phases.
6 . The component for turbocharger applications as claimed in claim 1 , wherein the component is at least one of a kinematics component, a wastegate component and a VTG component.
7 . An exhaust-gas turbocharger in particular for diesel engines, comprising at least one component consisting of an iron-based alloy having a ferritic base structure comprising a carbide and nitride structure.
8 . The exhaust-gas turbocharger as claimed in claim 7 , wherein the component comprises at least one of the elements selected from: W, Ti and Nb.
9 . The exhaust-gas turbocharger as claimed in claim 7 , wherein the component comprises substantially the following elements:
C: 0.1 to 0.5% by weight, in particular 0.25 to 0.4% by weight, Cr: 15 to 22% by weight, in particular 18 to 20% by weight, Mn: ≦1.3% by weight, in particular ≦1% by weight, Si: 0.8 to 2.1% by weight, in particular 1 to 1.8% by weight, Nb: 0.4 to 1.3% by weight, in particular 0.6 to 1.1% by weight, Ti: 0.2 to 0.6% by weight, in particular 0.3 to 0.5% by weight, W: 1.8 to 3.0% by weight, in particular 2 to 2.7% by weight, V: 0.3 to 1.0% by weight, in particular 0.5 to 0.8% by weight, N: ≦3% by weight, in particular ≦2% by weight, and Fe: ad 100% by weight.
10 . The exhaust-gas turbocharger as claimed in claim 7 , wherein the component is substantially free of sigma phases.
11 . The component for turbocharger applications as claimed in claim 1 , wherein the component is a VTG component and/or a flap mount part.
12 . The exhaust-gas turbocharger as claimed in claim 7 , wherein the component comprises at least one of the elements selected from: C, W, Cr, Mn, Ti, V, Nb and Si.Cited by (0)
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