US2012207608A1PendingUtilityA1
Final-stage rotor blade of a steam turbine
Est. expirySep 30, 2029(~3.2 yrs left)· nominal 20-yr term from priority
B29C 70/342B29L 2031/08Y02P70/50F05D 2300/603F05D 2300/2262B29K 2995/0087F01D 5/288Y02T50/60F01D 5/286F05D 2300/21B29C 70/088F01D 5/14F01D 5/28F05D 2300/133F05D 2300/44F01D 5/282Y10T29/4932B29L 2031/085F01D 5/284
32
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
A turbine blade is provided that includes at least certain regions made of fiber reinforced composite material. Also, the turbine blade has at least one anti-erosion component for protecting against erosion. The turbine blade could be, for example, a last stage blade of a steam turbine. Furthermore, methods for producing a turbine blade of this type using an impregnation mold are provided.
Claims
exact text as granted — not AI-modified1 - 13 . (canceled)
14 . A turbine blade, comprising:
at least a region made from fiber-reinforced composite material, and at least one anti-erosion component.
15 . The turbine blade according to claim 14 , wherein the anti-erosion component is inserted into the blade contour of the turbine blade.
16 . The turbine blade according to claim 15 , wherein the anti-erosion component is inserted into the blade contour of the turbine blade such that a smooth transition is created between the anti-erosion component and the turbine blade.
17 . The turbine blade according to claim 15 , wherein the inserted anti-erosion component is connected to the turbine blade by laminating, or gluing, or by a securing device, or combinations thereof.
18 . The turbine blade according to claim 17 , wherein the securing device is selected from the group consisting of: screws, rivets and pins.
19 . The turbine blade according claim 14 , wherein the anti-erosion component is made from carbide, titanium or ceramic.
20 . The turbine blade according to claim 14 , wherein an intermediate layer is arranged between the anti-erosion component and the turbine blade.
21 . The turbine blade according to claim 20 , wherein the intermediate layer comprises an elastic and/or viscoelastic layer.
22 . The turbine blade according to claim 14 , wherein the anti-erosion component has a multi-layer structure.
23 . The turbine blade according claim 14 , wherein an anti-erosion component is arranged at least at the leading edge and/or the trailing edge of the turbine blade.
24 . The turbine blade according claim 14 , wherein the turbine blade is a final-stage blade for a steam turbine.
25 . A method for making a turbine blade according to claim 14 using an impregnation mold, the method comprising:
laying fiber intermediates, together with the anti-erosion component, in the impregnation mold,
impregnating the fiber intermediates with a matrix material,
curing the matrix material,
removing the turbine blade from the impregnation mold.
26 . The method according to claim 25 , wherein the anti-erosion component is laminated into the turbine blade during impregnation.
27 . The method according to claim 26 , wherein the anti-erosion component, after it has been laminated in, is secured to the turbine blade by an additional securing device.
28 . The method according to claim 25 , wherein the anti-erosion component is provided, before impregnation, with a release agent and, after impregnation, is secured to the turbine blade by gluing and/or by an additional securing device.
29 . The method according to claim 25 , wherein the matrix material comprises resin.
30 . A method for making a turbine blade according to claim 14 using an impregnation mold, wherein the impregnation mold is constructed such that, after impregnation, a recess which is constructed to complement the anti-erosion component is present at the points on the turbine blade at which an anti-erosion component is to be attached, the method comprising:
laying fiber intermediates in the impregnation mold,
impregnating the fiber intermediates with a matrix material,
curing the matrix material,
removing the turbine blade from the impregnation mold, and
securing the anti-erosion component in the recesses in the turbine blade.
31 . The method according to claim 30 , wherein the matrix material comprises resin.
32 . The method according to claim 30 , wherein the securing is carried out by gluing and/or by using an additional securing means device.Join the waitlist — get patent alerts
Track US2012207608A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.