US2009081032A1PendingUtilityA1
Composite airfoil
Est. expirySep 20, 2027(~1.1 yrs left)· nominal 20-yr term from priority
Y02T50/60F05D 2300/43F01D 5/147F01D 5/282
40
PatentIndex Score
0
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Claims
Abstract
A turbine component includes mounting structure for attaching the turbine component. A core is attached to the mounting structure. The core is made from a structural material. A plastic airfoil portion envelopes at least a portion of the core.
Claims
exact text as granted — not AI-modified1 . A turbine component comprising:
mounting structure for attaching the turbine component; a core attached to the mounting structure, the core made from a structural material; and a plastic airfoil portion enveloping at least a portion of the core.
2 . The turbine component of claim 1 wherein the core has a leading edge and the airfoil portion envelopes at least the leading edge portion of the core.
3 . The turbine component of claim 1 wherein the airfoil portion envelopes the entire core.
4 . The turbine component of claim 1 wherein the core has at least one void therein.
5 . The turbine component of claim 4 wherein the airfoil portion is made from an injection molded plastic material that extends at least partially into the void in the core.
6 . The turbine component of claim 4 wherein the core has a plurality of voids extending through the core.
7 . The turbine component of claim 6 wherein the airfoil portion is made from an injection molded plastic material that extends at least partially into the voids in the core.
8 . The turbine component of claim 1 wherein the core is made from a material selected from the group of metal and ceramic.
9 . The turbine component of claim 1 wherein the core and mounting structure are integrally formed as one piece.
10 . The turbine component of claim 1 wherein the core is made from a forged, die cast or investment cast metal material formed into a desired shape.
11 . A turbine component comprising:
mounting structure for attaching the turbine component; a core attached to the mounting structure, the core made from a structural material and having at least one void formed in the core; and an airfoil portion enveloping at least a portion of the core, the airfoil portion made from a plastic material that extends at least partially into the void in the core.
12 . The turbine component of claim 11 wherein the core has a leading edge and the airfoil portion envelopes at least the leading edge portion of the core.
13 . The turbine component of claim 11 wherein the airfoil portion envelopes the entire core.
14 . The turbine component of claim 11 wherein the void extends through the core.
15 . The turbine component of claim 11 wherein the core is made from a material selected from the group of metal and ceramic.
16 . The turbine component of claim 11 wherein the core and mounting structure are integrally formed as one piece.
17 . The turbine component of claim 11 wherein the airfoil portion is injection molded onto the core.
18 . A component for a gas turbine having a plurality of compressor and turbine stages, the component comprising:
mounting structure for attaching the component to gas turbine structure; a core integrally formed as one piece with the mounting structure, the core made from a material selected from the group of metal and ceramic and having a plurality of voids extending through the core; and an airfoil enveloping the entire core, the airfoil made from an injection molded plastic material that extends at least partially into the voids in the core.
19 . The component of claim 18 wherein the airfoil extends into and completely fills the voids in entire core.
20 . The component of claim 18 wherein the component is used in one of the first gas turbine compressor stages.Join the waitlist — get patent alerts
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