Stationary turbine component with laminated skin
First Claim
1. A stationary turbine engine component comprising:
- an internal spar made of a plurality of internal spar laminates;
an external skin made of a plurality of external skin laminates, each external skin laminate having an outer wall and a retention portion, wherein the retention portion of each external skin laminate is disposed between and in interlocking engagement with two neighboring internal spar laminates, whereby the external skin laminates are held in place by their interlocking engagement with the internal spar laminates;
wherein the internal sear laminates each include retention portions extending chordwise;
wherein the external sear laminates each include retention portions extending chordwise and configured to be placed in interlocking arrangement with the retention portions of the internal spar laminates; and
wherein interfaces between adjacent internal spar laminates extend chordwise.
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Accused Products
Abstract
A stationary turbine engine component, such as a turbine vane, includes a internal spar and an external skin. The internal spar is made of a plurality of spar laminates, and the external skin is made of a plurality of skin laminates. The plurality of skin laminates interlockingly engage the plurality of spar laminates such that the external skin is located and held in place. This arrangement allows alternative high temperature materials to be used on turbine engine components in areas where their properties are needed without having to make the entire component out of such material. Thus, the manufacturing difficulties associated with making an entire component of such a material and the attendant high costs are avoided. The skin laminates can be made of advanced generation single crystal superalloys, intermetallics and refractory alloys.
25 Citations
20 Claims
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1. A stationary turbine engine component comprising:
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an internal spar made of a plurality of internal spar laminates; an external skin made of a plurality of external skin laminates, each external skin laminate having an outer wall and a retention portion, wherein the retention portion of each external skin laminate is disposed between and in interlocking engagement with two neighboring internal spar laminates, whereby the external skin laminates are held in place by their interlocking engagement with the internal spar laminates; wherein the internal sear laminates each include retention portions extending chordwise; wherein the external sear laminates each include retention portions extending chordwise and configured to be placed in interlocking arrangement with the retention portions of the internal spar laminates; and wherein interfaces between adjacent internal spar laminates extend chordwise. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
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13. A stationary turbine engine component comprising:
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a first and a second internal spar laminate, each internal spar laminate including a body portion having a substantially planar upper surface and a substantially planar lower surface, the first and a second internal spar laminates further including a retention portion extending at least partially about the body portion, each retention portion including a bridge portion extending outward from the body portion, the bridge portion transitioning into a transverse engaging portion that defines an outer peripheral surface of each internal spar laminate; and an external skin laminate having an outer wall and a retention portion, the retention portion including a bridge portion extending inward from the outer wall, the bridge portion transitioning to a transverse engaging portion, the laminates being arranged so that the retention portion of the external skin laminate is disposed between and in interlocking engagement with the retention portion of first and second internal spar laminates, and so that the upper planar surface of the first internal spar laminate is substantially adjacent to the lower planar surface of the second internal spar laminate, and so that the outer wall of the external skin laminate is spaced from the outer peripheral surface of the first and second internal spar laminates; wherein the retention portions of the internal spar laminates extend chordwise; wherein the retention portions of the external spar laminates extend chordwise and are configured to be laced into interlocking arrangement with the retention portions of the internal spar laminates; and wherein interfaces between adjacent internal spar laminates extend chordwise and interfaces between adjacent external skin laminates extend chordwise. - View Dependent Claims (14, 15, 16, 17)
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18. A turbine vane assembly comprising:
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an inner shroud; an outer shroud; and an airfoil extending between and operatively engaging the inner shroud and the outer shroud;
the airfoil including;an internal spar made of a plurality of generally airfoil shaped internal spar laminates, each internal spar laminate including a body portion and a retention portion extending at least partially about the body portion; an external skin made of a plurality of generally airfoil shaped external skin laminates, each external skin laminate having an outer wall and a retention portion, wherein the retention portion of each external skin laminate is disposed between and in interlocking engagement with the retention portion of two neighboring internal spar laminates, wherein each external skin laminate is held in place by interlocking engagement with the internal spar laminates, wherein at least one end of the outer wall of each external skin laminate abuts an end of the outer wall of a neighboring external skin laminate, wherein each external skin laminate is made of one of advanced generation single crystal superalloys, intermetallics, nickel-based intermetallics, refractory alloys and oxide dispersion strengthened alloys; wherein the retention portions of the internal spar laminates extend chordwise; wherein the retention portions of the external spar laminates extend chordwise and are configured to be placed into interlocking arrangement with the retention portions of the internal spar laminates; and wherein interfaces between adjacent internal spar laminates extend chordwise and interfaces between adjacent external skin laminates extend chordwise. - View Dependent Claims (19, 20)
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Specification