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A ceramic matrix composite (CMC) airfoil assembled from a pressure side wall (42) and a suction side wall (52) joined by interlocking joints (18, 19) at the leading and trailing edges (22, 24) of the airfoil to produce a tapered thin trailing edge. The trailing edge (24) is thinner than a combined t

A ceramic matrix composite (CMC) airfoil assembled from a pressure side wall (42) and a suction side wall (52) joined by interlocking joints (18, 19) at the leading and trailing edges (22, 24) of the airfoil to produce a tapered thin trailing edge. The trailing edge (24) is thinner than a combined thicknesses of the airfoil walls (42, 52). One or both of the interlocking joints (18, 19) may be formed to allow only a single direction of assembly, as exemplified by a dovetail joint. Each joint (18, 19) includes keys (44F, 54F, 56F, 46F) on one side and respective keyways (44K, 54K, 56K, 46K) on the other side. Each keyway may have a ramp (45) that eliminates indents in the airfoil outer surface that would otherwise result from the joint.

대표청구항 ▼

1. A ceramic matrix composite airfoil comprising: a first side wall comprising a thickness and a first trailing edge with first trailing edge keys;a second side wall comprising a thickness and a second trailing edge with second trailing edge keyways;wherein the first and second side walls, when join

1. A ceramic matrix composite airfoil comprising: a first side wall comprising a thickness and a first trailing edge with first trailing edge keys;a second side wall comprising a thickness and a second trailing edge with second trailing edge keyways;wherein the first and second side walls, when joined, form a hollow airfoil with an airfoil leading edge and an airfoil trailing edge;wherein the first trailing edge keys interlock into respective second trailing edge keyways to form the airfoil trailing edge; andwherein the airfoil trailing edge tapers to a thickness that is less than a sum of thicknesses of the first and second side walls. 2. The ceramic matrix composite airfoil of claim 1, wherein: the second side wall comprises second trailing edge keys;the second trailing edge keyways comprise respective gaps between the second trailing edge keys;the first side wall comprises first trailing edge keyways comprising respective gaps between the first trailing edge keys; andthe second trailing edge keys interlock in respective first trailing edge keyways. 3. The ceramic matrix composite airfoil of claim 1, wherein the first side wall further comprises first leading edge keys and first leading edge keyways, the second side wall further comprises second leading edge keys and second leading edge keyways, and the leading edge keys of each side wall interlock in respective keyways of the other side wall to form the airfoil leading edge. 4. The ceramic matrix composite airfoil of claim 1, wherein the airfoil trailing edge tapers to the thickness of the first or the second side wall. 5. The ceramic matrix composite airfoil of claim 1, wherein the airfoil trailing edge has a generally cylindrical distal surface with an average radius that is approximately half the thickness of the first or the second side wall. 6. The ceramic matrix composite airfoil of claim 1, further comprising a ramp in each second trailing edge keyway, each ramp comprising a proximal end having the thickness of the second side wall and tapering to a distal sharp edge; and wherein the first and second side walls are joined in opposition to each other, and each of the keys follows a ramp from the proximal end to the distal sharp edge thereof. 7. The ceramic matrix composite airfoil of claim 2, wherein the first and second trailing edge keys have side surfaces angled to allow only a single direction of assembly of the first and second trailing edges in interlocking relationship. 8. The ceramic matrix composite airfoil of claim 7, wherein the first and second trailing edge keys have side surfaces that are angled to form a dovetail interlock. 9. The ceramic matrix composite airfoil of claim 1, wherein the second trailing edge keyways are holes through the second trailing edge. 10. The ceramic matrix composite airfoil of claim 9, wherein: the first side wall comprises a first leading edge with first leading edge keys;the second side wall comprises a second leading edge with holes through an inward extending flap; andwherein the first and second side walls assemble to form the hollow airfoil by inserting the first leading edge keys into the second leading edge holes and inserting the first trailing edge keys into the second trailing edge holes to form interlocked leading and trailing edge joints of the airfoil. 11. The ceramic matrix composite airfoil of claim 1 wherein the respective first trailing edge keys and second trailing edge keyways are shaped to allow assembly from only a single direction that is approximately tangent to a mean camber line of the airfoil at the leading edge of the airfoil. 12. A ceramic matrix composite airfoil comprising: a pressure side wall comprising a thickness, a trailing edge, and trailing edge keys;a suction side wall comprising a thickness, a trailing edge, and trailing edge keys;wherein the pressure and suction side walls form a hollow airfoil with a leading edge and a trailing edge; andwherein respective trailing edge keys of the two walls interlock to form the trailing edge of the airfoil, which tapers to a thickness less than a combined thicknesses of the two walls, and the airfoil has an aerodynamically smooth outer surface. 13. The ceramic matrix composite airfoil of claim 12, wherein the pressure side wall further comprises leading edge keys, the suction side wall further comprises leading edge keys, and respective leading edge keys of the two walls interlock to form the leading edge of the airfoil. 14. The ceramic matrix composite airfoil of claim 12, wherein the pressure side wall and/or the suction side wall further comprises a ramp between each pair of the trailing edge keys, each ramp comprising a proximal end with the thickness of the respective side wall and tapering to a distal sharp edge; and wherein the pressure and suction side walls are joined in opposition to each other, and each of the trailing edge keys follows one of the ramps of the opposed side wall from the proximal end to the distal sharp edge of the ramp. 15. The ceramic matrix composite airfoil of claim 12, wherein the trailing edge keys have side surfaces angled to allow only a single direction of interlocking assembly of the trailing edge of the airfoil. 16. The ceramic matrix composite airfoil of claim 15, wherein the trailing edge keys have side surfaces that are angled to form a dovetail interlock. 17. The ceramic matrix composite airfoil of claim 12, wherein the respective trailing edge keys of the two walls are shaped to interlock from only a single direction that is approximately tangent to a mean camber line of the airfoil. 18. A ceramic matrix composite airfoil comprising: a pressure side wall part with leading and trailing edges;a suction side wall part with leading and trailing edges;the leading edges of the side wall parts joined by a leading edge interlocking joint;the trailing edges of the side wall parts joined by a trailing edge interlocking joint;each interlocking joint comprising a plurality of keys on one of the side wall parts received in mating plurality of respective keyways in the other of the side wall parts;wherein the a trailing edge of the airfoil is formed by the trailing edge interlocking joint to produce an airfoil trailing edge thickness that is less than a combined wall thickness of the pressure side wall part and the suction side wall part. 19. The ceramic matrix composite airfoil of claim 18 wherein the leading and trailing edge interlocking joints are shaped to only allow assembly from a single direction that is common to both interlocking joints. 20. The ceramic matrix composite airfoil of claim 18 wherein the assembly direction is approximately tangent to a mean camber line of the airfoil at the leading edge of the airfoil.