Turbine engine airfoil and platform assembly
A turbine airfoil ( 22 A) is formed by a first process using a first material. A platform ( 30 A) is formed by a second process using a second material that may be different from the first material. The platform ( 30 A) is assembled around a shank ( 23 A) of the airfoil. One or more pins ( 36 A) extend from the platform into holes ( 28 ) in the shank ( 23 A). The platform may be formed in two portions ( 32 A, 34 A) and placed around the shank, enclosing it. The two platform portions may be bonded to each other. Alternately, the platform ( 30 B) may be cast around the shank ( 23 B) using a metal alloy with better castability than that of the blade and shank, which may be specialized for thermal tolerance. The pins ( 36 A- 36 D) or holes for them do not extend to an outer surface ( 31 ) of the platform, avoiding stress concentrations.
1. A turbine airfoil and platform assembly comprising:
an airfoil comprising a shank, the airfoil and shank formed of a first material;
a platform formed of a second material, the platform enclosing or bracketing the shank; and
one or more pins through holes in the shank;
wherein said one or more pins engage the platform without holes therefore extending to an outer surface of the platform.
2. The turbine airfoil and platform assembly of claim 1 , wherein the second material has better castability than the first material.
3. The turbine airfoil and platform assembly of claim 1 , wherein the platform comprises a pressure side portion and a suction side portion that together enclose the shank.
4. The turbine airfoil and platform assembly of claim 3 wherein two platform portions are bonded to each other.
5. The turbine airfoil and platform assembly of claim 3 wherein two platform portions integrally form the platform, said one or more pins bridge the two platform portions continuously, and the second material has better castability than the first material.
6. The turbine airfoil and platform assembly of claim 1 , wherein the platform is cast around the shank, and wherein the first material has higher heat tolerance than the second material.
7. The turbine airfoil and platform assembly of claim 1 , wherein the platform comprises a pair of laterally extending opposed teeth that fit into corresponding depressions in a socket in a turbine rotor disk, and wherein the shank comprises a pair of laterally extending opposed teeth that fit into corresponding depressions in an inner surface of the platform, and wherein the teeth of the shank are aligned with the teeth of the platform.
8. The turbine airfoil and platform assembly of claim 1 , wherein the pins are formed and inserted through the holes in the shank, then the platform is bi-cast around the shank and the pins.
9. The turbine airfoil and platform assembly of claim 1 , wherein the airfoil comprises a cooling chamber, and the platform comprises a coolant passage between the cooling chamber and a side of the platform.
10. A turbine airfoil and platform assembly comprising:
a turbine airfoil extending from a shank;
the shank comprising a pin hole;
a platform comprising opposed pressure and suction side portions surrounding the shank;
a pair of opposed teeth on the opposed pressure and suction sides of the platform; and
a pin filling the pin hole in the shank;
wherein the pin engages the platform without a hole therefore extending to an outer surface of the platform.
11. The turbine airfoil and platform assembly of claim 10 , further comprising a turbine disk comprising a slot that matches and slidably receives the platform and teeth in an axial direction that interlocks the platform with the disk, preventing radial movement therebetween.
12. The turbine airfoil and platform assembly of claim 10 , further comprising a pair of opposed teeth extending laterally from opposite sides of the shank into respective matching sockets in the platform.
13. The turbine airfoil and platform assembly of claim 10 , wherein the airfoil and shank are formed integrally of a first material, and the platform is formed of a second material with better castability than the first material.
14. The turbine airfoil and platform assembly of claim 13 wherein the platform is formed of two portions bonded to each other around the shank.
15. The turbine airfoil and platform assembly of claim 13 , wherein the platform is cast around the shank.
16. The turbine airfoil and platform assembly of claim 10 , wherein the pins are formed and inserted through the holes in the shank, then the platform is bi-cast around the shank and the pins.
17. A method of assembling a turbine airfoil and platform comprising:
forming a turbine airfoil by a first process using a first material, the airfoil comprising a shank with a pin hole;
forming a platform by a second process using a second material;
enclosing or bracketing the shank with the platform; and
disposing a pin in the pin hole without forming a hole in the platform that extends to an outer surface of the platform.
18. The method of claim 17 wherein the second material is a different material than the first material.
19. The method of claim 17 wherein the platform is formed in the second process by placing a mold around the shank, casting the platform within the mold around the shank, which casting fills the pin hole with the second material, and wherein the first material has higher heat tolerance than the second material.
20. The method of claim 17 , wherein the pin is pre-formed and inserted through the hole in the shank, then the platform is bi-cast around the shank and the pin, completely covering the pin.