Turbine airfoil having outboard and inboard sections
A turbine airfoil usable in a turbine engine and formed from at least an outboard section and an inboard section such that an inner end of the outboard section is attached to an outer end of the inboard section. The outboard section may be configured to provide a tip having adequate thickness and may extend radially inward from the tip with a generally constant cross-sectional area. The inboard section may be configured with a tapered cross-sectional area to support the outboard section.
1. A turbine airfoil, comprising:
a generally elongated airfoil formed from an outer wall, and having a leading edge, a trailing edge, a pressure side, a suction side, a root at a first end of the airfoil and a tip at a second end opposite to the first end;
wherein the airfoil is formed from an outboard section and an inboard section such that an inner end of the outboard section is attached to an outer end of the inboard section;
wherein the outboard section has a generally non-tapered, linear cross-sectional area extending from the pressure side to the suction side and includes the tip of the generally elongated hollow airfoil at an outer end of the outboard section, and the inboard section has a tapered cross-sectional area extending from the pressure side to the suction side and is coupled to the root; and
wherein the outboard section may have a length up to about 30 percent of a length of the outboard and inboard sections combined and the outboard section has a sufficient length and is configured such that the configuration of the outboard and inboard sections may reduce the centrifugal loads by more than 15 percent.
2. The turbine airfoil of claim 1 , wherein the outboard and inboard sections are formed at least in part by different materials having similar chemistry and differing in specific composition.
3. The turbine airfoil of claim 1 , wherein the outboard section is formed at least partially from a material having a lesser density than a material used to form at least part of the inboard section.
4. The turbine airfoil of claim 1 , wherein the outboard and inboard sections are welded together.
5. The turbine airfoil of claim 1 , wherein the inner end of the outboard section and the outer end of the inboard section have matching cross-sectional configurations.
6. A turbine airfoil, comprising:
a generally elongated hollow airfoil formed from an outer wall, and having a leading edge, a trailing edge, a pressure side, a suction side, a root at a first end of the airfoil and a tip at a second end opposite to the first end, and a cooling system positioned within interior aspects of the generally elongated hollow airfoil;
wherein the airfoil is formed from an outboard section and an inboard section such that an inner end of the outboard section is attached to an outer end of the inboard section;
wherein the outboard section has a generally non-tapered, linear cross-sectional area extending from the pressure side to the suction side and includes the tip of the generally elongated hollow airfoil at an outer end of the outboard section, and the inboard section has a tapered cross-sectional area extending from the pressure side to the suction side and is coupled to the root; and
wherein the outboard section may have a length up to about 30 percent of a length of the outboard and inboard sections combined and the outboard section has a sufficient length and is configured such that the configuration of the outboard and inboard sections may reduce the centrifugal loads by more than 15 percent.
7. The turbine airfoil of claim 6 , wherein the outboard and inboard sections are formed at least in part by different materials having similar chemistry and differing in specific composition.
8. The turbine airfoil of claim 6 , wherein the outboard section is formed at least partially from a material having a lesser density than a material used to form at least part of the inboard section.
9. The turbine airfoil of claim 6 , wherein the outboard and inboard sections are welded together.
10. The turbine airfoil of claim 6 , wherein the inner end of the outboard section and the outer end of the inboard section have matching cross-sectional configurations.
11. A turbine airfoil, comprising:
a generally elongated hollow airfoil formed from an outer wall, and having a leading edge, a trailing edge, a pressure side, a suction side, a root at a first end of the airfoil and a tip at a second end opposite to the first end, and a cooling system positioned within interior aspects of the generally elongated hollow airfoil;
wherein the airfoil is formed from an outboard section and an inboard section such that an inner end of the outboard section is attached to an outer end of the inboard section;
wherein the outboard section has a generally non-tapered, linear cross-sectional area extending from the pressure side to the suction side and includes the tip of the generally elongated hollow airfoil at an outer end of the outboard section, and the inboard section has a tapered cross-sectional area extending from the pressure side to the suction side and is coupled to the root;
wherein the outboard and inboard sections are formed at least in part by different materials having similar chemistry and differing in specific composition;
wherein the inner end of the outboard section and the outer end of the inboard section have matching cross-sectional configurations; and
wherein the outboard section may have a length up to about 30 percent of a length of the outboard and inboard sections combined and the outboard section has a sufficient length and is configured such that the configuration of the outboard and inboard sections may reduce the centrifugal loads by more than 15 percent.
12. The turbine airfoil of claim 11 , wherein the outboard section is formed at least partially from a material having a lesser density than a material used to form at least part of the inboard section.
13. The turbine airfoil of claim 11 , wherein the outboard and inboard sections are welded together.