Compressor blade for a gas turbine engine
First Claim
1. An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape;
- wherein an origin point for the Cartesian coordinate values is at one of a mid-point of a suction or pressure side at a base of the airfoil shape or at a leading or trailing edge at the base of the airfoil shape; and
wherein the airfoil shape lies in an envelope within one of;
+/−
5% of a chord length in a direction normal to an airfoil surface location; and
+/−
0.25 inches in a direction normal to the airfoil surface location.
2 Assignments
0 Petitions
Accused Products
Abstract
An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.
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Citations
16 Claims
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1. An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape;
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wherein an origin point for the Cartesian coordinate values is at one of a mid-point of a suction or pressure side at a base of the airfoil shape or at a leading or trailing edge at the base of the airfoil shape; and wherein the airfoil shape lies in an envelope within one of;
+/−
5% of a chord length in a direction normal to an airfoil surface location; and
+/−
0.25 inches in a direction normal to the airfoil surface location. - View Dependent Claims (2, 3, 4, 5)
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6. An article of manufacture having a suction-side nominal airfoil profile substantially in accordance with suction-side Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete suction-side airfoil shape, the X, Y and Z coordinate values being scalable as a function of the number to provide one of a non-scaled, scaled-up and scaled-down airfoil profile;
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wherein an origin point for the Cartesian coordinate values is at one of a mid-point of a suction or pressure side at a base of the airfoil shape or at a leading or trailing edge at the base of the airfoil shape; and wherein the airfoil shape lies in an envelope within one of;
+/−
5% of a chord length in a direction normal to an airfoil surface location; and
+/−
0.25 inches in a direction normal to the airfoil surface location. - View Dependent Claims (7, 8, 9, 10, 11)
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12. A compressor comprising a plurality of stator vanes, each of the stator vanes including an airfoil having a suction-side airfoil shape, the airfoil having a nominal profile substantially in accordance with suction-side Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete suction-side airfoil shape;
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wherein an origin point for the Cartesian coordinate values is at one of a mid-point of a suction or pressure side at a base of the airfoil shape or at a leading or trailing edge at the base of the airfoil shape; and wherein the suction-side airfoil shape lies in an envelope within one of;
+/−
5% of a chord length in a direction normal to a suction-side airfoil surface location; and
+/−
0.25 inches in a direction normal to a suction-side airfoil surface location. - View Dependent Claims (13, 14, 15, 16)
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Specification