Airfoil shape for a compressor blade
View Patent ↗An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE A. X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances can be joined smoothly with one another to form a complete airfoil shape.
1. An article of manufacture, the article having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE A, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches, the profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.
2. An article of manufacture according to claim 1 , wherein the airfoil shape comprises an airfoil.
3. An article of manufacture according to claim 2 , wherein said airfoil shape lies in an envelope within ±0.160 inches in a direction normal to any article surface location.
4. An article of manufacture according to claim 1 , wherein the airfoil shape comprises a blade.
5. A compressor comprising a compressor casing having a plurality of blades, each of said blades including an airfoil having an airfoil shape, said airfoil having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE A, wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define the airfoil profile sections at each distance Z in inches, the profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.
6. A compressor comprising a compressor casing having a plurality of blades, each of said blades including an airfoil having an uncoated nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE A, wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches, the profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape, the X and Y distances being scalable as a function of the same constant or number to provide at least one of a scaled up blade airfoil and scaled down blade airfoil.
7. A compressor according to claim 6 wherein the compressor casing comprises a R0 stage of the compressor.
8. A compressor according to claim 6 wherein said airfoil shape lies in an envelope within ±0.160 inches in a direction normal to any airfoil surface location.