Compressor rotor blade airfoils

US12018585B2 · kind B2 · utility

Assignee

• GE Infrastructure Technology LLC · US

Inventors

• Marc Edward Blohm · Greenville, US
• Vasantharuban S · Kanchinakote, IN
• Michael James Dutka · Simpsonville, US
• Nandakumar A R · Kanchinakote, IN
• Sharan Shanti · Kanchinakote, IN
• Prakash Bavanjibhai Dalsania · Kanchinakote, IN
• Corey Lynn Hubbert · Manchester, US
• Siddaraja Mallikarjuna Devangada · Kanchinakote, IN
• Joshy John · Bengaluru, IN
• Nancy Chaudhary · Visnagar, IN
• Abel Christena Francis · Kanchinakote, IN
• Brandon Lamar Bush · Edmond, US
• Jeremy Peter Latimer · Greenville, US

Key dates

• Filing date: Mar 29, 2023
• Grant date: Jun 25, 2024
• Expiry date: Mar 29, 2043

Classification

• Technology area (CPC G): Physics
• CPC primary: G06T2207/30252
• WIPO field: Computer technology
• WIPO sector: Electrical engineering

Abstract

A rotor blade includes an airfoil having an airfoil shape. The airfoil shape has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, Table VIII, or Table IX. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape.