General Electric Company

Umesh Garg

Moorthi Subramaniyan

Michael James Dutka

Matthew John McKeever

Marc Edward Blohm

Joshy John

Ya-Tien Chiu

Paul Griffin Delvernois

Lakshmanan Valliappan

Govindarajan Rengarajan

Gang Liu

Edward Charles Schurr

Vignesh Radhakrishnan

Ryan Wesley Murphy

Roger Claude Beharrysingh

Srikanth Kathika

Vijaykumar Manohar Jain

SenthilKumar Narendran

Julianne Edna Baer

A turbine includes a compressor to intake a fluid and to compress the fluid, a combustion chamber to heat the fluid from the compressor, a turbine section to rotate a shaft with the heated fluid from the combustion chamber, and a bypass circuit to generate a bypass flow by removing a portion of the fluid from the compressor, to heat the bypass flow, and to insert the bypass flow to the turbine section.

Turbine to operate at part-load

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 TABLES 1-11, 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.

Airfoil shape for a compressor

A turbomachine component includes a compressor stator vane having an airfoil core shape. The airfoil core shape includes a nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in TABLE 1, 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 are joined smoothly with one another to form a complete airfoil core shape.

Airfoil core shape for a turbomachine component

An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE 1. 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 are joined smoothly with one another to form a complete airfoil shape.

Airfoil shape for a compressor blade

Growing community of inventors

Karnataka, India

Umesh Garg