General Electric Company

Joseph Block

Brendon James Leary

Changjie Sun

Thomas Earl Dyson

Ananda Barua

Prabhjot Singh

Xiuzhang James Zhang

Arvind Rangarajan

Melbourne James Myers

Dean Michael Robinson

Sathyanarayanan Raghavan

Camilo Andres Sampayo

Evan John Dozier

Lyndsay Marie Kibler

Stuart Samuel Collins

An article of manufacture includes an article body portion (); at least one pedestal (A,A,) integrally formed with the article body portion (), and disposed at an outer periphery of (), and structurally coupled to the article body portion (); and at least one internal feature () disposed at least partially within the article body portion () and at least partially within the pedestal (A,A,). At least a portion of the internal feature () is hollow.

Additive supports with integral film cooling

A method, medium, and system to receive a specification defining a model of a part to be produced by an additive manufacturing (AM) process; execute an AM simulation on the model of the part to determine a prediction of thermal distortions to the part; execute a topology optimization (TO) to create TO supports that counteract the predicted thermal distortions; generate at least one rule-based support based on a geometry of the part to interface with the part at one or more regions other than the TO supports; combining the TO supports and the at least one rule-based support to generate a set of hybrid supports; save a record of the set of hybrid supports; and transmit the record of the set of hybrid supports to an AM controller to control an AM system to generate a support structure for an AM production of the part.

Hybrid support structures for additively printed parts

The present disclosure is directed to a rotor blade for a gas turbine system. The rotor blade includes a platform having a radially inner surface and a radially outer surface. A shank portion extends radially inwardly from the radially inner surface of the platform. The shank portion and the platform collectively define a shank pocket. An airfoil extends radially outwardly from the radially outer surface of the platform. The shank portion, the platform, and the airfoil collectively define a cooling passage extending from a cooling passage inlet defined by the shank portion or the platform and directly coupled to the shank pocket through the platform to a cooling passage outlet defined by the airfoil.

Cooling passage for gas turbine system rotor blade

Growing community of inventors

Greenville, SC, United States of America

Joseph Block