General Electric Company

Adegboyega Masud Makinde

Steven Sebastian Burdgick

Christophe Lanaud

Stephen Francis Rutkowski

Wendy Wenling Lin

Dean Michael Robinson

Pinghai Yang

Amitabh Bansal

Tyler Nathaniel Nelson

William Dwight Gerstler

Venkat Subramaniam Venkataramani

Shyh-Chin Huang

Douglas Carl Hofer

Douglas Gerard Konitzer

Michael Francis Xavier Gigliotti

Steven Robert Hayashi

Wendy Wen-Ling Lin

Andrew Lee Trimmer

Brian David Przeslawski

Yuanfeng Luo

Joshua L Miller

Chiranjeev Kalra

Roger John Petterson

Manuel Acosta

Jerod Curtis Kruse

Grama Narasimhaprasad Praveen

Joseph Daniel Franzen, Jr

Joshua Leigh Miller

Jr Joseph Daniel Franzen

A compensation field indicating an amount of distortion compensation to be applied across at least a portion of a component is determined, and a nominal computer-aided design (CAD) model of a component is modified based on the compensation field. The amount of distortion compensation corresponds to a multiplication product of: (i) a deviation between the nominal CAD model and a physical representation of the component having been produced based on the nominal CAD model, and (ii) a nonlinear scale factor map that includes a map associating a plurality of locations of the nominal CAD model to corresponding ones of a plurality of scale factors respectively representing an increase or a decrease in the amount of distortion compensation to be applied based on a simulated effect upon the component in response to an iterative simulation process.

Hybrid measurement and simulation based distortion compensation system for additive manufacturing processes

A counter-flow heat exchanger including a core region and a plenum region. The core region including a first set of heat exchanging passageways and a second set of heat exchanging passageways disposed at least partially therein. A plenum region is disposed adjacent opposed distal ends of the core region. Each of the plenum regions including a fluid inlet plenum, a fluid outlet plenum and a tube plate disposed therebetween. The first set of heat exchanging passageways is truncated and defines a first tube-side fluid flow path in a first direction. The second set of heat exchanging passageways defines a second tube-side fluid flow path in a second opposing direction. Each of the heat exchanging passageways extending from a fluid inlet plenum to a fluid outlet plenum. The tube plates and the core region include one of a cast metal formed thereabout each of the heat exchanging passageways or a braze bond formed between each of the heat exchanging passageways.

Counter-flow heat exchanger

Methods for creating a cast component, along with the resulting cast components, are provided. The method may provide for a controlled grain structure in the resulting cast component. The methods may include heating at least a first portion mold under controlled conditions, such as when the first portion of the mold is buried in a ceramic powder.

Controlled grain microstructures in cast alloys

A method and system, the method including receiving a nominal computer-aided design (CAD) model of a component; producing a physical representation of the component based on the CAD model using an additive manufacturing (AM) process; measuring the produced physical representation of the component to obtain measurement data of the physical representation of the component; determining a deviation between a geometry of the CAD model and the measurement data of the physical representation of the component; calculating a nonlinear scale factor using an iterative simulation process; determining a compensation field based on the determined deviation between the geometry of the CAD model and the measurement data of the physical representation of the component and the calculated nonlinear scale factor; modifying the nominal CAD model by the determined compensation field; and producing a physical representation of the component based on the modified nominal CAD model.

A build assembly and a method of manufacturing the same are provided. The build assembly includes a first component, a second component, and a support structure coupling the two components together to fix their relative position. The support structure may be a 'ghost' structure that is not connected with or does not contact the components, but is positioned such that the components are restrained to prevent distortion. The support structure may also be connected to the components and may define channels for removing additive powder from within or around the components.

Additively manufactured build assemblies having reduced distortion and residual stress

The polishing system includes a power supply. The polishing system also includes a container including an interior portion. The interior portion includes a conductive material thereon. The conductive material is electrically coupled to the power supply. The polishing system also includes an electrolytic solution disposed within the container. The electrolytic solution includes a plurality of abrasive particles. The polishing system further includes a flexible media disposed within the container. The container is configured to contain an object. The power supply configured to electrically couple to the object. Each of the electrolytic solution, the flexible media, and the abrasive particles is configured to partially polish the object substantially simultaneously.

Method and apparatus for polishing metal parts with complex geometries

Shell molds and processes for making the shell molds that exhibit high emissivity in the red and infrared regions. In this manner, thermal resistance within a gap formed between solidifying cast metal and the interior mold surface is decreased. In one embodiment, the facecoat region is formed from a slurry composition comprising an aluminum oxide, a green chromium oxide and a silicon dioxide. In another embodiment, the facecoat region is formed from a slurry composition including zirconium silicate and silica with stucco layer of alumina is included.

High emittance shell molds for directional casting

A method for mechanically attaching a composite or polymeric material to a bucket in a radial airfoil includes creating at least one dovetail shape pocket in the bucket having inclined interfaces with respect to the radial airfoil, and filling the pocket with the composite or polymeric material.

Hybrid bucket dovetail pocket design for mechanical retainment

A method facilitates reducing stress in a turbine bucket including a metallic base metal. The method comprises providing a turbine bucket including at least one pocket formed therein, and filling at least one pocket defined in the bucket with a polymer composite having continuous fibers oriented in a resin matrix, such that the fibers have an orientation determined in accordance with a pre-selected frequency tuning of the bucket.

Methods and apparatus for reducing stress in turbine buckets

A method for making a turbine blade includes providing a bucket in the turbine blade with a plurality of window pockets passing all the way through a wall of the bucket, positioning the window pockets in regions minimizing or at least reducing stress concentrations on the window pockets, and casting a composite comprising a resin matrix and layers of a fabric material in the bucket.

Methods and apparatus for mechanical retainment of non-metallic fillers in pockets

A method of assembling a turbine bucket is provided. The bucket includes a dovetail portion, an airfoil portion, and a root that extends between the airfoil portion and the dovetail portion. The turbine bucket includes a pressure side and a suction side that are connected together at a leading edge and a trailing edge. The method includes forming at least one pocket within the turbine bucket, such that the pocket is formed within the pressure side. The method also includes forming at least one pin within the at least one pocket.

Methods and apparatus for assembling a steam turbine bucket

To address certain deficiencies of carbon fiber material as a filler in a hybrid blade, a glass composite layer is provided as a barrier layer between a carbon fiber resin filler and the metallic main body of the blade. The glass composite layer also advantageously provides a gradient in thermal expansion between the carbon fiber composite and the body of the blade (steel) to reduce interfacial residual stress.

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Niskayuna, NY, United States of America

Adegboyega Masud Makinde