Unison Industries, Inc.

General Electric Company

Ge Precision Healthcare LLC

Yanzhe Yang

Gordon Tajiri

Dattu G V Jonnalagadda

Emily Marie Phelps

Joseph Richard Schmitt

Michael Thomas Kenworthy

Jean-Baptiste Mathieu

Dattu Gv Jonnalagadda

Thomas Kwok-Fah Foo

Daniel Dyer

Manoj Ramprasad Shah

Ruxi Wang

Ramanujam Ramabhadran

Prabhjot Singh

Saban Kurucay

Balaraju Suresh

Sebastian Merin

William Thomas Carter

Bin Wei

Farshad Ghasripoor

Steven Robert Hayashi

Yong Yang

Andrew Lee Trimmer

Kevin Warner Flanagan

Michael Ralph Storage

James William Sears

Ramana Reddy Kollam

Pinghai Yang

Bruce Courtney Campbell Amm

Jian Lin

Merin Sebastian

Jason Levi Burdette

Ming Jia

Srinivasan Swaminathan

Hongqing Sun

Donald Templeton

Yibo Gao

Meisam Salahshoor Pirsoltan

Silke Maria Lechner-Greite

Huiyu Xu

Armando Bringas

Kenneth Paul Zarnock

Elizabeth Diane Turner

Tajiri Gordon

Gordan Tajiri

Vijay Shilpiekandula

Dattu Guruvenkata Jonnalagadda

Elizabeth Turner

A forming manifold and method for electroforming a component, including providing an electroforming cathode disposed within a first bath tank having a solution with a first metal ion concentration, overlaying at least a portion of the electroforming cathode with a forming manifold having a housing and applying a voltage to the electroforming cathode while disposed within the first bath tank.

Device and method for forming electroformed component

An apparatus and method for a mandrel used during an electroforming process. The mandrel is formed of a structural wax and includes a metallic layer utilized to formulate a metal component. During the electroforming process, the mandrel is actively cooled utilizing a closed loop. The closed loop includes the mandrel and a heat exchanger through which a coolant flows.

Mandrel for electroforming

A strengthened component includes a sacrificial material mold of the component having an outer surface, an insert having an inner surface and an outer surface opposite and spaced from the inner surface such that the strengthening insert inner surface abuts the mold outer surface, and a metallic layer deposited over the exposed mold outer surface and the exposed strengthening insert outer surface, where the sacrificial material mold is removed from the strengthened component.

Methods of forming a strengthened component

A system is configured for machining a workpiece (), the workpiece includes an interior surface () that defines an internal passage (). The system includes an electrode () located within the internal passage and electrically isolated from the workpiece, an electrolyte supply, a power supply, and a remover. The electrolyte supply is configured for circulating an electrolyte in a gap between the electrode and the workpiece. The power supply is configured for applying a voltage between the electrode and the workpiece to facilitate smoothing the interior surface. The remover is configured for completely removing the electrode from within the internal passage after smoothing the interior surface.

System and method for machining workpiece and article machined therefrom

A system includes a magnetic material supply for regulating a magnetic material flow rate of a magnetic material and a binder material supply for regulating a binder material flow rate of a binder material. A nozzle is configured for depositing a deposition mixture of the magnetic material and the binder material on a surface and a preheater is configured to preheat the deposition mixture before depositing on the surface. A controller is in operative communication with the magnetic material supply, the binder material supply, and the preheater. The controller is configured to receive an inductor core design file that represents a geometry and a magnetic permeability distribution of an inductor core, move the nozzle to one or more deposition locations, and adjust the magnetic material flow rate to the binder material flow rate to achieve a deposition mixture having a desired magnetic permeability at the deposition locations.

System for manufacturing an inductor core

A fan casing assembly, connection assembly and method for moving a fan casing cooler. The fan casing assembly for the turbine engine can include an annular fan casing with a peripheral wall having a flow path defined through the casing. A fan casing cooler can mount along the peripheral wall in order to confront a cooling fluid flow within the flow path in order to cool a fluid through the fan casing cooler.

Fan casing assembly and method

A component can be formed having an integral monolithic body. The integral monolithic body can be formed utilizing electroforming processes such as electrodeposition of metal alloys. The electroformed monolithic body can be formed utilizing multiple anodes powered by multiple power sources. The monolithic body can have differing local material properties determined during formation of the component.

Component with differing material properties

A manufacturing process for making aircraft engine parts utilizes reusable reconfigurable smart memory polymer mandrel tooling, low temperature metal deposition, and composite part lay-up with resin coated conformable braided carbon fiber sleeves, to fabricate both metal internal engine parts and non-metal external parts for turbine engines.

Method of manufacturing aircraft engine parts utilizing reusable and reconfigurable smart memory polymer mandrel

A method of forming a strengthened component includes forming a sacrificial material into a mold of the component having an outer surface, disposing an insert having an inner surface and an outer surface opposite and spaced from the inner surface such that the strengthening insert inner surface abuts the mold outer surface, forming the component by way of electrodisposition of a metallic layer over the exposed mold outer surface and the exposed strengthening insert outer surface, and removing the sacrificial material from the component.

An apparatus and method of forming a heat exchanger including a thermally compliant material and geometry with a core having a first set of flow passages and a second set of flow passages passing through the core. A first manifold of high temperature and strength material defines a fluid inlet for the first set of flow passages and a second manifold of high temperature and strength material defines a fluid inlet for the second set of flow passages. At least one of the first and second manifolds can include an in-situ compliant portion to provide for compliance during thermal expansion of the heat exchanger.

Heat exchanger assembly

A duct for a turbine engine, such as a gas turbine engine, can be utilized to carry a fluid from one portion of the engine to another. The duct can include a metallic tubular element having one of a varying wall thickness, a varying cross section, or a tight bend. Such a duct can be formed utilizing additive manufacturing or metal deposition on an additively manufactured mandrel.

Turbine engine duct

A tunable compliant mount structure for an engine such as a turbine engine can include a fluid conduit coupled to a fan casing by a connector. At a junction between the connector and the fluid conduit, a compliant mount structure can provide compliance and can be tuned to operate under variable stresses at the junction. The compliant mount structure can include a set of nested convolutions to provide compliance. The geometry of the convolutions can be used to tune the compliance, stiffness, or directionality. The tunable compliant attachment structure provides for additive in-situ manufacturing at the fluid conduit.

Tunable compliant attachment structure

The embodiments disclosed herein relate generally to magnetic resonance imaging systems and, more specifically, to the manufacturing of a gradient coil assembly for magnetic resonance imaging (MRI) systems. For example, in one embodiment, a method of manufacturing a gradient coil assembly for a magnetic resonance imaging system includes depositing a first layer comprising a base material onto a surface to form a substrate and depositing a second layer onto the first layer. The second layer may enable bonding between a conductor material and the substrate. The method also includes depositing a third layer onto the second layer using a consolidation process. The consolidation process uses the conductor material to form at least a portion of a gradient coil.

System and method for manufacturing magnetic resonance imaging gradient coil assemblies

The present disclosure discloses a method of manufacturing a structure with a wall, comprising manufacturing a structure with a wall by using additive manufacturing technology, and dissolving a surface of the wall for reducing thickness of the wall.

Method of manufacturing a fin structure for heat exchanger

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Mason, OH, United States of America

Yanzhe Yang