General Electric Company

Lynntech, Inc.

Exxonmobil Upstream Research Company

Ge Infrastructure Technology, LLC

Stanley Frank Simpson

Canan Uslu Hardwicke

Lisa Anne Wichmann

Oliver J Murphy

Stephen Francis Rutkowski

Dacong Weng

Jeffrey Todd Knapp

Benjamin Paul Lacy

Larry Neil Lewis

Aaron Ezekiel Smith

Slawomir Rubinsztajn

Andrew Philip Shapiro

Herbert Chidsey Roberts

Joseph Leonard Moroso

Jeffrey John Butkiewicz

George Martin Gilchrist

Timothy Michael Moricca

Alan J Cisar

Gary Charles Liotta

Xiwang Qi

Andres Jose Garcia-Crespo

Michael Douglas Arnett

Hasan Ul Karim

Carlos E Salinas

Herbert Chidsey Roberts, Iii

Carlos Miguel Miranda

John Charles Intile

Dipankar Pal

Jie Guan

Homayoun Moaddel

Steven Charles Rauch

Patrick Yerkes

Caitlin Shea Lucking

Kyle J Lewis

Pramod Kumar Biyani

James Edward Viggiani

Rong Fan

Daniel J Dorriety

Travis Edgar Garner

Kryzysztof Franaszczuk

Krishnakumar Rangarao

William Michael Genovese

James Daniel Power

A method for redirection of coolant flow is provided. The method includes an identifying step that identifies a hot spot on an exterior surface of a body of a component of a turbine system. A first parameter of the component indicates that a temperature of the exterior surface in the hot spot exceeds a threshold value. Another identifying step identifies a cool spot on the exterior surface. A second parameter of the component indicates that the temperature of the exterior surface in the cool spot is below the threshold value. A reconfiguring step reconfigures a plurality of cooling passages of the component to direct a portion of a coolant from the cool spot to the hot spot.

Thermal profile based redirection of turbine system component coolant by targeted alteration of cooling passage exit opening cross-sectional area

A robotic treatment system includes a robotic arm comprising a tool mount, and a plurality of tools, each of the plurality of tools removably connectable to the tool mount. The system further includes a distribution assembly, which includes a distribution source, a distribution feed cable, a distribution return cable, and a plurality of distribution valves. Each of the plurality of distribution valves regulates a distribution flow through the distribution feed cable to one of the plurality of tools or the distribution return cable from one of the plurality of tools. The system further includes a supply assembly, which includes a supply controller, a plurality of substrate feeders, and a plurality of supply feed cables. The system further includes a main controller, the main controller in operable communication with the robotic arm, the supply controller, and each of the plurality of distribution valves.

Robotic treatment systems and methods for providing automated component treatment

A method of forming a component having an internal passage defined therein is provided. The method includes positioning a jacketed core with respect to a mold. The jacketed core includes a hollow structure formed at least partially by an additive manufacturing process, and an inner core disposed within the hollow structure. The method also includes introducing a component material in a molten state into a cavity of the mold, and cooling the component material in the cavity to form the component. The inner core is positioned to define the internal passage within the component.

Method and assembly for forming components having an internal passage defined therein

A mold assembly for use in forming a component having an internal passage defined therein includes a mold defining a mold cavity therein, and a jacketed core positioned with respect to the mold. The jacketed core includes a hollow structure, and an inner core disposed within the hollow structure and positioned to define the internal passage within the component when a component material in a molten state is introduced into the mold cavity and cooled to form the component. The jacketed core also includes a first coating layer disposed between the hollow structure and the inner core.

Method and assembly for forming components having internal passages using a jacketed core

A method of forming a component having an internal passage defined therein includes positioning a jacketed core with respect to a mold. The jacketed core includes a hollow structure formed from at least a first material and a first catalyst, and an inner core disposed within the hollow structure. The method also includes introducing a component material in a molten state into a cavity of the mold, and cooling the component material in the cavity to form the component. The inner core defines the internal passage within the component.

Method and assembly for forming components having a catalyzed internal passage defined therein

A method of forming a component having an internal passage defined therein includes positioning a jacketed core with respect to a mold. The jacketed core includes a hollow structure formed from at least a first material and a second material, and an inner core disposed within the hollow structure. The method also includes introducing a component material in a molten state into a cavity of the mold, and cooling the component material in the cavity to form the component. The inner core defines the internal passage within the component.

A method of forming a component having an internal passage defined therein includes forming a precursor core having a shape corresponding to a shape of the internal passage, and forming a hollow structure around the precursor core. The method also includes removing the precursor core from within the hollow structure, and disposing an inner core within the hollow structure to form a jacketed core. The method further includes positioning the jacketed core with respect to a mold, and introducing a component material in a molten state into a cavity of the mold, such that the component material in the molten state at least partially absorbs the hollow structure from a portion of the jacketed core within the cavity. Additionally, the method includes cooling the component material in the cavity to form the component. The inner core defines the internal passage within the component.

A mold assembly for use in forming a component having an internal passage defined therein is provided. The component is formed from a component material. The mold assembly includes a mold that defines a mold cavity therein. The mold assembly also includes a lattice structure selectively positioned at least partially within the mold cavity. The lattice structure is formed from a first material that has a selectively altered composition in at least one region of the lattice structure. A channel is defined through the lattice structure, and a core is positioned in the channel such that at least a portion of the core extends within the mold cavity and defines the internal passage when the component is formed in the mold assembly.

Method and assembly for forming components having internal passages using a lattice structure

Matrix composite component repair processes are disclosed. The matrix composite repair process includes applying a repair material to a matrix composite component, securing the repair material to the matrix composite component with an external securing mechanism and curing the repair material to bond the repair material to the matrix composite component during the securing by the external securing mechanism. The matrix composite component is selected from the group consisting of a ceramic matrix composite, a polymer matrix composite, and a metal matrix composite. In another embodiment, the repair process includes applying a partially-cured repair material to a matrix composite component, and curing the repair material to bond the repair material to the matrix composite component, an external securing mechanism securing the repair material throughout a curing period, In another embodiment, the external securing mechanism is consumed or decomposed during the repair process.

Repair process and a repaired component

A turbine blade that includes an airfoil defined by a concave shaped pressure side outer wall and a convex shaped suction side outer wall that connect along leading and trailing edges and, therebetween, form a radially extending chamber for receiving the flow of a coolant. The turbine blade may further include a rib configuration that partitions the chamber into radially extending flow passages, and a blade outer shell that defines an outer surface of the airfoil. The rib configuration is a non-integral component to the blade outer shell.

Structural configurations and cooling circuits in turbine blades

A thermal actuator is provided and includes an expansion material disposed and configured to move a movable element from a first movable element position toward a second movable element position in accordance with an expansion condition of the expansion material. The expansion material includes an inorganic salt mixture or a metal oxide mixture.

Thermal actuator including fluid with high temperature stability

A method of controlling a power plant that comprises a working fluid and a recirculation loop, wherein the power plant includes a combustor operably connected to a turbine, the method including the steps of: recirculating at least a portion of the working fluid through the recirculation loop; controlling the power plant such that the combustor at least periodically operates at a preferred stoichiometric ratio; and extracting the working fluid from at least one of a first extraction point and a second extraction point positioned on the recirculation loop during the periods when the combustor operates at the preferred stoichiometric ratio.

Methods, systems and apparatus relating to combustion turbine power plants with exhaust gas recirculation

An exhaust gas recirculation system that includes an exhaust gas recirculation regulator operatively connectable to a turbomachine system, and regulating a predetermined amount of exhaust gas to be recirculated. The exhaust gas recirculation system further includes a measuring unit that measures fuel composition of incoming fuel, and a control unit connected to the EGR regulator and the measuring unit, and determining a Wobbe Index and/or reactivity of the incoming fuel based on the measured fuel composition and determining the predetermined amount of exhaust gas to be recirculated based on the determined Wobbe Index and/or reactivity.

Exhaust gas recirculation system, turbomachine system having the exhaust gas recirculation system and exhaust gas recirculation control method

In one aspect, the present subject matter discloses a seal including a substrate material. The substrate material has a first portion having a first abradability and a second portion having a second abradability, the first abradability being different from the second abradability.

Modification of turbine engine seal abradability

An airfoil includes an interior surface, an exterior surface opposed to the interior surface, a pressure side, a suction side opposed to the pressure side, a stagnation line between the pressure and suction sides, and a trailing edge between the pressure and suction sides and downstream from the stagnation line. A first column of overlapping stagnation trench segments is on the exterior surface, and the stagnation line passes through at least a portion of each of the overlapping stagnation trench segments. At least one cooling passage in each stagnation trench segment provides fluid communication from the interior surface to the exterior surface.

Airfoil

Growing community of inventors

Simpsonville, SC, United States of America

Stanley Frank Simpson