Transportation IP Holdings, LLC

General Electric Company

Ge Global Sourcing LLC

Christopher Joseph Homison

Daniel Edward Loringer

Louis Kobielski

Adam C Felton

Lukas William Johnson

Adam Edgar Klingbeil

Neil Xavier Blythe

Pradheepram Ottikkutti

Kevin McElhaney

Najeeb M Kuzhiyil

Michael Majewski

Raghav Shrikant Kulkarni

Rogier Giepman

Richard Scott

Jared Vaughn

Thomas Michael Lavertu

Roy James Primus

Eric David Peters

Kevin Paul Bailey

Jalal Hunain Zia

David Wright

Jacob Pedder

Deoras Prabhudharwadkar

Maruthi Manohar Jupudi

Kent Jeffries

Timothy Blackhurst

A system comprising a turbine assembly, a heat exchanger, and a compressor assembly is disclosed. The turbine assembly comprises a turbine housing configured to accept an exhaust stream generated by a fuel convertor and a turbine rotor configured to extract a driving energy from the exhaust stream based on an expansion of the exhaust stream through the turbine assembly. The heat exchanger comprises a first flow channel for accepting the exhaust stream from the turbine assembly, a second flow channel in thermal communication with the first channel for flowing a fuel for the fuel converter, and a third flow channel in fluid communication with the first flow channel. The compressor assembly comprises a compressor housing for accepting the exhaust stream from the first flow channel and a compressor rotor operable by the driving energy. A method and an energy recovery system are also disclosed.

Method and system for fuel conditioning

Methods and systems are provided for an electric turbocharger (e-turbo). In one example, a method may include monitoring an e-turbo parameter or an engine parameter, comparing the monitored e-turbo or engine parameter to a determined threshold value for the e-turbo or engine parameter, and signaling a status of the e-turbo in response to the monitored e-turbo or engine parameter differing from the determined threshold value by at least a threshold amount.

Methods and systems for an electric turbocharger

Various methods and systems are provided for an open vane nozzle for a turbine. In one example, the turbine may include at least one bias device arranged at an interface between a nozzle ring and a turbine shroud. The at least one bias device may be configured to exert an axial force on the nozzle ring to maintain contact between vane tips of the nozzle ring and a volute wall.

Semi-floating turbine nozzle ring

A system is provided for compressing gaseous fuel for injection into an engine. The system includes a turbine positioned in the exhaust passage of an engine and a compressor positioned in a gaseous fuel line upstream of the engine, where the compressor is coupled to the turbine.

Method and systems for a gaseous fuel turbo-compressor

A turbine-compressor assembly includes a turbine-compressor device fluidly coupled with a heat source, a compressor, and a turbine via plural valves. A power device is coupled with the turbine-compressor device via a shaft. A controller can control operation of the plural valves to control the movement of fluids within the assembly to selectively switch between the turbine-compressor device operating in one of plural operating modes. In a first mode of operation, the turbine-compressor device can generate electrical power and direct the electrical power to the power device to control an amount of power provided to or extracted from the shaft by the power device. In a second mode of operation, the turbine-compressor device can receive electrical power from the power device to consumer the electrical power.

Turbine-compressor assembly and method

Methods and systems are provided for a Brayton cycle system. In one example, a system for an air Brayton cycle includes a chamber that can receive a first energy source and a second energy source, a turbocharger, and a motor/generator coupled to a shaft of the turbocharger between a compressor and a turbine.

Methods and systems using a Brayton cycle

Methods and systems are provided for electric turbochargers. In one example, a turbocharger comprises a shaft coupling a compressor wheel to a turbine wheel, an electric machine including a stator encircling the shaft between the compressor wheel and the turbine wheel, and an oil supply passage formed in a housing of the electric machine and fluidly coupled to a first oil nozzle oriented toward the shaft.

System and method for an electric turbocharger

Various methods and systems are provided for an electric turbocharger. In one example, the electric turbocharger includes an electric motor circumferentially surrounding a shaft, a turbine coupled to a first end of the shaft, and a compressor coupled to a second end of the shaft, opposite of the first end. The compressor may include a volute with a curved portion protruding towards the turbine.

Inverted compressor for electric turbocharger

Methods and systems are provided for controlling a power output of a power source using a fluidic variable turbine turbocharger. In one example, a turbocharger system coupled to the power source includes a first turbocharger having a first compressor and a first turbine, and a second turbocharger having a second compressor and a second turbine, where boost air from the second compressor is directed to only a nozzle of the first turbine.

Methods and systems for turbocharger

A method and a turbine-compressor assembly of a system having a turbine-compressor device fluidly coupled with a heat source, a compressor, and a turbine via plural valves. A power device may be coupled with the turbine-compressor device. A controller may control operation of the plural valves to control movement of fluids within the assembly to selectively switch between the turbine-compressor device operating in one of plural modes. In a turbine mode of operation, the turbine-compressor device may generate electrical power and direct the electrical power to the power device. In a compressor mode of operation, the turbine-compressor device may receive electrical power from the power device to consume the electrical power.

Various methods and systems are provided for a radial turbocharger. In one example, the turbocharger comprises a turbine case housing a turbine wheel and a compressor case housing a compressor wheel, the turbine case including a vaneless turbine nozzle integrated into the turbine case, a bearing case surrounding a shaft connecting the turbine wheel to the compressor wheel and arranged between the turbine case and compressor case, a plurality of long bolts arranged around a circumference of the turbine case, and a plurality of slots arranged around a circumference of the turbine case, a slot length of each slot extending in a radial direction and adapted to receive a dowel pin having a diameter smaller than the slot length, where each dowel pin, via a corresponding slot, couples the bearing case to the turbine case.

Systems for a turbocharger

Various systems and methods are provided for a turbocharger system. In one example, a system for use with a power generator having a rotary machine including a combustor comprises: a heat exchanger positioned to receive exhaust gases from the combustor; and a turbocharger system, comprising: a low pressure compressor fluidly coupled to the heat exchanger and adapted to supply gases to the heat exchanger; a low pressure turbine and a high pressure turbine each fluidly coupled to the heat exchanger and adapted to receive gases from the heat exchanger; a high pressure compressor fluidly coupled to the rotary machine and the low pressure compressor, adapted to receive gases from the low pressure compressor and supply compressed air to the rotary machine; and a water injector adapted to inject water into a flow path between the low pressure compressor and the heat exchanger.

Systems and methods for increasing power output in a waste heat driven air Brayton cycle turbocharger system

Systems and methods are provided for a turbocharger system for use with a process gas capture system. In one example, the turbocharger system comprises: a heat exchanger positioned to receive inlet gas from a gas generating system via a first inlet; a low pressure compressor driven by a low pressure turbine and coupled to a first outlet of the heat exchanger; a mid-pressure compressor driven by a mid-pressure turbine and coupled in series with the low pressure compressor, the mid-pressure compressor configured to receive low pressure compressed gas from the low pressure compressor; and a high pressure compressor driven by a high pressure turbine and coupled in series with the mid-pressure compressor, the high pressure compressor configured to receive mid-pressure compressed gas from the mid-pressure compressor and output high pressure compressed gas to the process gas capture system and a second inlet of the heat exchanger.

Turbocharger systems and method for capturing a process gas

Various systems and methods are provided for a turbocharger system. In one example, system for use with a power generator having a rotary machine including a combustor comprises: a heat exchanger positioned to receive exhaust gases from the combustor; and a turbocharger system, comprising: a low pressure turbocharger including a low pressure turbine adapted to receive gas flow from the heat exchanger and a low pressure compressor adapted to supply compressed air to the heat exchanger; a high pressure turbocharger including a high pressure turbine adapted to receive gas flow from the heat exchanger and a high pressure compressor adapted to receive gas flow from the low pressure compressor and supply compressed air to the rotary machine; and a second combustor adapted to inject exhaust gases into a flow path arranged between the heat exchanger and an inlet to each of the high pressure turbine and the low pressure turbine.

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Wattsburg, PA, United States of America

Christopher Joseph Homison