Transportation IP Holdings, LLC

General Electric Company

Ge Global Sourcing LLC

Ai Alpine US Bidco Inc.

Adam Edgar Klingbeil

Thomas Michael Lavertu

Roy James Primus

James Robert Mischler

Eric Richard Dillen

Omowoleola Chukwuemeka Akinyemi

Kevin Paul Bailey

Kevin McElhaney

Victor Manuel Salazar

Pradheepram Ottikkutti

Bhaskar Tamma

Jennifer Lynn Jackson

Daniel George Norton

Neil Xavier Blythe

Daniel Yerace

John Patrick Dowell

Manuel Licon Flores

Brett Heher

Dattatraya Somnath Bhagoji

Ravichandra Srinivasa Jupudi

Ajith Kuttannair Kumar

Narendra Digamber Joshi

Shawn Michael Gallagher

Luke Michael Henry

Eric David Peters

Adam C Felton

Christopher Joseph Homison

Manoj Prakash Gokhale

James Henry Yager

Michael Majewski

Najeeb M Kuzhiyil

David James Walker

Michael Allen Easter

Barry Allen Record

Rogier Giepman

Sreenivasa Rao Gubba

Venu Gopal Gummadavelli

Scott Charles Evans

Vitali Victor Lissianski

Michael Joseph Dell'Anno

Sebastian Walter Freund

Bruce Gordon Barnett

Kevin Michael Fisher

Thomas Stephen Markham

Rahul Srinivas Prabhu

William James Mailander

Wontae Hwang

Robert James Boring

Prashanth D'Souza

Yogesh Kesrinath Potdar

Leslie Orin Trask

Venu Gummadavelli Gupta

Edward Joseph Hall

Sharad Nagappa

Chetan Sharadchandra Tulapurkar

Ricardo Hernandez Pereira

Henrique Moritz

Manoj Prakesh Gokhale

Kent Jeffries

Jay Richerson

Omowoleola Chukuwuemeka Akinyemi

Venu Gummadavelli

Methods and systems are provided for a turbocharger. In one example, a method includes adjusting one or more of a wastegate position and a position of vanes with operation of a turbocharger to reach a desired turbocharger speed via a controller. The method further includes adjusting engine operating parameters to reach the desired turbocharger speed.

Methods and systems for turbocharger

Systems and methods for controlling fuel factions delivered to different cylinders are provided. In one example, a controller is configured to, during a single engine cycle and responsive to a first condition, deliver a lower fraction of a first fuel into a donor cylinder in comparison to a fraction of the first fuel being injected into a non-donor cylinder and deliver a higher fraction of a second fuel into the donor cylinder in comparison to a fraction of the second fuel being injected into the non-donor cylinder.

Method for operating an engine

A vehicle control system and a method of operating thereof may include determining a first ratio at which to operate a vehicle system at a first location along a route along which the vehicle system moves. The first ratio may be based on an amount of a first fuel of a first fuel source relative to an amount of a second fuel of a second fuel source. The vehicle system may be powered by one or more of the first or the second fuel sources. First operational settings at which to control the vehicle system may be determined based on the first ratio between the first and second fuel sources at the first location along the route. Operation of the vehicle system may be controlled according to the first operational settings to move the vehicle system according to the first ratio at the first location along the route.

Vehicle control system and method

Various methods and systems are provided for energy management at a consist. In one example, a method for the energy management includes coordinating a distribution of a power demand in response to a power output of each of a fuel cell system, a battery system, and an engine system. The power output of each of the fuel cell system, the battery system, and the engine system may be selected based on a respective efficiency of each system.

Energy management for multi-input propulsion

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 multi-fuel engine. In one example, a method includes adjusting a substitution ratio based on an intake manifold temperature. The method further including adjusting the intake manifold temperature to increase the substitution ratio.

Methods and systems for multi-fuel engine

Methods and systems are provided for maintaining combustion stability in a multi-fuel engine. In one example, a system may include first and second fuel systems to deliver liquid and gaseous fuels, respectively, to at least one cylinder of the engine, and a controller. The controller may be configured to supply the gaseous fuel to the at least one cylinder, inject the liquid fuel to the at least one cylinder to compression ignite the liquid fuel and combust the gaseous fuel in the at least one cylinder, and retard an injection timing of the injection of the liquid fuel based on a measured parameter associated with auto-ignition of end gases subsequent to the compression-ignition of the liquid fuel. In some examples, the controller may further be configured to adjust an amount of the gaseous fuel relative to an amount of the liquid fuel based on the measured parameter.

Systems and method for controlling auto-ignition

Methods and systems are provided for adjusting a location of a fuel injection in response to a substitution rate and a desired EGR flow. In one example, a method may include injecting a first fuel to a combustion chamber via a direct injector positioned to inject directly into the combustion chamber, injecting a second, different, fuel to the combustion chamber via an exhaust port injector positioned to inject toward an exhaust valve of the combustion chamber, and combusting the first and second fuels together in the combustion chamber.

A multi-fuel injector assembly in one embodiment includes a first fuel injector assembly to deliver a first type of fuel and a second fuel delivery system to deliver a second type of fuel. The first fuel injector includes a first nozzle, at least one first needle, and at least one first actuator configured to move the at least one first needle. The at least one first actuator moves the at least one first needle to a first fuel delivery configuration that corresponds to a first fuel mixture composition, and a second fuel delivery configuration that corresponds to a second fuel mixture composition.

Systems and methods for fuel injector control

Various methods and systems are provided for using only hydrogen as fuel in a duel fuel engine. In one example, a method may include direct injecting only hydrogen as fuel to one or more engine cylinders and compression igniting the injected hydrogen.

Methods and systems for compression ignition in a multi fuel engine

Various methods and systems are provided for skipping fire in one or more cylinders in a dual fuel engine. In one example, a method may include injecting a combination of two fuels to a first set of cylinders of the engine while disabling fuel injection to all remaining cylinders of the engine.

Methods and systems for skip fire in a multi fuel engine

An insert device includes a body having an upper body portion configured to couple with a cylinder head of an engine cylinder and a lower body portion extending from the upper body portion toward a combustion chamber of the engine cylinder. The body includes an interior surface extending around a central volume positioned to receive liquid fuel from a fuel injector. The body includes gas inlet channels and fuel-and-gas mixture outlet channels. The gas inlet channels direct gas into the central volume where the gas mixes with the liquid fuel to form the fuel-and-gas mixture. The fuel-and-gas mixture outlet channels direct the mixture into the combustion chamber. The interior surface includes concave surface portions between the inlet channels and the outlet channels along a center axis of the body that are shaped to direct the gas into the central volume toward the liquid fuel in the central volume.

Insert device for fuel injection

Various methods and systems are provided for a method for a hybrid engine system. In one example, the method includes operating an electrical turbocharger to modify engine operating efficiency and to extend battery charge over a duration of a travel route based on a real-time status of the battery charge. The method allows fuel consumption to be decreased while meeting power demands of vehicle navigation.

Methods and systems for a hybrid engine system

An alignment system includes an optical sensor device that may be inserted into a passage of a body that is located between a fuel injector and a combustion chamber of an engine cylinder. The body is shaped to transmit fuel ejected from a spray hole in a fuel injector into the combustion chamber of the engine cylinder. The system also includes a controller that may examine output of the optical sensor device and determine whether the passage of the body is aligned with the spray hole of the fuel injector based on the output from the optical sensor device. The controller may change a position of one or more of the body or the fuel injector responsive to determining that the passage of the body is not aligned with the spray hole of the fuel injector.

Alignment system and associated method

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Niskayuna, NY, United States of America

Adam Edgar Klingbeil