Patent classifications
F02D19/0607
COMBUSTION CONTROL SYSTEM AND METHOD FOR SWITCHING BETWEEN SPARK AND PILOT-IGNITED OPERATING MODES IN DUAL FUEL ENGINE
A method of controlling a dual fuel engine system includes adjusting a phasing control parameter such as air-fuel ratio (AFR), based on a phasing signal to limit an error in a phasing of combustion of gaseous fuel. The cylinder is switched to a dual fuel liquid pilot-ignited mode by commanding direct injection of an early pilot shot of liquid fuel, based on the adjustment to the phasing control parameter, and production of a spark to ignite gaseous fuel in the cylinder. Switching the cylinder to the dual fuel liquid pilot-ignited mode is completed by commanding direct injection of an early pilot shot and a second pilot shot of liquid fuel to ignite gaseous fuel in response to combustion of the early and second pilot shots in the cylinder.
SYSTEM AND METHOD FOR ON-BOARD CATALYTIC UPGRADING OF HYDROCARBON FUELS
The present disclosure relates to a vehicle, system, and method for on-board catalytic upgrading of hydrocarbon fuels. In accordance with one embodiment of the present disclosure, a vehicle may include, amongst other things, an internal combustion engine configured to provide motive force to the vehicle, an unreformed fuel subsystem, a reformed fuel subsystem, and a fuel system control architecture. The unreformed fuel subsystem may be structurally configured to transfer unreformed hydrocarbon fuel from the on-board point-of-sale fuel tank to the internal combustion engine. The reformed fuel subsystem may be structurally configured to reform hydrocarbon fuel from the on-board point-of-sale fuel tank and transfer reformed fuel to the internal combustion engine along a reformed fuel supply pathway separated from the unreformed fuel supply pathway. The fuel system control architecture may include a reformate flow control device and a cetane rating controller. The cetane rating controller and the reformate flow control device may cooperate to deliver an upgraded hydrocarbon fuel to a combustion zone of the internal combustion engine.
Propulsion system, and method for operating a propulsion system
Various implementations include propulsion systems and related methods of operation. In one implementation, a system includes: an internal combustion engine, wherein the internal combustion engine has a combustion chamber for burning a fossil fuel, an electrolysis chamber for producing hydrogen gas and oxygen gas, a turbocharger, a supply line connecting a compressor of the turbocharger to the combustion chamber, the supply line designed to convey a gas mixture including at least a part of the hydrogen gas and the oxygen gas to the combustion chamber, a gasification tank with volatile organic compounds received therein, and an air supply for supplying compressed air into the gasification tank, wherein the gas mixture, which is guided via the supply line to the combustion chamber, also includes gasified organic compounds from the gasification tank.
PROPULSION SYSTEM, AND METHOD FOR OPERATING A PROPULSION SYSTEM
Various implementations include propulsion systems and related methods of operation. In one implementation, a system includes: an internal combustion engine, wherein the internal combustion engine has a combustion chamber for burning a fossil fuel, an electrolysis chamber for producing hydrogen gas and oxygen gas, a turbocharger, a supply line connecting a compressor of the turbocharger to the combustion chamber, the supply line designed to convey a gas mixture including at least a part of the hydrogen gas and the oxygen gas to the combustion chamber, a gasification tank with volatile organic compounds received therein, and an air supply for supplying compressed air into the gasification tank, wherein the gas mixture, which is guided via the supply line to the combustion chamber, also includes gasified organic compounds from the gasification tank.
DUAL FUEL ENGINE SYSTEM AND METHOD FOR CONTROLLING DUAL FUEL ENGINE SYSTEM
A method for controlling a dual fuel engine system includes estimating a total indicated engine load, where the total indicated engine load is based on a sum of a measured engine power and a power loss estimate. The method further includes determining a total fueling amount based on an engine speed and the total indicated engine load, where the total fueling amount includes a gas fueling amount and a diesel fueling amount. The method also includes controlling the dual fuel engine system using the total fueling amount.
Ship propulsion system, and method for operating a ship propulsion system
A ship propulsion system is disclosed comprising an internal combustion engine for driving a ship, wherein the internal combustion engine comprises a combustion chamber for combusting fossil fuel, a supply line for delivering a gas mixture to the combustion chamber, an electrolysis chamber for producing hydrogen gas and oxygen gas, and a vacuum pump for sucking the hydrogen gas and the oxygen gas from the electrolysis chamber. The ship propulsion system furthermore comprises a gasification tank with volatile organic compounds received therein, in particular methanol or ethanol, as well as a supply line for supplying a gas mixture to the combustion chamber, wherein the gas mixture comprises gasified organic compounds from the gasification tank and at least a part of the hydrogen gas and the oxygen gas. Furthermore a corresponding method for operation a ship propulsion system is disclosed.
System and methods for reducing particulate matter emissions
A method may comprise: positioning a pressure control valve (PCV) at an outlet of a fuel rail; positioning a volume control valve (VCV) at an inlet of a high pressure pump; and in response to an exhaust particulate matter (PM) level deviating from a target PM level, adjusting a fuel ratio of a first fuel and a second fuel delivered to an engine, and opening one of the PCV and the VCV. In this way, the fuel oxygen content may be adjusted to maintain a PM at or below a target level without a DPF over a broad range of engine designs and operating conditions, while maintaining fuel economy.
Fluid booster system
A fuel booster system having a fuel inlet port, a fuel outlet port, and a fuel accumulator fluidically coupled to both ports. The fuel inlet port allows fuel to be delivered to the fuel accumulator and the fuel outlet port is in fluid communication with a combustion engine to deliver fuel from the fuel booster system to the combustion engine. A source of pressurized gas is also fluidically coupled to the fuel accumulator to deliver pressurized gas through a gas port in one end of the fuel accumulator. A piston is located within the fuel accumulator and the source of pressurized gas can be discharged into the fuel accumulator to force accumulated fuel from the fuel accumulator and to the engine when the fuel booster system determines that the engine needs more fuel.
Supplemental fuel system for compression-ignition engine
A supplemental fuel system includes a supplemental fuel tank, an electronic valve, a voltage sensor, and a controller. The supplemental fuel tank is configured to store a supplemental fuel configured to supplement a primary fuel used by an engine. The electronic valve is configured to be positioned between the supplemental fuel tank and an air supply system for the engine. The voltage sensor is configured to acquire voltage data from a power supply indicative of a voltage of the power supply. The power supply is configured to receive power from an alternator driven by the engine. The controller is configured to control the electronic valve such that the electronic valve is closed in response to the voltage being less than a voltage threshold indicating that the engine is not operating and open/openable in response to the voltage being greater than the voltage threshold indicating that the engine is operating.
Supplemental fuel system for compression-ignition engine
A supplemental fuel system includes a fuel mixer having a nozzle and a stem. The nozzle is configured to be positioned within a conduit of an air supply system for an engine. The nozzle has a body defining a first inlet, an outlet, a passage extending from the first inlet to the outlet, and a second inlet positioned between the first inlet and the outlet. The body has a first cross-sectional dimension that is configured to be less than a second cross-sectional dimension of the conduit such that (i) a first portion of air flowing through the conduit flows through the passage and (ii) a second portion of the air flowing through the conduit flows around the nozzle. The stem has a first end that interfaces with the second inlet. The stem is configured to extend through a wall of the conduit.