Dual fuel injection compression ignition engine and method of operating same

Patent No. US8944027 (titled "Dual fuel injection compression ignition engine and method of operating same") on Jun 21, 2011. The application was issued on Feb 3, 2015.

What is this patent about?

’027 is related to the field of dual-fuel internal combustion engines, specifically those utilizing a combination of gaseous fuel, such as natural gas, and a liquid pilot fuel, like diesel, for compression ignition. In traditional dual-fuel systems, achieving a balance between high thermal efficiency and low emissions is difficult because gaseous fuels are hard to ignite and often result in high hydrocarbon output or excessive nitrogen oxides (NOx) depending on when they are introduced into the cylinder. The background context involves the challenge of managing the combustion rate and chemical reaction timing across a wide range of engine speeds and loads using a single injector hardware setup.

The underlying idea behind ’027 is to optimize the combustion process by dynamically splitting the gaseous fuel delivery into two distinct stages within a single power stroke: a pre-mixed charge and a post-ignition charge. By adjusting the mass ratio between these two quantities based on real-time engine speed and load data, the system can tailor the combustion environment. A small amount of liquid fuel acts as a chemical trigger, but the key insight is that the ratio of early-injected gas (which mixes thoroughly with air) to late-injected gas (which burns in a diffusion-like flame) allows the engine to switch between NOx-limiting and efficiency-maximizing strategies without hardware changes.

The claims of ’027 focus on a method and system for operating a dual-fuel engine where an electronic controller dictates a specific injection sequence. The independent claims require the controller to calculate and change a ratio of a pre-mix quantity to a post-ignition quantity of gaseous fuel as a function of engine speed or load. The sequence involves injecting the pre-mix gas first, followed by a pilot quantity of liquid fuel during an auto-ignition condition to trigger combustion, and finally ensuring the pre-mixed gas ignites only after the liquid pilot has successfully compression-ignited.

In practice, the invention utilizes a specialized dual-fuel injector capable of independent needle movements for gas and liquid. At high speeds and loads, the controller may also introduce a pre-mix quantity of liquid fuel early in the compression stroke. This early liquid fuel is kept below a specific threshold to prevent premature knocking, instead serving to accelerate the overall burn rate once the main pilot flame is established. This multi-stage approach allows the engine to maintain high power density at high RPMs while keeping emissions in check during low-load idling.

This approach differs from prior solutions that relied on either purely homogeneous pre-mixing or purely late-cycle direct injection. By utilizing a dynamic split-stream gaseous delivery, the invention avoids the high hydrocarbon emissions of early-only injection and the smoke or efficiency losses of late-only injection. The ability to shift the gas ratio allows the engine to behave like a lean-burn spark engine at certain points and a high-torque diesel engine at others, effectively bridging the gap between different combustion regimes through precise electronic timing of the gaseous fuel split.

How does this patent fit in bigger picture?

Technical Landscape

In the early 2010s when ’027 was filed, dual-fuel engine architectures were typically implemented using either intake manifold induction of gaseous fuel or direct injection of a gas charge following a liquid pilot ignition. At a time when systems commonly relied on fixed injection strategies for gaseous fuels, the management of combustion reaction rates across varying operating ranges was limited by the reliance on single-stage gas delivery. Hardware and software constraints of the era made the precise, dynamic partitioning of gaseous fuel within a single combustion cycle non-trivial, often resulting in a trade-off between high hydrocarbon emissions at low loads and reduced thermal efficiency or elevated nitrogen oxide levels at high speeds and loads.

Prosecution Position

The disclosed invention represents a technical advancement through the integration of a dynamic fuel-splitting strategy within an electronically controlled dual-fuel injection system. By dividing a single gaseous fuel charge into distinct pre-mix and post-ignition quantities and varying their ratio responsive to real-time changes in engine speed and load, the architecture enables active control over the combustion rate. This structural approach overcomes the constraints of static gas delivery by allowing the engine to optimize the homogenization of the fuel-air mixture versus the diffusion-controlled combustion phase. The resulting technical effect is the ability to maintain ignition stability and reduce emissions across a broad operational envelope without sacrificing power density or efficiency.

Claims

The patent contains a total of 20 claims, with claims 1 and 10 serving as the independent claims. These independent claims focus on a method and an electronically controlled engine system for managing dual fuel combustion by adjusting the ratio of premixed to post-ignition gaseous fuel based on engine speed or load, utilizing a dual fuel injector to coordinate gaseous fuel delivery with a pilot liquid fuel ignition. The dependent claims serve to further specify operational parameters such as the inclusion of premixed liquid fuel at high speeds, the adjustment of injection timing to control charge stratification, and the specific mechanical configuration of the dual fuel injector valves and outlets.

Key Claim Terms New

Definitions of key terms used in the patent claims.

Term (Source)Support for SpecificationInterpretation
Autoignition condition
(Claim 1, Claim 10)
The gaseous fuel is mixed with air prior to being ignited responsive to the pilot diesel injection near top dead center. A method of operating an engine includes injecting a pilot ignition quantity of liquid fuel into an engine cylinder from a dual fuel injector in an engine cycle during an auto ignition condition in the engine cylinder. The pilot ignition quantity of liquid fuel is compression ignited.A state within the engine cylinder, typically near top dead center, where temperature and pressure are sufficient to cause the compression ignition of the liquid fuel.
Dual fuel injector
(Claim 1, Claim 10)
This reference teaches the use of a fuel injector with nested needle valve members to facilitate injection of both the gaseous and liquid fuels from the same injector into each engine cylinder. The patent owner teaches direct injection of gaseous fuel into the engine cylinder after a pilot quantity of diesel fuel has been injected and ignited. An electronically controlled compression ignition dual fuel engine includes a dual fuel injector positioned for direct injection into an engine cylinder.A single fuel injection component capable of delivering both a liquid fuel (such as distillate diesel) and a gaseous fuel directly into an engine cylinder.
Pilot ignition quantity
(Claim 1, Claim 10)
Some gaseous fuel engines utilize a small amount of distillate diesel fuel that is compression ignited to in turn ignite a larger charge of gaseous fuel. The method includes injecting a pilot ignition quantity of liquid fuel into an engine cylinder from a dual fuel injector in an engine cycle during an auto ignition condition in the engine cylinder. The pilot ignition quantity of liquid fuel is compression ignited.A small amount of liquid fuel, such as distillate diesel, injected to facilitate ignition of a larger charge of gaseous fuel through compression ignition.
Post ignition quantity
(Claim 1, Claim 10)
The amount of gaseous fuel is divided to include a pre-mix quantity and a post ignition quantity of gaseous fuel, which are both greater than zero. The gaseous fuel is ignited after the pilot ignition quantity of liquid fuel is compression ignited. The electronic controller is configured to change a ratio of the pre-mix quantity of gaseous fuel to the post ignition quantity of gaseous fuel responsive to changing from a first engine speed and load to a second engine speed and load.A portion of gaseous fuel injected into the engine cylinder that is intended to be ignited after the compression ignition of the liquid pilot fuel has occurred.
Premix quantity
(Claim 1, Claim 10)
The gaseous fuel may be supplied to the engine intake manifold or metered directly into individual cylinders where it is mixed with air prior to being ignited responsive to the pilot diesel injection near top dead center. The amount of gaseous fuel is divided to include a pre-mix quantity and a post ignition quantity of gaseous fuel, which are both greater than zero. The pre-mix quantity of gaseous fuel is injected into the engine cylinder from the dual fuel injector in the engine cycle.A portion of gaseous fuel injected into the engine cylinder that is mixed with air prior to the compression ignition of a liquid pilot fuel.

Litigation Cases New

US Latest litigation cases involving this patent.

Case NumberFiling DateTitle
3:25-cv-00239May 14, 2025Champion Power Equipment, Inc. V. Westinghouse Electric Corporation

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US8944027

Application Number
US13164815A
Filing Date
Jun 21, 2011
Publication Date
Feb 3, 2015
External Links
Slate, USPTO , Google Patents