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.
’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.
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.
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.
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.
Definitions of key terms used in the patent claims.
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