Engine system operating strategy apportioning fuel injection between upstream and downstream injection locations
US-11384708-B1 · Jul 12, 2022 · US
US12553407B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12553407-B2 |
| Application number | US-202418428293-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 31, 2024 |
| Priority date | Jan 31, 2024 |
| Publication date | Feb 17, 2026 |
| Grant date | Feb 17, 2026 |
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Official abstract text for this publication.
An engine system includes an engine housing including a plurality of intake valve openings, an intake port extending to the plurality of intake valve openings and an injector bore extending to the intake port. The engine system also includes a fuel system having a port fuel injector, and a fuel distributor having a baffle wall. The baffle wall extends into the intake port and extends at least partially around a fuel spray axis, forming a fuel channel and having at least one of a circumferentially varied porosity or an axially varied cross sectional area. The baffle wall shields fuel spray of an injected fuel such as methanol to limit a bias in distribution of fuel among the plurality of intake valve openings.
Opening claim text (preview).
What is claimed is: 1 . An engine comprising: an engine housing having a cylinder formed therein, a plurality of intake valve openings, an intake port extending in an upstream to downstream direction to the plurality of intake valve openings, and an injector bore extending to the intake port; a fuel system including a port fuel injector within the injector bore defining a fuel spray axis, and a fuel distributor having a baffle wall; and the baffle wall extending outwardly of the injector bore into the intake port and at least partially around the fuel spray axis, and the baffle wall forming a fuel channel and having at least one of a circumferentially varied porosity or an axially varied cross-sectional area. 2 . The engine of claim 1 wherein: the intake port defines an air admission location, and the injector bore defines a fuel admission location; and the fuel admission location is further from the air admission location than one of the plurality of intake valve openings. 3 . The engine of claim 2 wherein the fuel spray axis advances upstream from the fuel admission location in opposition to an incoming flow of intake air. 4 . The engine of claim 1 wherein the baffle wall is part circumferential of the fuel spray axis. 5 . The engine of claim 4 wherein the baffle wall includes the axially varied cross-sectional area, and the axially varied cross-sectional area is reduced in size in a direction away from the injector bore. 6 . The engine of claim 1 wherein the fuel distributor includes a base and a distal tip, and the fuel channel is open, in a downstream direction, between the base and the distal tip. 7 . The engine of claim 6 wherein the fuel distributor includes a distal deflector having an airflow-impinged surface oriented transverse diagonally to the fuel spray axis. 8 . The engine of claim 6 wherein the base includes a cylindrical base fitted within the injector bore. 9 . The engine of claim 1 wherein the fuel distributor is key-fitted with at least one of the engine housing or the port fuel injector within the injector bore.
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