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US 11,045,776 B2Granted
Methods and systems for a fuel injector
AssigneeFord Global Technologies, LLC
InventorsXiaogang Zhang, Joseph Basmaji, Jianwen James Yi, Mark Meinhart
Life of this patent
Estimating the term…
Abstract
Methods and systems are provided for a fuel injector. In one example, a system may include an injection nozzle having a venturi shape with an upstream twisted fin arranged in a venturi inlet. The system may further include a downstream twisted fin arranged in a venturi outlet.
Claims18
A system, comprising:
- an injector having a venturi-shaped nozzle, wherein the nozzle comprises a plurality of upstream twisted fins arranged in a venturi inlet of the nozzle, and where a leading edge of an upstream twisted fin of the plurality of upstream twisted fins is perpendicular to a trailing edge of the upstream twisted fin, and further comprising a plurality of downstream twisted fins, wherein the pluralities of upstream and downstream twisted fins do not extend into a venturi throat.
An injector, comprising:
- a tip including at least one injection nozzle comprising a venturi throat arranged between a venturi inlet and a venturi outlet, and where the venturi inlet comprises at least one upstream twisted fin and the venturi outlet comprises at least one downstream twisted fin spaced away from the at least one upstream twisted fin;
- and
- an air entrainment system fluidly coupled to an extreme end of the venturi outlet and the venturi throat, and where the air entrainment system is arranged completely outside of the at least one injection nozzle, wherein the air entrainment system comprises two or more air entrainment passages directly fluidly coupled to a chamber, where the chamber extends around an entire circumference of the venturi throat.
A fuel injector, comprising:
- a curved tip comprising a central nozzle arranged along a central axis, a plurality of inner ring nozzles arranged around the central axis via a first diameter, a plurality of middle ring nozzles arranged around the central axis via a second diameter, and a plurality of outer ring nozzles arranged around the central axis via a third diameter, and where each of the pluralities of inner, middle, and outer ring nozzles are angled relative to the central axis, wherein one or more of the central nozzle and the pluralities of inner, middle, and outer rings nozzles comprises a venturi throat arranged between a venturi inlet and a venturi outlet, and where the venturi inlet comprises at least one upstream twisted fin, and where the venturi outlet comprises at least one downstream twisted fin, and where the at least one downstream twisted fin is misaligned with the at least one upstream twisted fin relative to a general direction of fuel mixture flow.
Dependencies are inferred from the claim text.