Fuel admission tube for gaseous fuel engine and engine operating method
A gaseous fuel engine system includes an engine housing forming a plurality of intake ports, and a plurality of fuel admission tubes oriented to admit a gaseous fuel into the plurality of intake ports. The fuel admission tubes include mixers having flow-impinged surfaces exposed to at least one of a flow of gaseous fuel or a flow of intake air and each including a detachment edge. The mixers may include fins, wedge structures, and/or a contoured outer surface of the fuel admission tube. Related apparatus and methodology is also disclosed.
1. An engine system comprising:
an engine housing forming a plurality of intake ports fluidly connected to an upstream intake air feed opening;
a plurality of fuel admission tubes each forming a fuel passage and defining an outgoing fuel axis extending into a respective one of the plurality of intake ports;
a fuel flow path for a gaseous fuel is defined through each respective one of the fuel passages, and an air flow path for intake air is defined through each of the plurality of intake ports between each respective one of the plurality of fuel admission tubes and the engine housing; and
the plurality of fuel admission tubes each further including a mixer formed by a plurality of flow-impinged surfaces located externally of the respective fuel passage and each extending to a flow-detachment edge.
2. The engine system of claim 1 wherein each of the plurality of fuel admission tubes includes a fuel inlet and a fuel outlet and defines a curvilinear tube axis line extending between the fuel inlet and the fuel outlet.
3. The engine system of claim 2 wherein the plurality of fuel admission tubes include among them at least one of a plurality of different tube lengths or a plurality of different tube shapes.
4. The engine system of claim 1 wherein each flow-detachment edge is located axially outward of the respective fuel outlet.
5. The engine system of claim 4 wherein each mixer includes a wedge extending outwardly of the respective one of the fuel outlets.
6. The engine system of claim 1 wherein each of the plurality of fuel admission tubes includes a tube outer surface, and each mixer is formed at least in part upon the respective tube outer surface.
7. The engine system of claim 6 wherein each mixer includes one or more fins.
8. The engine system of claim 6 wherein each mixer is formed by a varied contour of the respective tube outer surface.
9. The engine system of claim 1 wherein each of the plurality of intake ports extends from a common air cavity fluidly connected to the upstream intake air feed opening to two intake valve openings.
10. A method of operating an engine system comprising:
feeding intake air through an upstream intake air feed opening through a common air cavity to a plurality of intake ports in an engine housing;
feeding a gaseous fuel through a plurality of fuel passages in a plurality of fuel admission tubes each extending through the common air cavity to one of the plurality of intake ports;
impinging a flow of at least one of the intake air or the gaseous fuel upon a mixer of each one of the plurality of fuel admission tubes and located externally of the respective one of the plurality of fuel passages; and
conveying the intake air and gaseous fuel, mixed via detachment of the flow from the mixers, into a plurality of engine cylinders for combustion.
11. The method of claim 10 wherein the gaseous fuel includes gaseous molecular hydrogen.
12. The method of claim 10 wherein the at least one of intake air or gaseous fuel is impinged upon a plurality of flow-impinged surfaces of the mixers each extending to a flow-detachment edge, and the flow-detachment edges having at least one of a range of axial locations, a range of circumferential locations, or a range of angular orientations relative to a curvilinear tube axis line of the respective fuel admission tube.
13. The method of claim 10 wherein the mixers include a plurality of fins.
14. The method of claim 10 wherein the mixers include a plurality of wedges each located downstream of a fuel outlet of the respective fuel admission tube.
15. The method of claim 10 wherein the mixers are each formed by an outer tube surface having a varied contour circumferentially around the fuel passage of the respective fuel admission tube.
16. A fuel admission tube for a gaseous fuel engine comprising:
a tube body including an outer tube surface, and an inner tube surface forming a fuel passage defining a curvilinear tube axis line and extending between a first axial end including a connector forming a fuel inlet, and a second axial end including a fuel outlet and forming a terminal tip;
a mixer including a plurality of flow-impinged surfaces extending to a plurality of detachment edges, and the mixer being oriented to be impinged upon by at least one of a gaseous fuel exiting the fuel outlet or intake air conveyed along the outer tube surface;
the mixer being positioned externally of the fuel passage, and the plurality of detachment edges being biased in distribution in a direction of the terminal tip; and
the plurality of flow-detachment edges having among them a plurality of different orientations varied in at least one of an axial aspect, a circumferential aspect, or an angular aspect, relative to the curvilinear tube axis line.
17. The fuel admission tube of claim 16 wherein the mixer includes a plurality of fins upon the tube body.
18. The fuel admission tube of claim 16 wherein the mixer includes a wedge extending axially outward of the fuel outlet.
19. The fuel admission tube of claim 16 wherein the mixer includes a varied outer contour of the tube body adjacent to the second axial end.
20. The fuel admission tube of claim 19 wherein the varied outer contour includes a varied outer contour circumferentially around the curvilinear tube axis line.