Discrete jet atomizer
An atomizer including a fuel output portion shaped to provide a fuel output and an air swirler portion shaped to direct streams of air at the fuel. The air swirler portion includes an outer opening and an inner opening located radially inwardly relative to the outer opening. The inner and outer openings are arranged such that an air stream passed through the inner opening does not intersect a conical section defined by an air stream passed through the outer opening unless both of said air streams are moving at least partially radially outwardly.
1. An atomizer comprising:
a fuel output portion shaped to provide an output of fuel; and
an air swirler portion shaped to direct streams of air at said fuel, said air swirler portion including an outer opening and an inner opening located radially inwardly relative to said outer opening, said inner and outer openings being arranged such that an air stream passed through said inner opening does not intersect a body of rotation defined by an air stream passed through said outer opening unless both of said air streams are moving at least partially radially outwardly at said intersection.
2. The atomizer of claim 1 wherein said inner and outer openings are arranged such that the air streams passed therethrough are initially directed at least partially radially inwardly.
3. The atomizer of claim 1 wherein said atomizer has a central axis, and wherein a central axis of each opening forms an acute angle with a central axis of said air swirler portion.
4. The atomizer of claim 3 wherein said fuel output portion is shaped to create a spray of fuel which travels in a downstream axial direction.
5. The atomizer of claim 1 wherein said air swirler portion includes a plurality of outer openings arranged in a configuration and a set of inner openings arranged in a configuration that is generally concentric with said set of outer openings.
6. The atomizer of claim 5 wherein said atomizer has a central axis and each of said inner and outer openings are each arranged in a generally circular pattern about said central axis, and wherein each opening of said inner and outer set of openings is radially spaced apart from any adjacent openings.
7. The atomizer of claim 1 wherein said fuel output portion includes an orifice through which fuel can be passed to create said fuel spray when fuel is passed therethrough.
8. The atomizer of claim 7 wherein said fuel output portion is shaped to create a generally conical fuel spray when fuel is passed therethrough.
9. The atomizer of claim 1 wherein said fuel output portion includes a simplex, duplex, dual orifice or annular pre-filming atomizer tip.
10. The atomizer of claim 1 wherein said atomizer includes an outer wall portion located adjacent to said opening, said outer wail portion being generally curved and having a convex portion which generally conforms to the path of an air stream passed through said outer opening.
11. The atomizer of claim 1 wherein said air swirler portion includes a generally stepped inner surface having an inner tier and an outer tier, and wherein said inner opening is located on said inner tier and said outer opening is located on said outer tier.
12. The atomizer of claim 1 wherein said outer opening is larger than said inner opening.
13. The atomizer of claim 1 wherein said air streams passed through said openings follow a generally hyperbolic path for a distance of at least the radial offset of said outer set of openings.
14. An atomizer comprising:
a fuel output portion shaped to provide an output of fuel; and
an air swirler portion shaped to direct streams of air at said fuel, said air swirler portion including an outer opening and an inner opening radially spaced apart from a radial center of said atomizer by a radial offset distance, said inner and outer openings being arranged such that an air stream passed through one of said inner opening does not intersect a body of rotation defined by an air stream passed through one of said outer openings within an axial distance of at least about three times the radial offset distance measured from a front face of said atomizer.
15. An air swirler comprising:
a swirler body;
at least one set of outer openings located in said swirler body and arranged in a configuration; and
at least one set of inner openings located in said swirler body and arranged in a configuration that is generally concentric with said set of outer openings, said inner and outer openings being arranged such that an air stream passed through one of said inner openings does not intersect an air stream passed through one of said outer openings when at least one of said air streams is moving at least partially inwardly.
16. An atomizer comprising:
a fuel swirler portion shaped to create a film of fuel when fuel is introduced therein; and
an air swirler portion shaped to direct streams of air at said fuel film, said air swirler portion including a set of outer opening arranged in a configuration and a set of inner opening arranged in a configuration that is generally concentric with said set of outer openings, said inner and outer openings being arranged such that an air stream passed through one of said inner openings does not intersect an air stream passed through one of said outer openings unless both of said air streams are moving at least partially radially outwardly at said intersection.
17. An atomizer comprising:
a fuel output portion shaped to provide an output of fuel; and
an air swirler portion shaped to direct streams of air at said fuel, said air swirler portion including an outer opening and an inner opening located radially inwardly relative to said outer opening, said inner and outer openings being arranged such that the projection on a plane of an air stream passed through said inner opening does not intersect the projection on said plane of an air stream passed through said outer opening unless both of said air streams are moving at least partially radially outwardly at said intersection.
18. A method for designing an air swirler having a body with a central axis, a front face, an inner opening and an outer opening comprising the steps of:
selecting a radial offset of each opening relative to said central axis;
selecting a pinch point distance for an air stream passed through each of said openings, said pinch point distance being located along said central axis and spaced from said front face;
selecting an angular offset of each of said openings relative to said central axis; and
using said radial offset, said pinch point and said angular offset to determine the projection of the path of air streams passing through said openings based upon a hyperbola equation.
19. The method of claim 18 wherein said hyperbola equation is
y
2
a
2
-
(
x
-
h
)
2
b
2
=
1
wherein a represents the radial offset of said openings, h represents the pinch point, θ represents the angular offset of the openings, and b is a/(tan θ).
20. The method of claim 19 further comprising the step of repeating said selecting and determining steps to determine the path of air streams for a plurality of different values for said radial offset, pinch point and angular offset, and selecting selected ones of said values which provide a desired path of said air streams.
21. The method of claim 20 said selecting step includes selecting values for said radial offset, said pinch point and said angular offset such that an air stream passed through said inner opening does not intersect an air stream passed said outer opening unless said both of said intersecting air streams are moving at least partially outwardly relative to said central axis.
22. The atomizer of claim 1 wherein said air swirler portion is configured such that, in side view, the air streams passed therethrough do not intersect a radial centerline of said air swirler portion.
23. The atomizer of claim 1 wherein said air swirler portion includes a plurality of inner openings and a plurality of outer openings and is configured such that the air stream passed through one of said inner openings does not traverse an air stream passed through one of said outer openings.
24. The atomizer of claim 14 wherein said air swirler portion is configured such that, in side view, the air streams passed therethrough do not intersect a radial centerline of said air swirler portion.
25. The atomizer of claim 14 wherein said air swirler portion includes a plurality of inner openings and a plurality of outer openings and is configured such that the air stream passed through one of said inner openings does not traverse an air stream passed through one of said outer openings.
26. The atomizer of claim 15 wherein said air swirler portion is configured such that, in side view, the air streams passed therethrough do not intersect a radial centerline of said air swirler portion.
27. The atomizer of claim 15 wherein said air swirler portion is configured such that the air stream passed through one of said inner openings does not traverse an air stream passed through one of said outer openings.
28. The atomizer of claim 16 wherein said air swirler portion is configured such that, in side view, the air streams passed therethrough do not intersect a radial centerline of said air swirler portion.
29. The atomizer of claim 16 wherein said air swirler portion is configured such that the air stream passed through one of said inner openings does not traverse an air stream passed through one of said outer openings.
30. The atomizer of claim 17 wherein said air swirler portion is configured such that, in side view, the air streams passed therethrough do not intersect a radial centerline of said air swirler portion.
31. The atomizer of claim 17 wherein said air swirler portion includes a plurality of inner openings and a plurality of outer openings and is configured such that the air stream passed through one of said inner openings does not traverse an air stream passed through one of said outer openings.