Method and apparatus for affecting a recirculation zone in a cross flow
Disclosed is a cross flow apparatus including a surface and at least one outlet located at the surface. The cross flow apparatus further includes at least one guide at the surface configured to direct an intersecting flow flowing across the surface and increase a velocity of a cross flow being expelled from the at least one outlet downstream from the at least one outlet.
1. A cross flow apparatus comprising:
a swozzle vane having a surface;
at least one outlet located at the surface; and
at least one curved guide protruding from the surface having an upstream end and a downstream end, the upstream end being located farther from a line than the downstream end, the line intersecting the middle of the at least one outlet, the at least one curved guide being curved such that distances between the at least one curved guide and the line vary in a nonlinear relationship, the at least one curved guide being configured to direct an intersecting flow flowing across the surface and increase a velocity of a cross flow being expelled from the at least one outlet downstream from the at least one outlet, the surface extending around the curved guide.
2. The cross flow apparatus of claim 1 , wherein the at least one guide is a protruding vane.
3. The cross flow apparatus of claim 1 , wherein the at least one guide is a groove in the surface.
4. The cross flow apparatus of claim 1 , wherein the at least one guide is two guides for each of the at least one outlet and the two guides are on opposing sides of the cross flow.
5. The cross flow apparatus of claim 1 , wherein the at least one guide is configured to increase a penetration height of the cross flow further from the surface.
6. The cross flow apparatus of claim 1 , wherein the cross flow includes combustible fuel.
7. The cross flow apparatus of claim 1 , wherein the intersecting flow is compressed air.
8. The cross flow apparatus of claim 1 , further comprising a combustor receptive to the combination of the cross flow and the intersecting flow.
9. The cross flow apparatus of claim 1 , wherein at least one of the at least one guide is configured to increase the velocity of a plurality of cross flows.
10. A combustor swozzle comprising:
a swozzle vane having a surface;
an outlet located at the surface; and
a pair of curved guides at the surface flanking the outlet configured to direct an intersecting flow flowing across the surface and increase a velocity of a cross flow being expelled from the outlet downstream from the outlet, a distance between the pair of guides varying nonlinearly along a direction of the intersecting flow, the surface extending around the pair of curved guides.
11. The combustor swozzle of claim 10 , wherein the swozzle vane has two antipodal surfaces, each of the surfaces having at least one outlet.
12. The combustor swozzle of claim 10 , wherein the swozzle vane has a curved profile.
13. The combustor swozzle of claim 10 , further comprising a plurality of swozzle vanes.