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A combustor is provided and includes a liner through which fluid fed from at least two injection points flows from a head end to an interior of a transition piece, a first one of the at least two injection points being axially proximate to a fluid impenetrable coupling between the liner and the tran

A combustor is provided and includes a liner through which fluid fed from at least two injection points flows from a head end to an interior of a transition piece, a first one of the at least two injection points being axially proximate to a fluid impenetrable coupling between the liner and the transition piece and defining apertures disposed in fluid communication with a first passage leading to the head end, and a second one of the at least two injection points being disposed axially between the apertures and the head end and upstream from the apertures relative to a direction of fluid flow through the first passage, the second one of the at least two injection points being formed of openings disposed in fluid communication with a second passage leading to the head end.

대표청구항 ▼

1. A combustor, comprising: a liner through which first fluid flows from a head end to an interior of a transition piece;a first sleeve disposed about respective portions of the liner, the transition piece and a fluid impenetrable coupling thereof to define a first passage having an axially elongate

1. A combustor, comprising: a liner through which first fluid flows from a head end to an interior of a transition piece;a first sleeve disposed about respective portions of the liner, the transition piece and a fluid impenetrable coupling thereof to define a first passage having an axially elongate portion, the first sleeve being coupled to the transition piece and having apertures defined therein through which second fluid is injected into the first passage toward the head end; anda second sleeve disposed about the first sleeve to define a second passage having a second axially elongate portion and an entrance disposed axially between aft and forward edges of the first sleeve portion and into which third fluid is injected at the entrance such that the third fluid flows through the second axially elongate portion and toward the head end such that a pressure of the second fluid is substantially maintained along a length of the first passage,the second axially elongate portion of the second passage being disposed about the first axially elongate portion of the first passage,the first sleeve comprising a first sleeve portion and a frusto-conical portion defining the apertures and being coupled to an aft edge of the first sleeve portion and to the transition piece. 2. The combustor according to claim 1, wherein portions of the liner and the first and second sleeves are substantially coaxial. 3. The combustor according to claim 1, wherein portions of the liner and the first and second sleeves are each substantially tubular and the first and second passages are each substantially annular. 4. The combustor according to claim 1, wherein the fluid impenetrable coupling comprises sealant interposed between the respective portions of the liner and the transition piece. 5. The combustor according to claim 1, wherein the apertures are disposed axially proximate to the fluid impenetrable coupling. 6. The combustor according to claim 1, wherein the apertures are arrayed perimetrically about the liner. 7. The combustor according to claim 1, wherein the apertures are radially aligned with one another. 8. The combustor according to claim 1, wherein the apertures are substantially ovoid. 9. The combustor according to claim 1, further comprising edge treatments disposed at the apertures to disturb a flow of the second fluid. 10. The combustor according to claim 1, wherein the second sleeve comprises a bell mouth shaped opening at an entrance to the second passage. 11. The combustor according to claim 1, wherein the liner is formed to define a radial aperture in fluid communication with the first passage and comprises: a flange coupled to an interior surface of the liner; anda baffle coupled to the flange and formed to define a cooling channel into which a portion of the second fluid, which is directed to flow through the radial aperture, is injected toward the transition piece interior. 12. The combustor according to claim 11, wherein the portion of the second fluid injected toward the transition piece interior is interposed between the first fluid and an interior surface of the transition piece. 13. The combustor according to claim 1, wherein an aft portion of the first sleeve portion is coaxial with a forward portion of the transition piece and a forward portion of the first sleeve portion is coaxial with an aft portion of the second sleeve. 14. The combustor according to claim 13, wherein the aft portion of the second sleeve comprises a bell mouth shaped opening at an entrance to the second passage.