Lance of a burner
US-8943831-B2 · Feb 3, 2015 · US
US11339968B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11339968-B2 |
| Application number | US-201916528927-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 1, 2019 |
| Priority date | Aug 30, 2018 |
| Publication date | May 24, 2022 |
| Grant date | May 24, 2022 |
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A lance for a burner includes an innermost conduit defining a first fluid passage and a plurality of first fuel injection channels, each first fuel injection channel terminating at a first outlet; an intermediate conduit circumferentially surrounding the innermost conduit, the intermediate conduit defining a second fluid passage and a plurality of second fuel injection channels, each second fuel injection channel terminating at a second outlet; an outermost conduit circumferentially surrounding the intermediate conduit, the outermost conduit defining a third fluid passage, a plurality of third air outlets through the outermost conduit and surrounding the first outlets, a plurality of fourth air outlets through the outermost conduit and surrounding the second outlets, and a plurality of cooling microchannels; wherein each cooling microchannel includes and extends between a microchannel inlet in fluid communication with the third fluid passage and a microchannel outlet on an outer surface of the outermost conduit.
Opening claim text (preview).
What is claimed is: 1. A lance for a burner comprising: an innermost conduit defining a first fluid passage and a plurality of first fuel injection channels, each first fuel injection channel terminating at a first outlet; an intermediate conduit circumferentially surrounding the innermost conduit, the intermediate conduit defining a second fluid passage and a plurality of second fuel injection channels, each second fuel injection channel terminating at a second outlet; an outermost conduit circumferentially surrounding the intermediate conduit, the outermost conduit defining a third fluid passage, a plurality of third air outlets through the outermost conduit and surrounding the first outlets, a plurality of fourth air outlets through the outermost conduit and surrounding the second outlets, and a plurality of cooling microchannels disposed in areas prone to high temperatures during operation; wherein the innermost conduit, the intermediate conduit, and the outermost conduit have respective conduit inlets co-axial with a longitudinal axis of the lance; wherein each of the innermost conduit, the intermediate conduit, and the outermost conduit comprises an upstream arcuate portion fluidly connected to the respective conduit inlet; a vertically oriented portion fluidly connected to the upstream arcuate portion and parallel to the longitudinal axis; and a downstream portion fluidly connected to the vertically oriented portion and transverse to the longitudinal axis, wherein the respective downstream portions of each of the innermost conduit, the intermediate conduit, and the outermost conduits comprise an upper curved surface and a lower curved surface; wherein the innermost conduit, the intermediate conduit, and the outermost conduit terminate in a tip portion that is perpendicular to the longitudinal axis of the lance; wherein each cooling microchannel includes and extends between a microchannel inlet defined through the outermost conduit and in fluid communication with the third fluid passage of the outermost conduit and a microchannel outlet on an outer surface of the outermost conduit to produce a cooling film along the outer surface; and wherein the plurality of cooling microchannels comprises a first set of cooling microchannels disposed in the vertically oriented portion of the outermost conduit; and wherein the first set of cooling microchannels are oriented in a transverse direction across an upstream surface of the vertically oriented portion. 2. The lance of claim 1 , wherein the plurality of cooling microchannels comprises a second set of cooling microchannels disposed in the tip portion of the outermost conduit. 3. The lance of claim 2 , wherein the respective microchannel inlets of the second set of cooling microchannels are disposed in a circumferential array downstream of the longitudinal axis of the lance; and wherein the respective microchannel outlets of the second set of cooling microchannels are disposed proximate to a lance tip of the tip portion. 4. The lance of claim 1 , wherein the tip portion is part of the downstream portion of the lance; and wherein the upper curved surface and the lower curved surface of each respective conduit curve toward one another and are joined at a lance tip. 5. The lance of claim 1 , wherein the respective microchannel inlets of a first sub-set of the first set of cooling microchannels are disposed on a first side of the upstream surface of the outermost conduit, and the respective microchannel outlets of the first sub-set of the first set of cooling microchannels are disposed on a second side of the upstream surface of the outermost conduit; and wherein the respective microchannel inlets of a second sub-set of the first set of cooling microchannels are disposed on the second side of the upstream surface of the outermost conduit, and the respective microchannel outlets of the second sub-set of the first set of cooling microchannels are disposed on the first side of the upstream surface of the outermost conduit. 6. The lance of claim 5 , wherein the respective microchannel inlets of the first sub-set of the first set of cooling microchannels are alternately arranged with the respective microchannel outlets of the second sub-set of the first set of cooling microchannels; and wherein the respective microchannel outlets of the first sub-set of the first set of cooling microchannels are alternately arranged with the respective microchannel outlets of the second sub-set of the first set of cooling microchannels. 7. The lance of claim 1 , wherein the plurality of cooling microchannels comprises a third set of cooling microchannels extending in a direction generally parallel to the longitudinal axis; and wherein the respective microchannel inlets of the third set of cooling microchannels are disposed in a common plane within the vertically oriented portion of the outermost conduit. 8. The lance of claim 7 , wherein the respective microchannel outlets of a first sub-set of the third set of cooling microchannels are disposed upstream of a joint between the vertically oriented portion and the downstream portion of the outermost conduit; and wherein the respective outlets of a second sub-set of the third set of cooling microchannels are disposed downstream of the joint between the vertically oriented portion and the downstream portion of the outermost conduit. 9. The lance of claim 8 , wherein the plurality of cooling microchannels comprises a fourth set of cooling microchannels disposed in the downstream portion proximate to the joint between the vertically oriented portion and the downstream portion of the outermost conduit; and wherein the respective microchannel inlets of the fourth set of cooling microchannels are disposed in an alternating arrangement with the respective microchannels outlets of the first sub-set of the third set of cooling microchannels. 10. The lance of claim 1 , further comprising a support arm coupled to an upstream end of the upstream arcuate portion of the outermost conduit and a balcony extending from the vertically oriented portion of the outermost conduit to the support arm. 11. The lance of claim 10 , wherein at least one additional cooling microchannel extends in a generally transverse direction through the balcony in closer proximity to a lower surface of the balcony than an upper surface of the balcony, the at least one additional cooling microchannel having a microchannel inlet along the upper surface of the balcony and a microchannel outlet along the lower surface of the balcony. 12. A lance for a burner comprising: an innermost conduit defining a first fluid passage and a plurality of first fuel injection channels, each first fuel injection channel terminating at a first outlet; an intermediate conduit circumferentially surrounding the innermost conduit, the intermediate conduit defining a second fluid passage and a plurality of second fuel injection channels, each second fuel injection channel terminating at a second outlet; an outermost conduit circumferentially surrounding the intermediate conduit, the outermost conduit defining a third fluid passage, a plurality of third air outlets through the outermost conduit and surrounding the first outlets, a plurality of fourth air outlets through the outermost conduit and surrounding the second outlets, and a plurality of cooling microchannels disposed in areas prone to high temperatures during operation; wherein the innermost conduit, the intermediate conduit, and the outermost conduit have respective conduit inlets co-axial with a longitudinal axis of the lance; wherein each of the innermost conduit, the intermediate conduit, and the outermost conduit comp
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