Tubular radiant syngas cooler
A system includes a gasifier that may gasify a feedstock to produce a syngas and a syngas cooler that includes a cooling chamber having a tapered configuration. The cooling chamber includes a first section that may separate particulates from the syngas and includes a first opening and a second opening. The first opening has a smaller width than the second opening. The system also includes a second section in fluid communication with the first section that includes a plurality of tubes surrounding the first section. A first portion of the plurality of tubes is arranged parallel to a longitudinal axis of the cooling chamber and a second portion of the plurality of tubes is angled such that the second portion of the plurality of tubes forms the tapered configuration. The system further includes a passage to flow a seal gas between a shell of the radiant syngas cooler and the second section. The shell encloses the cooling chamber.
1. A system, comprising:
a gasifier configured to gasify a feedstock to produce a syngas; and
a syngas cooler comprising a cooling chamber having a tapered configuration, wherein the cooling chamber comprises:
a first section disposed downstream of the gasifier along a centerline of the syngas cooler and configured to separate particulates from the syngas and comprising a first opening and a second opening, wherein the first opening is fluidly coupled to the gasifier and has a smaller width than the second opening, and the first section is configured to decrease a velocity of the syngas;
a second section in fluid communication with the first section comprising a plurality of tubes surrounding the first section, wherein a first portion of the plurality of tubes is arranged parallel to a longitudinal axis of the cooling chamber, and wherein a second portion of the plurality of tubes is angled such that the second portion of the plurality of tubes forms the tapered configuration, and the radiant syngas cooler is configured to flow a coolant through the plurality of tubes;
a membrane wall configured to separate the first section from the second section, wherein the membrane wall blocks a flow of the syngas into the second section; and
a passage circumferentially about the second section, wherein the passage is in fluid communication with a seal gas and configured to flow the seal gas between a shell of the radiant syngas cooler and the second section, wherein the shell encloses the cooling chamber.
2. The system of claim 1 , wherein the second portion of the plurality of tubes at least partially defines an inner wall of the cooling chamber.
3. The system of claim 1 , comprising a wall adjacent to the plurality of tubes and configured to separate the second section from the passage.
4. The system of claim 3 , wherein the wall is configured to block a flow of the seal gas into the second section.
5. The system of claim 1 , wherein the membrane wall comprises one or more by-pass passages configured to allow the flow of a portion of the syngas from the first section into the second section.
6. The system of claim 5 , wherein the one or more by-pass passages comprise gaps between the second portion of the plurality of tubes.
7. The system of claim 1 , wherein the second opening is in fluid communication with the second section.
8. The system of claim 1 , wherein the first opening comprises an orifice plate configured to restrict a flow of the syngas into the first section.
9. A system, comprising:
a vessel, comprising:
a cooling chamber comprising:
a first section configured to be disposed downstream of a gasifier and along a centerline of the vessel, wherein the first section comprises comprising a first opening and a second opening, the first opening is configured to be fluidly coupled to the gasifier and is configured to receive a syngas from the gasifier the first opening has a smaller width than the second opening, and the first section is configured to decrease a velocity of the syngas;
a second section in fluid communication with the first section and comprising a plurality tubes, wherein a first portion of the plurality of tubes is arranged parallel to a longitudinal axis of the vessel, and a second portion of the plurality of tubes is angled relative to the centerline axis of the vessel such that the second portion of the plurality of tubes forms a tapered configuration;
a membrane wall configured to separate the first section from the second section, wherein the membrane wall blocks a flow of the syngas into the second section: and
a passage circumferentially about the cooling chamber, wherein the passage is in fluid communication with a seal gas and configured to flow the seal gas between a shell of the vessel and the second section, wherein the shell encloses the cooling chamber.
10. The system of claim 9 , wherein a first portion of the plurality of tubes at least partially defines an outer wall of the cooling chamber.
11. The system of claim 9 , wherein the second portion of the plurality of tubes at least partially defines an inner wall of the cooling chamber.
12. The system of claim 9 , wherein the first opening comprises an orifice plate configured to restrict the flow of the syngas into the first section.
13. The system of claim 9 , wherein the membrane wall comprises one or more by-pass passages configured to allow the flow of a portion of the syngas from the first section into the second section, wherein the flow of the portion of the syngas through the by-pass passages further decreases a velocity of the portion of the syngas to increase a residence time of the portion of the syngas within the second section.
14. The system of claim 9 , wherein a portion of the first section comprises a refractory material.
15. The system of claim 9 , wherein the second section is disposed circumferentially about the first section.
16. The system of claim 9 , wherein the first portion of the plurality of tubes and second portion of the plurality of tubes are fluidly coupled to one another.