High efficiency direct contact heat exchanger

• US 9,383,093 B2
• Filed: 03/11/2013
• Issued: 07/05/2016
• Est. Priority Date: 06/25/2012
• Status: Active Grant

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Orbital ATK Inc. (Northrop Grumman Corporation)
• Inventors: Tilmont, Daniel, Alifano, Joseph A.
• Primary Examiner(s): Tompkins, Alissa
• Assistant Examiner(s): Johnson, Benjamin W
• Application Number:
  US13/793,891
• Publication Number:
  US 20130340691A1
• Time in Patent Office: 1,212 Days
• Field of Search: 122/31.1, 122/31.2, 122/44.1, 122/118, 122/404, 122/442, 122/367.1, 122/367.2, 122/367.3, 166/303, 165/60, 165/120, 126/404
• US Class Current: 1/1
• CPC Class Codes: E21B 36/02 using burners
• CPC Class Codes: E21B 43/122 Gas lift
• CPC Class Codes: E21B 43/24 using heat, e.g. steam injection
• CPC Class Codes: E21B 43/243 Combustion in situ
• CPC Class Codes: E21B 43/263 using explosives
• CPC Class Codes: F22B 1/1853 coming in direct contact with water in bulk or in sprays
• CPC Class Codes: F22B 27/02 built-up from fire tubes
• CPC Class Codes: F22B 27/12 built-up from rotary heat-exchange elements, e.g. from tube assemblies
• CPC Class Codes: F23D 14/02 Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
• CPC Class Codes: F23D 14/70 Baffles or like flow-disturbing devices
• CPC Class Codes: F23Q 7/00 Incandescent ignition; Igniters using electrically-produced heat, e.g. lighters for cigarettes circuits therefor H01T15/00; Electrically-heated glowing plugs
• CPC Class Codes: F23R 3/343 Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00
• CPC Class Codes: Y10T 137/0329 Mixing of plural fluids of diverse characteristics or conditions

Abstract

A direct contact heat exchanger assembly is provided. The direct contact heat exchanger assembly includes an evaporator jacket and an inner member. The inner member is received within the evaporator jacket. A sleeve passage is formed between the evaporator jacket and the inner member. The sleeve passage is configured and arranged to pass a flow of liquid. The inner member has an inner exhaust chamber that is configured to pass hot gas. The inner member further has a plurality of exhaust passages that allow some of the hot gas passing through the inner exhaust chamber to enter the flow of liquid in the sleeve passage.

Claims

1. A direct contact heat exchanger assembly comprising:

an evaporator jacket; and

an inner member received within the evaporator jacket, a sleeve passage defined between the evaporator jacket and the inner member, the sleeve passage configured and arranged to pass a flow of water therethrough, the inner member defining an inner exhaust chamber configured to pass hot gas from a combustor therethrough, the inner member further having a plurality of exhaust passages extending from the inner exhaust chamber through a sidewall of the inner member to the sleeve passage to enable at least a portion of the hot gas passing through the inner exhaust chamber to enter the flow of water in the sleeve passage;

wherein the evaporator jacket is elongated and generally cylindrical in shape, and the inner member comprises;

a generally cylindrical turning vane received within the evaporator jacket, the turning vane having an inner surface defining at least part of the inner exhaust chamber, the turning vane configured to pass hot fluid from the combustor through the inner exhaust chamber, an outer surface of the turning vane and an inner surface of the evaporator jacket are spaced to form, at least in part, the sleeve passage, the sleeve passage exhibiting an annular shape and extending around the outer surface of the turning vane, the turning vane having a plurality of elongated raised directional turning fins extending out from the outer surface of the turning vane within the sleeve passage, the turning fins positioned to direct a flow of water in the sleeve passage into a swirling path around the turning vane; and

a generally cylindrical stator received within the evaporator jacket, the stator longitudinally coupled to the turning vane, the stator having an inner surface configured and arranged to form at least another part of the inner exhaust chamber, the stator having an outer surface, the outer surface of the stator and the inner surface of the evaporator jacket spaced to form at least another part of the sleeve passage, the stator having a plurality of elongated raised directional maintaining fins extending out from the outer surface of the stator within the sleeve passage to maintain the swirling path of the flow of water directed by the turning fins of the turning vane, the plurality of exhaust passages extending from an interior of the stator between the inner exhaust chamber and the sleeve passage.

2. The direct contact heat exchanger assembly of claim 1, wherein each turning fin includes a curved side surface configured and oriented to direct the flow of fluid in the swirling path in the sleeve passage.

3. The direct contact heat exchanger assembly of claim 1, wherein at least one of the directional maintaining fins further includes a length defined between a first leading end and a second trailing end, the first leading end being rounded, the second trailing end of the at least one directional maintaining fin having an opening from one of the exhaust passages to the sleeve passage.

4. The direct contact heat exchanger assembly of claim 1, wherein at least one exhaust passage of the plurality of exhaust passages extends through a portion of an associated directional maintaining fin on the stator.

5. The direct contact heat exchanger assembly of claim 1, further comprising:

a cylindrical end portion having a first end coupled longitudinally to the stator, the cylindrical end portion received within the evaporator jacket, the cylindrical end portion having an inner surface forming, another part of the inner exhaust chamber, the cylindrical end portion further having an outer surface, the outer surface of the cylindrical end portion spaced a distance from the evaporator jacket to form, another part of the sleeve passage, the cylindrical end portion further having a second end, the inner surface having a smaller diameter at the second end of the cylindrical end portion than a diameter at the first end of the cylindrical end portion.

6. The direct contact heat exchanger assembly of claim 5, wherein the outer surface of the cylindrical end portion comprises a shoulder, and the direct contact heat exchanger assembly further comprises:

a thermal growth spring having a first end and a second end, the first end of the thermal growth spring contacting the shoulder of the cylindrical end portion; and

a radial support coupled to the evaporator jacket proximate an end thereof, the second end of the thermal growth spring extending longitudinally from the shoulder of the outer surface of the cylindrical end portion to contact a portion of the radial support.

7. The direct contact heat exchanger assembly of claim 5, further comprising:

an orifice end cap coupled to the second end of the end portion, the orifice end cap having a central opening configured to enable combustion products to pass out of the inner exhaust chamber; and

an orifice member received within the end cap, the orifice member having an orifice passage leading from the inner exhaust chamber to the central opening of the end cap.

8. The direct contact heat exchanger assembly of claim 1, wherein the stator further comprises:

at least a first stator portion and a longitudinally adjacent second stator portion, the first stator portion having a first diameter, the second stator portion having a second, smaller diameter; and

at least one reducer coupling the first stator portion having the first diameter to the second stator portion having the second, smaller diameter.

17. A method of operating the direct contact heat exchanger of claim 1, the method comprising:

passing hot gas through the inner exhaust chamber;

passing a flow of water through the sleeve passage; and

injecting hot gas into the flow of water in the sleeve passage through the plurality of exhaust passages extending from the inner exhaust chamber to the sleeve passage.

18. The method of claim 17, further comprising:

causing the flow of water through the sleeve passage to exhibit a swirling path.

19. The method of claim 17, further comprising:

swirling the flow of water in the sleeve passage around the inner member; and

injecting a portion of the hot gas passing through the inner exhaust chamber into the flow of water through the plurality of exhaust passages extending from the inner exhaust chamber to the sleeve passage.

20. The method of claim 19, wherein swirling the flow of water around the inner member in the sleeve passage further comprises:

engaging the flow of water with elongated raised directional turning fins positioned within the sleeve passage.

21. The method of claim 19, further comprising:

creating back pressure of hot gas passing through the inner exhaust chamber.

22. The method of claim 19, further comprising:

thermally extending the length of the sleeve passage responsive to heat of the hot gas passing through the inner exhaust chamber.

9. A direct contact heat exchanger assembly, comprising:

an elongated cylindrical evaporator jacket;

a cylindrical inner member received within the evaporator jacket, the inner member having an inner surface defining an inner exhaust chamber, the inner member configured and arranged to pass hot gas through the inner exhaust chamber, an outer surface of the inner member and an inner surface of the evaporator jacket spaced to form an annular shaped sleeve passage extending around the outer surface of the inner member, the sleeve passage configured and arranged to pass a flow of water therethrough, the inner member having a plurality of exhaust passages extending from the inner exhaust chamber through a sidewall of the inner member to the sleeve passage, the plurality of exhaust passages allowing some of the hot gas passing in the inner exhaust chamber to mix with the flow of water passing in the sleeve passage to create a gas mix in the sleeve passage; and

a plurality of raised fins extending out from the outer surface of the inner member within the sleeve passage configured and oriented to impart or maintain a swirling path to the flow of water in the sleeve passage;

wherein at least some of the plurality of exhaust passages each pass through an associated fin of the plurality of raised fins to the sleeve passage.

10. The direct contact heat exchanger assembly of claim 9, wherein the plurality of raised fins further comprises:

a plurality of elongated raised directional turning fins extending out from the outer surface of the inner member within the sleeve passage, the turning fins positioned to direct the flow of water in the sleeve passage into the swirling path around the inner member; and

a plurality of elongated raised directional maintaining fins longitudinally spaced from the plurality of elongated raised directional turning fins and extending out from the outer surface of the inner member within the sleeve passage to maintain the swirling path started by the directional turning fins.

11. The direct contact heat exchanger assembly of claim 10, wherein each turning fin includes a curved side surface configured and arranged to direct the swirling path into the flow of water in the sleeve passage.

12. The direct contact heat exchanger assembly of claim 10, wherein at least one of the directional maintaining fins further includes a length defined between a first leading end and a second trailing end, the second trailing end of the directional maintaining fin having an opening extending from one of the exhaust passages to the sleeve passage.

13. The direct contact heat exchanger assembly of claim 9, further comprising:

a cylindrical end portion having a first end coupled to the stator, the cylindrical end portion received within the evaporator jacket, the cylindrical end portion having an inner surface that forms part of the inner exhaust chamber, the cylindrical end portion further having an outer surface, the outer surface of the cylindrical end portion spaced a distance from the evaporator jacket to form part of the sleeve passage, the cylindrical end portion further having a second end, the inner surface having a smaller diameter at the second end of the cylindrical end portion than a diameter at the first end of the end portion;

a thermal growth spring having a first end and a second end, the first end of the thermal growth spring contacting the shoulder of the end portion; and

a radial support coupled to the evaporator jacket proximate an end thereof, the second end of the thermal growth spring extending longitudinally from the shoulder of the cylindrical end portion and contacting a portion of the radial support.

14. The direct contact heat exchanger assembly of claim 13, further comprising:

an orifice end cap coupled to the second end, the orifice end cap having a central opening enabling combustion products to pass out of the inner exhaust chamber; and

an orifice member received within the end cap, the orifice member having an orifice passage leading from the inner exhaust chamber to the central opening of the end cap.

15. The direct contact heat exchanger assembly of claim 9, wherein the inner member further comprises:

a generally cylindrical turning vane, a plurality of elongated raised directional turning fins extending outward from an outer surface of the turning vane within the sleeve passage to impart the swirling path to the flow of water within the sleeve passage; and

at least one generally cylindrical stator coupled longitudinally to the turning vane, a plurality of elongated raised directional maintaining fins extending outward from an outer surface of the at least one stator within the sleeve passage to maintain the swirling path imparted to the flow of water within the sleeve passage by the turning fins of the turning vane.

16. The direct contact heat exchanger assembly of claim 15, wherein the at least one stator further comprises:

at least a first stator portion and a second, longitudinally adjacent stator portion, the first stator portion having a first diameter, the second stator portion having a second, smaller diameter; and

at least one reducer coupling the first stator portion having the first diameter to the second stator portion having the second, smaller diameter.