Heat exchanger

Patent metadata

Field	Value
Publication number	US-10767942-B2
Application number	US-201113309123-A
Country	US
Kind code	B2
Filing date	Dec 1, 2011
Priority date	Jan 31, 2011
Publication date	Sep 8, 2020
Grant date	Sep 8, 2020

Abstract

A u-tube heat exchanger has inlet tubes arranged in a pressure neutral inlet tube plate, a heating medium flows via the inlet tubes into u-tubes arranged in a tube sheet where the medium splits in two and flows from both ends of the u-tubes into a heating medium outlet chamber and exits the heat exchanger via an outlet nozzle.

First claim

What is claimed is:

1. A u-tube heat exchanger, comprising:
a cooling chamber with an inlet and an outlet;
an inlet chamber with an inlet;
an outlet chamber with an outlet, the inlet chamber arranged within the outlet chamber;
a tube sheet with a plurality of circularly arranged tube sheet holes, the tube sheet separates the cooling chamber on a first side from the outlet chamber on the second side;
said u-tube heat exchanger having a central, longitudinal axis, a plurality of heat exchange u-tubes circumferentially arranged around said central, longitudinal axis, each of said u-tubes having a feed end and a discharge end, each of said plurality of heat exchange u-tubes comprising, in sequence:
a first tube extending from said feed end to a downstream end,
a u-bend, and
a second tube extending from said u-bend and terminating at said discharge end, each u-bend being entirely radially spaced from said central longitudinal axis of said heat exchanger, such that the first tube, the u-bend and the second tube of each u-tube are all radially offset on one common side of said central longitudinal axis,
a tapered tubular wall section within said first tube which tapers towards and is closer to said u-bend than said feed end, wherein an inner diameter of said feed end and an inner diameter of an upstream end of said tapered tubular wall section are the same;

a plurality of inlet tubes each having open inlet and discharge ends, each inlet tube respectively cooperating with one of said circularly arranged holes of the tube sheet and each discharge end extending into and terminating within said first tube upstream of said tapered tubular wall section, each of said plurality of inlet tubes including an outer surface layer of insulation, said outer surface layer of insulation being spaced from an inner wall surface of said first tube to define an annular flow channel, wherein said outer surface layer of insulation terminates prior to said discharge end of said inlet tube to provide a wider portion of said annular flow channel at said discharge end of said inlet tube, said discharge end cooperating with said tapered tubular wall to split and force a portion of synthesis gas emanating from said inlet tube into said wider portion of said annular flow channel, and flow in a direction opposite to said emanating synthesis gas, through said tube sheet into said outlet chamber, and a second portion of said synthesis gas that continues to flow towards the u-bend of the u-tube, through said second tube and through said tube sheet into said outlet chamber, such that synthesis gas flowing in said opposite direction through said annular flow channel and exiting said annular flow channel through said tube sheet and into said outlet chamber, and synthesis gas flowing forward through said second tube and exiting said discharge end through said tube sheet and into said outlet chamber, will be cooled by indirect heat transfer in said cooling chamber, such that the tube sheet will only come in direct contact with cooled synthesis gas passing through said annular flow channel of said inlet tube and cooled synthesis gas passing through said outlet chamber, and wherein the pressure drops and heat transfer coefficients of the synthesis gas flowing through the first and second tubes and exiting the u-tubes are equalized by reducing the diameter of the second tubes relative to the diameter of the feed end of the first tubes, such that cooled synthesis gas exiting the annular flow channel at the feed end of each of the first tubes of the plurality of u-tubes and passing through the tube sheet has a temperature equal to the cooled synthesis gas exiting the discharge end of the second tubes of the plurality of u-tubes and passing through the tube sheet, thereby avoiding a temperature gradient across the tube sheet;
an inlet tube plate arranged so that it separates the inlet chamber from the outlet chamber, wherein the inlet tube plate has a plurality of circularly arranged inlet tube plate holes, each of which is connected to said open inlet end of each of said inlet tubes;
said plurality of heat exchange u-tubes extend within the cooling medium chamber in contact with the cooling medium on a shell side of the u-tubes,
wherein the only fluid connection between the inlet chamber and the tube sheet and the inside of the u-tubes is via a fluid passage of the inlet tubes, whereby both ends of the u-tubes as well as the tube sheet are in contact with only the cooled synthesis gas on the tube side of the u-tubes and the tube sheet, and
wherein the insulation layer prevents heat transfer between synthesis gas flowing inside the inlet tubes and in the annular channel.

2. The u-tube heat exchanger according to claim 1 , wherein the cooling medium is water or steam, synthesis gas or process gas.

3. The u-tube heat exchanger according to claim 1 , wherein the heat exchanger is a synthesis gas waste heat boiler.

4. The u-tube heat exchanger according to claim 1 , wherein the temperature difference between the cooled synthesis gas exiting the first end of each of the plurality u-tubes and the cooled synthesis gas exiting the second end of each of the plurality of u-tubes is in the range of 0° C.-50° C.

5. The u-tube heat exchanger according to claim 1 , wherein the plurality of inlet tubes are not in contact with the plurality of u-tubes.

6. A process for cooling synthesis gas via indirect heat exchange with a cooling medium in the u-tube heat exchanger according to claim 1 , the process comprising the steps of:
a) providing a flow of the cooling medium via the cooling chamber inlet into the cooling chamber, where the cooling medium contacts the shell side of the u-tubes, and out of the cooling chamber via the cooling chamber outlet,
b) providing a flow of the synthesis gas into the inlet chamber via the inlet of the inlet chamber,
c) providing the flow of the synthesis gas further through the holes of the tube sheet into the inlet ends of the inlet tubes, further through the inlet tubes and out of the outlet ends of inlet tubes and into each of the corresponding u-tubes,
d) splitting the synthesis gas flow in each of the u-tubes into a first part flow which flows through the first tube of each u-tube in the annular flow channel between the inlet tube and the u-tube before the first part flow exits each u-tube via the feed end, and a second part flow which flows through the second tube of each u-tube and exits each u-tube via the discharge end, both the first and the second tube flow being in indirect heat-exchange with the cooling medium via the u-tubes walls, the synthesis gas being cooled by the cooling medium while it flows through the u-tubes, and
e) collecting all of the cooled synthesis gas flows in the outlet chamber, where the cooled synthesis gas is in contact with the tube sheet, and further providing a flow of the cooled synthesis gas out of the outlet chamber via the outlet of the outlet chamber.

7. A process for cooling synthesis gas via indirect heat exchange with a cooling medium according to claim 6 , wherein the cooling medium is water or steam.

8. A process for cooling synthesis gas via indirect heat exchange with a cooling medium according to claim 6 , wherein the cooling medium inlet temperature is in the range of 100° C.-350° C., the cooling medium outlet temperature in the range of 100° C.-350° C., the synthesis gas inlet temperature is in the range of 300° C.-500° C., and the synthesis gas outlet temperature in the range of 120° C.-390° C.

9. A process cooling synthesis gas via indirect heat exchange with a cooling medium according to claim 6 , wherein the temperature difference between the first and second portions of each of the synthesis gas is in the rang

Assignees

• Hoest Madsen Svend
• Haldor Topsoe As

Inventors

• Høst-Madsen Svend

Classifications

• Y02P20/129

  Energy recovery, e.g. by cogeneration, H2recovery or pressure recovery turbines · CPC title

• F28D15/00 Primary

  Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls {; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies (F28D17/00, F28D19/00, F28D20/00 take precedence)} · CPC title

• F02G5/02

  Profiting from waste heat of exhaust gases · CPC title

• F25B27/02

  using waste heat, e.g. from internal-combustion engines · CPC title

• F28D2021/0075

  for syngas or cracked gas cooling systems · CPC title