IP Library Granted Patent US 8,771,604
Granted Patent B2
US 8,771,604 · App. 11/702,999 · Granted Jul 8, 2014

Gasifier liner

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Quick Facts
Patent No.
US 8,771,604
App. No.
11/702,999
Granted
Jul 8, 2014
Kind
B2
Abstract

A liner for use within a gasifier vessel includes a plurality of elongated channels and a plurality of ceramic sheaths. The elongated channels pass coolant through the gasifier. The ceramic sheaths surround the elongated channels.

Claims (34)

1. A liner for use within a gasifier vessel, the liner comprising:

a plurality of elongated channels having an inner surface and an outer surface for passing coolant through the gasifier vessel; and

a plurality of ceramic sheaths covering the elongated channels and aligned with each other to form a circular cross section and define an inner surface and outer surface of the liner, wherein each sheath covers one of the elongated channels, and wherein the sheaths are in thermal communication with the elongated channels so that the inner surface of the liner is cooled by coolant flowing through the elongated channels and slag is frozen onto the inner surface of the liner, and wherein the sheaths and the elongated channels are decoupled, wherein the plurality of elongated channels are tubes, wherein each tube includes a respective tip flange at an end thereof, wherein each of the plurality of sheaths are supported on the respective tip flange.

2. The liner of claim 1 , wherein the ceramic sheaths are formed of at least one of the group consisting of: a ceramic and a ceramic matrix composite.

3. The liner of claim 1 , wherein the ceramic sheaths covering a single elongated channel are segmented.

4. The liner of claim 3 , wherein the ceramic sheaths covering a single elongated channel are connected to each other by at least one of the group consisting of: bevel joints and rabbet joints.

5. The liner of claim 1 , wherein the elongated channels extend along a length of the liner.

6. The liner of claim 1 , and further comprising a first tip circumferentially surrounding only one elongated channel of the plurality of elongated cooling channels and maintaining one ceramic sheath of the plurality of ceramic sheaths in position over the one elongated channel.

7. The liner of claim 1 , wherein the ceramic sheaths float on the elongated cooling channels.

8. The liner of claim 1 , wherein the plurality of ceramic sheaths have a non-uniform axial length relative to one another.

9. The liner of claim 1 , wherein the plurality of elongated channels are formed of metal.

10. The liner of claim 1 , wherein the plurality of elongated channels are tubes arranged parallel to one another, and are spaced apart from each other.

11. The liner of claim 10 , wherein the plurality of elongated channels are disposed in a cylindrical arrangement.

12. A gasifier comprising:

a vessel;

a plurality of elongated channels housed within the vessel, wherein each of the elongated channels has a head end, an aft end, an inner surface and an outer surface;

a metal flange for connecting the head ends of each of the elongated channels;

a plurality of ceramic sheaths, each sheath decoupled from but surrounding one of the plurality of elongated channels, wherein the ceramic sheaths are aligned with each other to form a circular cross section; and

a liner having an inner surface defined by the plurality of ceramic sheaths, wherein the ceramic sheaths are positioned to be cooled by coolant flowing through the elongated channels so that slag freezes onto the inner surface of the liner, wherein a plurality of tips supporting the plurality of ceramic sheaths are attached to the plurality of elongated channels at the aft ends of the plurality of elongated channels.

13. The gasifier of claim 12 , wherein the ceramic sheaths surrounding a single elongated channel are segmented.

14. The gasifier of claim 13 , wherein the ceramic sheaths surrounding a single elongated channel are connected to each other by at least one of the group consisting of: bevel joints and rabbet joints.

15. The gasifier of claim 12 , wherein the ceramic sheaths are formed of at least one of the group consisting of: a monolithic ceramic and a ceramic matrix composite.

16. The gasifier of claim 12 , and further comprising a plurality of tips for maintaining the ceramic sheaths in position over the elongated channels, wherein each tip is positioned over only one elongated channel.

17. The gasifier of claim 12 , wherein the ceramic sheaths float on the elongated cooling channels.

18. The gasifier of claim 12 , wherein the plurality of ceramic sheaths have a non-uniform axial length relative to one another.

19. The gasifier of claim 12 , wherein an axially aft end of channel suspended in the vessel and in fluid communication with the vessel.

20. The gasifier of claim 12 , wherein the plurality of elongated channels are formed of metal.

21. The gasifier of claim 12 , wherein a plurality of tips supporting the plurality of ceramic sheaths are stacked on the plurality of elongated channels.

22. A gasifier comprising:

a vessel;

a plurality of elongated channels housed within the vessel, wherein each of the elongated channels has a head end, an aft end, an inner surface and an outer surface;

a metal flange for connecting the head ends of each of the elongated channels;

a plurality of ceramic sheaths, each sheath decoupled from but surrounding one of the plurality of elongated channels, wherein the ceramic sheaths are aligned with each other to form a circular cross section; and

a liner having an inner surface defined by the plurality of ceramic sheaths, wherein the ceramic sheaths are positioned to be cooled by coolant flowing through the elongated channels so that slag freezes onto the inner surface of the liner, wherein aft ends of the plurality of elongated channels are suspended within the vessel, wherein the plurality of elongated channels are arranged to communicate coolant into the vessel at the aft end.

Assignments (7)
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
CORRECTIVE ASSIGNMENT TO CORRECT THE INCORRECT ASSIGNMENT OF U.S. PATENT NO. 8,711,604 PREVIOUSLY RECORDED ON REEL 036395 FRAME 0477. ASSIGNOR(S) HEREBY CONFIRMS THE PATENT NO. IS IMPROPERLY LISTED AS 8,711,604 IT SHOULD BE 8,771,604 (APPL. NO. 11/702,999). Recorded Oct 29, 2015
From: AEROJET ROCKETDYNE OF DE, INC.
To: GAS TECHNOLOGY INSTITUTE
Reel/Frame 037007/0312 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 18, 2015
From: AEROJET ROCKETDYNE OF DE, INC.
To: GAS TECHNOLOGY INSTITUTE
Reel/Frame 036395/0477 →
CHANGE OF NAME Recorded Jul 30, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 030902/0313 →
SECURITY AGREEMENT Recorded Jun 21, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0615 →
SECURITY AGREEMENT Recorded Jun 17, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 030628/0408 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 6, 2007
From: FITZSIMMONS, MARK ANDREW; YOWS, STEPHEN ARTHUR; FUSSELMAN, STEVEN P.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 018962/0059 →