IP Library Granted Patent US 10,337,728
Granted Patent B2
US 10,337,728 · App. 14/863,563 · Granted Jul 2, 2019

Low NOx, high efficiency, high temperature, staged recirculating burner and radiant tube combustion system

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Quick Facts
Patent No.
US 10,337,728
App. No.
14/863,563
Granted
Jul 2, 2019
Kind
B2
Abstract

Embodiments of the present invention include high-temperature staged recirculating burners and radiant tube burner assemblies that provide high efficiency, low NOx and CO emissions, and uniform temperature characteristics. One such staged recirculating burner includes a combustion tube having inside and outside helical fins forming opposing spiral pathways for combustion gases and products of combustion, a combustion nozzle coupled to the combustion tube, a gas tube running axially into the combustion tube, and a staging gas nozzle coupled to the gas tube, where the staging gas nozzle includes radial exit holes into the combustion tube and an axial gas staging tube extending into the combustion nozzle to stage combustion.

Claims (28)

1. A staged recirculating burner comprising:

a combustion tube including inside and outside helical fins forming opposing spiral pathways, the opposing spiral pathways including a first spiral pathway for combustion gases and a second spiral pathway for products of combustion;

a combustion nozzle coupled to the combustion tube;

a gas tube running axially into the combustion tube, the first spiral pathway bounded between the gas tube and combustion tube; and

a staging gas nozzle coupled to the gas tube, the staging gas nozzle including radial exit holes into the combustion tube and an axial gas staging tube extending into the combustion nozzle to stage combustion, wherein the radial exit holes are configured to inject fuel into a spiral flow of preheated air flowing through the first spiral pathway and the staging gas nozzle is positioned such that the fuel mixes with the preheated air flowing through the first spiral pathway to form a fuel-air mixture that continues to travel along the first spiral pathway before moving into the combustion nozzle.

2. A staged recirculating burner as in claim 1 wherein the direction of flow of the combustion gases and the direction of flow of the products of combustion are opposite, and the combustion tube includes a ceramic wall separating the flow of the combustion gases and the flow of the products of combustion.

3. A staged recirculating burner as in claim 1 wherein the combustion tube is made of silicon carbide.

4. A staged recirculating burner as in claim 1 wherein the combustion nozzle is a conically shaped combustion nozzle.

5. A staged recirculating burner as in claim 1 further comprising a heat exchanger coupled to the combustion tube to heat the combustion gases provided to the combustion tube using the products of combustion from the combustion tube.

6. A staged recirculating burner as in claim 5 wherein the combustion tube and the heat exchanger are connected by a specialized silicon carbide thread allowing the combustion tube to be adjustable.

7. A staged recirculating burner as in claim 5 wherein the gas tube extends through the central axis of the heat exchanger and into the combustion tube.

8. A staged recirculating burner as in claim 1 wherein the staging gas nozzle is configured to inject gas radially into the spiral flow of preheated air flowing through the combustion tube.

9. A staged recirculating burner as in claim 8 wherein the staging gas nozzle is configured to inject only a portion of the gas through the radial holes of the staging gas nozzle to create a gas mixture that is substantially lean to suppress the temperature of products of combustion, and is configured to inject the reminder of the gas through the axial gas staging tube.

10. A radiant tube burner system comprising:

the staged recirculating burner of claim 1 ;

an outer radiant tube coupled to the staged recirculating burner;

an inner recirculating tube located concentrically inside the outer radiant tube, the outer radiant tube and the inner recirculating tube forming an annulus therebetween; and

a turning vane spacer located inside the outer radiant tube and positioned between the distal end of the inner recirculating tube and the distal end of the outer radiant tube to cause products of combustion to flow through the annulus between the outer radiant tube and the inner recirculating tube.

11. A radiant tube burner system as in claim 10 wherein the direction of flow of the combustion gases and the direction of flow of the products of combustion are opposite, and the combustion tube includes a ceramic wall separating the flow of the combustion gases and the flow of the products of combustion.

12. A radiant tube burner system as in claim 10 wherein the combustion tube is made of silicon carbide.

13. A radiant tube burner system as in claim 10 wherein the combustion nozzle is a conically shaped combustion nozzle.

14. A radiant tube burner system as in claim 10 further comprising a heat exchanger coupled to the combustion tube to heat the combustion gases provided to the combustion tube using the products of combustion from the combustion tube.

15. A radiant tube burner system as in claim 14 wherein the combustion tube and the heat exchanger are connected by a specialized silicon carbide thread allowing the combustion tube to be adjustable.

16. A radiant tube burner system as in claim 14 wherein the gas tube extends through the central axis of the heat exchanger and into the combustion tube.

17. A radiant tube burner system as in claim 10 wherein the staging gas nozzle is configured to inject only a portion of the gas through the radial holes of the staging gas nozzle to create a gas mixture that is substantially lean to suppress the temperature of products of combustion, and is configured to inject the reminder of the gas through the axial gas staging tube.

18. A radiant tube burner system as in claim 10 wherein the outer radiant tube and the inner recirculating tube are made of silicon carbide.

19. A radiant tube burner system as in claim 10 wherein the combustion nozzle entrains a portion of the products of combustion flowing through the annulus between the outer radiant tube and the inner recirculating tube.

20. A radiant tube burner system as in claim 14 , wherein the heat exchanger is positioned axially adjacent to the combustion tube and configured with respect to the gas tube to enable heat transfer between the products of combustion and the fuel in the gas tube at a location in the gas tube upstream of the staging gas nozzle.

Assignments (8)
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNOR NAME PREVIOUSLY RECORDED ON REEL 056846 FRAME 0220. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Sep 22, 2021
From: SPINWORKS INTERNATIONAL CORPORATION
To: SAINT-GOBAIN CERAMICS & PLASTICS, INC.
Reel/Frame 057569/0379 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE NAME PREVIOUSLY RECORDED ON REEL 056706 FRAME 0064. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Jul 13, 2021
From: SPINWORKS INTERNATIONAL COMPANY
To: SAINT-GOBAIN CERAMICS & PLASTICS, INC.
Reel/Frame 056846/0220 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 29, 2021
From: SPINWORKS INTERNATIONAL CORPORATION
To: SAINT-GOBAIN PERFORMANCE PLASTICS, INC.
Reel/Frame 056706/0064 →
SECURITY INTEREST Recorded Dec 23, 2019
From: LIONHEART INDUSTRIAL GROUP LLC
To: PNC BANK, NATIONAL ASSOCIATION
Reel/Frame 051403/0098 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2019
From: JPMORGAN CHASE BANK, N.A.
To: SELAS HEAT TECHNOLOGY COMPANY LLC
Reel/Frame 051218/0114 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 14, 2019
From: CORNELIUS, MITCHELL D.
To: SELAS HEAT TECHNOLOGY COMPANY LLC
Reel/Frame 049472/0624 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 11, 2018
From: VANDEGRIFT, CHRIS E
To: SELAS HEAT TECHNOLOGY COMPANY LLC
Reel/Frame 046039/0100 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 28, 2017
From: BRISELDEN, THOMAS D; REILLY, THOMAS M; ZAMBANINI, ANTHONY J
To: SPINWORKS INTERNATIONAL CORPORATION
Reel/Frame 044235/0174 →