Burner apparatus, submerged combustion melters including the burner, and methods of use

• US 8,875,544 B2
• Filed: 10/07/2011
• Issued: 11/04/2014
• Est. Priority Date: 10/07/2011
• Status: Active Grant

• Current Assignee: Johns Manville Corporation (Berkshire Hathaway Incorporated)
• Original Assignee: Johns Manville Corporation (Berkshire Hathaway Incorporated)
• Inventors: Charbonneau, Mark William
• Primary Examiner(s): Daniels, Matthew
• Assistant Examiner(s): HERRING, LISA L
• Application Number:
  US13/268,028
• Publication Number:
  US 20130086949A1
• Time in Patent Office: 1,124 Days
• Field of Search: 431/284
• US Class Current: 65/347
• CPC Class Codes: C03B 2211/23 using oxygen, i.e. pure oxygen or oxygen-enriched air
• CPC Class Codes: C03B 2211/60 oxy-fuel burner construction
• CPC Class Codes: C03B 5/18 Stirring devices; Homogenisation mixing in general B01F
• CPC Class Codes: C03B 5/2353 by combustion with pure oxygen or oxygen-enriched air, e.g. using oxy-fuel burners or oxygen lances
• CPC Class Codes: C03B 5/2356 Submerged heating, e.g. by using heat pipes, hot gas or submerged combustion burners bubblers C03B5/193
• CPC Class Codes: F23D 11/108 medium and fuel intersecting downstream of the burner outlet
• CPC Class Codes: F23D 11/12 characterised by the shape or arrangement of the outlets from the nozzle
• CPC Class Codes: F23D 11/36 Details , e.g. burner cooling means, noise reduction means
• CPC Class Codes: F23D 11/38 Nozzles; Cleaning devices therefor
• CPC Class Codes: F23D 14/20 Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone F23D14/38 takes precedence
• CPC Class Codes: F23D 14/32 using a mixture of gaseous fuel and pure oxygen or oxygen-enriched air F23D14/38 takes precedence
• CPC Class Codes: F23D 14/48 Nozzles
• CPC Class Codes: F23D 14/58 characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
• CPC Class Codes: F23D 14/64 with injectors
• CPC Class Codes: F23D 14/78 Cooling burner parts
• CPC Class Codes: F23D 2900/00006 Liquid fuel burners using pure oxygen or O2-enriched air as oxidant
• CPC Class Codes: Y02E 20/34 Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery
• CPC Class Codes: Y10T 137/87249 Multiple inlet with multiple outlet

Abstract

Apparatus includes a first and second conduits configured to form an annulus between them. An adjustable structure includes a body having an upper surface, a lower surface, and a circumferential surface abutting a portion of the internal surface of the second conduit. The structure is adjustable axially in relation to and removably attached to the first conduit via a hub. The hub defines a central passage for fuel or oxidant. The body has one or more non-central through passages configured such that flow of an oxidant or fuel therethrough causes the fuel or oxidant to intersect flow of fuel or oxidant exiting from the central passage in a region above the upper surface of the body.

Claims

1. A submerged combustion burner comprising:

a first conduit comprising a first end, a second end, a longitudinal bore having a longitudinal axis, and an external surface;

a second conduit substantially concentric with the first conduit, the second conduit comprising a first end, a second end, and an internal surface;

the first and second conduits configured to form a primary annulus between the external surface of the first conduit and the internal surface of the second conduit;

an adjustable structure comprising a body having an upper surface forming a constant angle α

with the longitudinal axis, a lower surface, a circumferential surface abutting a portion of the internal surface of the second conduit, the body including a circumferential lip extension extending away from the upper surface of the body and generally parallel to the longitudinal axis, and a generally cylindrical central hub concentric with the longitudinal axis, the structure adjustable axially in relation to and removably attached to the first end of the first conduit via the hub, the hub defining a central passage having an exit at the upper surface, the body comprising one or more non-central through passages extending from the lower to the upper surface, the non-central passages configured such that flow of a first fluid through the non-central passages causes the first fluid to intersect a flow of a second fluid in a mixing region above the upper surface of the body; and

a third substantially concentric conduit comprising a first end, a second end, and an internal surface, the internal surface of the third conduit forming, with an exterior surface of the second conduit, a secondary annulus external to the primary annulus, wherein the first end of the third conduit extends beyond the first end of the second conduit, the first end of the second conduit extends beyond the first end of the first conduit, and the secondary annulus is capped by an end cap connecting the first end of the second conduit and the first end of the third conduit, wherein the end cap is half-torus shaped, the half-torus having an inner diameter equal to an inner diameter of the circumferential lip extension of the hub body, the diameters configured so that the end cap does not obstruct flow of combustion products out of the burner.

2. The apparatus of claim 1 wherein the non-central passages are generally linear and angled at an angle β

measured from the longitudinal axis, the β

angle ranging from about 10 degrees to about 45 degrees.

3. The apparatus of claim 1 wherein the lip extension abuts an overhang portion of the end cap.

4. The apparatus of claim 1 wherein the end cap extends above the exit of the substantially central passage of the structure a distance L1 ranging from about 0.5 inch to about 6 inches.

5. The apparatus of claim 1 wherein the lip extension extends a length L2 from the overhang portion to the upper surface of the structure, where L2 ranges from about 0.25 inch to about 2 inches.

6. The apparatus of claim 1 wherein the angle α

ranges from about 45 to about 90 degrees.

7. The apparatus of claim 1 wherein the exit of the substantially central passage has a diameter L4 ranging from about 0.25 inch to about 3.0 inches.

8. An adjustable submerged combustion burner apparatus comprising:

a first conduit comprising a first end, a second end, a longitudinal bore having a longitudinal axis, and an external surface, the first end comprising threads on the external surface,

a second conduit substantially concentric with the first conduit, the second conduit comprising a first end, a second end, and an internal surface,

the first and second conduits configured to form a primary annulus between the external surface of the first conduit and the internal surface of the second conduit;

a body having an upper surface forming a constant angle α

with the longitudinal axis, a lower surface, a circumferential surface abutting a portion of the internal surface of the second conduit, the body including a circumferential lip extension extending away from the upper surface of the body and generally parallel to the longitudinal axis, and a generally cylindrical central hub concentric with the longitudinal axis, the structure adjustable axially in relation to and threadedly attached to the threads of first end of the first conduit via the hub, the hub defining a central passage having an exit at the upper surface, the body comprising one or more non-central through passages extending from the lower to the upper surface, the non-central passages configured such that flow of a first fluid through the non-central passages causes the first fluid to intersect a flow of a second fluid in a mixing region above the upper surface of the body;

a third substantially concentric conduit comprising a first end, a second end, and an internal surface, the internal surface of the third conduit forming, with an exterior surface of the second conduit, a secondary annulus external to the primary annulus;

the first end of the third conduit extending beyond the first end of the second conduit, the first end of the second conduit extending beyond the first end of the first conduit, and the secondary annulus is capped by an end cap connecting the first end of the second conduit and the first end of the third conduit, wherein the end cap is half-torus shaped, the half-torus having an inner diameter equal to an inner diameter of the circumferential lip extension of the hub body, the diameters configured so that the end cap does not obstruct flow of combustion products out of the burner; and

the second end of the second conduit sealed around the first conduit, and the second end of the third conduit sealed around the second conduit, forming a cavity for fluid to circulate.

9. The apparatus of claim 8 wherein the non-central passages are generally linear and angled at an angle β

measured from the longitudinal axis, the β

angle ranging from about 10 degrees to about 45 degrees.

10. The apparatus of claim 8 comprising a source of oxidant fluidly connected to the second conduit for routing the oxidant to the primary annulus, wherein the oxidant is selected from the group consisting of air and oxygen-enriched air, and a source of fuel fluidly connected to the second end of the first conduit for routing the fuel to the longitudinal bore.

11. The apparatus of claim 10 wherein the oxidant has an oxygen content of 90 mole percent or more supplied from a unit operation selected from the group consisting of pipeline, cylinder, storage facility, cryogenic air separation unit, membrane permeation separator, adsorption unit, and combinations thereof.

12. The apparatus of claim 8 wherein the conduits are comprised of material selected from the group consisting of metal, ceramic, ceramic-lined metal, or combination thereof.

13. The apparatus of claim 8 further comprising a source of coolant fluidly connected to the cavity to cool the burner during combustion.

14. The apparatus of claim 8 wherein the non-central passages have diameter sufficient for directing oxygen into the flow path of fuel exiting the exit of the body.

15. The apparatus of claim 8 wherein a number of non-central passages ranges from about 2 to about 20.

16. The apparatus of claim 8 wherein all of the non-central passages are circular in cross-section and have the same diameter.

17. The apparatus of claim 8 wherein the non-central passages are all equal in length.

18. The apparatus of claim 8 positioned in a side panel or a floor of a submerged combustion melter apparatus such that the longitudinal axis makes an angle to the side panel or floor of the melter ranging from about 30 to about 90 degrees.