Burner for a flare

Patent metadata

Field	Value
Publication number	US-2019195491-A1
Application number	US-201716325212-A
Country	US
Kind code	A1
Filing date	Aug 24, 2017
Priority date	Aug 24, 2016
Publication date	Jun 27, 2019
Grant date	—

Abstract

A tip burner for a flare comprises a diffuser ( 7 ) which is sealingly connected downstream to a shroud ( 9 ) comprising a tightly packed bed of granular material ( 13 ). The stream of fuel and oxidizer flows to a diffuser where is mixed and tangentially swirled by a swirler ( 8 ) located either in the diffuser or in a closed proximity to the diffuser inlet. The mixture flows next to the shroud where the granular material provides a tortious flow path for the stream, restructuring it aerodynamically and reducing its velocity, preferably to sub sonic level. A combustible mixture exits the shroud as multiple of jet, at low velocity and low turbulence. The mixture is ignited by a pilot burner installed above but in close proximity of the shroud, resulting in a stable flame which generates a low noise level.

First claim

1 . A burner [for a flare stack] comprising in co-operating arrangement:
i) an open upwardly expanding truncated conical mixing diffuser having an inlet receiving a gaseous feed comprising at least one fuel and an oxidant in a ratio to provide for the substantially complete combustion of the fuel at the burner exit; ii) above and co-operating with the outlet of said mixing diffuser an upper shroud, which can be in a shape of an open upwardly expanding truncated cone or a cylinder; iii) two perforated plates which constitute the inlet and the outlet of the said shroud; iv) within the shroud, a bed of inert, solid or hollow rigid tightly packed granules, said bed having the height at least equivalent to one inlet radius of the said shroud, and having a total cross sectional area of interstitial voids among the granules at the shroud inlet of not less than 2 times the cross sectional area of the inlet of the said diffuser; and iv) one or more pilot burners above and proximate to the surface of the upper perforated plate which constitutes the shroud exit.

2 . The burner according to claim 1 further comprising one or more arrays of swirling vanes either:
i) inside the said diffuser, the said array comprising a set of vanes forming a series of radially enclosed channels to swirl, mix and discharge said streams of fuel and oxidizer, in a radially outward and tangential manner wherein the sum of the cross section areas of said channels is not less than 95% of the total cross section area of the diffuser inlet; or
ii) inside the passages or tubing which deliver fuel and oxidizer to the said diffuser, and in proximity to the diffuser inlet,

said arrays comprising a set of vanes forming a series of radially enclosed channels to swirl and discharge said respective streams of fuel and oxidizer in a radially outward and tangential manner into the mixing diffuser, wherein the sum of the cross section areas of said channels is not less than 95% of the total cross section area of the diffuser inlet.

3 . The burner according to claim 2 , wherein said perforated plates which constitute the inlet and outlet of the said shroud are selected from the group consisting of a wire mesh, a perforated plate and a grid of parallel metal bars defining openings there through, having a maximum size opening not more than 70% of the characteristic smallest dimension of the inert granular packing.

4 . The burner according to claim 3 , wherein the inert granular packing comprises the particles of the same size and the same regular shape selected from the group consisting of solid spheres, rods, pellets, prills, saddles, and rings, and mixtures thereof made of the material selected from the group consisting of metal, ceramic and polymeric materials, having a melting temperature not less than 50° C. greater than the combustion temperature of the mixture of said at least one fuel and said oxidant.

5 . The burner according to claim 4 , wherein the inert granular packing comprises a mixture of irregularly shaped or differently shaped particles, with size distribution within ±25% of the average mean dimension.

6 . The burner according to claim 5 , wherein the inert granular packing is cleaned and sieved gravel having a size distribution within ±25% of average sieve size.

7 . The burner according to claim 5 , wherein the shroud containing the granular material, has a diameter substantially the same size as the outlet of said diffuser and has a length to radius ratio of not less than 1:2.

8 . The burner according to claim 5 , wherein the shroud has an exit diameter from 2 to 15 times the diameter the said diffuser outlet and has a length to radius ratio of not less than 1:1.

9 . The burner according to claim 5 , wherein in the mixing diffuser the angle α of the side wall is from 10° to 50° off vertical.

10 . The burner according to claim 9 , wherein said closed diffuser is an upward opening truncated cone.

11 . The burner according to claim 10 , wherein in said r diffuser contains swirling vanes, which are uniformly radially spaced.

12 . The burner according to claim 13 , wherein said vanes have a tangential deflective angle greater than 5°.

13 . The burner according to claim 12 , wherein said vanes have straight parallel deflective edges.

14 . The burner according to claim 13 , wherein said vanes are wedged shaped.

15 . The burner according to claim 12 , wherein said vanes are curved.

16 . The burner according to claim 10 , wherein upstream and proximate to the inlet to the diffuser, separate arrays of swirling vanes are in the oxidant passage and in the fuel passage, so the gas and the oxidant are separately swirled, before they tangentially enter the diffuser inlet.

17 . The burner according to claim 10 , wherein the swirling vanes are mounted upstream and proximate to the inlet of the diffuser in the oxidant passage(s) so only oxidant is swirled, before it tangentially enters the diffuser.

18 . The burner according to claim 10 , wherein the swirling vanes are mounted upstream and proximate to the inlet of the diffuser in the fuel passage(s) so only fuel stream is swirled, before it tangentially enters the diffuser.

Assignees

• Nova Chem Int Sa

Inventors

• Petela Grazyna

Classifications

• F23G7/08 Primary

  using flares, e.g. in stacks · CPC title

• F23D2212/105

  Particles · CPC title

• F23D14/58

  characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration · CPC title

• F23D14/24

  at least one of the fluids being submitted to a swirling motion · CPC title

• F23D2212/203

  Particles · CPC title