Inlet assembly

Patent metadata

Field	Value
Publication number	US-10865983-B2
Application number	US-201716302488-A
Country	US
Kind code	B2
Filing date	Apr 24, 2017
Priority date	May 18, 2016
Publication date	Dec 15, 2020
Grant date	Dec 15, 2020

Abstract

An inlet assembly for a burner includes an inlet nozzle defining an inlet aperture, a non-circular outlet aperture, and a nozzle bore extending along a longitudinal axis between the inlet aperture and the outlet aperture for conveying an effluent gas stream from the inlet aperture to the outlet aperture for delivery to the combustion chamber of the burner. The nozzle bore extends from the inlet aperture to the non-circular outlet aperture. A baffle couples the inlet portion with the outlet portion, and defines a baffle aperture positioned within the nozzle bore. The baffle aperture has a reduced cross-sectional area compared to that of the outlet portion adjacent the baffle. A secondary gas stream nozzle provides a secondary gas stream. The secondary gas stream nozzle being positioned to mix the secondary gas stream with the effluent gas stream within the nozzle bore.

First claim

The invention claimed is:

1. An inlet assembly for a burner, said inlet assembly comprising:
an inlet nozzle defining
an inlet aperture coupleable with an inlet conduit providing an effluent gas stream for treatment by said burner,
a non-circular outlet aperture,
a nozzle bore extending along a longitudinal axis between said inlet aperture and said outlet aperture for conveying said effluent gas stream from said inlet aperture to said outlet aperture for delivery to a combustion chamber of said burner, said nozzle bore having an inlet portion extending from said inlet aperture and an outlet portion extending to said non-circular outlet aperture,
a baffle coupling said inlet portion with said outlet portion, said baffle defining a baffle aperture positioned within said nozzle bore, said baffle aperture having a reduced cross-sectional area compared to that of said outlet portion adjacent said baffle, and
a secondary gas stream nozzle coupleable with a secondary gas stream conduit providing a secondary gas stream, said secondary gas stream nozzle being positioned to mix said secondary gas stream with said effluent gas stream within said nozzle bore wherein said baffle aperture is configured to generate a vortex in said effluent gas stream within said outlet portion and said secondary gas stream nozzle is positioned to inject said secondary gas stream to flow tangentially with a direction of flow of said vortex.

2. The inlet assembly as claimed in claim 1 , wherein said secondary gas stream nozzle is positioned proximate said baffle.

3. The inlet assembly as claimed in claim 1 , wherein said secondary gas stream nozzle is positioned within at least one of said inlet portion and said outlet portion.

4. The inlet assembly as claimed in claim 1 , wherein said secondary gas stream nozzle is orientated to inject said secondary gas stream at an angle of between 10° and 40°.

5. The inlet assembly as claimed in claim 1 , wherein said outlet aperture is elongate, extending along a major axis and secondary gas stream nozzle is orientated to inject said secondary gas stream within a plane defined by said major axis.

6. The inlet assembly as claimed in claim 1 , wherein said secondary gas stream nozzle is positioned within said outlet portion, proximate said baffle aperture.

7. The inlet assembly as claimed in claim 1 , comprising a plurality of said gas stream nozzles.

8. The inlet assembly as claimed in claim 1 , wherein said baffle aperture is configured to generate a plurality of vortices in said effluent gas stream within said outlet portion and each secondary gas stream nozzle is positioned to inject said secondary gas stream to flow tangentially to one of said vortices.

9. An inlet assembly for a burner, said inlet assembly comprising:
an inlet nozzle defining
an inlet aperture coupleable with an inlet conduit providing an effluent gas stream for treatment by said burner,
a non-circular outlet aperture,
a nozzle bore extending along a longitudinal axis between said inlet aperture and said outlet aperture for conveying said effluent gas stream from said inlet aperture to said outlet aperture for delivery to a combustion chamber of said burner, said nozzle bore having an inlet portion extending from said inlet aperture and an outlet portion extending to said non-circular outlet aperture,
a baffle coupling said inlet portion with said outlet portion, said baffle defining a baffle aperture positioned within said nozzle bore, said baffle aperture having a reduced cross-sectional area compared to that of said outlet portion adjacent said baffle, and
a secondary gas stream nozzle coupleable with a secondary gas stream conduit providing a secondary gas stream, said secondary gas stream nozzle being positioned to mix said secondary gas stream with said effluent gas stream within said nozzle bore wherein said baffle aperture is configured to generate a vortex in said effluent gas stream within said outlet portion and wherein said vortex has an inner flow region proximate said baffle aperture and an outer flow region proximate said outlet portion nozzle bore and said secondary gas stream nozzle is positioned to inject said secondary gas stream to flow tangentially with a direction of flow of said vortex in said inner flow region.

Assignees

• Edwards Ltd

Inventors

• Benzeval Ian David

Classifications

• F23D14/12

  Radiant burners · CPC title

• F23D14/70

  Baffles or like flow-disturbing devices · CPC title

• F23G7/065 Primary

  using gaseous or liquid fuel · CPC title

• F23D14/583 Primary

  of elongated shape, e.g. slits · CPC title

• F23D14/64

  with injectors · CPC title