Combustor assembly for low-emissions and alternate liquid fuels

Patent metadata

Field	Value
Publication number	US-10677458-B2
Application number	US-201715484197-A
Country	US
Kind code	B2
Filing date	Apr 11, 2017
Priority date	Apr 12, 2016
Publication date	Jun 9, 2020
Grant date	Jun 9, 2020

Abstract

Implementations of a combustor assembly yield low emissions, require low power, are suitable for alternate liquid fuels, including highly viscous fuels, and are scalable for various heat release rates. The combustor assembly includes a fuel injector and a swirler. The fuel injector may include a choke portion and a spacer. The choke portion is disposed just upstream of an outlet of a liquid fuel conduit and prevents atomizing gas from interrupting continuous flow of the liquid fuel through the liquid fuel conduit. The spacer is disposed downstream of the outlet to precisely control the gap and thus, bifurcation of atomizing gas flow, between the outlet of liquid fuel conduit and an inlet of an orifice plate. The swirler is disposed radially outwardly and adjacent the fuel injector and includes a plurality of angled vanes.

First claim

The invention claimed is:

1. A fuel injector comprising:
an inner injector tube comprising an outlet portion defining an outlet and a choke portion, the choke portion being disposed upstream of the outlet 10 D to 20 D, wherein D is the inner diameter of the inner injector tube;
an outer injector tube spaced radially apart from at least the outlet portion of the inner injector tube, the outer injector tube having an outer injector tube outlet disposed radially adjacent the outlet of the inner injector tube; and
an orifice plate defining a central opening having an inlet side and an outlet side, the central opening defining a frustoconical cross-sectional shape as taken along a central axis extending through the central opening, wherein an inner diameter of the inlet side is smaller than an inner diameter of the outlet side and the inner diameter of the inlet side is substantially the same as an inner diameter of the outlet of the inner injector tube, wherein the orifice plate directly contacts the outer injector tube, wherein the outer injector tube is co-axial with the inner injector tube, and wherein the central opening of the orifice plate is co-axial with the outlet of the inner injector tube, and the inlet side is spaced apart axially downstream from the outlet of the inner injector tube.

2. The fuel injector of claim 1 , wherein the choke portion is a venturi constriction portion having an inner diameter that is smaller than the inner diameter of the outlet of the inner injector tube.

3. The fuel injector of claim 1 , wherein the choke portion is a check valve.

4. The fuel injector assembly of claim 1 , wherein the choke portion is integrally formed in the inner injector tube.

5. The fuel injector of claim 1 , wherein the choke portion is formed separately from the inner injector tube and disposed therein.

6. The fuel injector of claim 1 , wherein the choke portion has an inner diameter of between 0.2 D and 0.4 D.

7. The fuel injector of claim 1 , wherein:
the fuel injector comprises a spacer ring comprising an annular wall, the annular wall defining a central axial opening and having an upper annular surface;
the upper annular surface of the spacer ring defines a plurality of axial slots, and
the spacer ring is disposed adjacent the outlet of the inner injector tube, the outer injector tube outlet, and the inlet of the orifice plate such that the central opening of the orifice plate and the outlet of the inner injector tube are co-axial with the central axial opening of the spacer ring.

8. The fuel injector of claim 7 , wherein the annular wall further defines a plurality of radially extending openings, the radially extending openings being defined circumferentially between the axial slots and spaced apart circumferentially around the annular wall.

9. The fuel injector of claim 7 , wherein each axial slot has a height that is at least 0.2 D and a width that is twice the height of the slot, the width being measured in a direction that is tangent to a circumference of the annular wall.

10. A combustor assembly comprising:
a fuel injector comprising:
an inner injector tube comprising an outlet portion defining an outlet;
an outer injector tube spaced radially apart from at least the outlet portion of the inner injector tube, the outer injector tube having an outer injector tube outlet disposed radially adjacent the outlet of the inner injector tube; and
an orifice plate defining a central opening having an inlet side and an outlet side, the central opening defining a frustoconical cross-sectional shape as taken along a central axis extending through the central opening, wherein an inner diameter of the inlet side is smaller than an inner diameter of the outlet side and the inner diameter of the inlet side is substantially the same as an inner diameter of the outlet of the inner injector tube, and wherein the central opening of the orifice plate is co-axial with the outlet of the inner injector tube, and the inlet side is spaced apart axially downstream from the outlet of the inner injector tube; and

a swirler disposed radially outwardly and adjacent the outer injector tube outlet, the swirler comprising a central hub, a first plurality of vanes extending therefrom at a first angle greater than 0 degrees from a plane extending perpendicular to a central axis of the central hub, and a second plurality of vanes disposed radially outwardly of the first plurality of vanes and at a second angle greater than 0 degrees from the plane, wherein the swirler is in fluid communication with a gas supply plenum adjacent an inlet side of the swirler and a combustion housing adjacent an outlet side of the swirler,
wherein the orifice plate directly contacts the outer injector tube, and
wherein the outer injector tube is co-axial with the inner injector tube.

11. The combustor assembly of claim 10 , wherein the fuel injector comprises a choke portion, the choke portion being disposed upstream of the outlet 10 D to 20 D wherein D is the inner diameter of the inner injector tube.

12. The combustor assembly of claim 11 , wherein the choke portion is disposed 10 D upstream of the outlet.

13. The combustor assembly of claim 10 , wherein the first and second plurality of swirler vanes are disposed at an angle of 30 degrees relative to the plane.

14. The combustor assembly of claim 10 , wherein the fuel injector further comprises a spacer ring, the spacer ring comprising an annular wall, the annular wall defining a central axial opening and having an upper annular surface,
wherein:
the upper annular surface defines a plurality of axial slots, and
the spacer ring is disposed adjacent the outlet of the inner injector tube, the outer injector tube outlet, and the inlet of the orifice plate such that the central opening of the orifice plate and the outlet of the inner injector tube are co-axial with the central axial opening of the spacer ring.

15. The combustor assembly of claim 14 , wherein the annular wall further defines a plurality of radially extending openings, the radially extending openings being defined circumferentially between the axial slots and spaced apart circumferentially around the annular wall.

16. The combustor assembly of claim 14 , wherein each axial slot has a height that is at least 0.2 D and a width that is twice the height of the slot, the width being measured in a direction that is tangent to a circumference of the annular wall, wherein D is the inner diameter of the inner injector tube.

17. The fuel injector of claim 1 , wherein the inlet side is spaced apart by not more than 0.25 D axially downstream from the outlet of the inner injector tube, wherein D is the inner diameter of the inner injector tube.

18. The combustor assembly of claim 13 , wherein the inlet side is spaced apart by not more than 0.25 D axially downstream from the outlet of the inner injector tube, wherein D is the inner diameter of the inner injector tube.

Assignees

• Univ Alabama

Inventors

• Agrawal Ajay K

Classifications

• F23D17/002

  gaseous or liquid fuel · CPC title

• F23D11/101

  medium and fuel meeting before the burner outlet · CPC title

• F23D11/107 Primary

  at least one of both being subjected to a swirling motion · CPC title

• F23D11/14

  with a single outlet, e.g. slit · CPC title

• F23D11/383

  with swirl means · CPC title