Annular vortex combustor

• US 5,025,622 A
• Filed: 07/10/1990
• Issued: 06/25/1991
• Est. Priority Date: 08/26/1988
• Status: Expired due to Term

• Current Assignee: Sol-3 Resources Incorporated
• Original Assignee: Sol-3 Resources Incorporated
• Inventors: Melconian, Jerry O.
• Primary Examiner(s): Casaregola, Louis J.
• Assistant Examiner(s): Thorpe, Timothy S.
• Application Number:
  US07/550,800
• Time in Patent Office: 350 Days
• Field of Search: 60/755, 60/756, 60/759, 60/753, 60/732, 60/748, 60/39.36, 60/39.464, 60/39.37, 60/733, 60/750, 431/352
• US Class Current: 60/39.464
• CPC Class Codes: F23R 3/425 Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes
• CPC Class Codes: F23R 3/50 Combustion chambers comprising an annular flame tube within an annular casing toroidal combustion chambers F23R3/52
• CPC Class Codes: F23R 3/58 Cyclone or vortex type combustion chambers

Abstract

A circumferentially stirred variable residence time vortex combustor including a primary combustion chamber for containing an annular combustion vortex and a first plurality of louvres peripherally disposed about the primary combuston chamber and longitudinally distributed along its primary axis, the louvres inclined to impel air circumferentially about the primary axis within the primary combustion chamber, to cool its interior surfaces, to impel air inwardly to assist in driving the annular combustion vortex in a helical path, and to feed combustion in the primary combustion chamber. The vortex combustor further includes a second annular combustion chamber and a narrow annular waist region interconnecting the output of the primary combustion chamber with the second annular combustion chamber for passing only lower density particles and trapping higher density particles for substantial combustion in the annular combustion vortex of the primary annular combustion chamber.

Claims

1. A circumferentially stirred variable residence time vortex combustor comprising:

a toroidal shaped primary annular combustion chamber disposed around a primary axis in the X-direction including an inner primary wall and an outer primary wall for containing an annular combustion vortex, at least one of said inner primary and said outer primary walls defining a first plurality of louvres peripherally disposed about said primary combustion chamber and longitudinally distributed along its primary axis, said louvres inclined to impel air circumferentially about the primary axis within said primary combustion chamber to cool its interior surfaces, to impel air inwardly to assist in driving the annular combustion vortex in a helical path and to feed combustion in said primary combustion chamber;

a secondary annular combustion chamber including an inner secondary wall and an outer secondary wall; and

a narrow annular waist region, interconnecting the output of said primary combustion chamber with said secondary annular combustion chamber and defined by said outer wall, for passing only lower density particles and trapping higher density particles in the annular combustion vortex in said primary annular combustion chamber for substantial combustion.

2. The vortex combustor of claim 1 in which said secondary annular combustor chamber includes a second plurality of louvres inclined to drive air within said secondary annular combustion chamber in approximately the same helical path established by said louvres in said primary annular combustion chamber, to cool the inner surfaces of said second annular combustion chamber, to complete the combustion process, and to assist in cooling combustion gases.

3. The vortex combustor of claim 2 in which said second plurality of louvres are inclined to tailor the helical path of the combustor exit gases to that acceptable to a turbine.

4. The vortex combustor of claim 1 further including a series of radially opposed air jets at said waist region to quench combustion gases, minimize formation of nitrogen oxides, and further feed combustion.

5. The vortex combustor of claim 1 in which said toroidal shaped primary annular combustion chamber further includes scrolling means, in communication with the interior of said primary annular combustion chamber and disposed circumferentially about its exterior surfaces most remote from said primary axis, for removing ash and other by-products developed during combustion.

6. The vortex combustor of claim 1 in which said primary combustion chamber further includes means for introducing fuel into the annular combustion vortex.

7. The vortex combustor of claim 6 in which said means for introducing fuel includes a fuel injector for injecting fuel circumferentially into the annular combustion vortex to form a fuel-air mixture.

8. The vortex combustor of claim 7 in which said primary annular combustion chamber further includes an ignitor for igniting the fuel-air mixture.

9. The vortex combustor of claim 1 in which said first plurality of louvres are inclined to circumferentially drive air within said primary combustion chamber for establishing a vortex generally centered about the primary axis of said primary combustion chamber.

10. The vortex combustor of claim 1 in which said first plurality of louvres are inclined to impel air approximately tangential to the surfaces of the walls of said primary combustion chamber.

11. The vortex combustor of claim 1 in which said inner and outer walls are coaxial.

12. The vortex combustor of claim 1 in which said primary and secondary chambers are formed by a plurality of plates successively arranged about the primary axis to establish a plurality of junctions.

13. The vortex combustor of claim 12 in which each of said plates including interlocking means for interconnecting that plate with adjacent plates.

14. The vortex combustor of claim 12 in which said plates define at each junction at least one slot for establishing at least one louvre at that junction.

15. The vortex combustor of claim 12 in which each of said plurality of plates has portions that overlap adjacent plates to establish a junction.

16. The vortex combustor of claim 15 further including spacer means disposed between overlapping portions of adjacent plates for securing the overlapping plates in a spaced relationship to define louvres therebetween.

17. The vortex combustor of claim 12 in which said plurality of plates are made from ceramic plates.

21. The vortex combustor of claim 1 in which both of said inner primary wall and said outer primary wall define said first plurality of louvres.

18. A circumferentially stirred variable residence time vortex combustor comprising:

a toroidal shaped primary annular combustion chamber disposed around a primary axis in the X-direction including an inner primary wall and an outer primary wall for containing an annular combustion vortex, at least one of said inner primary and said outer primary walls defining a first plurality of louvres peripherally disposed about said primary combustion chamber and longitudinally distributed along its primary axis, said louvres inclined to impel air circumferentially about the primary axis within said primary combustion chamber to cool its interior surfaces, to impel air inwardly to assist in driving the annular combustion vortex in a helical path, and to feed combustion in said primary combustion chamber;

a secondary annular combustion chamber including a second plurality of louvres for driving air within said secondary annular combustion chamber in approximately the same helical path established by said first plurality of louvres to cool the inner surfaces of said secondary annular combustion chamber and to assist in cooling combustion gases; and

a narrow annular waist region, interconnecting the output of said primary combustion chamber with said secondary annular combustion chamber and defined by said outer wall for passing only lower density particles and trapping higher density particles in the annular combustion vortex in said primary annular combustion chamber for substantial combustion, and including a set of radially opposing air jets to quench the combusting gases and minimize the formation of nitrogen oxides.

19. A circumferentially stirred variable residence time vortex combustor comprising;

a toroidal shaped primary annular combustion chamber disposed around a primary axis in the X-direction for containing an annular combustion vortex, said primary combustion chamber established by a plurality of plates successively arranged about the primary axis of said combustor to form an inner and an outer wall for said primary chamber;

a plurality of louvres defined by said plates, said louvres inclined to impel air circumferentially about the primary axis within said primary combustion chamber to cool its interior surfaces, to impel air inwardly to assist in driving the annular combustion vortex in a helical path and to feed combustion in said primary combustion chamber;

a secondary annular combustion chamber; and

a narrow annular waist region, interconnecting the output of said primary combustion chamber with said secondary annular combustion chamber and defined by said outer wall, for passing only lower density particles and trapping higher density particles in the annular combustion vortex in said primary annular combustion chamber for substantial combustion.

20. The circumferentially stirred variable residence time vortex combustor of claim 19 in which said second annular combustion chamber is established by a plurality of plates successively arranged to form an inner and outer wall.