Pre-mixed fuel burner with perforated flame holder

1. A combustion system, comprising:

a premix chamber configured to receive an oxidant and a fuel,

wherein the premix chamber is configured to provide an oxidant-fuel mixture into a chamber volume; and

a perforated reaction holder positioned within the chamber volume,

wherein the perforated reaction holder is displaced from the premix chamber and aligned with the premix chamber to receive the oxidant-fuel mixture;

wherein the perforated reaction holder carries a combustion reaction while at least part of the oxidant-fuel mixture combusts;

wherein the premix chamber is configured to receive an oxidant inlet extending at least partially into the premix chamber and a fuel inlet at least partially carried within the oxidant inlet; and

wherein the oxidant inlet is terminated, inside the premix chamber, at an angle that directs incoming fuel and oxidant away from an outlet of the premix chamber and causes the fuel stream and the oxidant stream to mix in a pair of counter-rotating vortices within the premix chamber mix prior to passing through the outlet.

2. The combustion system of claim 1 , wherein a flame arrestor is positioned between the premix chamber and the perforated reaction holder.

3. The combustion system of claim 2 , wherein the premix chamber includes an opening through which the oxidant-fuel mixture flows, and

wherein the flame arrestor entirely covers the opening.

4. The combustion system of claim 2 , wherein the flame arrestor includes a mesh screen.

5. The combustion system of claim 2 , wherein the flame arrestor includes at least one perforated metal sheet and is configured to prevent flashback into the premix chamber to least to 1600° F.

6. The combustion system of claim 1 , wherein the premix chamber includes an opening through which the oxidant-fuel mixture flows,

wherein the premix chamber includes a chamber width and a chamber length, and

wherein the opening includes an opening width that is the same as the chamber width and includes an opening length that is the same as the chamber length.

7. The combustion system of claim 1 , wherein the premix chamber includes an opening through which the oxidant-fuel mixture flows,

wherein the premix chamber includes a chamber width and a chamber length, and

wherein the opening includes an opening width that is shorter than the chamber width and includes an opening length that is shorter than the chamber length.

8. The combustion system of claim 1 , further comprising:

a flame arrestor coupled to the premix chamber,

wherein the premix chamber includes a chamber width and a chamber length, and

wherein the flame arrestor includes an arrestor width that is the same as the chamber width and includes an arrestor length that is the same as the chamber length.

9. The combustion system of claim 1 , further comprising:

a flame arrestor coupled to the premix chamber,

wherein the premix chamber includes an opening through which the oxidant-fuel mixture flows,

wherein the opening includes an opening width and an opening length, and

wherein the flame arrestor includes an arrestor width that is longer than the opening width and includes an arrestor length that is longer than the opening length.

10. The combustion system of claim 1 , wherein the premix chamber is coupled to an oxidant source to receive the oxidant, and

wherein the oxidant source is a blower.

11. The combustion system of claim 1 , wherein the fuel is a hydrocarbon gas.

12. The combustion system of claim 1 , wherein the fuel is a vaporized hydrocarbon liquid.

13. The combustion system of claim 1 , wherein the premix chamber includes an inlet aperture configured to receive both a fuel inlet and an oxidant inlet.

14. The combustion system of claim 13 , wherein the fuel inlet is housed by the oxidant inlet while the oxidant inlet at least partially extends through the inlet aperture.

15. The combustion system of claim 13 , wherein the oxidant inlet at least partially extends through the inlet aperture, and

wherein the fuel inlet and the oxidant inlet are configured to concurrently inject fuel and oxidant into the premix chamber through the inlet aperture.

16. A method of generating a combustion reaction, comprising:

receiving an oxidant in a premix chamber from an oxidant inlet extending at least partially into the premix chamber;

receiving a hydrocarbon fuel into the premix chamber from a fuel inlet at least partially carried within the oxidant inlet;

mixing the hydrocarbon fuel in the premix chamber, to generate an oxidant-fuel mixture, wherein the oxidant inlet terminates inside the premix chamber at an angle that directs incoming hydrocarbon fuel and oxidant away from an outlet of the premix chamber and causes a stream of the hydrocarbon fuel and a stream of the oxidant to mix in a pair of counter-rotating vortices within the premix chamber mix prior to passing through the outlet of the premix chamber;

delivering the oxidant-fuel mixture into a chamber volume to enable combustion of the oxidant-fuel mixture by a perforated reaction holder,

wherein the perforated reaction holder is separated from the premix chamber by a predetermined distance; and

maintaining the combustion reaction with a plurality of perforations through the perforated reaction holder, by receiving the oxidant-fuel mixture at an inlet surface of the perforated reaction holder, and by releasing flue gases at an outlet surface of the perforated reaction holder.

17. The method of claim 16 , wherein maintaining the combustion reaction includes:

preheating the oxidant-fuel mixture proximate to the inlet surface of the perforated reaction holder; and

combusting the oxidant-fuel mixture within at least some of the plurality of perforations between the inlet surface and the outlet surface of the perforated reaction holder.

18. The method of claim 17 , wherein receiving includes:

receiving the hydrocarbon fuel and oxidant through an oxidant inlet operably coupled to an inlet aperture; and

receiving the hydrocarbon fuel through a hydrocarbon fuel inlet that is at least partially housed within the oxidant inlet to enable the hydrocarbon fuel and the oxidant to concurrently flow into the premix chamber through the inlet aperture.

19. The method of claim 16 , wherein delivering the oxidant-fuel mixture includes passing the oxidant-fuel mixture through a flame arrestor prior to exposing the perforated reaction holder to the oxidant-fuel mixture.

20. The method of claim 16 , wherein receiving the hydrocarbon fuel and the oxidant in the premix chamber includes:

receiving the hydrocarbon fuel from a hydrocarbon fuel inlet that is coupled to a first side of the premix chamber; and

receiving the oxidant from an oxidant inlet that is coupled to a second side of the premix chamber.

21. The method of claim 20 , wherein the first side and the second side are on opposite sides of the premix chamber.

22. The method of claim 20 , wherein the first side and the second side are a same side of the premix chamber.

23. The method of claim 16 , wherein receiving the hydrocarbon fuel and the oxidant in the premix chamber includes concurrently receiving the hydrocarbon fuel and the oxidant to cause counter-rotational vortex mixing of the hydrocarbon fuel and the oxidant in the premix chamber.

24. The combustion system of claim 1 , wherein the premix chamber is circular.

25. The method of claim 16 , wherein the premix chamber is circular.