Duplex burner with velocity-compensated mesh and thickness

Patent metadata

Field	Value
Publication number	US-10539326-B2
Application number	US-201715667565-A
Country	US
Kind code	B2
Filing date	Aug 2, 2017
Priority date	Sep 7, 2016
Publication date	Jan 21, 2020
Grant date	Jan 21, 2020

Abstract

A combustion system includes a perforated reaction holder having perforations defined to compensate for a non-uniform velocity of fuel and/or oxidant received across an input face of the perforated reaction holder.

First claim

What is claimed is:

1. A combustion system, comprising:
a combustion chamber;
a fuel and oxidant source oriented to emit fuel and oxidant into the combustion chamber; and
a perforated reaction holder disposed in the combustion chamber and oriented to receive the fuel and the oxidant at an input face, the perforated reaction holder defining a plurality of perforations of different sizes, the perforations arranged by size to accommodate a combustion reaction substantially within each perforation when the fuel and the oxidant are received at different velocities across the input face of the perforated reaction holder.

2. The combustion system of claim 1 , wherein the fuel and oxidant source is oriented to emit the fuel and the oxidant toward the input face of the perforated reaction holder about a fuel and oxidant propagation axis, an average velocity of the fuel and the oxidant at the fuel and oxidant propagation axis being higher than at locations peripheral to the fuel and oxidant propagation axis.

3. The combustion system of claim 2 , wherein:
the perforated reaction holder defines the plurality of perforations;
the plurality of perforations include central perforations and peripheral perforations that extend between the input face and an output face of the perforated reaction holder, the central perforations disposed in a central region of the perforated reaction holder have a central axis that is aligned substantially coaxial to the fuel and oxidant propagation axis, and the peripheral perforations disposed in a peripheral region peripheral to the central region; and
the central perforations have a first dimension and the peripheral perforations have a second dimension different from the first dimension.

4. The combustion system of claim 3 , wherein the first dimension is an average ratio of length to cross-sectional area for the central perforations and the second dimension is an average ratio of length to cross-sectional area for the peripheral perforations, a respective length of each perforation of the plurality of perforations being a distance between the input face and the output face of the perforated reaction holder at each respective perforation, and the cross-sectional area being transverse to the thickness; and
wherein the average ratio for the central perforations is larger than the average ratio for the peripheral perforations.

5. The combustion system of claim 4 , wherein the ratio of length to cross-sectional area for successive perforations decreases with distance from the fuel and oxidant propagation axis for perforations in at least one of the central region and the peripheral region.

6. The combustion system of claim 4 , wherein the ratio of length to cross-sectional area is decreased step-wise in at least one step with distance from the fuel and oxidant propagation axis for at least one of the central perforations and the peripheral perforations.

7. The combustion system of claim 3 , wherein the first dimension is an average length of the central perforations between the input face and the output face of the perforated reaction holder and the second dimension is an average length of the peripheral perforations between the input face and the output face of the perforated reaction holder.

8. The combustion system of claim 7 , wherein the central region of the perforated reaction holder includes a plurality of layers not all of which are also in the peripheral region, each layer having layer perforations, consecutive layer perforations of the plurality of layers together constituting the central perforations.

9. The combustion system of claim 8 , wherein a lateral dimension of the layer perforations for a first layer of the plurality of layers is different from a lateral dimension of layer perforations for a second layer of the plurality of layers.

10. The combustion system of claim 3 , wherein the first dimension and the second dimension are average lateral dimensions respectively of the central perforations and of the peripheral perforations transverse to a thickness of the perforated reaction holder, and wherein the lateral dimensions of the central perforations are, on average, smaller than the lateral dimensions of the peripheral perforations, the lateral dimensions of the central perforations and the peripheral perforations respectively selected to compensate for the difference in the average velocity of the fuel and the oxidant received across the input face at the central perforations and the peripheral perforations for said support of the combustion reaction within the central perforations and the peripheral perforations.

11. The combustion system of claim 10 , wherein the lateral dimensions of the central perforations and the lateral dimensions of the peripheral perforations are respectively cross-sectional areas of the central perforations and peripheral perforations.

12. The combustion system of claim 3 , wherein the first dimension and the second dimension are respective average lengths of the central perforations and the peripheral perforations through the thickness of the perforated reaction holder, and the lengths of individual perforations of at least one of the central perforations and the peripheral perforations are successively shorter with distance from the fuel and oxidant propagation axis along the input face of the perforated reaction holder.

13. The combustion system of claim 12 , wherein the average length of the central perforations is greater than the average length of the peripheral perforations, the lengths of the plurality of perforations being selected to compensate for the difference in the average velocity of the fuel and the oxidant received across the input side at the central perforations and the peripheral perforations for said support of the combustion reaction within the central perforations and the peripheral perforations.

14. The combustion system of claim 3 , wherein the first dimension and the second dimension are average lateral dimensions respectively of the central perforations and the peripheral perforations transverse to a thickness of the perforated reaction holder, and the lateral dimensions of respective perforations of at least one of the central perforations and the peripheral perforations are successively wider with distance from the fuel and oxidant propagation axis.

15. The combustion system of claim 14 , wherein the average lateral dimension of the central perforations is smaller than the average lateral dimension of the peripheral perforations, the lateral dimensions of the plurality of perforations being selected to compensate for the difference in the average velocity of the fuel and the oxidant for said support of the combustion reaction within the central perforations and the peripheral perforations.

16. The combustion system of claim 3 , further comprising additional fuel and oxidant sources each having a respective fuel and oxidant propagation axis, wherein the perforated reaction holder includes a plurality of the central regions each aligned substantially coaxial respectively to at least one of the respective fuel and oxidant propagation axes.

17. The combustion system of claim 3 , wherein the perforated reaction holder is a reticulated ceramic perforated reaction holder.

18. The combustion system of claim 17 , wherein the perforated reaction holder includes a plurality of reticulated fibers and wherein the perforations are branching perforations.

19. The combustion system of claim 18 , wherein the perforated reaction holder is configured to support at least a p

Assignees

• Clearsign Comb Corp

Inventors

• Karkow Douglas W
• Breidenthal Robert E
• Colannino Joseph
• Wiklof Christopher A

Classifications

• F23Q7/22

  Details · CPC title

• F23D14/60

  Devices for simultaneous control of gas and combustion air · CPC title

• F23D14/02

  Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone · CPC title

• F23Q7/10 Primary

  for gaseous fuel, e.g. in welding appliances · CPC title

• F23D14/26 Primary

  with provision for a retention flame (pilot flame igniters F23Q9/00) · CPC title