Non-catalytic porous-phase combustor

Claim 2

A non-catalytic porous phase combustor comprising: housing means for retaining a porous plate across one open end and confining a combustible mixture in a distribution chamber across the opposite end; input means for introducing a combustible mixture into said distribution chamber; and a multilayer porous plate comprising at least two discrete and contiguous porous layers, a first layer adjacent said distribution chamber comprising a material having a low inherent thermal conductivity, and a second layer adjacent said open end comprising a material having a high inherent thermal conductivity and having a radiating outer surface for emitting heat energy as radiant energy, said first and second layers having pores of substantially the same size.

Claim 3

A non-catalytic porous phase combustor according to claim 1 wherein said first layer comprises a material having an inherent thermal conductivity of from about 1/2 to about 3 Btu/hr-ft 2 -° F/ft.

Claim 4

A non-catalytic porous phase combustor according to claim 2 wherein said second layer comprises a material having an inherent thermal conductivity of from about 3 to about 50 Btu/hr - ft 2 - ° F/ft.

Claim 5

A non-catalytic porous phase combustor according to claim 3 wherein a ratio of said inherent thermal conductivity of said second layer to said inherent thermal conductivity of said first layer is from about 3 to about 15.

Claim 6

A non-catalytic porous phase combustor according to claim 2 wherein said first layer comprises a refractory material selected from the group consisting of: cordierite, zirconia, silica, alumina, and ceramic materials.

Claim 7

A non-catalytic porous phase combustor according to claim 3 wherein said second layer comprises a refractory material selected from the group consisting of: high purity magnesia, silicon carbide, and silicon nitride.

Claim 8

A non-catalytic porous phase combustor according to claim 3 wherein said first layer and said second layer both have a porosity of about 10 percent to about 70 percent.

Claim 9

A non-catalytic porous phase combustor according to claim 7 wherein said first layer and said second layer both have a porosity of about 15 percent to about 40 percent.

Claim 10

A non-catalytic porous phase combustor according to claim 7 wherein the pore sizes in said first and second layers are from about 0.01 to about 0.10 inch in diameter.

Claim 11

A non-catalytic porous phase combustor according to claim 9 wherein said pore sizes in said first and second layers are from about 0.04 to 0.07 inch in diameter.

Claim 12

A non-catalytic porous phase combustor according to claim 1 wherein a ratio of said inherent thermal conductivity of said second layer to said inherent thermal conductivity of said first layer is from about 3 to about 15.

Claim 13

A non-catalytic porous phase combustor according to claim 11 wherein the thickness of said first layer is about 1/4 inch to about 1/2 inch and the thickness of said second layer is about 1/16 inch to about 1/4 inch.

Claim 14

An improved process for generating radiant energy comprising the sequential steps of: introducing a combustible mixture through an inlet means and distributing said combustible mixture within a distribution chamber; passing said combustible mixture through and preheating said combustible mixture in pores of a first discrete layer of a multilayer porous plate, said first layer comprising a material having a low inherent thermal conductivity; passing said combustible mixture through and combusting said combustible mixture in pores of a second discrete layer of said multilayer porous plate, said pores of said second layer being of substantially the same size as said pores of said first layer, said second layer comprising a material having a high inherent thermal conductivity; and converting heat energy produced by said combustion to radiant energy at a radiating surface on said second layer and emitting said radiant energy from said radiating surface.

Claim 15

An improved process for generating radiant energy comprising the sequential steps of: introducing a combustible mixture through an inlet means and distributing said combustible mixture within a distribution chamber; passing said combustible mixture through and preheating said combustible mixture in pores of a first discrete layer of a multilayer porous plate, said first layer comprising a material having a low inherent thermal conductivity; passing said combustible mixture through and combusting said combustible mixture in pores of a second discrete layer of said multilayer porous plate, said pores of said second layer being of substantially the same size as said pores of said first layer, said second layer comprising a material having a high inherent thermal conductivity; and converting heat energy produced by said combustion to radiant energy at a radiating surface on said second layer and emitting said radiant energy from said radiating surface.

Claim 16

An improved process for generating radiant energy according to claim 13 wherein said combustible mixture is selected from the group consisting of: methane/air, propane/air and town gas/air.

Claim 17

An improved process for generating radiant energy according to claim 13 wherein said combustible mixture is preheated to temperatures approaching combustion temperature in said first layer.

Claim 18

An improved process for generating radiant energy according to claim 15 wherein a thermal gradient is established within said first layer, with the lowest temperature at the interface of said first layer with said distribution chamber and the highest temperature at the interface of said first layer and said second layer.

Claim 19

An improved process for generating radiant energy according to claim 15 wherein combustion temperatures are maintained substantially throughout said second layer.

Claim 20

An improved process for generating radiant energy according to claim 16 wherein substantially all combustible mixture is consumed within said second layer.

Claim 21

An improved process for generating radiant energy according to claim 13 wherein combustion is initiated on said radiating surface and is subsequently transferred to the interior of said second layer.

Claim 22

An improved process for generating radiant energy according to claim 13 wherein the combustion intensity in said second layer is from about 400,000 to about 750,000 Btu/hr - ft 2 .