US 5,545,031 A · Method and apparatus for injecting fuel and oxidant into a combustion burner

Abstract

A method and apparatus for injecting fuel and oxidant into a combustion burner. At an exit plane of a nozzle, fuel is discharged in a generally planar fuel layer which has an upper boundary and a lower boundary. Also at the exit plane, oxidant is preferably discharged in both a top layer along the upper boundary of the fuel layer and a bottom layer along the lower boundary of the fuel layer. In a downstream flow direction, the fuel and oxidant preferably converge in a generally vertical plane and diverge in a generally horizontal plane. The discharged fuel and oxidant form a fishtail or fan-shaped flame configuration. A refractory manifold can be used to further enhance the fishtail or fan-shaped flame configuration.

Claims4

Dependent claims

A method of dispersing fuel and oxidant from a burner, the method including the steps of:

dispersing the fuel from an inner nozzle in a generally planar fuel layer, the inner nozzle having upper and lower substantially planar walls converging with respect to each other and side walls diverging with respect to each other;
an outer nozzle spaced about said inner nozzle and having upper and lower substantially planar walls converging with respect to each other and side walls diverging with respect to each other passing an oxidant through the outer nozzle, about said inner nozzle and in contact with the fuel dispersed from the inner nozzle.

Dependencies are inferred from the claim text.

Method and apparatus for injecting fuel and oxidant into a combustion burner

Life of this patent

Method and apparatus for injecting fuel and oxidant into a combustion burner

Life of this patent

Abstract

Claims4