US 11,585,528 B2Granted

Apparatus and method for a burner assembly

AssigneePower Flame Incorporated

InventorsKenneth Ray George, Michael Joseph Purdon, Michael Ryan Martinie

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Abstract

A burner assembly having a blower housing, a blower to supply air to the burner assembly, a blast tube having a longitudinal axis, a fuel source to supply fuel to the burner assembly, a center tube that is substantially parallel to the longitudinal axis and conveys air and fuel to a center tube burner end opening, a plurality of premix tubes, each of which is substantially parallel to the longitudinal axis and conveys air and fuel to a premix tube burner end opening, a diffuser that is disposed in the center tube near the center tube burner end opening, a nozzle that is disposed in the center tube substantially perpendicular to the diffuser. The center tube air and fuel mixture is fuel rich and the premix tubes air and fuel mixture is fuel lean. A method for burning the center tube air and fuel mixture and the premix tubes mixtures.

Claims11

Dependent claims

A burner assembly comprising:

a blast tube having a longitudinal axis and having a blast tube end;
a blower configured to supply air to the blast tube;
a center tube disposed within the blast tube, oriented substantially parallel to the longitudinal axis, and terminating at a center tube burner end opening located proximate the blast tube end, wherein the center tube is in fluid communication with the blast tube so as to receive a first air portion of the air supplied to the blast tube by the blower;
a plurality of premix tubes disposed within the blast tube and encircling the center tube, each premix tube of the plurality of premix tubes oriented substantially parallel to the longitudinal axis and terminating at a premix tube burner end opening located proximate the blast tube end, wherein each premix tube of the plurality of premix tubes is in fluid communication with the blast tube so as to receive a second air portion of the air supplied to the blast tube by the blower;
a plurality of center tube orifices provided in the center tube at a first longitudinal position along the longitudinal axis, each of the center tube orifices configured to receive fuel and to provide fuel received to the center tube;
a plurality of premix tube orifices provided in each of the plurality of premix tubes and located at a second longitudinal position along the longitudinal axis that is upstream of the plurality of center tube orifices such that the center tube orifices are longitudinally located between the blast tube end and the plurality of premix tube orifices, wherein each of the plurality of premix tube orifices is configured to receive fuel and to provide fuel received to each respective one of the plurality of premix tubes;
a fuel source configured to supply a first fuel portion to the center tube via the plurality of center tube orifices and a second fuel portion to each of the plurality of premix tubes via the plurality of premix tube orifices;
and
a pilot for igniting air and fuel mixtures,
wherein the first air portion mixes with the first fuel portion in the center tube to form a fuel rich center tube air and fuel mixture that travels through the center tube toward the center tube burner end opening and longitudinally past the pilot so as to be ignited by the pilot to produce a fuel rich center flame, and
wherein the second air portion mixes with the second fuel portion in each of the premix tubes to form a fuel lean premix tube air and gaseous fuel mixture that travels through the premix tube toward the premix tube burner end opening and longitudinally past the pilot so as to be ignited by the center flame to produce a fuel lean mixture flame.

8 more elements

A method of operating a burner assembly to product a low NOx flame, the method comprising the steps of:

providing a burner assembly comprising:
a blast tube having a longitudinal axis and having a blast tube end;
a blower;
a center tube disposed within the blast tube, oriented substantially parallel to the longitudinal axis, and terminating at a center tube burner end opening located proximate the blast tube end, wherein the center tube is in fluid communication with the blast tube;
a plurality of premix tubes disposed within the blast tube and encircling the center tube, each premix tube oriented substantially parallel to the longitudinal axis and terminating at a premix tube burner end opening located proximate the blast tube end, wherein each of the plurality of premix tubes is in fluid communication with the blast tube;
a plurality of center tube orifices provided in the center tube at a first longitudinal position along the longitudinal axis;
a plurality of premix tube orifices provided in each of the plurality of premix tubes and located at a second longitudinal position along the longitudinal axis that is upstream of the plurality of center tube orifices such that the center tube orifices are longitudinally located between the blast tube end and the plurality of premix tube orifices;
a fuel source;
and
a pilot;
with the blower, supplying air to the blast tube;
with the center tube, receiving a first air portion of the air supplied by the blower;
with each of the plurality of premix tubes, receiving a second air portion of the air supplied by the blower;
with the fuel source, providing a first fuel portion to the center tube;
with the center tube, via the plurality of center tube orifices, receiving the first fuel portion;
with the fuel source, providing a second fuel portion to each of the plurality of premix tubes;
with each of the plurality of premix tubes, via the plurality of premix tube orifices, receiving the second fuel portion;
in the center tube, mixing the first air portion with the first fuel portion to form a fuel rich center tube air and fuel mixture that travels through the center tube toward the center tube burner end opening and longitudinally past the pilot;
with the pilot, igniting the fuel rich center tube air and fuel mixture to produce a fuel rich center flame;
in each of the plurality of premix tubes, mixing the second air portion with the second fuel portion to form a fuel lean premix tube air and gaseous fuel mixture that travels through the premix tube toward the premix tube burner end opening and longitudinally past the pilot;
with the fuel rich center flame, igniting the fuel lean premix tube air and gaseous fuel mixtures to produce a low NOx flame.

18 more elements

Dependencies are inferred from the claim text.

Facts

Application: 16/715,372Filed 16 Dec 2019 · us provisional application
Priority: 14 Dec 2018
Published: US 2020/0191381 A118 Jun 2020
Granted: 21 Feb 2023
Term ends: Not estimatedThe source records don’t support an estimate.

Classification18 codes

F23C 1/08
Combustion apparatus specially adapted for combustion of two or more kinds of fuel simultaneously or alternately, at least one kind of fuel…
F23D 14/02
Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid: premix gas burners, i.e. in which gaseous fuel is mixed with…
F23C 3/002
Combustion apparatus characterised by the shape of the combustion chamber: the chamber having an elongated tubular form, e.g. for a radiant tube
F23C 7/008
Combustion apparatus characterised by arrangements for air supply: flow control devices