Burner construction
AssigneeZwick Energy Research Organization, Inc.
InventorsEugene B. Zwick, Dung D. Nguyen, William D. Brigham, Kenneth Hoffman
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AssigneeZwick Energy Research Organization, Inc.
InventorsEugene B. Zwick, Dung D. Nguyen, William D. Brigham, Kenneth Hoffman
Estimating the term…
A burner having a burner body in which combustion air is injected in an air flow pattern which establishes a relatively stagnant air region positioned within the flow of combustion air. A pilot flame injector is positioned to generate a pilot flame extending into the stagnant air region. The pilot flame can, thus, be maintained during the operation of the burner because the stable air conditions within the stagnant air region minimize disruption of the pilot flame by the flow of combustion air. A method for maintaining a uniform pilot flame within a burner operating over a range of combustion air flow rates by introducing combustion air into the burner and providing the combustion air with a flow configuration that establishes a stagnant air zone within the burner that is relatively independent of the flow rate of the combustion air. The pilot flame is then positioned within the stagnant air zone. An injector for feeding finely divided fuel to a burner. The injector includes means to provide an annular passage through which air may flow at high velocity for discharge into a burner. Means are provided to feed fuel into the annular passage such that the fuel may be broken up into minute droplets by the air flow through the passage. Additionally the means to feed fuel are positioned to minimize contact between the fuel and the passage surfaces. Thus, the fuel may be broken up into minute droplets within the air flow stream with the finely divided fuel being discharged into a burner.
A fuel burner comprising means forming a burner chamber of cylindrical shape and defining a burner axis therein, said chamber having an inlet opening at one end and including a peripheral cylindrical wall extending from one end to the other and displaced from said axis by a predetermined radial dimension, means forming a vortex box disposed in coupled relation to said inlet opening for introducing combustion air into said body and along said axis, said vortex box having a plurality of internal vanes arranged in a circle surrounding said axis and radially tilted thereto for imparting spiral flow to air passing through and along the axis of said burner, port means coupling said vortex box to said chamber and having a radial dimension from the axis which is less than the radial dimension of said burner wall, said coupling means and burner wall being constructed and arranged to form an expansion step for combustion air flowing therebetween so that a flow pattern through the burner is established in which combustion air is introduced through said inlet in an axial direction to produce a swirling air flow about said axis and along a generally cylindrically annular combustion zone, the combustion air moving forwardly and outwardly as it passes past the step and through said zone, a portion thereof recirculating by moving in a rearward direction along the axis of the burner and towards the inlet opening and vortex box to produce a secondary flow in opposition to the general flow of combustion air therethrough to thereby establish a stagnant air region at the inlet to said burner which region remains relatively constant with respect to the overall flow rate of combustion air therethrough, pilot injector means for injecting a limited quantity of liquid fuel into said stagnant region and directed along the axis of said chamber, said fuel being ignited therein to form a stable pilot flame for said burner, main fuel injector means for injecting finely divided liquid fuel generally along said burner axis and into the region of said combustion zone, said injector means being constructed and arranged to limit the injected liquid to a region bounded by a cylindrical surface surrounding said stagnant zone and extending radially therefrom to said main fuel injector means.
A fuel burner comprising means forming a burning chamber of cylindrical shape and defining a burner axis therein, said chamber having an inlet opening at one end and including a peripheral cylindrical wall extending from one end to the other and displaced from said axis by a predetermined radial dimension means forming a vortex box disposed in coupled relation to said inlet opening for introducing combustion air into said body and along said axis, having a back wall spaced away from said inlet opening and having a plurality of internal vanes arranged in a circle surrounding said axis and radially tilted thereto for imparting spiral flow to air passing through and along the axis of said burner, port means coupling said vortex box to said chamber and having a radial dimension from the axis which is less than the radial dimension of said burner wall, said coupling means and burner wall being constructed and arranged to form an expansion step for combustion air flowing therebetween, so that a flow pattern through the burner is established in which combustion air is introduced through said inlet in an axial direction to produce a swirling air flow about said axis and along a generally cylindrical annular combustion zone, the combustion air moving forwardly and outwardly as it passes past the step and through said zone, a portion thereof recirculating by moving in a rearward direction along the axis of the burner and towards the inlet opening and vortex box to produce a secondary flow in opposition to the general flow of combustion air therethrough to thereby establish a stagnant air region at the inlet to said burner which region remains relatively constant with respect to the overall flow rate of combustion air therethrough, pilot injector means comprising a nozzle mounted to discharge fuel immediately adjacent to said back wall for injecting a limited quantity of liquid fuel into said stagnant region and directed along the axis of said chamber, said fuel being ignited therein to form a stable pilot flame for said burner, main fuel injector means for injecting finely divided liquid fuel generally along said burner axis and into the region of said combustion zone, a plurality of nozzles disposed along an annular ring surrounding said pilot injector means and having outlet orifices located substantially proximate to said back wall, said injector means being constructed and arranged to limit the injection to a region bounded by a cylindrical surface surrounding said stagnant zone and extending radially therefrom to said main fuel injector means and a conical surface intersecting the main fuel injector means and passing adjacent said port means.
Dependencies are inferred from the claim text.