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US4019851A Expired / Lapsed US ⏱️ 0.0 years remaining

High energy arc ignitor for burner

Assignee: Combustion Engineering Inc
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Filing: 1975-09-22
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Granted: 1977-04-26
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Expires: 1995-09-22
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Abstract

Abstract A main burner oil gun in which hard to ignite liquid fuels can be burned, including an ignition means for the oil gun which will reliably light the oil gun time after time. The oil is sprayed from the oil gun tip in the shape of a hollow cone. Air is introduced surrounding the oil gun, and flows over a baffle plate located transversely of the oil gun, creating eddies of air, some of which break through the curtain of fuel issuing from the tip in a conical shape. This current of air that breaks through the fuel carries some fine droplets of fuel along with it, and forms a recirculation zone extending back to the oil gun tip. The ignition means is located within the hollow conical fuel flow, along the inner edge of the recirculation zone, so that the initial flame established is carried back to a point directly in front of the oil gun tip.

Inventors

  • 👤 Donald Arthur Smith
  • 👤 John Joseph Marshall

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 19:53
CPC Classifications
F; F23; F23C; F23C9/00; F23C9/006; F23D; F23D11/00; F23D11/36; F23D11/40; F23D2207/00

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 160 words
In combination, a first longitudinal pipe supplied with combustion air at its inlet end and open at its discharge end, a second pipe positioned axially within the first pipe, said second pipe being supplied at a first end with a hard to ignite liquid fuel, the second pipe having a tip at its second end containing fuel passages located such that the fuel is discharged in the shape of a hollow conical curtain, baffle means transverse to the second pipe and surrounding it adjacent to the tip such that eddy currents of air are formed on the downstream side thereof, some of the eddy currents breaking through the curtain of fuel and forming a recirculation zone having an inner edge inside the conical curtain flowing back to point directly in front of the tip of the second pipe, and ignition means positioned within the conical curtain and along the inner edge of the recirculation zone for igniting the liquid fuel.
Claim 2
Dependent Claim 160 words
In combination, a first longitudinal pipe supplied with combustion air at its inlet end and open at its discharge end, a second pipe positioned axially within the first pipe, said second pipe being supplied at a first end with a hard to ignite liquid fuel, the second pipe having a tip at its second end containing fuel passages located such that the fuel is discharged in the shape of a hollow conical curtain, baffle means transverse to the second pipe and surrounding it adjacent to the tip such that eddy currents of air are formed on the downstream side thereof, some of the eddy currents breaking through the curtain of fuel and forming a recirculation zone having an inner edge inside the conical curtain flowing back to point directly in front of the tip of the second pipe, and ignition means positioned within the conical curtain and along the inner edge of the recirculation zone for igniting the liquid fuel.
Claim 3
Dependent Claim 39 words
The combination set forth in claim 1, including passage means through the baffle means through which a small amount of air is introduced on the downstream side of the baffle means adjacent to the tip of the second pipe.
Claim 4
Independent Claim 125 words
The method of igniting a hard to ignite liquid fuel comprising the steps of establishing a longitudinal flow of combustion air, introducing fuel into the air flow in the shape of a hollow cone which has the same longitudinal axis as the air flow, placing a transverse baffle means in the air flow at a point longitudinally adjacent the apex of the cone, so that eddy currents of air break through the fuel cone into the center thereof, setting up a recirculation zone having an inner edge within the cone and traveling towards the apex of the cone, and positioning an ignition means along the inner edge of the recirculation zone, so that the initial flame established travels back towards the apex of the cone.
Claim 5
Independent Claim 125 words
The method of igniting a hard to ignite liquid fuel comprising the steps of establishing a longitudinal flow of combustion air, introducing fuel into the air flow in the shape of a hollow cone which has the same longitudinal axis as the air flow, placing a transverse baffle means in the air flow at a point longitudinally adjacent the apex of the cone, so that eddy currents of air break through the fuel cone into the center thereof, setting up a recirculation zone having an inner edge within the cone and traveling towards the apex of the cone, and positioning an ignition means along the inner edge of the recirculation zone, so that the initial flame established travels back towards the apex of the cone.
Claim 6
Dependent Claim 36 words
The method set forth in claim 3, including the step of introducing a small amount of air to the downstream side of the baffle means at a point closely adjacent to the apex of the cone.
Claim 7
Dependent Claim 15 words
The combination set forth in claim 1, wherein the ignition means is a spark ignitor.
Claim 8
Dependent Claim 22 words
The combination set forth in claim 5, wherein the baffle means includes a surface transverse to the flow of the combustion air.

References Cited (Backward Citations)

US1474867A Cited
US2289675A Cited
US2395614A Cited
US3003548A Cited
US3161228A Cited
US3869244A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-04-25 1980-10-25 1981-04-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-04-25 1984-10-25 1985-04-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-04-25 1988-10-25 1989-04-26 $7700.00 Window Closed / Lapsed

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