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US3637336A Expired / Lapsed US ⏱️ 0.0 years remaining

Opposed vortex combustion chamber

Assignee: Boeing North American Inc
•
Filing: 1969-12-29
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Granted: 1972-01-25
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Expires: 1989-12-29
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Abstract

Abstract A combustion chamber for burning fuel oil or the like consists of a tubular housing wherein a source of air is introduced axially along the interior walls of the chamber, the air being directed by baffles inwardly in two streams which flow in opposite circumferential directions. The counter rotating vortices intersect each other within the chamber. Fuel is introduced at some point along or near the dividing line of the vortices for uniform fuel-air mixing thereby enhancing the combustion properties of the mixture.

Inventors

  • 👤 Wallace W Velie
  • 👤 Robert D Scherer

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 17:53
CPC Classifications
F; F23; F23D; F23D11/00; F23D11/36; F23D11/40; F23D11/404

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 140 words
In a fuel burner apparatus including one or more primary fuel atomizing means, an ignition means and a tubular housing extending from said atomizing means and forming an elongated combustion chamber, the improvement which comprises; one or more longitudinal baffle means partially extending circumferentially around and spaced from the inner periphery of the housing, means adjacent said baffle means for injecting air between said baffle means and the interior periphery of said housing, and means to direct said air along the curved wall of said inner periphery of said housing inwardly into said combustion chamber in at least two oppositely directed streams from one of said partially extending baffle means, thereby forming at least a pair of impinging longitudinally extending, counterrotating vortices adjacent the axis of injection of atomized fuel from said primary fuel atomizing means into said combustion chamber.
Claim 2
Dependent Claim 140 words
In a fuel burner apparatus including one or more primary fuel atomizing means, an ignition means and a tubular housing extending from said atomizing means and forming an elongated combustion chamber, the improvement which comprises; one or more longitudinal baffle means partially extending circumferentially around and spaced from the inner periphery of the housing, means adjacent said baffle means for injecting air between said baffle means and the interior periphery of said housing, and means to direct said air along the curved wall of said inner periphery of said housing inwardly into said combustion chamber in at least two oppositely directed streams from one of said partially extending baffle means, thereby forming at least a pair of impinging longitudinally extending, counterrotating vortices adjacent the axis of injection of atomized fuel from said primary fuel atomizing means into said combustion chamber.
Claim 3
Dependent Claim 86 words
The invention as set forth in claim 1 wherein said tubular housing contains a plurality of said baffle means each of which is convex in shape and are axially aligned about the inner periphery of said housing, the exterior edges of each of said baffles defining, with said periphery, axially aligned slots between the baffle and the housing so as to direct said air through said slots along the curved wall of said inner periphery inwardly of said combustion chamber forming a plurality of counterrotating vortices.
Claim 4
Dependent Claim 67 words
The invention as set forth in claim 1 wherein each of said baffle means includes means forming a radially oriented extended slot therein adjacent the end of said baffle means opposite said atomizing means, said slot directing a portion of said air radially across the end of said combustion chamber forming a pneumatic restriction partially confining combustion products within said combustion chamber to insure more uniform combustion.
Claim 5
Dependent Claim 69 words
The invention as set forth in claim 1 in which the baffle means comprises a concave baffle plate spaced from the interior wall of said housing thereby forming at least a pair of axially aligned slots adjacent the edges of said plate to direct said air along the curved wall of said inner periphery outwardly of said slots in opposite directions forming at least a pair of counterrotating vortices.
Claim 6
Dependent Claim 34 words
The invention as set forth in claim 4 wherein the concave wall forming the baffle plate converges with the wall of said housing to form a narrowed slot to accelerate the exiting air therefrom.
Claim 7
Dependent Claim 154 words
A fuel burner apparatus including one or more primary fuel atomizing means, an injection means and a tubular housing extending from said atomizing means forming an elongated combustion chamber comprising; a plurality of longitudinal baffle means convex in shape partially extending circumferentially around and spaced from the inner periphery of the housing, and means adjacent said baffle means for injecting air between said baffle means and the inner periphery of said housing, the exterior edges of each of said convex baffles defining with said inner periphery axially aligned slots between the baffle and the housing, said air being directed through said slots along the curved wall of said inner periphery inwardly of said combustion chamber in at least two oppositely directed streams from one of said convex baffles, forming a plurality of counterrotating vortices which impinge adjacent the axis of injection of atomized fuel from said primary fuel atomizing means into said combustion chamber.
Claim 8
Dependent Claim 154 words
A fuel burner apparatus including one or more primary fuel atomizing means, an injection means and a tubular housing extending from said atomizing means forming an elongated combustion chamber comprising; a plurality of longitudinal baffle means convex in shape partially extending circumferentially around and spaced from the inner periphery of the housing, and means adjacent said baffle means for injecting air between said baffle means and the inner periphery of said housing, the exterior edges of each of said convex baffles defining with said inner periphery axially aligned slots between the baffle and the housing, said air being directed through said slots along the curved wall of said inner periphery inwardly of said combustion chamber in at least two oppositely directed streams from one of said convex baffles, forming a plurality of counterrotating vortices which impinge adjacent the axis of injection of atomized fuel from said primary fuel atomizing means into said combustion chamber.

References Cited (Backward Citations)

US2411048A Cited
US2516063A Cited
US2930194A Cited
US3306334A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-01-24 1975-07-26 1976-01-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-01-24 1979-07-26 1980-01-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-01-24 1983-07-26 1984-01-25 $7700.00 Window Closed / Lapsed

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