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US4613299A Expired / Lapsed US ⏱️ 0.0 years remaining

Device for combustion of a fuel and oxygen mixed with a part of the combustion gases formed during the combustion

Assignee: United Stirling AB and Co
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Filing: 1985-05-29
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Granted: 1986-09-23
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Expires: 2005-05-29
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Abstract

Abstract A device for combustion of a fuel with substantially pure oxygen using partial recirculation of the combustion gases which has separate ejectors suspended between discs which are in turn connected to a resiliently suspended hub.

Inventors

  • 👤 Tommy Backheim

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 11:22
CPC Classifications
F; F02; F02G; F02G1/00; F02G1/04; F02G1/043; F02G1/053; F23; F23C; F23C9/00; F02G2254/00; F02G2254/10; F23L; F23L2900/00; F23L2900/07001; Y; Y02; Y02E; Y02E20/00; Y02E20/32

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 299 words
A device for combustion of fuel admitted from a fuel supply and oxygen admitted from an oxygen supply and mixed with a part of the combustion gases formed during the combustion, said device comprising a shroud, walls defining a generally rotation-symmetrical plenum chamber within said shroud in which the combustion is completed, said walls comprising heater tubes leaving gaps between them through which the combustion gases may leave the plenum chamber, an annular chamber surrounding the plenum chamber for receiving the combustion gases, and device also comprising a fuel nozzle communicating with the fuel supply, and a plurality of ejectors surrounding, and directed toward, said fuel nozzle and using pure oxygen as driving gas for sucking in, and mixing with, a part of the combustion gas which has passed said gaps between the heater tubes, said device further comprising an oxygen supply tube communicating with said oxygen supply and attached to said shroud and extending into said chamber; a hub supported by said oxygen supply tube and having an annular oxygen supply channel in flow communication with said oxygen supply tube; a plurality of ejector support tubes, said support tubes being bent approximately 180 degrees and connected to said hub and communicating with said annular oxygen supply channel therein, said tubes also being connected to support respective ejectors at ejector ends distant said fuel nozzle, said hub being carried by said oxygen supply tube; and two disc shaped covers mounted on said hub and leaving a space between them in which said ejectors are located, the outer peripheries of said discs terminating adjacent to, and communicating with, said annular combustion gas receiving chamber downsteam of said heater tubes relative to the combustion gas flow direction, said space between said discs forming the combustion gas flow path to said ejectors.
Claim 2
Independent Claim 299 words
A device for combustion of fuel admitted from a fuel supply and oxygen admitted from an oxygen supply and mixed with a part of the combustion gases formed during the combustion, said device comprising a shroud, walls defining a generally rotation-symmetrical plenum chamber within said shroud in which the combustion is completed, said walls comprising heater tubes leaving gaps between them through which the combustion gases may leave the plenum chamber, an annular chamber surrounding the plenum chamber for receiving the combustion gases, and device also comprising a fuel nozzle communicating with the fuel supply, and a plurality of ejectors surrounding, and directed toward, said fuel nozzle and using pure oxygen as driving gas for sucking in, and mixing with, a part of the combustion gas which has passed said gaps between the heater tubes, said device further comprising an oxygen supply tube communicating with said oxygen supply and attached to said shroud and extending into said chamber; a hub supported by said oxygen supply tube and having an annular oxygen supply channel in flow communication with said oxygen supply tube; a plurality of ejector support tubes, said support tubes being bent approximately 180 degrees and connected to said hub and communicating with said annular oxygen supply channel therein, said tubes also being connected to support respective ejectors at ejector ends distant said fuel nozzle, said hub being carried by said oxygen supply tube; and two disc shaped covers mounted on said hub and leaving a space between them in which said ejectors are located, the outer peripheries of said discs terminating adjacent to, and communicating with, said annular combustion gas receiving chamber downsteam of said heater tubes relative to the combustion gas flow direction, said space between said discs forming the combustion gas flow path to said ejectors.
Claim 3
Dependent Claim 25 words
The device according to claim 1 characterized in that the ends of said ejectors remote from the tubes are additionally vertically positioned by said hub.
Claim 4
Dependent Claim 38 words
The device according to claim 1 wherein said fuel nozzle is connected to said shroud by a flexible fuel tube, and wherein said hub is horizontally positioned by said fuel nozzle extending through an opening in said hub.
Claim 5
Dependent Claim 23 words
The device according to claim 1 wherein the outer peripheries of said disc shaped covers are guided in part by said heater tubes.
Claim 6
Dependent Claim 35 words
The device according to claim 1 further comprising a heater plug retractably insertable into said plenum chamber for initiating combustion in said device, wherein said hub includes an aperture for receiving said inserted heater plug.
Claim 7
Dependent Claim 22 words
The device according to claim 1 wherein said oxygen supply tube is bent to render it flexible to accommodate thermally induced stresses.
Claim 8
Dependent Claim 26 words
The device according to claim 1 wherein said hub includes a central bore into which said fuel and said mixed oxygen and combustion gas are delivered.

References Cited (Backward Citations)

US762129A Cited
US2110209A Cited
US3869244A Cited
US4277942A Cited
US4287857A Cited
US4345426A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-09-22 1990-03-24 1990-09-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-09-22 1994-03-24 1994-09-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-09-22 1998-03-24 1998-09-23 $7700.00 Window Closed / Lapsed

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