US20170074509A1 - Hydrocarbon Burner - Google Patents

Hydrocarbon Burner Download PDF

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Publication number
US20170074509A1
US20170074509A1 US15/262,686 US201615262686A US2017074509A1 US 20170074509 A1 US20170074509 A1 US 20170074509A1 US 201615262686 A US201615262686 A US 201615262686A US 2017074509 A1 US2017074509 A1 US 2017074509A1
Authority
US
United States
Prior art keywords
burner
perforated
hydrocarbon
air supply
tube
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US15/262,686
Inventor
Donald Allen Camp
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Green Air Burner Systems LLC
Original Assignee
Green Air Burner Systems LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Green Air Burner Systems LLC filed Critical Green Air Burner Systems LLC
Priority to US15/262,686 priority Critical patent/US20170074509A1/en
Assigned to Green Air Burner Systems, LLC reassignment Green Air Burner Systems, LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CAMP, DONALD ALLEN, MR
Publication of US20170074509A1 publication Critical patent/US20170074509A1/en
Abandoned legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details
    • F23D14/62Mixing devices; Mixing tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners
    • F23D2203/10Flame diffusing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners
    • F23D2203/10Flame diffusing means
    • F23D2203/102Flame diffusing means using perforated plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/14Special features of gas burners
    • F23D2900/14641Special features of gas burners with gas distribution manifolds or bars provided with a plurality of nozzles

Definitions

  • the field of the embodiments is hydrocarbon burners. More specifically, the devices at which the combustion process takes place.
  • the embodiments of the Hydrocarbon Burner are comprised of a fuel supply connection, an air supply 90-degree connector, an air supply support tube, a perforated air supply tube, an air supply connector, fuel supply connection, a support angle, an intake manifold, a support plate, two side perforated burner tubes, a middle perforated burner tube, two side plates, and a manifold.
  • the Hydrocarbon Burner can be used in oil field, gas field, landfill, and coal field off-gas combustion.
  • FIG. 1 is a perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 2 is an exploded view of an embodiment of the Hydrocarbon Burner.
  • FIG. 3 is a front perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 4 is a top perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 5 is a bottom perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 6 is a top view of an embodiment of the Hydrocarbon Burner.
  • FIG. 7 is a sectional view of an embodiment of the Hydrocarbon Burner.
  • FIG. 8 is a sectional view of an embodiment of the Hydrocarbon Burner focusing on the air inlet pipe.
  • FIG. 9 is a side view of an embodiment of the Hydrocarbon Burner.
  • FIG. 10 is a side view of an embodiment of the Hydrocarbon Burner.
  • FIG. 11A is a side view of another embodiment of the Hydrocarbon burner showing the arrangement of the air supply air tube within a perforated burner tube
  • FIG. 11B is a sectional view of another embodiment of the Hydrocarbon Burner showing the arrangement of the air supply air tube within a perforated burner tube.
  • the embodiments of the Hydrocarbon Burner 100 are comprised of a fuel supply connection, 108 , an air supply 90-degree connector 112 , an air supply support tube 111 , a perforated air supply tube 110 , an air supply connector 109 , fuel supply connection 108 , one or more support angles 107 , an intake manifold 106 , a support plate 105 , two side perforated burner tubes 103 , a middle perforated burner tube 104 , two side plates 102 , and an end manifold 101 .
  • the hydrocarbon fuel enters the intake manifold 106 via the fuel supply connection 108 .
  • Fuel flows from the intake manifold 106 into a plurality of perforated burner tubes 103 , 104 .
  • Air enters the Hydrocarbon Burner through an air supply 90-degree connector 112 and into the perforated air supply tube 110 . Air then leaves the perforated air supply air tube 110 and mixes with the hydrocarbon fuel as it enters the intake manifold. Air and fuel continue to mix within the intake manifold 106 .
  • the air fuel mixture enters the perforated burner tubes 103 , 104 and the combustion process begins as it exits the perforations on the perforated burner tubes 103 , 104 .
  • the perforated air supply tube 110 is fabricated from a highly heat conducting material.
  • the perforated air supply tube 110 is fabricated from copper or copper alloy material to facilitate heat transfer.
  • the perforated air supply tube 110 is fitted within the air supply connector 109 and the air supply support tube 111 in part to maintain a thermal connection to the outside surfaces of the Hydrocarbon Burner to facilitate heat transfer.
  • the 1 ⁇ 4′′ coupling is a 1 ⁇ 4′′ tank flange. Further, in another embodiment of the Hydrocarbon Burner, there will not be a short nipple or a coupling coming out of the top of tank flange rather there will be a plastic plug that holds the aspirator inside the burner until it is ready to be installed.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

The embodiments of the Hydrocarbon Burner are comprised of a fuel supply connection, an air supply 90-degree connector, an air supply support tube, a perforated air supply tube, an air supply connector, fuel supply connection, a support angle, an intake manifold, a support plate, two side perforated burner tubes, a middle perforated burner tube, two side plates, and a manifold.

Description

    STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
  • Not applicable
  • FIELD OF THE EMBODIMENTS
  • The field of the embodiments is hydrocarbon burners. More specifically, the devices at which the combustion process takes place.
  • BACKGROUND OF THE EMBODIMENTS
  • There are numerous instances in industrial practice that requires the combustion of hydrocarbons to meet a variety of goals. Those goals include energy production and hydrocarbon destruction. Efficient burners are a key component in these combustion systems. Many burners in practice today do not rely on efficient processes to meet the overall combustion goals. The embodiments of the instant invention are designed to meet those goals.
  • SUMMARY OF THE EMBODIMENTS
  • The embodiments of the Hydrocarbon Burner are comprised of a fuel supply connection, an air supply 90-degree connector, an air supply support tube, a perforated air supply tube, an air supply connector, fuel supply connection, a support angle, an intake manifold, a support plate, two side perforated burner tubes, a middle perforated burner tube, two side plates, and a manifold. The Hydrocarbon Burner can be used in oil field, gas field, landfill, and coal field off-gas combustion.
  • There has thus been outlined, rather broadly, the more important features of the embodiments of the Hydrocarbon Burner in order that the detailed description thereof that follows may be better understood, and in order that the present contribution to the art may be better appreciated. There are, of course, additional features of the embodiments that will be described hereinafter and which will form the subject matter of the claims appended hereto.
  • In this respect, before explaining at least one embodiment of the embodiments in detail, it is to be understood that the embodiment is not limited in this application to the details of construction and to the arrangements of the components set forth in the following description or illustrated in the drawings. The embodiment or embodiments are capable of other embodiments and of being practiced and carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein are for the purpose of description and should not be regarded as limiting. As such, those skilled in the art will appreciate that the conception, upon which this disclosure is based, may readily be used as a basis for the designing of other structures, methods and systems for carrying out the several purposes of the embodiments. Additional benefits and advantages of the embodiments will become apparent in those skilled in the art to which the present embodiments relate from the subsequent description of the preferred embodiment and the appended claims, taken in conjunction with the accompanying drawings. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the embodiments.
  • Further, the purpose of the foregoing abstract is to enable the U.S. Patent and Trademark Office and the public generally, and especially the scientist, engineers and practitioners in the art who are not familiar with patent or legal terms or phraseology, to determine quickly from a cursory inspection the nature and essence of the technical disclosure of the application. The abstract is neither intended to define the embodiments of the application which is measured by the claims, nor is it intended to be limiting as to the scope of the embodiments in any way.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 2 is an exploded view of an embodiment of the Hydrocarbon Burner.
  • FIG. 3 is a front perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 4 is a top perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 5 is a bottom perspective view of an embodiment of the Hydrocarbon Burner.
  • FIG. 6 is a top view of an embodiment of the Hydrocarbon Burner.
  • FIG. 7 is a sectional view of an embodiment of the Hydrocarbon Burner.
  • FIG. 8 is a sectional view of an embodiment of the Hydrocarbon Burner focusing on the air inlet pipe.
  • FIG. 9 is a side view of an embodiment of the Hydrocarbon Burner.
  • FIG. 10 is a side view of an embodiment of the Hydrocarbon Burner.
  • FIG. 11A is a side view of another embodiment of the Hydrocarbon burner showing the arrangement of the air supply air tube within a perforated burner tube; FIG. 11B is a sectional view of another embodiment of the Hydrocarbon Burner showing the arrangement of the air supply air tube within a perforated burner tube.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • The embodiments of the Hydrocarbon Burner 100 are comprised of a fuel supply connection, 108, an air supply 90-degree connector 112, an air supply support tube 111, a perforated air supply tube 110, an air supply connector 109, fuel supply connection 108, one or more support angles 107, an intake manifold 106, a support plate 105, two side perforated burner tubes 103, a middle perforated burner tube 104, two side plates 102, and an end manifold 101.
  • The hydrocarbon fuel enters the intake manifold 106 via the fuel supply connection 108. Fuel flows from the intake manifold 106 into a plurality of perforated burner tubes 103, 104. In one embodiment of the Hydrocarbon Burner there are three perforated burner tubes, a middle perforated burner tube 104 and two side perforated burner tubes 103. Air enters the Hydrocarbon Burner through an air supply 90-degree connector 112 and into the perforated air supply tube 110. Air then leaves the perforated air supply air tube 110 and mixes with the hydrocarbon fuel as it enters the intake manifold. Air and fuel continue to mix within the intake manifold 106. The air fuel mixture enters the perforated burner tubes 103, 104 and the combustion process begins as it exits the perforations on the perforated burner tubes 103, 104.
  • The perforated air supply tube 110 is fabricated from a highly heat conducting material. In one preferred embodiment, the perforated air supply tube 110 is fabricated from copper or copper alloy material to facilitate heat transfer. The perforated air supply tube 110 is fitted within the air supply connector 109 and the air supply support tube 111 in part to maintain a thermal connection to the outside surfaces of the Hydrocarbon Burner to facilitate heat transfer.
  • In another embodiment of the Hydrocarbon Burner, the ¼″ coupling is a ¼″ tank flange. Further, in another embodiment of the Hydrocarbon Burner, there will not be a short nipple or a coupling coming out of the top of tank flange rather there will be a plastic plug that holds the aspirator inside the burner until it is ready to be installed.

Claims (7)

What is claimed is:
1. A hydrocarbon burner comprising a fuel supply connection, an air supply 90-degree connector, an air supply support tube, a perforated air supply tube, an air supply connector, fuel supply connection, a support angle, an intake manifold, a support plate, two side perforated burner tubes, a middle perforated burner tube, two side plates, and a manifold.
2. A hydrocarbon burner described in claim 1 wherein the hydrocarbon fuel enters the intake manifold via the fuel supply connection and wherein fuel flows from the intake manifold (106) into a plurality of perforated burner tubes (103, 104)
3. A hydrocarbon burner described in claim 2 comprising three perforated burner tubes, a middle perforated burner tube (104) and two side perforated burner tubes (103).
4. A hydrocarbon burner described in claim 2 wherein air enters the hydrocarbon burner through an air supply 90-degree connector and into the perforated air supply tube (110).
5. A hydrocarbon burner described in claim 2 wherein air leaves the perforated air supply air tube and mixes with the hydrocarbon fuel as it enters the intake manifold.
6. A hydrocarbon burner described in claim 2 wherein air and fuel continue to mix within the intake manifold.
7. A hydrocarbon burner described in claim 2 wherein the air fuel mixture enters the perforated burner tubes and the combustion process begins as it exits the perforations on the perforated burner tubes.
US15/262,686 2015-09-11 2016-09-12 Hydrocarbon Burner Abandoned US20170074509A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US15/262,686 US20170074509A1 (en) 2015-09-11 2016-09-12 Hydrocarbon Burner

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201562217776P 2015-09-11 2015-09-11
US15/262,686 US20170074509A1 (en) 2015-09-11 2016-09-12 Hydrocarbon Burner

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US15/262,686 Abandoned US20170074509A1 (en) 2015-09-11 2016-09-12 Hydrocarbon Burner

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114034043A (en) * 2021-11-23 2022-02-11 中国科学院大连化学物理研究所 Gas and air gas mixing structure and combustor

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US860192A (en) * 1906-02-26 1907-07-16 Ind Alcohol Heat And Light Company Hydrocarbon-burner.
US1517394A (en) * 1923-02-03 1924-12-02 Hjalmer Swanson Gas burner
US1940226A (en) * 1932-05-11 1933-12-19 Ingersoll Rand Co Carburetor
US3042499A (en) * 1958-09-29 1962-07-03 John E Morris Burner-muffler
US3399024A (en) * 1966-08-09 1968-08-27 Robertshaw Controls Co Burner construction and the like
US3540258A (en) * 1966-08-09 1970-11-17 Robertshaw Controls Co Burner construction and method and apparatus for making the same and the like
US3545698A (en) * 1968-07-30 1970-12-08 Koppers Co Inc Method and apparatus for preventing the collapse of a spool of filament reinforcements
US3721239A (en) * 1969-07-09 1973-03-20 R Myers Anesthetic gas exhaust system
US3897198A (en) * 1972-04-17 1975-07-29 Radiation Ltd Gaseous fuel burners
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US4189297A (en) * 1977-10-26 1980-02-19 Slyman Manufacturing Corporation Matrix mounting means for gas burners
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US5240411A (en) * 1992-02-10 1993-08-31 Mor-Flo Industries, Inc. Atmospheric gas burner assembly
JPH06272825A (en) * 1993-03-16 1994-09-27 Aisin Seiki Co Ltd High temperature heat radiation body
JPH0771723A (en) * 1993-08-31 1995-03-17 Sanyo Electric Co Ltd Combustion device
US5743727A (en) * 1997-01-21 1998-04-28 Burner Systems International, Inc. Premixed gas burner
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US7523603B2 (en) * 2003-01-22 2009-04-28 Vast Power Portfolio, Llc Trifluid reactor
US20090188484A1 (en) * 2008-01-18 2009-07-30 Roberto Nevarez Open Loop Gas Burner
US20090226852A1 (en) * 2008-03-07 2009-09-10 Feese James J Premix lean burner
US20100291501A1 (en) * 2007-05-15 2010-11-18 3Force B.V. Burner system having premixed burners and flame transfer means
US20100316965A1 (en) * 2007-12-19 2010-12-16 Joseph Le Mer Device and method for stabilizing the pressure and the flow of a gaseous mixture supplied to a surface-combustion cylindrical burner
US8197251B2 (en) * 2007-12-17 2012-06-12 Bekaert Combustion Technology B.V. Premix burner
US20120178034A1 (en) * 2011-01-12 2012-07-12 Lynx Grills, Inc. Barbeque radiant burner
US20130035531A1 (en) * 2011-08-02 2013-02-07 Basf Se Reactor for carrying out an autothermal gas-phase dehydrogenation
JP2014126278A (en) * 2012-12-26 2014-07-07 Mitsubishi Heavy Ind Ltd Combustion burner and pressurized gasification furnace
US20140251302A1 (en) * 2013-03-05 2014-09-11 Char-Broil, Llc Thin Profile Multi-Manifold Multi-Tube Burner for Gas Grills
US20150290597A1 (en) * 2014-04-09 2015-10-15 Therapeutic Proteins International, LLC Aeration device for bioreactors
JP2019167621A (en) * 2018-03-23 2019-10-03 日本製鉄株式会社 α + β TYPE TITANIUM ALLOY EXTRUSION SHAPE

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* Cited by examiner, † Cited by third party
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US20090188484A1 (en) * 2008-01-18 2009-07-30 Roberto Nevarez Open Loop Gas Burner
US20090226852A1 (en) * 2008-03-07 2009-09-10 Feese James J Premix lean burner
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US20180228316A1 (en) * 2013-03-05 2018-08-16 Char-Broil, Llc Thin profile multi-tube burner for gas grill
US20150290597A1 (en) * 2014-04-09 2015-10-15 Therapeutic Proteins International, LLC Aeration device for bioreactors
JP2019167621A (en) * 2018-03-23 2019-10-03 日本製鉄株式会社 α + β TYPE TITANIUM ALLOY EXTRUSION SHAPE

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114034043A (en) * 2021-11-23 2022-02-11 中国科学院大连化学物理研究所 Gas and air gas mixing structure and combustor

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