US20210048194A1 - Low consumption assisted flare apparatus and method - Google Patents
Low consumption assisted flare apparatus and method Download PDFInfo
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- US20210048194A1 US20210048194A1 US16/540,355 US201916540355A US2021048194A1 US 20210048194 A1 US20210048194 A1 US 20210048194A1 US 201916540355 A US201916540355 A US 201916540355A US 2021048194 A1 US2021048194 A1 US 2021048194A1
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- inner conduit
- conduit
- longitudinal end
- flare
- venturi
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- 238000000034 method Methods 0.000 title claims abstract description 15
- 230000000712 assembly Effects 0.000 claims abstract description 12
- 238000000429 assembly Methods 0.000 claims abstract description 12
- 238000002347 injection Methods 0.000 claims description 13
- 239000007924 injection Substances 0.000 claims description 13
- 230000001965 increasing effect Effects 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 2
- 239000012530 fluid Substances 0.000 claims description 2
- 238000010793 Steam injection (oil industry) Methods 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 abstract description 20
- 239000007789 gas Substances 0.000 description 24
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 7
- 239000000203 mixture Substances 0.000 description 5
- 239000000446 fuel Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000000779 smoke Substances 0.000 description 4
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 239000002912 waste gas Substances 0.000 description 2
- 241000239290 Araneae Species 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- -1 petrochemical Substances 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000004227 thermal cracking Methods 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G7/00—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
- F23G7/06—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
- F23G7/08—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases using flares, e.g. in stacks
- F23G7/085—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases using flares, e.g. in stacks in stacks
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
- F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L17/00—Inducing draught; Tops for chimneys or ventilating shafts; Terminals for flues
- F23L17/16—Induction apparatus, e.g. steam jet, acting on combustion products beyond the fire
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
- F23L7/002—Supplying water
- F23L7/005—Evaporated water; Steam
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2203/00—Gaseous fuel burners
- F23D2203/007—Mixing tubes, air supply regulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/14—Special features of gas burners
- F23D2900/14681—Adding steam or water vapor to primary or secondary combustion air
Definitions
- the present invention relates to flare apparatuses and methods in which steam or other entrainment media is injected to (i) induce additional air into the flare combustion zone, (ii) create turbulence which enhances mixing and improves combustion efficiency, (iii) inhibit smoke generation, and (iv) provide reduced emissions.
- Flare systems are used in many applications to burn off fuels, waste gases, and other gases that can be harmful if vented to the atmosphere without burning. Flare systems are widely used in the refining, chemical, petrochemical, petroleum production, and other industries for burning flammable and/or toxic materials which are released due to upset or startup conditions, or which are released simply as a result of the process itself.
- flares are comprised of a pipe with a flame stabilization device at the top thereof. Flare gas flows through the pipe and burns at the stabilization device. However, when the flow of flare gas becomes too great for the amount of air that will naturally mix with the flare gas at the combustion zone, the combustion of the flare gas occurs under sub-stoichiometric conditions. When the flare gas is burned under sub-stoichiometric conditions, smoke will typically be produced. Smoke produced by flare systems contributes to smog. In addition, the combustion of the flare gas under sub-stoichiometric conditions produces atmospheric emissions such as: nitrogen oxides (NO x ); carbon monoxide (CO); unburned hydrocarbon emissions (UHC's); and particulates (PM10).
- NO x nitrogen oxides
- CO carbon monoxide
- UHC's unburned hydrocarbon emissions
- PM10 particulates
- steam-assisted flare assemblies have been used in which steam is injected (i) into the flare gas stream flowing upwardly through the flare stack, (ii) around the upper end of the stack, and/or (iii) into one or more tubes within the flare stack.
- the injected steam can operate to: induce additional air into the combustion mixture; create increased turbulence for better mixing; lower the combustion flame temperature for reduced NO x emissions and less thermal cracking; shape the combustion flame; cool the flare tip; and/or reduce noise.
- venturi structures are used in one or more flare tip nozzle assemblies to increase the amount of air which is inducted into the flare combustion zone.
- the inventive apparatus and method are well suited for use in elevated flares, but can also be used in enclosed flares and other types of flare systems.
- an apparatus for combusting a flare gas comprising one or more flare nozzle assemblies.
- Each of the flare nozzle assemblies preferably comprises: (i) an outer conduit having a longitudinal axis, a rearward longitudinal end, and a forward longitudinal end and (ii) an inner conduit for a flow of an entrainment media and air.
- the inner conduit preferably comprises: an inlet opening at a rearward longitudinal end of the inner conduit; a discharge opening at a forward longitudinal end of the inner conduit; a longitudinally extending straight venturi section having a substantially constant interior cross-sectional area; and a longitudinally extending diverging venturi section which increases in interior cross-sectional area as the diverging venturi section extends forwardly from a forward longitudinal end of the straight venturi section.
- Each flare nozzle assembly also preferably comprises an injection structure positioned outside of the inlet opening of the inner conduit for injecting the entrainment media into the inlet opening of the inner conduit.
- each nozzle assembly preferably extends into the rearward longitudinal end of the outer conduit such that (i) the rearward longitudinal end of the inner conduit is positioned outside of the rearward longitudinal end of the outer conduit and (ii) the discharge opening of the inner conduit is positioned substantially at the forward longitudinal end of the outer conduit.
- a longitudinally extending flow annulus for the flare gas is formed in the outer conduit between the interior surface of the outer conduit the exterior of the inner conduit.
- the longitudinally extending flow annulus (i) laterally surrounds the longitudinal axis of the outer conduit, (ii) has an inlet opening at the rearward longitudinal end of the outer conduit for receiving the flare gas, and (iii) has a discharge opening for the flare gas at the forward longitudinal end of the outer conduit.
- a method of combusting a flare gas which preferably comprises the steps of: (a) delivering the flare gas upwardly through an annulus between an inner surface of an outer conduit and an exterior of an inner conduit, the inner conduit extending upwardly into a lower end of the outer conduit, the annulus having a discharge opening at an upper end of the outer conduit, the inner conduit having a discharge opening substantially at the upper end of the outer conduit, and the inner conduit having an inlet opening at a lower end of the inner conduit which is positioned outside of and spaced downwardly from the lower end of the outer conduit; (b) injecting an entrainment media into the inlet opening of the inner conduit from an injection structure which is spaced downwardly from the inlet opening of the inner conduit so that the entrainment media inducts an amount of air into the inner conduit as the entrainment media travels through a gap between the injection structure and the inlet opening of the inner conduit; and (c) increasing the amount of air inducted into the inner conduit by the entrainment media in
- the venturi structure comprises (i) an upwardly extending straight venturi section of the inner conduit having a substantially constant interior cross-sectional area followed by (ii) a diverging venturi section of the inner conduit which increases in interior cross-sectional area as it extends upwardly from the straight venturi section.
- FIG. 1 is an elevational side view illustrating an embodiment 2 of the flare apparatus provided by the present invention.
- FIG. 2 is an elevational side view of a portion of the inventive flare apparatus 2 illustrating a flare tip nozzle assembly 8 used in the inventive flare apparatus 2 .
- FIG. 3 is an elevational view of an inner conduit 15 used in the inventive flare apparatus 2 .
- FIGS. 1-3 An embodiment 2 of the flare apparatus provided by the present invention is illustrated in FIGS. 1-3 .
- the inventive flare apparatus 2 comprises a plenum 4 on the upper end of a flare stack 6 .
- a flare gas is delivered to the plenum 4 through the flare stack 6 .
- the inventive flare apparatus 2 further comprises one or more (preferably a plurality) of flare tip nozzle assemblies 8 which receive the flare gas from the plenum 4 and discharge the flare gas from the upper (or forward) ends 10 of the nozzle assemblies 8 for combustion.
- the term “flare gas” can refer to any type of single or two phase fuel, waste gas, or other stream from a plant, refinery, oil or gas production site, or other source which is suitable for combustion in a flare system.
- Each of the one or more flare tip nozzle assemblies 8 of the inventive apparatus 2 preferably comprises: an outer conduit 14 ; an inner conduit 15 ; a flow annulus 16 for the flare gas which is formed between the inner surface 18 of the outer conduit 14 and the exterior surface 20 of the inner conduit 15 ; an injection structure 22 for injecting steam or other entrainment media into the lower (or rearward) longitudinal end 26 of the inner conduit 15 ; and an exterior clean-up ring or assembly 28 positioned around the upper (or forward) longitudinal end 30 of the outer conduit 14 .
- the outer conduit 14 of each nozzle assembly 2 comprises; a longitudinal axis 32 ; a longitudinally extending outer wall 34 which surrounds the longitudinal axis 32 ; an inlet opening 36 at the lower (or rearward) longitudinal end 38 of the outer conduit 14 ; and a discharge opening 40 at the upper (or forward) longitudinal end 30 of the outer conduit 14 .
- the flow annulus 16 formed between the inner surface 18 of the outer conduit 14 and the exterior 20 of the inner conduit 15 also surrounds the longitudinal axis 32 of the outer conduit and extends longitudinally from the lower longitudinal end 38 to the upper longitudinal end 30 of the outer conduit 14 .
- the flow annulus 16 has an inlet opening 42 at the lower longitudinal end 38 of the outer conduit 14 and a discharge opening 44 at the upper longitudinal end 30 of the outer conduit 14 .
- the outer conduit 14 is preferably cylindrical but can alternatively have an elliptical, oval, rectangular, square, triangular or other cross-sectional shape.
- the interior of the outer conduit 14 will preferably have a substantial constant interior cross-sectional area along its entire length, it will be understood that the entire length or any portion of the longitudinal length of the interior surface 18 of the outer conduit 14 can alternatively have a converging or diverging shape.
- each nozzle assembly 8 is connected to the plenum 4 in a manner which places the inlet opening 42 of the nozzle flow annulus 16 in fluid communication with the interior 46 of the plenum 4 .
- the lower end 38 of the outer conduit 14 is connected to the upper wall 48 of the plenum 4 such that the inlet opening 42 of the flow annulus 16 is positioned over a flow opening 50 formed through the upper wall 48 .
- a lower portion of the outer conduit 14 can extend through an opening in the upper wall 48 of the plenum 4 such that the lower end 38 of the outer conduit 14 and the inlet opening 42 of the flow annulus 16 would be located inside the interior 46 of the plenum 4 .
- the upper wall 48 of the plenum 4 can be flat, outwardly dished, or have any other shape.
- each nozzle assembly 8 extends upwardly (or forwardly) through the lower wall 51 of the plenum 4 and into the lower end 38 of the outer conduit 14 such that (a) the upper (or forward) longitudinal end 52 of the inner conduit 14 is located substantially at (i.e., preferably within ⁇ 40 inches of, more preferably within ⁇ 30 inches of, more preferably within ⁇ 20 inches of, more preferably within 10 inches of, more preferably within ⁇ 5 inches of, more preferably within ⁇ 2.5 inches of, more preferably within ⁇ +1 inch of, and most preferably at) the upper longitudinal end 30 of the outer conduit 14 , (b) the lower (or rearward) longitudinal end 26 of the inner conduit 15 is located outside of and spaced downwardly (or rearwardly) from the lower longitudinal end 38 of the outer conduit 14 , and (c) the inlet opening 56 at the lower end 26 of the inner conduit 15 is located outside of the plenum 4 .
- the lower wall 51 of the plenum can be flat, outwardly dished, or have any other
- the inner conduit 15 of each nozzle assembly 8 is configured such that at least a lower portion of the inner conduit 15 is in the form of a venturi flow structure 58 for the steam or other entrainment media which is injected into the lower end 26 of the inner conduit 15 .
- the flow of the steam or other entrainment media through the venturi flow structure 58 of the inner conduit 15 operates to further reduce the pressure at the lower inlet opening 56 of the inner conduit 15 so that, as compared to an entirely straight inner conduit design with no venturi flow, significantly more air is inducted by the entrainment media into the inner conduit 15 .
- the venturi flow structure 58 of the inner conduit 15 preferably comprises: a venturi inlet bell structure 60 at the lower (or rearward) end 26 of the inner conduit 15 ; a straight venturi section 62 which extends upwardly (or forwardly) from the inlet bell structure 60 ; and a diverging venturi bell outlet section 64 which extends upwardly (or forwardly) from the upper or forward end of the straight section 62 .
- the interior cross-sectional flow area of the straight venturi section 62 is substantial constant along the entire length of the straight section 62 .
- the interior cross-sectional flow area of the diverging bell outlet section 64 increases as the bell outlet section 64 extends upwardly or forwardly from the straight venturi section 62 .
- the interior surface of the bell outlet section 64 preferably diverges at an angle 66 in the range of from about 5° to about 60°, more preferably from about 5° to about 45° and more preferably from about 5′ to about 30° with respect to the longitudinal axis 32 of the outer and inner conduits 14 and 15 .
- the diverging bell outlet section 64 of the venturi structure 58 can extend all of the way to the discharge opening 68 at the upper (or forward) longitudinal end 52 of the inner conduit 15 .
- the inner conduit 15 can further comprise an upper or forward discharge section 69 of substantially constant internal cross-sectional flow area which extends from the upper or forward end 65 of the diverging venturi bell outlet section 64 to the discharge opening 68 of the inner conduit 15 . If the inner conduit 15 includes an upper or forward discharge section 69 as just described, the upper or forward end 65 of the diverging bell outlet section 64 of the venturi structure 58 can be located prior to or inside the outer conduit 14 .
- the longitudinal length of the venturi flow structure 58 will preferably be at least 10%, more preferably at least 20% and more preferably at least 25%, of the entire longitudinal length of the inner conduit 15 .
- the longitudinal length of the straight venturi section 62 of the venturi flow structure 58 will preferably be at least 5%, more preferably at least 10%, of the entire length of the venturi structure 58 .
- the longitudinal length of the diverging bell outlet section 64 of the venturi structure 58 will preferably be at least 10%, more preferably at least 20% and more preferably at least 30%, of the entire length of the venturi structure 58 .
- the inner conduit 15 and each section of the venturi flow structure 58 of the inner conduit 15 will preferably have a circular cross-sectional shape such that, at least in the interior thereof, the interior surface of the straight venturi section 62 is cylindrical and the interior surface of the diverging venturi bell section 64 has a conical shape.
- the cross-section of the inner conduit 15 and of each section of the venturi structure 58 can alternatively be elliptical, oval, rectangular, square, triangular or other non-circular shape.
- the interior surface 59 of the venturi flow structure 58 can be smooth or roughened.
- the entrainment media used in the inventive apparatus and method will preferably be steam.
- examples of other types of entrainment media suitable for use in the inventive apparatus and method include, but are not limited to, carbon dioxide, air, nitrogen, or argon.
- the injection structure 22 for the entrainment media is located outside of the plenum 4 and is spaced downwardly or rearwardly apart from the inlet bell opening 56 at the lower end 26 of the inner conduit 15 so that a gap 70 is formed between the injection structure 22 and the inlet bell opening 56 of the inner conduit 15 .
- the injection structures 22 for the entrainment media can be single port tips, multi-port spiders, or other types of ejectors for supersonic, sonic, or subsonic ejection flow.
- the flare gas delivered to the plenum 4 flows upwardly or forwardly through the flow annulus 16 of each flare tip nozzle assembly 8 and is discharged for combustion from the discharge opening 44 of the flow annulus 16 at the upper or forward longitudinal end 30 of the outer conduit 14 .
- steam or other entrainment media is ejected from the injection structure 22 toward the inlet bell opening 56 at the lower or rearward end 26 of the inner conduit 15 .
- the ejected entrainment media travels through the gap 70 between the injection structure 22 and the inlet bell opening 56 , atmospheric air is entrained by the media and pulled into the inner conduit 15 .
- the venturi flow structure 58 incorporated in the inner conduit 15 of the inventive flare tip nozzle assembly 8 increases the amount of air delivered by the entrainment media into the inner conduit 15 by an amount of at least 5% (more preferably at least 10%, at least 15%, at least 20%, or at least 25%).
- the air inducted into the inner conduit 15 mixes with the entrainment media and is discharged from the discharge opening 68 of the inner conduit 15 for combustion of the inducted air with the flare gas discharged from the discharge opening 44 of the flow annulus 16 . Because the discharge opening 68 of the inner conduit 15 is located substantially at the upper or forward longitudinal end 30 of the outer conduit 14 , rather than inside the outer conduit 14 , substantially no mixing of the flare gas with the entrainment media and inducted air occurs within the outer conduit 14 , thus further reducing the pressure at the inlet opening 56 of the inner conduit 15 and causing even more air to be inducted into the inner conduit 15 .
- the exterior clean-up ring or apparatus 28 at the upper (or forward) longitudinal end 30 of the outer conduit 14 comprises a series of ejection ports, nozzles or other ejection structures which eject steam into the combustion mixture discharged from the flare tip nozzle assemble 8 .
- the steam ejected from the clean-up ring 28 operates to induct additional air into the combustion mixture and can also be used to shape the combustion flame or assist in maintaining the shape of the flame in high wind conditions.
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Abstract
Description
- The present invention relates to flare apparatuses and methods in which steam or other entrainment media is injected to (i) induce additional air into the flare combustion zone, (ii) create turbulence which enhances mixing and improves combustion efficiency, (iii) inhibit smoke generation, and (iv) provide reduced emissions.
- Flare systems are used in many applications to burn off fuels, waste gases, and other gases that can be harmful if vented to the atmosphere without burning. Flare systems are widely used in the refining, chemical, petrochemical, petroleum production, and other industries for burning flammable and/or toxic materials which are released due to upset or startup conditions, or which are released simply as a result of the process itself.
- Most utility-type flares are comprised of a pipe with a flame stabilization device at the top thereof. Flare gas flows through the pipe and burns at the stabilization device. However, when the flow of flare gas becomes too great for the amount of air that will naturally mix with the flare gas at the combustion zone, the combustion of the flare gas occurs under sub-stoichiometric conditions. When the flare gas is burned under sub-stoichiometric conditions, smoke will typically be produced. Smoke produced by flare systems contributes to smog. In addition, the combustion of the flare gas under sub-stoichiometric conditions produces atmospheric emissions such as: nitrogen oxides (NOx); carbon monoxide (CO); unburned hydrocarbon emissions (UHC's); and particulates (PM10).
- To reduce smoke production, as well as the production of harmful emissions, steam-assisted flare assemblies have been used in which steam is injected (i) into the flare gas stream flowing upwardly through the flare stack, (ii) around the upper end of the stack, and/or (iii) into one or more tubes within the flare stack. Depending upon the type and location of the injection system, the injected steam can operate to: induce additional air into the combustion mixture; create increased turbulence for better mixing; lower the combustion flame temperature for reduced NOx emissions and less thermal cracking; shape the combustion flame; cool the flare tip; and/or reduce noise.
- However, although the benefits provided by steam-assisted flare systems can be significant, the fuel costs and other costs incurred for producing and delivering the amount of high pressure steam which these systems require can also be substantial. In addition, due to the offsetting emissions which are produced as a result of the combustion of gas or liquid fuels for generating the steam used in the steam-assisted flare systems, the benefits provided by these systems for the flare combustion process are somewhat nullified.
- Consequently, a need exists for an improved assisted flare apparatus and method in which the amount of steam or other entrainment media required for inducing a desired amount of air into the flare combustion mixture to provide a smokeless operation is significantly reduced.
- The present invention satisfies the needs and alleviates the problems discussed above. In the inventive apparatus and method, venturi structures are used in one or more flare tip nozzle assemblies to increase the amount of air which is inducted into the flare combustion zone. The inventive apparatus and method are well suited for use in elevated flares, but can also be used in enclosed flares and other types of flare systems.
- In one aspect, there is provided an apparatus for combusting a flare gas comprising one or more flare nozzle assemblies. Each of the flare nozzle assemblies preferably comprises: (i) an outer conduit having a longitudinal axis, a rearward longitudinal end, and a forward longitudinal end and (ii) an inner conduit for a flow of an entrainment media and air. The inner conduit preferably comprises: an inlet opening at a rearward longitudinal end of the inner conduit; a discharge opening at a forward longitudinal end of the inner conduit; a longitudinally extending straight venturi section having a substantially constant interior cross-sectional area; and a longitudinally extending diverging venturi section which increases in interior cross-sectional area as the diverging venturi section extends forwardly from a forward longitudinal end of the straight venturi section. Each flare nozzle assembly also preferably comprises an injection structure positioned outside of the inlet opening of the inner conduit for injecting the entrainment media into the inlet opening of the inner conduit.
- The inner conduit of each nozzle assembly preferably extends into the rearward longitudinal end of the outer conduit such that (i) the rearward longitudinal end of the inner conduit is positioned outside of the rearward longitudinal end of the outer conduit and (ii) the discharge opening of the inner conduit is positioned substantially at the forward longitudinal end of the outer conduit. In addition, a longitudinally extending flow annulus for the flare gas is formed in the outer conduit between the interior surface of the outer conduit the exterior of the inner conduit. The longitudinally extending flow annulus (i) laterally surrounds the longitudinal axis of the outer conduit, (ii) has an inlet opening at the rearward longitudinal end of the outer conduit for receiving the flare gas, and (iii) has a discharge opening for the flare gas at the forward longitudinal end of the outer conduit.
- In another aspect, there is provided a method of combusting a flare gas which preferably comprises the steps of: (a) delivering the flare gas upwardly through an annulus between an inner surface of an outer conduit and an exterior of an inner conduit, the inner conduit extending upwardly into a lower end of the outer conduit, the annulus having a discharge opening at an upper end of the outer conduit, the inner conduit having a discharge opening substantially at the upper end of the outer conduit, and the inner conduit having an inlet opening at a lower end of the inner conduit which is positioned outside of and spaced downwardly from the lower end of the outer conduit; (b) injecting an entrainment media into the inlet opening of the inner conduit from an injection structure which is spaced downwardly from the inlet opening of the inner conduit so that the entrainment media inducts an amount of air into the inner conduit as the entrainment media travels through a gap between the injection structure and the inlet opening of the inner conduit; and (c) increasing the amount of air inducted into the inner conduit by the entrainment media in step (b) by delivering the entrainment media upwardly through a venturi structure, which forms at least a lower portion of the inner conduit, and out of the discharge opening of the inner conduit substantially at the upper end of the outer conduit. The venturi structure comprises (i) an upwardly extending straight venturi section of the inner conduit having a substantially constant interior cross-sectional area followed by (ii) a diverging venturi section of the inner conduit which increases in interior cross-sectional area as it extends upwardly from the straight venturi section.
- Further aspects, features, and advantages of the present invention will be apparent to those in the art upon examining the accompanying drawings and upon reading the following detailed description of the preferred embodiments.
-
FIG. 1 is an elevational side view illustrating anembodiment 2 of the flare apparatus provided by the present invention. -
FIG. 2 is an elevational side view of a portion of theinventive flare apparatus 2 illustrating a flaretip nozzle assembly 8 used in theinventive flare apparatus 2. -
FIG. 3 is an elevational view of aninner conduit 15 used in theinventive flare apparatus 2. - An
embodiment 2 of the flare apparatus provided by the present invention is illustrated inFIGS. 1-3 . Theinventive flare apparatus 2 comprises aplenum 4 on the upper end of a flare stack 6. A flare gas is delivered to theplenum 4 through the flare stack 6. Theinventive flare apparatus 2 further comprises one or more (preferably a plurality) of flaretip nozzle assemblies 8 which receive the flare gas from theplenum 4 and discharge the flare gas from the upper (or forward)ends 10 of thenozzle assemblies 8 for combustion. As used herein and in the claims, the term “flare gas” can refer to any type of single or two phase fuel, waste gas, or other stream from a plant, refinery, oil or gas production site, or other source which is suitable for combustion in a flare system. - Each of the one or more flare
tip nozzle assemblies 8 of theinventive apparatus 2 preferably comprises: anouter conduit 14; aninner conduit 15; aflow annulus 16 for the flare gas which is formed between theinner surface 18 of theouter conduit 14 and theexterior surface 20 of theinner conduit 15; aninjection structure 22 for injecting steam or other entrainment media into the lower (or rearward)longitudinal end 26 of theinner conduit 15; and an exterior clean-up ring orassembly 28 positioned around the upper (or forward)longitudinal end 30 of theouter conduit 14. - The
outer conduit 14 of eachnozzle assembly 2 comprises; alongitudinal axis 32; a longitudinally extendingouter wall 34 which surrounds thelongitudinal axis 32; an inlet opening 36 at the lower (or rearward)longitudinal end 38 of theouter conduit 14; and a discharge opening 40 at the upper (or forward)longitudinal end 30 of theouter conduit 14. Theflow annulus 16 formed between theinner surface 18 of theouter conduit 14 and theexterior 20 of theinner conduit 15 also surrounds thelongitudinal axis 32 of the outer conduit and extends longitudinally from the lowerlongitudinal end 38 to the upperlongitudinal end 30 of theouter conduit 14. Theflow annulus 16 has an inlet opening 42 at the lowerlongitudinal end 38 of theouter conduit 14 and a discharge opening 44 at the upperlongitudinal end 30 of theouter conduit 14. - The
outer conduit 14 is preferably cylindrical but can alternatively have an elliptical, oval, rectangular, square, triangular or other cross-sectional shape. In addition, although the interior of theouter conduit 14 will preferably have a substantial constant interior cross-sectional area along its entire length, it will be understood that the entire length or any portion of the longitudinal length of theinterior surface 18 of theouter conduit 14 can alternatively have a converging or diverging shape. - The
outer conduit 14 of eachnozzle assembly 8 is connected to theplenum 4 in a manner which places the inlet opening 42 of thenozzle flow annulus 16 in fluid communication with theinterior 46 of theplenum 4. In theembodiment 2 of the inventive flare apparatus illustrated inFIGS. 1 and 2 , thelower end 38 of theouter conduit 14 is connected to theupper wall 48 of theplenum 4 such that the inlet opening 42 of theflow annulus 16 is positioned over aflow opening 50 formed through theupper wall 48. Alternatively, a lower portion of theouter conduit 14 can extend through an opening in theupper wall 48 of theplenum 4 such that thelower end 38 of theouter conduit 14 and the inlet opening 42 of theflow annulus 16 would be located inside theinterior 46 of theplenum 4. - The
upper wall 48 of theplenum 4 can be flat, outwardly dished, or have any other shape. - The
inner conduit 15 of eachnozzle assembly 8 extends upwardly (or forwardly) through thelower wall 51 of theplenum 4 and into thelower end 38 of theouter conduit 14 such that (a) the upper (or forward)longitudinal end 52 of theinner conduit 14 is located substantially at (i.e., preferably within ±40 inches of, more preferably within ±30 inches of, more preferably within ±20 inches of, more preferably within 10 inches of, more preferably within ±5 inches of, more preferably within ±2.5 inches of, more preferably within ±+1 inch of, and most preferably at) the upperlongitudinal end 30 of theouter conduit 14, (b) the lower (or rearward)longitudinal end 26 of theinner conduit 15 is located outside of and spaced downwardly (or rearwardly) from the lowerlongitudinal end 38 of theouter conduit 14, and (c) the inlet opening 56 at thelower end 26 of theinner conduit 15 is located outside of theplenum 4. Thelower wall 51 of the plenum can be flat, outwardly dished, or have any other desired shape. - The
inner conduit 15 of eachnozzle assembly 8 is configured such that at least a lower portion of theinner conduit 15 is in the form of aventuri flow structure 58 for the steam or other entrainment media which is injected into thelower end 26 of theinner conduit 15. The flow of the steam or other entrainment media through theventuri flow structure 58 of theinner conduit 15 operates to further reduce the pressure at the lower inlet opening 56 of theinner conduit 15 so that, as compared to an entirely straight inner conduit design with no venturi flow, significantly more air is inducted by the entrainment media into theinner conduit 15. - The
venturi flow structure 58 of theinner conduit 15 preferably comprises: a venturiinlet bell structure 60 at the lower (or rearward)end 26 of theinner conduit 15; astraight venturi section 62 which extends upwardly (or forwardly) from theinlet bell structure 60; and a diverging venturibell outlet section 64 which extends upwardly (or forwardly) from the upper or forward end of thestraight section 62. The interior cross-sectional flow area of thestraight venturi section 62 is substantial constant along the entire length of thestraight section 62. The interior cross-sectional flow area of the divergingbell outlet section 64 increases as thebell outlet section 64 extends upwardly or forwardly from thestraight venturi section 62. The interior surface of thebell outlet section 64 preferably diverges at an angle 66 in the range of from about 5° to about 60°, more preferably from about 5° to about 45° and more preferably from about 5′ to about 30° with respect to thelongitudinal axis 32 of the outer andinner conduits - The diverging
bell outlet section 64 of theventuri structure 58 can extend all of the way to thedischarge opening 68 at the upper (or forward)longitudinal end 52 of theinner conduit 15. Alternatively, theinner conduit 15 can further comprise an upper orforward discharge section 69 of substantially constant internal cross-sectional flow area which extends from the upper orforward end 65 of the diverging venturibell outlet section 64 to thedischarge opening 68 of theinner conduit 15. If theinner conduit 15 includes an upper orforward discharge section 69 as just described, the upper orforward end 65 of the divergingbell outlet section 64 of theventuri structure 58 can be located prior to or inside theouter conduit 14. - The longitudinal length of the
venturi flow structure 58 will preferably be at least 10%, more preferably at least 20% and more preferably at least 25%, of the entire longitudinal length of theinner conduit 15. The longitudinal length of thestraight venturi section 62 of theventuri flow structure 58 will preferably be at least 5%, more preferably at least 10%, of the entire length of theventuri structure 58. The longitudinal length of the divergingbell outlet section 64 of theventuri structure 58 will preferably be at least 10%, more preferably at least 20% and more preferably at least 30%, of the entire length of theventuri structure 58. - The
inner conduit 15 and each section of theventuri flow structure 58 of theinner conduit 15 will preferably have a circular cross-sectional shape such that, at least in the interior thereof, the interior surface of thestraight venturi section 62 is cylindrical and the interior surface of the divergingventuri bell section 64 has a conical shape. However, the cross-section of theinner conduit 15 and of each section of theventuri structure 58 can alternatively be elliptical, oval, rectangular, square, triangular or other non-circular shape. Also, theinterior surface 59 of theventuri flow structure 58 can be smooth or roughened. - The entrainment media used in the inventive apparatus and method will preferably be steam. However, examples of other types of entrainment media suitable for use in the inventive apparatus and method include, but are not limited to, carbon dioxide, air, nitrogen, or argon.
- The
injection structure 22 for the entrainment media is located outside of theplenum 4 and is spaced downwardly or rearwardly apart from the inlet bell opening 56 at thelower end 26 of theinner conduit 15 so that agap 70 is formed between theinjection structure 22 and the inlet bell opening 56 of theinner conduit 15. Theinjection structures 22 for the entrainment media can be single port tips, multi-port spiders, or other types of ejectors for supersonic, sonic, or subsonic ejection flow. - In the method of the present invention, the flare gas delivered to the
plenum 4 flows upwardly or forwardly through theflow annulus 16 of each flaretip nozzle assembly 8 and is discharged for combustion from the discharge opening 44 of theflow annulus 16 at the upper or forwardlongitudinal end 30 of theouter conduit 14. At the same time, steam or other entrainment media is ejected from theinjection structure 22 toward the inlet bell opening 56 at the lower or rearward end 26 of theinner conduit 15. As the ejected entrainment media travels through thegap 70 between theinjection structure 22 and theinlet bell opening 56, atmospheric air is entrained by the media and pulled into theinner conduit 15. - In accordance with the present invention, by causing the injected entrainment media to flow through the
venturi flow structure 58 which forms at least a lower or rearward portion of theinner conduit 15, the pressure at the inlet bell opening 56 is further reduced, thus resulting in significantly more air being induced by the flow of the entrainment media into theinner conduit 15. As compared to a nozzle tip using an entirely straight inner conduit design, theventuri flow structure 58 incorporated in theinner conduit 15 of the inventive flaretip nozzle assembly 8 increases the amount of air delivered by the entrainment media into theinner conduit 15 by an amount of at least 5% (more preferably at least 10%, at least 15%, at least 20%, or at least 25%). - The air inducted into the
inner conduit 15 mixes with the entrainment media and is discharged from the discharge opening 68 of theinner conduit 15 for combustion of the inducted air with the flare gas discharged from the discharge opening 44 of theflow annulus 16. Because the discharge opening 68 of theinner conduit 15 is located substantially at the upper or forwardlongitudinal end 30 of theouter conduit 14, rather than inside theouter conduit 14, substantially no mixing of the flare gas with the entrainment media and inducted air occurs within theouter conduit 14, thus further reducing the pressure at the inlet opening 56 of theinner conduit 15 and causing even more air to be inducted into theinner conduit 15. - The exterior clean-up ring or
apparatus 28 at the upper (or forward)longitudinal end 30 of theouter conduit 14 comprises a series of ejection ports, nozzles or other ejection structures which eject steam into the combustion mixture discharged from the flare tip nozzle assemble 8. The steam ejected from the clean-upring 28 operates to induct additional air into the combustion mixture and can also be used to shape the combustion flame or assist in maintaining the shape of the flame in high wind conditions. - Thus, the present invention is well adapted to carry out the objectives and attain the ends and advantages mentioned above as well as those inherent therein. While presently preferred embodiments have been described for purposes of this disclosure, numerous changes and modifications will be apparent to those in the art. Such changes and modifications are encompassed within the invention as defined by the claims.
Claims (14)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16/540,355 US20210048194A1 (en) | 2019-08-14 | 2019-08-14 | Low consumption assisted flare apparatus and method |
PCT/US2020/046276 WO2021030649A1 (en) | 2019-08-14 | 2020-08-14 | Low consumption assisted flare apparatus and method |
EP20853481.8A EP4013996A4 (en) | 2019-08-14 | 2020-08-14 | Low consumption assisted flare apparatus and method |
KR1020227008081A KR20220044345A (en) | 2019-08-14 | 2020-08-14 | Low Consumption Support Flare Devices and Methods |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16/540,355 US20210048194A1 (en) | 2019-08-14 | 2019-08-14 | Low consumption assisted flare apparatus and method |
Publications (1)
Publication Number | Publication Date |
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US20210048194A1 true US20210048194A1 (en) | 2021-02-18 |
Family
ID=74566908
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US16/540,355 Pending US20210048194A1 (en) | 2019-08-14 | 2019-08-14 | Low consumption assisted flare apparatus and method |
Country Status (4)
Country | Link |
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US (1) | US20210048194A1 (en) |
EP (1) | EP4013996A4 (en) |
KR (1) | KR20220044345A (en) |
WO (1) | WO2021030649A1 (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3547567A (en) * | 1968-07-25 | 1970-12-15 | Smoke Ban Mfg Inc | Flare stack combustion tip |
US20100089066A1 (en) * | 2007-05-15 | 2010-04-15 | Alstom Technology Ltd | Cool flame combustion |
US20100089367A1 (en) * | 2008-10-10 | 2010-04-15 | General Electric Company | Fuel nozzle assembly |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2007830B (en) * | 1977-10-08 | 1982-05-19 | Gkn Birwelco Ltd | Flare tip |
WO2006010693A1 (en) * | 2004-07-26 | 2006-02-02 | Nv Bekaert Sa | Flare stack having enclosed flame combustion |
US7967600B2 (en) * | 2006-03-27 | 2011-06-28 | John Zink Company, Llc | Flare apparatus |
US20100291492A1 (en) * | 2009-05-12 | 2010-11-18 | John Zink Company, Llc | Air flare apparatus and method |
US9643871B2 (en) * | 2013-06-13 | 2017-05-09 | Corning Incorporated | Submerged combustion melters and burners therefor |
US9470418B2 (en) * | 2014-06-05 | 2016-10-18 | David Bacon | Gas assist assembly for use with a waste gas flare stack |
AU2016379435B2 (en) * | 2015-12-23 | 2021-08-19 | John Zink Company, Llc | Staged steam injection system |
US20190086079A1 (en) * | 2017-09-15 | 2019-03-21 | Honeywell International Inc. | Low steam consumption high smokeless capacity waste gas flare |
CN110017488A (en) * | 2018-01-09 | 2019-07-16 | 中国石油化工股份有限公司 | Steam combustion-supporting type torch burner |
-
2019
- 2019-08-14 US US16/540,355 patent/US20210048194A1/en active Pending
-
2020
- 2020-08-14 KR KR1020227008081A patent/KR20220044345A/en unknown
- 2020-08-14 EP EP20853481.8A patent/EP4013996A4/en active Pending
- 2020-08-14 WO PCT/US2020/046276 patent/WO2021030649A1/en unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3547567A (en) * | 1968-07-25 | 1970-12-15 | Smoke Ban Mfg Inc | Flare stack combustion tip |
US20100089066A1 (en) * | 2007-05-15 | 2010-04-15 | Alstom Technology Ltd | Cool flame combustion |
US20100089367A1 (en) * | 2008-10-10 | 2010-04-15 | General Electric Company | Fuel nozzle assembly |
Also Published As
Publication number | Publication date |
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EP4013996A4 (en) | 2023-09-06 |
KR20220044345A (en) | 2022-04-07 |
WO2021030649A1 (en) | 2021-02-18 |
EP4013996A1 (en) | 2022-06-22 |
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