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AU2021356482B2 - Staged gas injection system - Google Patents
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AU2021356482B2 - Staged gas injection system - Google Patents

Staged gas injection system

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Publication number
AU2021356482B2
AU2021356482B2 AU2021356482A AU2021356482A AU2021356482B2 AU 2021356482 B2 AU2021356482 B2 AU 2021356482B2 AU 2021356482 A AU2021356482 A AU 2021356482A AU 2021356482 A AU2021356482 A AU 2021356482A AU 2021356482 B2 AU2021356482 B2 AU 2021356482B2
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Australia
Prior art keywords
gas
gas injection
stage
injection assembly
source
Prior art date
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Active
Application number
AU2021356482A
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AU2021356482A1 (en
Inventor
Wesley Ryan Bussman
James Charles Franklin
Dennis Lee Knott
Jeff William White
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John Zink Co LLC
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John Zink Co LLC
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Filing date
Publication date
Priority claimed from US17/066,494 external-priority patent/US20210025589A1/en
Application filed by John Zink Co LLC filed Critical John Zink Co LLC
Publication of AU2021356482A1 publication Critical patent/AU2021356482A1/en
Application granted granted Critical
Publication of AU2021356482B2 publication Critical patent/AU2021356482B2/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G7/00Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
    • F23G7/06Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
    • F23G7/08Incinerators 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
    • F23G7/085Incinerators 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G5/00Incineration of waste; Incinerator constructions; Details, accessories or control therefor
    • F23G5/44Details; Accessories
    • F23G5/442Waste feed arrangements

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  • Engineering & Computer Science (AREA)
  • Environmental & Geological Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Separation By Absorption (AREA)

Abstract

A staged gas injection system for a flare tip that can discharge waste gas into a combustion zone is provided. The staged gas injection system includes, for example, a first gas injection assembly and a second stage gas injection assembly. The first gas injection assembly is configured to inject a gas (for example steam or a gas other than steam) at a high flow rate and a high pressure into the flare tip or the combustion zone. The second gas injection assembly is configured to inject a gas (for example, steam and/or a gas other than steam) at a low flow rate and a high pressure into the flare tip or the combustion zone. A flare tip including the staged gas injection system is also provided.

Description

2021356482 12 2023
STAGED GAS INJECTION SYSTEM
Apr
CROSS-REFERENCETOTORELATED CROSS-REFERENCE RELATED APPLICATIONS APPLICATIONS
[0001] This application claims priority to United States Patent Application No. 17/066,494 filed on October 09, 2020 which is incorporated by reference herein. 2021356482
BACKGROUND BACKGROUND
[0002] The discussion of the background to the invention herein is intended to facilitate an understanding of the invention. However, it should be appreciated that the discussion is not an acknowledgement or admission that any aspect of the discussion was part of the common general knowledge as at the priority date of the application.
[0002a] Where any or all of the terms "comprise", "comprises", "comprised" or "comprising" are used in this specification (including the claims) they are to be interpreted as specifying the presence of the stated features, integers, steps or components, but not precluding the presence of one or more other features, integers, steps or components.
[0002b] Industrial flares for burning and disposing of combustible gases are well known. Such flares typically include one or more flare tips mounted on a flare stack. The flare tips initiate combustion of the gases and release the combustion products to the atmosphere. The flares are located at production, refining, processing plants, and the like. In many cases, more than one flare is included at a single facility.
[0003] For example, industrial flares are used for disposing of flammable gas, waste gas and other types of gas (collectively referred to as “waste gas”) that need to be disposed. For example, industrial flares are used to safely combust flammable gas streams that are diverted and released due to system venting, plant shut-downs and upsets, and plant emergencies (including fires and power failures). A properly operating flare system can be a critical component to the prevention of plant disruption and damage.
[0004] It is desirable and often required for an industrial flare to operate in a relatively smokeless manner. For example, smokeless operation can usually be achieved by making sure
that the waste gas is admixed with a sufficient amount of air in a relatively short period of time to sufficiently oxidize the soot particles formed in the flame. In applications where the gas pressure is low, the momentum of the waste gas stream alone may not be sufficient to provide 2021356482 12 smokeless operation. In such cases, an assist medium such as steam and/or air can be used to provide the necessary motive force to entrain ambient air from around the flare apparatus. Many factors, including local energy costs and availability, are taken into account in selecting a smoke 2021356482
suppressing assist medium.
[0005] The most common assist medium for adding momentum to low-pressure gases is steam. Steam is typically injected through one or more groups of nozzles that are associated
1a
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with the flare tip. In addition to adding momentum and entraining air, steam can also dilute the
gas and participate in the chemical reactions involved in the combustion process, both of which
assist with smoke suppression. In one example of a simple steam assist system, several steam
injectors extend from a steam manifold or ring that is mounted near the exit of the flare tip. The
steam injectors direct jets of steam into the combustion zone adjacent the flare tip. One or more
valves (which, for example, can be remotely controlled by an operator or automatically
controlled based on changing operating parameters) are used to adjust the steam flow to the flare
tip. The steam jets aspirate air from the surrounding atmosphere into the discharged waste gas
with high levels of turbulence. This prevents wind from causing the flame to be pulled down
from the combustion zone into and around the flare tip. Injected steam, educted air, and the
waste gas combine to form a mixture that helps the waste gas burn without visible smoke.
[0006] A steam injection system for injecting steam into a waste gas stream entails control
valves, piping to deliver the steam to the flare tip, steam injection nozzles, and distribution
piping to deliver the steam to the steam injection nozzles. Some flares have multiple steam lines
with multiple sets of steam injection nozzles for discharging steam into different locations
associated with the flare tip.
[0007] Various issues can arise with steam injection systems. For example, steam injection
systems use the momentum of the steam to entrain air and mix the air with the waste gas stream
for smokeless combustion. At design flow rates, for example, steam discharges from the steam
nozzles at sonic velocity (Mach=1 or greater). As the steam flow rate is decreased, the steam
pressure at the steam nozzles decreases and eventually the flow rate is decreased low enough SO
that the steam discharge velocity is less than sonic. As the steam velocity decreases, the
efficiency with which the steam entrains air and mixes it with the waste gas stream decreases.
As an example, a flare tip at design flow rates may require 0.3 pounds of steam per pound of
waste gas to generate smokeless combustion. At turndown conditions (e.g., lower steam
injection pressure), the same flare tip and same waste gas stream (in terms of composition) can
require 1.2 pounds or more of steam per pound of waste gas to achieve smokeless combustion.
This can increase the operational cost of the flare.
[0008] Additionally, when a flare tip operates at low waste gas flow rates, it's possible for air
and waste gas to mix within the flare tip. This is usually caused by the waste gas being less
WO wo 2022/074475 PCT/IB2021/057760
dense than the surrounding air and the wind driving air down into the flare tip. When air and
waste gas mix, combustion can occur. When combustion occurs within the flare tip, the internal
tubes of the flare tip can experience a rise in temperature. If the tubes get too hot, material
degradation and deformation can occur, which can reduce the usable life of the flare tip.
[0009] In order to prevent such damage to the flare tip, manufacturers recommend
continuously injecting steam into or around the flare tip (depending on the nature of the steam
injection assembly) at a minimum flow rate, often referred to as a minimum steam rate.
Continuous injection of steam at a minimum steam rate helps keep the temperature of the
internal metal tubes and other equipment below the point at which rapid deterioration occurs.
For example, the minimum steam rate causes a sufficient flow of steam and air through the
internal tubes to transfer enough heat from the internal tubes to keep the temperatures of the
tubes in acceptable ranges.
[0010] New regulations recently published by the United States government may alter the
way operators control their flares. In the future, operators may have to account for not only the
heating value of the waste gas as current regulations require, but also the amount of steam sent to
the flare. This may cause issues when the flare is operating at turndown conditions. For
example, operators may be required to enrich the waste gas with a supplemental gas (for
example, natural gas) to maintain a net heating value in the combustion zone of 270 btu/scf or
greater. Depending at least in part on the cost of the supplemental gas, such a requirement may
cost operators anywhere from hundreds of thousands of dollars to millions of dollars a year per
flare.
[0011] One way to reduce the amount of supplemental gas that may be needed is to reduce
the minimum steam rate. However, a reduced minimum steam rate will likely reduce the service
life of the flare, necessitating more frequent plant shutdowns and associated cost increases. A
related problem that can occur is "water hammer." If a sufficient amount of steam is not
provided to keep the steam lines warm and the steam lines cool off, the subsequent introduction
of steam into the cold lines can cause problematic knocking or water hammer.
[0012] There are also situations in which a flare tip with multiple discharges is utilized with
a waste gas that is lighter than air. When waste gas of this type is discharged at low waste gas
flow rates, there is a possibility that the waste gas will preferentially flow through only a few of
2021356482 12 2023
the internal tubular modules. If this occurs, air can flow down the internal tubular modules that do not receive waste gas. A fuel and air mixture can ensue which can ultimately flashback into Apr the tip and cause a flame to stabilize within the flare tip. A flow of steam at a minimum steam rate can provide enough momentum to limit the amount of air that can flow into the flare tip and address this problem. 2021356482
SUMMARY
[0013] By this disclosure, a staged gas injection system for a flare tip that can discharge waste gas into a combustion zone is provided. Also provided is a flare tip that can discharge waste gas into a combustion zone.
[0013a] According to one form of the present invention there is provided a staged gas injection system for a flare tip that can discharge waste gas into a combustion zone downstream from the flare tip, and the flare tip includes an inner tubular member disposed within an outer tubular member so as to form a pre-mix zone downstream from the inner tubular member and within the outer tubular member, the staged gas injection system comprising a first stage gas source, the first stage gas source being a source of first stage gas, wherein the first stage gas consists of alternative gas; a first gas injection assembly, said first gas injection assembly being configured to inject the first stage gas at a high flow rate and a high pressure into the inner tubular member of the flare tip and including a first gas injection nozzle fluidly connected to said first stage gas source from which said first stage gas is received by the first gas injection nozzle; a second stage gas source, said second stage gas source being a source of second stage gas; a second gas injection assembly, said second gas injection assembly configured to inject said second stage gas at a low flow rate and a high pressure into the inner tubular member of the flare tip and including a second gas injection nozzle fluidly connected to said second stage gas source from which said second stage gas is received by the second gas injection nozzle, wherein said first gas injection assembly and said second gas injection assembly are proximate to each other and oriented in the same direction such that said first gas injection assembly injects first stage gas into the inner tubular member of the flare tip and the second gas injection assembly injects second stage gas into the inner tubular member of the flare tip, and wherein the low flow rate means the first gas injection assembly and second gas injection assembly are configured such that, on a per nozzle basis, the low flow rate is one-half or less than the high flow rate.
4
[0013b] According to another form of the present invention there is provided a staged gas injection system for a flare tip that can discharge waste gas into a combustion zone downstream from the flare tip, comprising a first stage gas source, the first stage gas source being a source of 2021356482 12 first stage gas, wherein the first stage gas consists of alternative gas; a first gas injection assembly, said first gas injection assembly being configured to inject the first stage gas at a high flow rate and a high pressure into the combustion zone and including a first gas injection nozzle fluidly 2021356482
connected to said stage gas source from which said first stage gas is received by the first gas injection nozzle; a second stage gas source, said second stage gas source being a source of second stage gas; a second gas injection assembly, said second gas injection assembly configured to inject said second stage gas at a low flow rate and a high pressure into the combustion zone and including a second gas injection nozzle fluidly connected to said second stage gas source from which said second stage gas is received by the second gas injection nozzle, wherein said first gas injection assembly and said second gas injection assembly are proximate to each other and oriented in the same direction such that said first gas injection assembly injects first stage gas into the combustion zone and said second gas injection assembly injects second stage gas into the combustion zone, and wherein the low flow rate means the first gas injection assembly and second gas injection assembly are configured such that, on a per nozzle basis, the low flow rate is one- half or less than the high flow rate.
[0014] In one embodiment, the staged gas injection system provided by this disclosure is for a flare tip that can discharge waste gas into a combustion zone and includes an inner tubular member disposed within an outer tubular member. In this embodiment, the staged gas injection system comprises a first gas injection assembly and a second gas injection assembly. The first gas injection assembly is configured to inject a gas at a high flow rate and a high pressure into the inner tubular member of the flare tip, and includes a first stage gas source and a first gas injection nozzle fluidly connected to the first stage gas source. The first stage gas source can be a source of steam and/or alternative gas. The second gas injection assembly is configured to inject a gas at a low flow rate and a high pressure into the inner tubular member of the flare tip, and includes a second stage gas source and a second gas injection nozzle fluidly connected to the second stage gas source. The first gas injection assembly and second gas injection assembly are proximate to each other and oriented in the same direction such that both the first gas injection assembly and the second gas injection assembly inject gas into the inner tubular member of the flare tip.
4a
2021356482 12 2023
[0015] In another embodiment, the staged gas injection system provided by this disclosure is for a flare tip that can discharge waste gas into a combustion zone. In this embodiment, the staged Apr gas injection system comprises a first gas injection assembly and a second gas injection assembly. The first gas injection assembly is configured to inject gas at a high flow rate and a high pressure into the combustion zone, and includes a first stage gas source and a first gas injection nozzle fluidly connected to the first stage gas source. The first stage gas source is a source of steam 2021356482
and/or an alternative gas. The second gas injection assembly is configured to
4b
WO wo 2022/074475 PCT/IB2021/057760
inject a gas at a low flow rate and a high pressure into the combustion zone, and includes a
second stage gas source and a second gas injection nozzle fluidly connected to the second stage
gas source. The first gas injection assembly and second gas injection assembly are proximate to
each other and oriented in the same direction such that both the first gas injection assembly and
the second gas injection assembly inject gas into the combustion zone.
[0016] In one embodiment, the flare tip provided by this disclosure can discharge waste gas
into a combustion zone and includes an inner tubular member disposed within an outer tubular
member and a staged gas injection system. In this embodiment of the flare tip, the staged gas
injection system comprises a first gas injection assembly and a second gas injection assembly.
The first gas injection assembly is configured to inject gas at a high flow rate and a high pressure
into the inner tubular member of the flare tip, and includes a first stage gas source and a first gas
injection nozzle fluidly connected to the first stage gas source. The first stage gas source is a
source of steam and/or an alternative gas. The second gas injection assembly is configured to
inject a gas at a low flow rate and a high pressure into the inner tubular member of the flare tip,
and includes a second stage gas source and a second gas injection nozzle fluidly connected to the
second stage gas source. The first gas injection assembly and second gas injection assembly are
proximate to each other and oriented in the same direction such that both the first gas injection
assembly and the second gas injection assembly inject gas into the inner tubular member of the
flare tip.
[0017] In another embodiment, the flare tip provided by this disclosure can discharge waste
gas into a combustion zone and includes a staged gas injection system. In this embodiment of
the flare tip, the staged gas injection system comprises a first gas injection assembly and a
second gas injection assembly. The first gas injection assembly is configured to inject gas at a
high flow rate and a high pressure into the combustion zone, and includes a first stage gas source
and a first gas injection nozzle fluidly connected to the first stage gas source. The first stage gas
source is a source of steam and/or an alternative. The second gas injection assembly is
configured to inject a gas at a low flow rate and a high pressure into the combustion zone, and
includes a second stage gas source and a second gas injection nozzle fluidly connected to the
second stage gas source. The first gas injection assembly and second gas injection assembly are
proximate to each other and oriented in the same direction such that both the first gas injection
assembly and the second gas injection assembly inject gas into the combustion zone.
WO wo 2022/074475 PCT/IB2021/057760
BRIEF DESCRIPTION OF THE DRAWINGS
[0018] The drawings included with this application illustrate certain aspects of the
embodiments described herein. However, the drawings should not be viewed as exclusive
embodiments. The subject matter disclosed is capable of considerable modifications, alterations,
combinations, and equivalents in form and function, as will occur to those skilled in the art with
the benefit of this disclosure.
[0019] FIG. 1A is a sectional view of the one embodiment of the staged gas injection system
disclosed herein.
[0020] FIG. 1B is a sectional view of another embodiment of the staged gas injection system
disclosed herein.
[0021] FIG. 2A is a sectional view showing the staged gas injection system shown by FIG.
1A in a different flare configuration.
[0022] FIG. 2B is a sectional view showing the staged gas injection system shown by FIG.
1B in a different flare configuration.
[0023] FIG. 3A is a sectional view of an additional embodiment of the staged gas injection
system shown by FIG. 1A.
[0024] FIG. 3B is a sectional view of an additional embodiment of the staged gas injection
system shown by FIG. 1B.
[0025] FIG. 4A is a sectional view of an additional embodiment of the staged gas injection
system shown by FIG. 1A.
[0026] FIG. 4B is a sectional view of an additional embodiment of the staged gas injection
system shown by FIG. 1B.
[0027] FIG. 5 is a side view of an embodiment of the staged gas injection system disclosed
herein.
[0028] FIG. 6 is a top view of the embodiment of the staged gas injection system shown by
FIG. 5.
[0029] FIG. 7 is a side view of one embodiment of a gas injection nozzle disclosed herein.
WO wo 2022/074475 PCT/IB2021/057760
[0030] FIG. 8 is a top view of the gas injection nozzle shown by FIG. 7.
[0031] FIG. 9 is a sectional view of an embodiment of a three-stage gas injection system
disclosed herein.
[0032] FIG. 10 is a side view of another embodiment of a three-stage gas injection system
disclosed herein.
[0033] FIG. 11 is a top view of the gas injection assembly illustrated by FIG. 10.
[0034] FIG. 12 is a sectional view illustrating the staged gas injection assembly shown by
FIGS. 10 and 11 as directed to an inner tubular member of a single flare tip.
[0035] FIG. 13 is a graph comparing a plot of the normalized steam/hydrocarbon ratio (lb/lb)
to the normalized flare fuel rate (lb/hr) corresponding to a high flow rate, high pressure steam
nozzle to a plot of the normalized steam/hydrocarbon ratio (lb/lb) to the normalized flare fuel
rate (lb/hr) corresponding to a low flow rate, high pressure steam nozzle.
[0036] FIG. 14 is a graph comparing the air entrainment performance using both steam and
air as the first stage gas source.
DETAILED DESCRIPTION
[0037] The present disclosure may be understood more readily by reference to this detailed
description. For simplicity and clarity of illustration, where appropriate, reference numerals may
be repeated among the different figures to indicate corresponding or analogous elements. In
addition, numerous specific details are set forth in order to provide a thorough understanding of
the various embodiments described herein. However, it will be understood by those of ordinary
skill in the art that the embodiments described herein can be practiced without these specific
details. In other instances, methods, procedures and components have not been described in
detail SO as not to obscure the related relevant feature being described. Also, the description is
not to be considered as limiting the scope of the embodiments described herein. The drawings
are not necessarily to scale and the proportions of certain parts have been exaggerated to better
illustrate details and features of the present disclosure.
[0038] By this disclosure, a staged gas injection system and a flare tip including the staged
gas injection system are provided.
WO wo 2022/074475 PCT/IB2021/057760
[0039] It has been discovered that the above issues can be addressed by providing a staged
gas injection system that has the ability to discharge steam, an alternative gas, or steam and an
alternative gas to the flare apparatus at various stages (that is, at various flow rates and
pressures). For example, the staged gas injection system disclosed herein can be a two-stage
system that includes two gas injection nozzles, one for injecting steam and/or an alternative gas
into the flare tip at a high flow rate and high pressure (for example, as in a traditional, standard
steam injection system), and one for injecting steam and/or an alternative gas into the flare tip at
the same location at a low flow rate and high pressure. As another example, the staged gas
injection system can be a three-stage system that includes three gas injection nozzles, one for
injecting steam and/or an alternative gas into the flare tip at a high flow rate and a high pressure
(for example, as in a traditional, standard steam injection system), one for injecting steam and/or
an alternative gas into the flare tip at the same location at a lower flow rate and a high pressure,
and one for injecting steam and/or an alternative gas into the flare tip at the same location at an
even lower flow rate and at a high pressure. The number of stages that can be used is not
limited. For example, four or five gas injection nozzles, each having the ability to discharge
steam and/or an alternative gas to the flare apparatus at a different flow rate and pressure, can
also be used. The number of stages that should be used in a given application is dependent, for
example, on the type of flare apparatus, the location of the staged gas injection system with
respect to the flare tip and other factors known to those skilled in the art with the benefit of this
disclosure.
[0040] The staged gas injection system of the present disclosure allows a gas-assisted flare to
operate with less steam and/or other assist gases at reduced waste gas flow rates. For example,
the staged gas injection system disclosed herein provides the momentum necessary to efficiently
entrain and mix air with the waste gas at turndown conditions. Additionally, when steam is used
as at least one of the staged gases, such a system provides the ability to maintain temperatures at
acceptable levels within the steam lines. The system uses less steam at turndown conditions
without impacting the service life of the flare tip.
[0041] As used herein and in the appended claims, "waste gas" means waste gas, flammable
gas, plant gas, and any other type of gas that can be disposed of by an industrial flare. An
alternative gas means a gas other than steam. Examples of alternative gases that can be used
include air, nitrogen, plant gas, natural gas and mixtures thereof. As described above, an
WO wo 2022/074475 PCT/IB2021/057760
alternative gas can be discharged by the staged gas injection system through one or more of the
gas injection nozzles that inject gas into the flare tip at a relatively low flow rate (as compared to
the relatively high flow rate associated with, for example, a traditional standard steam injection
system). Whether an alternative gas is used and the specific alternative gas (or gases) used will
depend, for example, on the desired flame profile and properties. When the same type of gas is
used in connection with more than one gas injection nozzle, the corresponding gas sources can
be the same. For example, in a two-stage system in which each stage uses only steam, the first
stage gas source and second stage gas source can be the same gas source, namely, a source of
steam.
[0042] Referring now to the drawings, the staged gas injection system disclosed herein,
generally designated by the reference numeral 40, will be described. For example, FIGS. 1A,
2A, 3A, and 4A show an embodiment of the staged gas injection system 40 that includes two
separate gas injection assemblies, as used in conjunction with four different flare tip
configurations. FIGS. 1B, 2B, 3B, and 4B show an embodiment of the staged gas injection
system 40 that includes two separate gas injection assemblies that are combined in part into a
single unit, as used in conjunction with the same four different flare tip configurations shown by
FIGS. 1A, 2A and 4A. FIGS. 5 and 6 illustrate the two-stage gas injection assembly shown by
FIGS. 1B, 2B, 3B and 4B in more detail. FIGS. 7 and 8 illustrate another embodiment of a two-
stage gas injection assembly that can be used herein. FIG. 9 shows an embodiment of the staged
gas injection system 40 that includes three separate gas injection assemblies, as used in
conjunction with the flare tip configuration shown by FIGS. 1A and 1B. FIGS. 10 and 11
illustrate an embodiment of the staged gas injection system 40 in which three separate gas
injection assemblies are combined in part into a single unit. FIG. 12 shows the three-stage gas
injection assembly illustrated by FIGS. 10 and 11, as used in conjunction with the flare tip
configuration shown by FIGS. 1A and 1B. FIG. 13 illustrates results achieved by testing the
staged gas injection system disclosed herein.
[0043] As used herein and the appended claims, injection of steam and/or alternative gas at a
"high flow rate and a high pressure" means that on a per nozzle basis, the steam is injected from
the corresponding gas injection nozzles at a flow rate (flow capacity) of at least 2000 1b/hr, and
at a pressure of at least 50 psig. As used herein and in the appended claims, injection of steam
and/or an alternative gas at a "low flow rate and a high pressure" means that on a per nozzle wo 2022/074475 WO PCT/IB2021/057760 basis, the steam and/or alternative gas is injected from the corresponding gas injection nozzles at a flow rate (flow capacity) of one-half or less of the flow rate (flow capacity) at which the steam and/or other gas is injected from the corresponding gas injection nozzles used at the next larger stage, and at a pressure of at least 50 psig. For example, in a two-stage system, injection of steam and/or an alternative gas at a "low flow rate and a high pressure" in the second stage means that on a per nozzle basis the steam and/or alternative gas is injected from the corresponding gas injection nozzles at a flow rate (flow capacity) of one-half or less of the corresponding high flow/high pressure nozzle flow rate (flow capacity), and at a pressure of at least 50 psig. For example, in a three-stage system, injection of steam and/or an alternative gas at a "low flow rate and a high pressure" in the third stage means that on a per nozzle basis the steam and/or alternative gas is injected from the corresponding gas injection nozzles at a flow rate (flow capacity) of one-half or less of the nozzle flow rate (flow capacity) used in the second stage, and at a pressure of at least 50 psig. For example, the decrease in the nozzle flow rate
(flow capacity) in the second stage and subsequent stages (if used) to one-half or less of the
nozzle flow rate (flow capacity) used in the next larger stage can be accomplished by using
nozzles that each contain one or more discharge ports having a total discharge area of one-half or
less of the total discharge area of the discharge port(s) of each nozzle used in the next larger
stage.
[0044] The pressures at which the steam and/or other gas is injected from the gas injection
nozzles used in the various stages can also vary from stage to stage. For example, the pressures
utilized can vary from 5 psig to 300 psig, including 60, 90, 100, 120, 150, 180, 210, 240, and 270
psig. Suitable pressure ranges can include 5 psig to 200 psig, 5 psig to 100 psig, 20 psig to 300
psig, 20 psig to 200 psig, 20 psig to 100 psig, 40 psig to 300 psig, 40 psig to 200 psig, 40 psig to
100 psig, 60 psig to 300 psig, 60 psig to 200 psig, and 60 psig to 100 psig. The gas injection
assemblies and corresponding nozzles can utilize the available steam at the production, refining,
or processing plant where the flare assembly is installed.
[0045] The staged gas injection system 40 is used in connection with a flare assembly (not
shown in full). The flare assembly includes a flare riser (not shown) for conducting a waste gas
stream to a flare tip 10. The flare tip 10 is attached to the flare riser and configured to discharge
a waste gas stream into a combustion zone 70 in the atmosphere adjacent the flare tip.
WO wo 2022/074475 PCT/IB2021/057760
[0046] For example, in the configuration shown by FIGS. 1A, 1B, 9 and 12, the flare tip 10
includes an outer tubular member 12, inner tubular member 14, and a pre-mix zone 16. The
outer tubular member 12 includes an inlet 18, an outlet 20, and a gas passage 22. The inner
tubular member 14 includes an inlet 24, an outlet 26, and a gas passage 28. The inner tubular
member 14 is coaxially disposed in the outer tubular member 12. For example, waste gas is
conducted through the inlet 18 of the outer tubular member 12 into the gas passage 22, into the
pre-mix zone 16 and through the outlet 20 of the outer tubular member into the combustion zone
70. The pre-mix zone 16 is located between the outlet 26 of the inner tubular member 14 and the
outlet 20 of the outer tubular member 12. In the pre-mix zone 16, steam and/or an alternative gas
discharged through the outlet 26 of the inner tubular member 14 are mixed with waste gas and
discharged through the outlet 20 of the outer tubular member 12 into the combustion zone 70
therewith. The discharge of the waste gas mixture from the pre-mix zone 16 into the combustion
zone 70 entrains additional air into the waste gas. As understood by those skilled in the art with
the benefit of this disclosure, a pilot assembly (not shown) can also be associated with the flare
tip 10 to ignite the waste gas/air mixture in the combustion zone 70.
[0047] For example, in the configuration shown by FIGS. 2A and 2B, the flare tip 10
includes an outer tubular member 12, two inner tubular members 14, and a pre-mix zone 16. The
outer tubular member 12 includes an inlet (not shown), an outlet 20, and a gas passage 22. The
inner tubular members 14 each include an inlet 24, an outlet 26, and a gas passage 28. The inner
tubular members 14 are disposed in the outer tubular member 12. For example, although two
inner tubular members 14 are shown by FIGS. 2A and 2B, more than 2 (for example, 4 or 6)
inner tubular members 14 can be positioned in the outer tubular member 12. For example, waste
gas is conducted through the inlet of the outer tubular member 12 (not shown) into the gas
passage 22, into the pre-mix zone 16 and through the outlet 20 of the outer tubular member into
the combustion zone 70. The pre-mix zone 16 is located between the outlets 26 of the inner
tubular members 14 and the outlet 20 of the outer tubular member 12. In the pre-mix zone 16,
steam and/or an alternative gas discharged through the outlets 26 of the inner tubular members
14 are mixed with waste gas and discharged through the outlet 20 of the outer tubular member 12
into the combustion zone 70 therewith. The discharge of the waste gas mixture from the pre-mix
zone 16 into the combustion zone 70 entrains additional air into the waste gas. As understood by
WO wo 2022/074475 PCT/IB2021/057760
those skilled in the art with the benefit of this disclosure, a pilot assembly (not shown) can also
be associated with the flare tip 10 to ignite the waste gas/air mixture in the combustion zone 70.
[0048] For example, in the configuration shown by FIGS. 3A and 3B, the flare tip 10
includes an outer tubular member 12 and two inner tubular members 14. The outer tubular
member 12 includes an inlet (not shown), an outlet 20, and a gas passage 22. The inner tubular
members 14 each include inlets (not shown), an outlet 26, and a gas passage 28. The inner
tubular members 14 are disposed in the outer tubular member 12. For example, although two
inner tubular members 14 are shown by FIGS. 3A and 3B, more than 2 (for example, 4 or 6)
inner tubular members 14 can be positioned in the outer tubular member 12. For example, waste
gas is conducted through the inlet of the outer tubular member 12 into the gas passage 22, and
through the outlet 20 of the outer tubular member into the combustion zone 70. A stage gas
(steam and/or an alternative gas) is conducted through the inner tubular members 14, through the
outlets 26 thereof and into the combustion zone 70. The discharge of the waste gas and stage gas
mixture into the combustion zone 70 entrains additional air into the waste gas. As understood by
those skilled in the art with the benefit of this disclosure, a pilot assembly (not shown) can also
be associated with the flare tip 10 to ignite the waste gas/air mixture in the combustion zone 70.
[0049] For example, in the configuration shown by FIGS. 4A and 4B, the flare tip 10
includes two outer tubular members 12, two inner tubular members 14, and two pre-mix zones
16. The outer tubular members 12 each include an inlet 18, an outlet 20, and a gas passage 22.
The inner tubular members 14 each include an inlet 24, an outlet 26, and a gas passage 28. The
inner tubular members 14 are disposed in the outer tubular member 12. A waste gas manifold 30
having an inlet 32, an outlet 34 and a gas passage 36 surrounds the outer tubular members 12.
For example, waste gas is conducted through the inlet 32 into the gas passage 36 of the waste gas
manifold 30, through the outlet 34 of the waste gas manifold into the inlets 18 of the outer
tubular members 12, into the gas passages 22, into the pre-mix zones 16 and through the outlets
20 of the outer tubular member into the combustion zone(s) 70 (in this flare tip configuration,
two separate combustion zones can be created). The pre-mix zones 16 are located between the
outlets 26 of the inner tubular members 14 and the outlets 20 of the outer tubular members 12.
In the pre-mix zones 16, steam and/or an alternative gas discharged through the outlets 26 of the
inner tubular members 14 are mixed with waste gas and discharged through the outlets 20 of the
outer tubular members 12 into the combustion zone(s) 70 therewith. The discharge of the waste
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gas mixture from the pre-mix zones 16 into the combustion zone(s) 70 entrains additional air into
the waste gas. As understood by those skilled in the art with the benefit of this disclosure, one or
more pilot assemblies (not shown) can also be associated with the flare tip 10 to ignite the waste
gas/air mixture in the combustion zone(s) 70.
[0050] Referring now specifically to FIGS. 1A, 2A, 3A, and 4A, one embodiment of the
staged gas injection system 40 disclosed herein will be described in more detail. In FIGS. 2A,
3A and 4A, two staged gas injection systems 40 (each of this embodiment) are used. In this
embodiment, the staged gas injection system 40 includes a first gas injection assembly 50 and a
second gas injection assembly 60 that are proximate to each other and oriented in the same
direction such that both gas injection assemblies inject steam and/or an alternative gas into the
flare tip 10 (as shown by FIGS. 1A, 2A and 4A) or combustion zone 70 (as shown by FIG. 3A).
As used herein and in the appended claims, the statement that the first gas injection assembly 50
and second gas injection assembly 60 are proximate to each other and oriented in the same
direction such that both gas injection assemblies inject steam (and/or an alternative gas in the
case of assembly 60) into the flare tip 10 or combustion zone 70 means that at least part of each
gas injection assembly (for example, the gas injection nozzles) are proximate to each other and
oriented in the same direction such that both gas injection assemblies inject steam and/or an
alternative gas into the flare tip 10 or combustion zone 70. For example, the gas sources of the
assemblies are not necessarily oriented in the same direction.
[0051] The first gas injection assembly 50 is configured to inject steam and/or an alternative
gas at a high flow rate and a high pressure into the flare tip 10 (as shown by FIGS. 1A, 2A and
4A) or combustion zone 70 (as shown by FIG. 3A). The first gas injection assembly 50 includes
a first stage gas source 52 and a gas injection nozzle 54 fluidly connected to the first stage gas
source. The first stage gas source 52 is a source of steam and/or an alternative gas, and provides
such first stage gas to the gas injection nozzle 54.
[0052] The second gas injection assembly 60 is configured to inject a gas (steam and/or an
alternative gas) at a low flow rate and a high pressure into the flare tip 10 (as shown by FIGS.
1A, 2A and 4A) or combustion zone 70 (as shown by FIG. 3A). The second gas injection
assembly 60 includes a second stage gas source 62 and a second gas injection nozzle 64 fluidly
connected to the second stage gas source. The second stage gas source 62 provides steam and/or
13
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an alternative gas to the second gas injection nozzle 64. The second gas injection nozzle 64
includes at least one discharge port that has a total discharge area of no greater than one-half of
the corresponding total discharge area of the discharge port(s) of the high flow rate, high
pressure gas injection nozzle 54. This allows the second gas injection assembly 60 to inject gas
at a low flow rate and high pressure.
[0053] As shown by FIGS. 1A, 2A and 4A, the first gas injection assembly 50 is configured
to inject a first stage gas (steam and/or an alternative gas) at a high flow rate and a high pressure
into the inner tubular member(s) 14 of the flare tip 10. The second gas injection assembly 60 is
configured to inject a second stage gas (steam and/or an alternative gas) at a low flow rate and a
high pressure into the inner tubular member(s) 14 of the flare tip 10. Injection of the first stage
gas by the first gas injection assembly 50 and the second stage gas by the second gas injection
assembly 60 into the inner tubular member(s) 14 aspirates air from the surrounding environment
into the pre-mix zone(s) 16 of the flare tip 10 and into the waste gas conducted by the gas
passage(s) 22 to the pre-mix zone(s).
[0054] As shown by FIG. 3A, the first gas injection assembly 50 is configured to inject a first
stage gas (steam and/or an alternative gas) at a high flow rate and a high pressure into the
combustion zone 70. The second gas injection assembly 60 is configured to inject a second stage
gas (steam and/or an alternative gas) at a low flow rate and a high pressure into the combustion
zone 70. Injection of the first stage gas by the first gas injection assembly 50 and the second
stage gas by the second gas injection assembly 60 into the combustion zone 70 aspirates air
from the surrounding environment which is mixed with the waste gas.
[0055] Referring now to FIGS. 1B, 2B, 3B, 4B, 5, and 6, another embodiment of the staged
gas injection system 40 disclosed herein will be described. In FIGS. 2B, 3B and 4B, two staged
gas injection systems 40 (each of this embodiment) are used.
[0056] The embodiment of the staged gas injection system 40 shown by FIGS. 1B, 2B, 3B,
4B, 5, and 6 is the same in all respects as the embodiment of the staged gas injection 40 shown
by FIGS. 1A, 2A, 3A and 4A, except the first gas injection assembly 50 and second gas injection
assembly 60 are combined, in part, to form a single unit. The partial combination of the gas
injection assemblies into a single unit improves the distribution of stage gas by the system 40.
For example, the gas injection nozzle(s) 54 and gas injection nozzle(s) 64 are combined together
WO wo 2022/074475 PCT/IB2021/057760
into a single unit. The first gas injection assembly 50 and second gas injection assembly 60 are
still proximate to each other and oriented in the same direction such that both gas injection
assemblies inject steam (and/or an alternative gas in the case of assembly 60) into the flare tip 10
(as shown by FIGS. 1B, 2B and 4B) or combustion zone 70 (as shown by FIG. 3B). The first gas
injection assembly 50 is still configured to inject a first stage gas (steam and/or an alternative
gas) at a high flow rate and a high pressure into the flare tip 10 (as shown by FIGS. 1B, 2B, and
4B) or combustion zone 70 (as shown by FIG. 3B). The second gas injection assembly 60 is still
configured to inject a second stage gas (steam and/or an alternative gas) at a low flow rate and a
high pressure into the flare tip 10 (as shown by FIGS. 1B, 2B and 4B) or combustion zone 70 (as
shown by FIG. 3B). The second gas injection nozzle(s) 64 still includes at least one discharge
port that has a total discharge area of no greater than one-half of the corresponding total
discharge area of the discharge port(s) of the high flow rate, high pressure gas injection nozzle
54.
[0057] As best shown by FIG. 6, the second gas injection nozzle 64 includes a plurality of
discharge ports 64a, 64b, 64c, 64d, 64e and 64f. The gas injection nozzle 64 can include more
than 6 or less than 6 discharge ports as desired. For example, from 6 to 24 discharge ports can be
used. As with the other embodiments of the staged gas injection system 40, the discharge of
stage gas steam and/or an alternative gas) aspirates air from the surrounding atmosphere which is
mixed with the waste gas and helps promote smokeless combustion.
[0058] Referring now to FIGS. 7 and 8, another embodiment of the staged gas injection
system 40 will be described. This embodiment is the same in all respects as the embodiment of
the staged gas injection system 40 shown by FIGS. 1B, 2B, 3B and 4B, except for the
configuration of the second gas injection nozzle 64. In this embodiment, as shown by FIGS. 7
and 8, the discharge area of the second gas injection nozzle 64 is positioned above the vertical
center axis of the first gas injection nozzle 54. Alternatively, the discharge area of the second
gas injection nozzle 64 can be flush with or positioned below the first gas injection nozzle 54.
For example, the embodiment of the staged gas injection system 40 shown by FIGS. 7 and 8 can
be substituted for the embodiment of the staged gas injection system 40 shown by FIGS. 1B, 2B,
3B, 4B, 5 and 6.
wo 2022/074475 WO PCT/IB2021/057760
[0059] FIG. 9 illustrates another embodiment of the staged gas injection system 40 as used in
connection with the flare assembly and flare tip 10 shown by FIG. 1A. In this embodiment, the
staged gas injection system 40 is a three-stage gas injection system that includes a first gas
injection assembly 100, a second gas injection assembly 102, and a third gas injection assembly
104. The first gas injection assembly 100, second gas injection assembly 102, and third gas
injection assembly 104 are all proximate to each other and oriented in the same direction such
that all three gas injection assemblies inject stage gas (steam and/or an alternative gas) into the
inner tubular member 14 of the flare tip 10.
[0060] The first gas injection assembly 100 is configured to inject a first stage gas (steam
and/or an alternative gas) at a high flow rate and a high pressure into the inner tubular member
14 of the flare tip 10 of the flare assembly. The first gas injection assembly 100 includes a first
stage gas source 108 fluidly connected to a first gas injection nozzle 110. The first stage gas
source 108 provides the first stage gas to the first gas injection nozzle 110. The first gas
injection nozzle 110 discharges first stage gas into the inner tubular member 14 and in doing SO
aspirates air from the surrounding atmosphere into the pre-mix zone 16.
[0061] The second gas injection assembly 102 is configured to inject a second stage gas
(steam and/or an alternative gas) at a low flow rate and a high pressure into the inner tubular
member 14. The second gas injection assembly 102 includes a second stage gas source 112 that
is fluidly connected to a second gas injection nozzle 114. The second stage gas source 112
provides second stage gas to the second gas injection nozzle 114. The second gas injection
nozzle 114 includes at least one discharge port that has a total discharge area of no greater than
one-half of the corresponding total discharge area of the discharge port(s) of the high flow rate,
high pressure first gas injection nozzle 110. This allows the second gas injection assembly 102
to inject gas at a low flow rate and high pressure.
[0062] The third gas injection assembly 104 is configured to inject a third stage gas (steam
and/or an alternative gas) at a low flow rate and a high pressure into the inner tubular member 14
of the flare tip 10 of the flare assembly. The third gas injection assembly 104 includes a third
stage gas source 116 that is fluidly connected to a third gas injection nozzle 118. The third stage
gas source 116 provides the third stage gas to the third gas injection nozzle 118. The third gas
injection nozzle 118 includes at least one discharge port that has a total discharge area of no
WO wo 2022/074475 PCT/IB2021/057760
greater than one-half of the corresponding total discharge area of the discharge port(s) of the
second gas injection nozzle 114. This allows the third gas injection assembly 104 to inject gas at
an even lower flow rate and at high pressure. As with the other embodiments of the staged gas
injection system 40, the discharge of stage gas (steam and/or an alternative gas) aspirates air
from the surrounding atmosphere which is mixed with the waste gas and promotes smokeless
combustion.
[0063] Referring now to FIGS. 10 and 11, another embodiment of the staged gas injection
system 40 will be described. This embodiment of the staged gas injection system 40 is the same
in all respects as the embodiment of the staged gas injection 40 shown by FIG. 9, except the first
gas injection assembly 100, second gas injection assembly 102, and third gas injection assembly
104 are combined, in part, to form a single unit. The partial combination of the gas injection
assemblies into a single unit improves the distribution of stage gas by the system 40. For
example, the gas injection nozzles 110, 114 and 118 are combined together into a single unit.
The gas injection assemblies 100, 102 and 104 are still proximate to each other and oriented in
the same direction such that all three gas injection assemblies inject stage gas (steam and/or an
alternative gas) into the flare tip 10 or combustion zone 70. The first gas injection assembly 100
is still configured to inject a first stage gas at a high flow rate and a high pressure into the flare
tip 10 or combustion zone 70. The second and third gas injection assemblies 102 and 104 are
still configured to inject a gas (steam and/or an alternative gas) at a lower flow rate and a high
pressure into the flare tip 10 or combustion zone 70. The second gas injection nozzle 114 still
includes at least one discharge port that has a total discharge area of no greater than one-half of
the corresponding total discharge area of the discharge port(s) of the high flow rate, high
pressure gas injection nozzle 110. The third gas injection nozzle 118 still includes at least one
discharge port that has a total discharge area of no greater than one-half of the corresponding
total discharge area of the discharge port(s) of the gas injection nozzle 114. For example, this
embodiment of the staged gas injection system 40 can be substituted for the staged gas injection
system 40 shown by FIG. 9.
[0064] As best shown by FIG. 11, the second gas injection nozzle 114 includes a plurality of
discharge ports 114a, 114b, 114c, 114d, 114e and 114f). The gas injection nozzle 114 can
include more than 6 or less than 6 discharge ports as desired. For example, from 6 to 24
discharge ports can be used. The second gas injection nozzle 114 is positioned around the first
WO wo 2022/074475 PCT/IB2021/057760
gas injection nozzle 110. The third gas injection nozzle 118 is positioned on the vertical center
axis of the first gas injection nozzle 110. Although FIG. 11 shows the third gas injection nozzle
118 positioned above the first gas injection nozzle 110, the third gas injection nozzle can also be
flush with or positioned below the first gas injection nozzle. As with the other embodiments of
the staged gas injection system 40, the discharge of stage gas (steam and/or an alternative gas)
aspirates air from the surrounding atmosphere which is mixed with the waste gas and helps
promote smokeless combustion.
[0065] FIG. 12 illustrates use of the embodiment of the staged gas injection system 40 shown
by FIGS. 10 and 11 in connection with the flare configurations shown by FIGS. 1A and 1B. The
first gas injection nozzle 110, second gas injection nozzle 114, and third gas injection nozzle 118
each discharge stage gas (steam and/or an alternative gas) into the inner tubular member 14 to
aspirate air from the surrounding atmosphere into the pre-mix zone 16 in the outer tubular
member 12 of the flare tip 10. The aspirated air entrains into the waste gas conducted through
the gas passage 22 before it exits the flare tip 10. The waste gas/air mixture then exits the flare
tip 10. This again has the advantage of promoting smokeless combustion of the waste gas.
[0066] Although not shown by the drawings, additional features can also be included in the
staged gas injection system 40 disclosed herein. For example, in applicable embodiments, the
second gas injection assembly 60 can be thermally connected to the first gas injection assembly
50. This allows for the second gas injection assembly 60 to transfer heat into the first gas
injection assembly 50 and help keep the temperature of the steam lines in the first gas injection
assembly elevated to an acceptable level. For example, the temperature of the steam lines can be
maintained at the saturation temperature of water at local barometric pressure, or higher.
[0067] In another embodiment, the staged gas injection system 40 includes one gas injection
assembly. The gas injection assembly includes a stage gas source (steam source and/or
alternative gas source) and a fluidly connected gas injection nozzle. The stage gas source
provides stage gas (steam and/or alternative gas) to the gas injection nozzle. The gas injection
nozzle is a variable area gas injection nozzle having the ability to vary the exit area of the stage
gas as the stage gas pressure is increased, achieving the effect of low flow at high pressure and
high flow at high pressure.
WO wo 2022/074475 PCT/IB2021/057760
[0068] An advantage of using steam to entrain air into the waste gas is that it achieves
smokeless combustion of the waste gas. An advantage of having a staged gas injection system
that includes a gas injection assembly for injecting steam (and/or an alternative gas) at a low
flow rate and a high pressure is that it allows the flare assembly to operate using less steam at
turndown conditions. It allows for the necessary momentum to entrain air into the waste gas at
turndown conditions while utilizing less steam. For example, a standard steam nozzle of an
XPTM flare (sold by John Zink Hamworthy Combustion of Tulsa, Oklahoma) operating at 330
lb/hr of steam operates at less than 0.11 psig pressure and produces approximately 3 pounds
force (lbf) of momentum. A low flow nozzle operating at approximately 5 psig would also
produce approximately 3 lbf of momentum but would require less than 70 lb/hr of steam to do
SO. so.
[0069] The flare tip provided by the present disclosure includes a flare tip that includes the
staged gas injection system 40 described above. The flare tip can include any of the
configurations of the flare tip 10 described above. Any of the embodiments of the staged gas
injection system 40 described above can be used in association with the flare tip. As will be
understood, the stage gas for the various stages can be the same gas or different. For example,
the first stage gas, second stage gas and third stage gas (if used) can all be steam; or the first
stage gas can be steam and the second can be an alternative gas (such as nitrogen or air); or the
first stage gas can be an alternative gas (such as nitrogen or air) and the second stage gas can be
steam; or the first stage can be steam and an alternative gas, and the second stage can be an
alternative gas; or the first stage can be air, the second stage can be nitrogen, and the third can be
steam. Other combinations can also be utilized.
EXAMPLE
[0070] The staged gas injection system shown by FIG. 4B herein was tested. As shown, the
flare tip 10 included both standard high flow high pressure (HFHP) steam nozzles and low flow
high pressure (LFHP) steam nozzles. In carrying out the tests, steam was injected through both
the HFHP nozzles and the LFHP nozzles.
[0071] The first phase of the test consisted of various flow rates of steam being sent to the
HFHP nozzles while the steam flow to the LFHP nozzles was turned off. For each flow rate of
WO wo 2022/074475 PCT/IB2021/057760
HFHP steam, the hydrocarbon flow rate to the flare tip was adjusted to the maximum that still
produced smokeless combustion.
[0072] The second phase of the test consisted of various flow rates of steam being sent to the
LFHP nozzles while the steam flow to the HFHP nozzles was turned off. For each flow rate of
LFHP steam, the hydrocarbon flow rate to the flare was adjusted to the maximum that still
produced smokeless combustion.
[0073] FIG. 13 illustrates the results of the tests. In summary, the tests showed that the
amount of steam needed for smokeless combustion at turndown conditions can be reduced by
using LFHP steam nozzles.
[0074] Additionally, a computer model simulation (based on experimental test data) was
performed comparing the air entrainment performance using both steam and air as the first stage
gas source. FIG. 14 illustrates the results of the simulation. The results show that for a given first
stage gas source pressure, the air entrainment performance for both air and gas is nearly
identical. Thus, illustrating that the first stage gas can be steam or an alternative gas.
[0075] Therefore, the present disclosure is well adapted to attain the ends and advantages
mentioned, as well as those that are inherent therein. The particular embodiments disclosed
above are illustrative only, as the present disclosure may be modified and practiced in different,
but equivalent, manners apparent to those skilled in the art having the benefit of the teachings
herein. Furthermore, no limitations are intended to the details of construction or design herein
shown, other than as described in the claims below. It is therefore evident that the particular
illustrative examples disclosed above may be altered or modified, and all such variations are
considered within the scope and spirit of the present disclosure. While apparatus and methods
may be described in terms of "comprising," "containing," "having," or "including" various
components or steps, the apparatus and methods can also, in some examples, "consist essentially
of" or "consist of" the various components and steps. Whenever a numerical range with a lower
limit and an upper limit is disclosed, any number and any included range falling within the range
are specifically disclosed. In particular, every range of values (of the form, "from about a to
about b," or, equivalently, "from approximately a to b," or, equivalently, "from approximately a-
b") disclosed herein is to be understood to set forth every number and range encompassed within
WO wo 2022/074475 PCT/IB2021/057760
the broader range of values. Also, the terms in the claims have their plain, ordinary meaning
unless otherwise explicitly and clearly defined by the specification.

Claims (14)

  1. 2021356482 12 2023
    The claims defining the invention are as follows:
    Apr 1. 1. A staged gas injection system for a flare tip that can discharge waste gas into a combustion zone downstream from the flare tip, and the flare tip includes an inner tubular member disposed within an outer tubular member so as to form a pre-mix zone downstream from the inner tubular member and within the outer tubular member, the staged gas injection system comprising: 2021356482
    a first stage gas source, the first stage gas source being a source of first stage gas, wherein the first stage gas consists of alternative gas; a first gas injection assembly, said first gas injection assembly being configured to inject the first stage gas at a high flow rate and a high pressure into the inner tubular member of the flare tip and including: a first gas injection nozzle fluidly connected to said first stage gas source from which said first stage gas is received by the first gas injection nozzle; a second stage gas source, said second stage gas source being a source of second stage gas; a second gas injection assembly, said second gas injection assembly configured to inject said second stage gas at a low flow rate and a high pressure into the inner tubular member of the flare tip and including: a second gas injection nozzle fluidly connected to said second stage gas source from which said second stage gas is received by the second gas injection nozzle, wherein said first gas injection assembly and said second gas injection assembly are proximate to each other and oriented in the same direction such that said first gas injection assembly injects first stage gas into the inner tubular member of the flare tip and the second gas injection assembly injects second stage gas into the inner tubular member of the flare tip, and wherein the low flow rate means the first gas injection assembly and second gas injection assembly are configured such that, on a per nozzle basis, the low flow rate is one-half or less than the high flow rate.
  2. 2. The staged gas injections system of claim 1, wherein the second stage gas comprises an alternative gas.
  3. 3. The staged gas injection system of claim 1, wherein the second stage gas comprises steam.
    22
  4. 4. The staged gas injection system of any preceding claim, wherein said first stage gas consists of air.
  5. 5. 5. The staged gas injection system of any preceding claim, further comprising: a third gas injection assembly, said third gas injection assembly configured to inject gas at a low flow rate and a high pressure into the inner tubular member of the flare tip, and 2021356482
    wherein said first gas injection assembly, said second gas injection assembly and said third gas injection assembly are proximate to each other and oriented in the same direction such that said first gas injection assembly, second gas injection assembly and third gas injection assembly inject gas into the inner tubular member of the flare tip.
  6. 6. The staged gas injection system of claim 5, wherein: the third gas injection assembly includes: a third stage gas source, said third stage gas source being a source of third stage gas; a third gas injection nozzle fluidly connected to said third stage gas source such that the third stage gas is injected at a low flow rate and a high pressure by the third gas injection assembly into the inner tubular member of the flare tip.
  7. 7. 7. The staged gas injection system of claim 6, wherein said third stage gas is an alternative gas.
  8. 8. The staged gas injection system of any one of claims 5 to 7, wherein the low flow rate for the second gas injection assembly means the first gas injection assembly and second gas injection assembly are configured such that, on a per nozzle basis, the low flow rate of the second gas injection assembly is one-half or less than the high flow rate, and the low flow rate for the third gas injection assembly means the second gas injection assembly and third gas injection assembly are configured such that, on a per nozzle basis, the low flow rate of the third gas injection assembly is one-half or less than the low flow rate of the second gas injection assembly.
  9. 9. A staged gas injection system for a flare tip that can discharge waste gas into a combustion zone downstream from the flare tip, comprising:
    2021356482 12 2023
    a first stage gas source, the first stage gas source being a source of first stage gas, wherein the first stage gas consists of alternative gas; Apr a first gas injection assembly, said first gas injection assembly being configured to inject the first stage gas at a high flow rate and a high pressure into the combustion zone and including a first gas injection nozzle fluidly connected to said stage gas source from which said first stage gas is received by the first gas injection nozzle; 2021356482
    a second stage gas source, said second stage gas source being a source of second stage gas; a second gas injection assembly, said second gas injection assembly configured to inject said second stage gas at a low flow rate and a high pressure into the combustion zone and including a second gas injection nozzle fluidly connected to said second stage gas source from which said second stage gas is received by the second gas injection nozzle, wherein said first gas injection assembly and said second gas injection assembly are proximate to each other and oriented in the same direction such that said first gas injection assembly injects first stage gas into the combustion zone and said second gas injection assembly injects second stage gas into the combustion zone, and wherein the low flow rate means the first gas injection assembly and second gas injection assembly are configured such that, on a per nozzle basis, the low flow rate is one-half or less than the high flow rate.
  10. 10. The staged gas injections system of claim 9, wherein the second stage gas comprises an alternative gas.
  11. 11. The staged gas injection system of claim 9, wherein the second stage gas comprises steam.
  12. 12. The staged gas injection system of any one of claims 9 to 11, wherein said first stage gas consists of air.
  13. 13. The staged gas injection system of any one of claims 9 to 12, further comprising: a third gas injection assembly, said third gas injection assembly configured to inject gas at a low flow rate and a high pressure into the combustion zone, and wherein said first gas injection assembly, said second gas injection assembly and said third gas injection assembly are proximate to each other and oriented in the
    same direction such that said first gas injection assembly, second gas injection assembly and third gas injection assembly inject gas into the combustion zone.
  14. 14. 14. The staged gas injection system of claim 13, wherein: the third gas injection assembly includes: a third stage gas source, said third stage gas source being a source 2021356482
    of third stage gas; a third gas injection nozzle fluidly connected to said third stage gas source such that the third stage gas is injected at a low flow rate and a high pressure by the third gas injection assembly into the combustion zone.
    15. The staged gas injection system of either claims 13 or 14, wherein the low flow rate for the second gas injection assembly means the first gas injection assembly and second gas injection assembly are configured such that, on a per nozzle basis, the low flow rate of the second gas injection assembly is one-half or less than the high flow rate, and the low flow rate for the third gas injection assembly means the second gas injection assembly and third gas injection assembly are configured such that, on a per nozzle basis, the low flow rate of the third gas injection assembly is one-half or less than the low flow rate of the second gas injection assembly.
    WO 2022/074475 2022/07445 oM PCT/IB2021/057760
    OZ 70 2/14 20 20 16 16
    10 10
    26 26
    12 12
    18
    22 22
    14 14 28 28
    24
    50,54
    60,64
    40 40
    62 62
    WO 2022/074475 2022/07445 OM PCT/IB2021/057760
    3/14 70 OZ 20 16
    10
    26 26
    22
    12
    28
    28 14 14
    14
    24 24 64 64 954 9 54
    09 50 50 09 09 60 09 60
    40 10
    62 52
    WO 2022/074475 2022/07445 oM PCT/IB2021/057760 PCT/IB2021/057760
    200 4/14 70 20 16
    10
    26 26
    28
    22
    12 12 28
    28
    28 14
    14 24 24 24 50,54
    50,54 60,64 60,64
    10 40
    62 52
    -
    WO 2022/074475 2022/07447 OM PCT/IB2021/057760 PCT/IB2021/057760
    5/14 70
    64 64 9 54 20 954 266 26 26 09 60 50 09 09 50 09 60
    10 40
    10 12 12
    14 22 14,28 62 52 52 I
    70 OL
    200 50,54 20 50,54 26 26 26 60,64 60,64
    40 10
    12
    10
    62 14,28 22 14,28 52 52
    I
    I
    WO 2022/074475 2022/07445 OM PCT/IB2021/057760
    7/14 70 OZ OZ 70
    200 16 20 20 16
    10 10 10
    22 22 26 26
    12
    12 28
    14 28 14
    34 18 18 18
    30 00 14
    24 24 50,54 36 9£ 50,54 60,64 60,64
    01 40 32 40 10
    62 62 62
    52 52 52
    50,54 50,54
    60,64
    60,64
    60,64 40
    62 52
    60,64,64c
    60,64,64d 60,64,64b
    50,54
    60,64,64e 60,64,64a
    40 60,64,64f
    go
    WO 2022/074475 2022/07447 OM PCT/IB2021/057760
    9/14 64 64 OZ 70 60,64
    50,54
    10 40
    52 62
    I - 94 64
    50,54
    60,64
    10 40
    age edite
    -
    PCT/IB2021/057760
    10/14 70 70 20 16
    10 26
    12
    18
    22
    14 28
    24 118 110 104 114
    102 40 100
    116
    108 112
    104,118
    100,110
    40
    102,114
    102,114
    136
    134 132
    102,114c
    102,114b 102,114d
    138 100,110
    104,118 118
    100,110
    102,114e 102,114a
    40 102,114f
    H
    WO 2022/074475 2022/07445 OM PCT/IB2021/057760
    OL 70 12/14 200 20 16
    10 10
    26
    12
    18
    22
    14 14 28
    24
    104,118 100,110
    102,114 102,114
    10 40 136
    132 134
    apply
    WO 2022/074475
    Flow Fuel Normalied VS Ratio Steam/Hydrocarbon Normalized 1 High Through Flow Steam High Through Flow Steam 0.9 Nozzle Pressure High Rate, Flow Nozzle Pressure High Rate, Flow 0.8 Low Through Flow Steam Low Through Flow Steam Nozzle Pressure High Rate, Flow Nozzle Pressure High Rate, Flow 0.7 0.6 0.5 0.4 0.3
    Normalized S/HC Ratio(Ib/lb) 0.2 0.1
    0 0.1 0.3 0.4
    0.2 0.9 and
    1
    0 0.8
    0.7
    0.6
    0.5 Rate(lb/hr) Fuel Flare Normalized Rate(Ib/hr) Fuel Flare Normalized wo 2022/074475
    Performance Entrainment Air of Simulation Model Computer Performance Entrainment Air of Simulation Model Computer Source Gas Stage First the as Air And Steam Using Source Gas Stage First the as Air And Steam Using 1 Source Gas Stage First As Air Source Gas Stage First As Air 0.9 Source Gas Stage First As Steam Source Gas Stage First As Steam 0.8 0.7 14/14
    0.6 0.5 0.4 0.3 0,5 and
    1
    0.4
    0.2 0.6
    0.1 0.3 0.7 0.9
    0.8
    Normalized Source, Gas Stage First of Pressure Normalized Source, Gas Stage First of Pressure PCT/IB2021/057760
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US3822985A (en) * 1973-08-13 1974-07-09 Combustion Unltd Inc Flare stack gas burner
US4101257A (en) * 1977-06-16 1978-07-18 Combustion Unlimited Incorporated Pilot gas conservation system for flare stacks
US20190024889A1 (en) * 2015-12-23 2019-01-24 John Zink Company, Llc Staged Steam Injection System

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1323674A (en) * 1969-06-24 1973-07-18 Ici Ltd Flare stacks and steam/air mixing devices therefor
US7967600B2 (en) * 2006-03-27 2011-06-28 John Zink Company, Llc Flare apparatus
US8629313B2 (en) * 2010-07-15 2014-01-14 John Zink Company, Llc Hybrid flare apparatus and method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3822985A (en) * 1973-08-13 1974-07-09 Combustion Unltd Inc Flare stack gas burner
US4101257A (en) * 1977-06-16 1978-07-18 Combustion Unlimited Incorporated Pilot gas conservation system for flare stacks
US20190024889A1 (en) * 2015-12-23 2019-01-24 John Zink Company, Llc Staged Steam Injection System

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