CA2240646C - Flameless combustor - Google Patents
Flameless combustor Download PDFInfo
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- CA2240646C CA2240646C CA002240646A CA2240646A CA2240646C CA 2240646 C CA2240646 C CA 2240646C CA 002240646 A CA002240646 A CA 002240646A CA 2240646 A CA2240646 A CA 2240646A CA 2240646 C CA2240646 C CA 2240646C
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- Prior art keywords
- combustion
- combustor
- fuel
- combustion chamber
- tubular
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- 238000002485 combustion reaction Methods 0.000 claims abstract description 118
- 239000000446 fuel Substances 0.000 claims abstract description 52
- 239000003054 catalyst Substances 0.000 claims abstract description 36
- 239000000203 mixture Substances 0.000 claims abstract description 30
- 238000007254 oxidation reaction Methods 0.000 claims abstract description 22
- 230000015572 biosynthetic process Effects 0.000 claims description 44
- 239000007800 oxidant agent Substances 0.000 claims description 28
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 claims description 25
- 238000000034 method Methods 0.000 claims description 19
- 230000001590 oxidative effect Effects 0.000 claims description 19
- 238000010438 heat treatment Methods 0.000 claims description 12
- 229910052763 palladium Inorganic materials 0.000 claims description 12
- 229910000510 noble metal Inorganic materials 0.000 claims description 10
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims description 10
- 238000000576 coating method Methods 0.000 claims description 7
- 239000011248 coating agent Substances 0.000 claims description 6
- 239000000567 combustion gas Substances 0.000 claims description 6
- 230000035699 permeability Effects 0.000 claims description 5
- 238000004891 communication Methods 0.000 claims description 4
- 229910052697 platinum Inorganic materials 0.000 claims description 4
- 239000010970 precious metal Substances 0.000 claims description 3
- 230000001939 inductive effect Effects 0.000 claims description 2
- 239000004058 oil shale Substances 0.000 claims description 2
- 229910000314 transition metal oxide Inorganic materials 0.000 claims description 2
- 230000003197 catalytic effect Effects 0.000 abstract description 17
- 238000009826 distribution Methods 0.000 abstract description 12
- 230000003647 oxidation Effects 0.000 abstract description 12
- 238000006243 chemical reaction Methods 0.000 abstract description 4
- 238000006454 non catalyzed reaction Methods 0.000 abstract 1
- 238000005755 formation reaction Methods 0.000 description 39
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 30
- 239000002737 fuel gas Substances 0.000 description 17
- GQPLMRYTRLFLPF-UHFFFAOYSA-N Nitrous Oxide Chemical class [O-][N+]#N GQPLMRYTRLFLPF-UHFFFAOYSA-N 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 239000004568 cement Substances 0.000 description 7
- 239000007789 gas Substances 0.000 description 7
- 229910052799 carbon Inorganic materials 0.000 description 6
- 229930195733 hydrocarbon Natural products 0.000 description 6
- 150000002430 hydrocarbons Chemical class 0.000 description 6
- 238000002156 mixing Methods 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 238000002347 injection Methods 0.000 description 5
- 239000007924 injection Substances 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 4
- 238000010276 construction Methods 0.000 description 4
- 238000011084 recovery Methods 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 229910002092 carbon dioxide Inorganic materials 0.000 description 3
- 238000009841 combustion method Methods 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 230000001965 increasing effect Effects 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 230000000153 supplemental effect Effects 0.000 description 3
- MFRCZYUUKMFJQJ-UHFFFAOYSA-N 1,4-dioxane-2,5-dione;1,3-dioxan-2-one Chemical compound O=C1OCCCO1.O=C1COC(=O)CO1 MFRCZYUUKMFJQJ-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 239000000571 coke Substances 0.000 description 2
- 230000020169 heat generation Effects 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 239000003345 natural gas Substances 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 238000009834 vaporization Methods 0.000 description 2
- 230000008016 vaporization Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 101150033248 AME1 gene Proteins 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 235000015076 Shorea robusta Nutrition 0.000 description 1
- 244000166071 Shorea robusta Species 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
- 150000002632 lipids Chemical class 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000001272 nitrous oxide Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000002002 slurry Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B36/00—Heating, cooling or insulating arrangements for boreholes or wells, e.g. for use in permafrost zones
- E21B36/02—Heating, cooling or insulating arrangements for boreholes or wells, e.g. for use in permafrost zones using burners
Landscapes
- Geology (AREA)
- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mining & Mineral Resources (AREA)
- Geochemistry & Mineralogy (AREA)
- Fluid Mechanics (AREA)
- Environmental & Geological Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Physics & Mathematics (AREA)
- Gas Burners (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Wick-Type Burners And Burners With Porous Materials (AREA)
- Gasification And Melting Of Waste (AREA)
- Incineration Of Waste (AREA)
Abstract
A flameless combustor eliminates the flamme as a radiant heat source, which results in a more even temperature distribution throughout the length of the burner. Flameless combustion is accomplished by preheating the fuel and the combustion air to a temperature above the autoignition temperature of the mixture. The present invention lowers the autoignition temperature by placing a catalytic surface within the desired combustion chamber. Temperatures are maintained above the catalyzed autoignition temperature but less than the noncatalyzed autoignition temperatures for noncatalyzed reaction. Thus, the amount and location of reaction can be controlled by varying the amount and distribution of catalyst within the burner. Removing heat from the combustion chamber in amounts that correspond to the oxidation of fuel within different segments of the combustion chamber can result in low temperatures and relatively even distribution of heat from the burner.
Description
FLAMELESS COMBUSTOR
This invention relates to a flameless combustion ' apparatus and method.
U.S. Patent Nos. 4,640,352 and 4,886,118 disclose conductive heating of subterranean formations of low permeability that contain oil to recover oil therefrom.
Low permeability formations include diatomites, lipid , coals, and oil shales. Formations of low permeability are not amiable to secondary oil recovery methods such as steam, carbon dioxide, or fire flooding. Flooding materials tend to penetrate formations that have low permeabilities preferentially through fractures. The injected materials bypass most of the formation hydro-carbons. In contrast, conductive heating does not require fluid transport into the formation. Oil within the formation is therefore not bypassed as in a flooding process. When the temperature of a formation is increased by conductive heating, vertical temperature profiles will tend to be relatively uniform because formations generally have relatively uniform thermal conductivities and specific heats. Transportation of hydrocarbons in a thermal conduction process is by pressure drive, vaporization, and thermal expansion of oil and water trapped within the pores of the formation rock. Hydrocarbons migrate through small fractures created by the expansion and vaporization of the oil and water.
U.S. Patent No. 5,255,742 discloses a flameless combustor useful for heating subterranean formations that utilizes preheated fuel gas and/or combustion air wherein the fuel gas is combined with the combustion air in increments that are sufficiently small that flames are avoided. Creation of NOx is almost eliminated, and cost of the heaters can be significantly reduced because of less expensive materials of construction. Preheating the fuel gas in accordance with the method disclosed in this prior art reference may result in coke formation unless C02, H2, or steam is added to the fuel gas. Further, start-up of the known heater is a time consuming process because it must operate at temperatures above the uncatalyzed autoignition temperature of the fuel gas mixture.
Catalytic combustors are also known. For example, U.S. Patent No. 3,928,961 discloses a catalytically-sup-ported thermal combustion apparatus wherein formation of NOx is eliminated by combustion at temperatures above auto-ignition temperatures of the fuel, but less than those temperatures at which result in substantial formation of oxides of nitrogen.
Metal surfaces coated with oxidation catalyst are disclosed in, for example, U.S. Patent Nos. 5,355,668 and 4,065,917. These patents suggests catalytic coated surfaces on components of a gas turbine engine. Said US
Patent 4,065,917 suggests use of catalytic coated surfaces for start-up of the turbine, and suggests a mass transfer control limited phase of the start-up operation.
The combustor and flameless combustion method in accordance with the preamble of claims 1 and 16 are disclosed in U.S. Patent No. 3,817,332. In the known method fuel and oxidant are fed to the combustion chamber via separate supply conduits which is expensive but necessary to avoid premature combustion of the fuel in the supply conduit.
It is an object of the present invention to provide a flameless combustor wherein fuel and oxidant can be AMEt'~~D SHEET
fPE~P
- 2a -combined initially, and distribution of combustion determined by distribution of catalytic surfaces within a combustion chamber.
It is also an object of the present invention to provide a combustion method and apparatus which is flameless, and does not require additives in a fuel gas stream to prevent formation of coke. In another aspect of the present invention, it is an object to provide a combustion method and apparatus wherein formation of NOX is minimal.
A~~~i~~'~ ~~~ t v ~n~~~r:
WO 97/24510 PCTlEP96/05754 These and other objects are accomplished by a flameless combustor for combustion of a fuel and oxidant mixture, the combustor comprising:
a combustion chamber in communication with an inlet and with a combustion product outlet;
a mixed fuel and oxidant supply in communication with the inlet; and a catalyst surface within the combustion chamber wherein the catalyst surface is effective to cause oxidization of an amount of fuel wherein the oxidization of the amount of fuel does not result in a temperature above an uncatalyzed autoignition temperature of the fuel and oxidant mixture.
The flameless combustor of the present invention results in minimal production of nitrous oxides because temperatures that would result from adiabatic combustion of the fuel-oxidant mixture are avoided. Other measures to remove or prevent the formation of nitrous oxides are therefore not required. Relatively even heat distribu-tion over a large area and long lengths are possible, and relatively inexpensive materials of construction for the combustor of the present invention can be used because of lower combustion temperatures.
Acceptable catalyst materials include noble metals, semi-precious metals, and transition metal oxides.
Generally, known oxidation catalysts are useful in the present invention. Mixtures of such metals or metal oxides could also be useful.
The flameless combustor of the present invention is particularly useful as a heat injector for heating subterranean formations for recovery of hydrocarbons.
The catalytic surfaces also improve operability and start-up operations of such heat injectors. The present invention eliminates a need to transport fuels and oxidants in separate conduits to the combustion zone in such heat injectors. This results in significant cost savings.
Tn accordance with the invention there is also provided a method of heating a subterranean formation by ' flameless combustion. The method according to the invention comprises:
installing a combustion tubular which defines a downhole combustion chamber in a wellbore within the formation to be heated;
feeding fuel and oxidant to the chamber via an inlet;
inducing the fuel and oxidant mixture to flow along a catalyst surface within the combustion chamber wherein the catalyst surface is effective to cause oxidization of an amount of fuel at such a rate that the average temperature in the combustion chamber remains below the uncatalyzed autoignition temperature of the fuel and oxidant mixture; and allowing combustion products to flow to the surface via a combustion product outlet conduit within the wellbore.
Preferably the combustion chamber is defined by a lower portion of a well casing and a plug near the bottom of the well casing and the catalyst surface is provided by a catalyst coating on the inner and/or outer surface of a tubular which is co-axially suspended within the well casing such that an axial spacing is maintained between a lower end of the suspended tubular and the plug.
It is also preferred that the suspended tubular is used as a mixed fuel and air inlet conduit and the annular space between the suspended tubular and the well casing is used as a combustion product outlet conduit or , vice versa.
These and other features, objects and advantages of the combustor and method according to the present invention will become apparent from the accompanying drawings, in which:
FIG. 1 shows a combustor according to the present ' invention; and FIG. 2 is a plot of methane consumption vs.
' temperature in a test apparatus demonstrating the present invention.
Generally, flameless combustion is accomplished by preheating combustion air and fuel gas sufficiently that when the two streams are combined the temperature of the mixture exceeds the autoignition temperature of the mixture, but to a temperature less than that which would result in the oxidation upon mixing being limited by the rate of mixing. Without a catalyst surface present, preheating of the streams to a temperature between about 815 C and about 1260 C and then mixing the fuel gas into the combustion air in relatively small increments will result in flameless combustion.
With an effective catalytic surface present, the temperature at which oxidation reactions occur in a region affected by the catalytic surface is significantly lowered. This reduced temperature is referred to herein as a catalyzed autoignition temperature. In turbulent flow, fluid-in a boundary layer that contacts the catalytic surface will be oxidized almost quantitatively, but almost no oxidation will occur outside of the boundary layer if the bulk temperatures remain below the non-catalyzed autoignition temperatures of the mixture.
Thus, reaction in the temperature range between the catalyzed autoignition temperature and the noncatalyzed autoignition temperature is mass-transfer limited, at a rate that is relatively independent of temperature. This is suggested in references such as U.S. Patent No. 4,065,917. This mass transfer limited reaction mechanism is utilized in the present invention to control distribution of heat generation within the combustion chamber of the flameless combustor. Heat generation and heat removal can be balanced so that the average stream temperature of the mixed oxidant, fuel, and combustion ' products remains between the catalyzed autoignition temperature and the noncatalyzed autoignition temper- "
ature.
The heater of the present invention can be controlled by such variables as fuel-oxidant ratio, fuel-oxidant flowrate. Depending on the particular application, the heat load~may be subject to controls.
An important feature of the flameless combustor of the present invention is that heat is removed along the axis of the combustion chamber so that a temperature is maintained that is significantly below the adiabatic combustion temperature. This almost eliminates formation of NOxs, and also significantly reduces metallurgical requirements resulting in a relatively inexpensive combustor.
Referring to FIG. 1, a combustor within a heat injection well capable of carrying out the present invention is shown. A formation to be heated, 1, is below an overburden, 2. A wellbore, 3, extends through the overburden and to a position that is preferably near the bottom of the formation to be heated. A vertical well is shown, but the wellbore could be deviated or horizontal.
Horizontal heat injector wells may be provided in formations that fracture horizontally to recover hydrocarbons by a parallel drive process. Shallow oil shale formations are examples of formations where horizontal heaters may be useful. Horizontal heaters may also be effectively used when thin layers are to be , heated to limit heat loss to overburden and base rock.
In the embodiment shown in Figure 1, the wellbore-is cased with a casing, 4. The lower portion of the wellbore WO 97/24510 PCTlEP96/05754 _ 7 _ may be cemented with a cement, 7, having characteristics suitable for withstanding elevated temperatures and transferring heat. A cement which is a good thermal ' insulator, 8, is preferred for the upper portion of the wellbore to prevent heat loss from the system. A
combustion mixture conduit, 10, extends from the wellhead (not shown) to the lower portion of the wellbore.
High temperature cements suitablefor cementing casing and conduits within the high temperature portions of the wellbore are available. Examples are disclosed in U.S. Patent Nos. 3,507,332 and 3,180,748. Alumina contents above about 50 percent by weight based on cements slurry solids are preferred.
In shallow formations, it may be advantageous to hammer-drill the heater directly into the formation.
When the heater is hammer-drilled directly into the formation, cementing of the heater in the formation may not be required, but an upper portion of the heater may be cemented to prevent fluid loss to the surface.
Choice of a diameter of the casing, 4, in the embodiment of FIG. 1 is a trade-off between the expense of the casing, and the rate at which heat may be transferred into the formation. The casing, due to the metallurgy required, is generally the most expensive component of the injection well. The heat that can be transferred into the formation increases significantly with increasing casing diameter. A casing of between about l0 and about 20 cm in internal diameter will typically provide an optimum trade-off between initial cost and capability to transferheat from the wellbore.
A cement plug 23 is shown at the bottom of the . casing, the cement plug being forced down the casing during the cementing operation to force cement out the bottom of the casing.
WO 97!24510 PCT/EP96/05754 _ g _ Catalyst surfaces 20 are provided within the combustion chamber 14 to provide a limited region~where.in the oxidation reaction temperature is lowered.
Distribution of these catalyst surfaces 20 as a coating which covers at least part ofthe inner and/or outer surface of a lower portion of the conduit 10 provide for "
distribution of heat release within the combustion chamber. The catalyst surfaces are sized to accomplish a nearly even temperature distribution along the casing. A
nearly even temperature profile within the casing results in more uniform heat distribution within the formation to be heated. A nearly uniform heat distribution within the formation will result in more efficient utilization of heat in a conductive heating hydrocarbon recovery process. A more even temperature profile will also result in the lower maximum temperatures for the same heat release. Because the materials of construction of the burner and well system dictate the maximum temper-atures, even temperature profiles will increase the heat release possible for the same materials of construction.
As the combustion products rise in the wellbore above the formation being heated, heat is exchanged between the combustion air and the fuel gas travelling down the flow conduits and the rising combustion products. This heat exchange not only conserves energy, but permits the desirable flameless combustion of the present invention.
The fuel gas and the combustion air are preheated as they travel down the respective flow conduits sufficiently that the mixture of the two streams at the ultimate mixing point is at a temperature above the catalyzed autoignition temperature of the mixture, but below the noncatalyzed autoignition temperature. Combustion on the , catalyst surface and flameless combustion within boundary layers adjacent to effective catalyst surfaces results, , avoiding a flame as a radiant heat source_ Heat is therefore transferred from the wellbore in an essentially uniform fashion.
It is important in the operation of a combustor of the present invention that heat be removed from the combustion chamber along the length of the combustion chamber. In the application of the present invention to a wellbore heat injector, heat is transferred to the formation around the wellbore. The heater of the present invention could also be used in other applications, such as steam generation and chemical industry process heaters and reactors.
Fuel gas and combustion air transported to the bottom of the wellbore through a mixed fuel and oxidant supply (22) which is shown as an annular volume surrounding the combustion product conduit. The mixed fuel and air react within the wellbore volume adjacent to the catalyst surfaces 14 forming combustion products. The combustion products travel up the wellbore and out an exhaust vent (not shown) at the wellhead through the combustion product conduit 10. From the exhaust vent, the combustion products may be routed to atmosphere through an exhaust stack (not shown). Alternatively, the combustion gases may be treated to remove pollutants, although nitrous oxides would not be present and would not therefore need to be removed. Additional energy recovery from the combustion products by an expander turbine or heat exchanger may also be desirable.
Preheating of the fuel gases to obtain flameless combustion without a catalyst would result in significant generation of carbon unless a carbon formation suppressant is included in the fuel gas stream. The need to provide such a carbon formation suppressant is therefore avoided by operating the heater at a temperature that is less than the carbon formation temperature. This is another significant advantage of AMEf~GED SHEE'!' IPE~P
WO 97/24510 PCT/EP9b/05754 - to -the present invention because the carbon suppressant increases the volume of gases to be passed through the heater and therefore increases the size of conduits required.
Cold start-up of a well heater of the present -invention may utilize combustion with a flame. Initial ignition may be accomplished by injecting pyrophoric material, an el-ectrical igniter, a spark igniter, temporally lowering an igniter into the wellbore, or an electrical resistance heater. The burner is preferably rapidly brought to a temperature at which a flameless combustion is sustained to minimize the time period at which a flame exists within the wellbore. The rate of heating up the burner will typically be limited by the thermal gradients the burner can tolerate.
The combustion mixture conduit can be utilized as a resistance heater to bring the combustor up to an operating temperature. To utilize this conduit as a resistance heater, an electrical lead 15 can be connected with a clamp 16 or other connection to the combustion mixture conduit 10 near the wellhead below an electrically insulating coupling to supply electrical energy. Electrical ground can be provided near the bottom of the borehole with one or more electrically conducting centralizers 17 around the combustion mixture conduit 10. Centralizers on the combustion mixture conduit above the electrically grounding centralizers are electrically insulating centralizers. Sufficient heat is preferably applied to result in the combustion mixture being, at the location of the initial catalyst surface, at a temperature that is above the catalyzed autoignition temperature but below the noncatalyzed auto ignition , temperature.
Thickness of the combustion mixture conduit can be varied to result is release of heat at preselected WO 97I245I0 PCTlEP96/05754 segments of the length of the fuel conduit. For example, in a well heat injector application, it may be desirably to electrically heat the lowermost portion of the wellbore in order to ignite the mixed gas stream at the highest concentration of fuel, and to burn the fuel before exhaust gasses are passed back up through the wellbore. Thin section 21 is shown in the combustion mixture conduit to provide a surface of elevated temperature for start-up of the combustor.
Oxidation reaction temperature of the fuel gas-oxidant mixture is lowered by provision of a noble metal surface, or another effective catalyst surface.
Catalytic surface is preferably provided on the either the inside, outside, or both inside and outside surface of the combustion products conduit 10. Alternatively, a surface, or a tubular or other noble metal containing surface, could be separately placed within the combustion chamber. Other noble metal coated surfaces could be provided, for example, in the combustion product annulus outside of the combustion gas conduit. This additional catalyst surface could ensure that complete combustion occurred within the wellbore, where generation of heat is desired.
Start-up of the flameless combustor of the present invention can be further enhanced by provision of supplemental oxidants during the start-up phase, or by use of a fuel that has a lower autoignition temperature such as hydrogen. Preferred supplemental oxidants include supplemental oxygen and nitrous oxide. Hydrogen could be provided along with a natural gas stream, and could be provided as shift gas, with carbon monoxide present and carbon dioxide present.
Start-up oxidants and/or fuels are preferably only used until the combustor has been heated to a temperature sufficient to enable operation with methane (natural gas) as fuel and air as the oxidant (i.e., the combustor has heated to a temperature above the catalyzed autoignition temperature of methane in air).
US patent 5,255,742 disclosed using an electrical ' resistance nicrome heater to generate heat for start-up of the flameless combustor. Such an electrical heater may be used in the practice of the present invention.
Noble metals such as palladium or platinum, or semi-precious metal, base metal or transition metal can l0 be coated, preferably by electroplating, onto a surface within the combustion chamber to enhance oxidation of the fuel at lower temperatures. The metal could then be oxidized as necessary to provide a catalytically effective surface. Such catalytic surface has been found to be extremely effective in-promoting oxidation of methane in air at temperatures as~low as 260 °C. This reaction rapidly occurs on the catalytic surface and in the adjacent boundary layer. An advantage of having a significant catalytic surface within the combustion chamber is that the temperature range within which the flameless combustor can operate can be significantly increased.
FXAMPT~F~
A thermal reactor was used to establish temperatures at which oxidation reactions would occur with various combinations of fuels, oxidants and catalyst surfaces.
The reactor was a 2.54 cm stainless steel pipe wrapped with an electrical resistance heating coil, and covered with insulation. A thermocouple for temperature control was placed underneath the insulation adjacent to the outer surface of the pipe. Thermocouples were also provided inside the pipe at the inlet, at the middle, and , at the outlet. Test ribbons of noble metals or stainless steel strips with noble metal coatings were hung in the pipe to test catalytic activity. Air preheated to a temperature somewhat below the desired temperature of the test was injected into the electrically heated test section of the pipe. Electrical power to the electrical resistance heater was varied until the desired temperature in the test section was obtained and a steady state, as measured by the thermocouples mounted inside the pipe, was achieved. Fuel was then injected through a mixing tee into the stream of preheated air and allowed to flow into the electrically heated test section. Four platinum ribbons one eighth of an inch (= 0.32 cm) wide and about sixteen inches (= 40 cm) long or a stainless steal strip three eighths of an inch (= 0.95 cm) wide and about one sixteenth of an inch (= 0.16 cm) thick and about sixteen inches (= 40 cm) long coated on both sides with either platinum or palladium were suspended within the pipe to test catalytic activity. When the test section contained a catalyst coated strep or ribbon of noble metal and was at or above the catalyzed autoignition temperature, the addition of fuel caused a temperature increase at the inside middle and outlet thermocouples.
Below the catalyzed autoignition temperature, such a temperature was not observed. When no catalytic coated strips or noble metal ribbons were present, the test section had to be heated to the autoignition temperature of the fuel before a temperature increase was observed. The non-catalyzed and catalyzed autoignition temperatures as measured are summarized in the TABLE, with the measured non-catalyzed or catalyzed autoignition temperature referred to as the measured autoignition temperature.
- AME1~ ~~~ ~~~
WO 97/24510 PCTlEP96/05754 TABLE
FUEL MEASURED AIR FLOW FUEL ACCEL. CATALYST
AUTO- RATE CONC. o OF AIR
IGNITION CC/MIN o OF AIR VOLo TEMP. C VOL. o NAT. GAS 788 380 10.5 NAT. GAS 732 380 2.6 N20/21 NAT. GAS 677 380 2.6 02/40 DIMETHYL 510 380 2.6 , ETHER
DIMETHYL 316 380 2.6 N20/21 ETHER
H2 49 380 13 pt 66.6%H2 676 380 13 33.3~C0 66.6~H2 213 380 13 pt 33.3~C0 66.6~H2 211 380 13 N20/44.7 Pt 33.3~C0 66.6~H2 149 0 13 380CC/MIN Pt 33.3~C0 1000 N20-Methane 310 380 13 - pd H2 149 380 13 - pd 66.6~H2 154 380 13 - Pd 33.3~C0 . . ._ ._-._.~..f~-~:'~.-~%
From the TABLE it can be seen that addition of N20 to the fuel stream greatly reduces the measured autoignitic~n temperature of the mixtures. Further, inclusion of hydrogen as a fuel and presence of the catalytic surface also significantly reduces the dynamic auto-ignition temperatures.
A 3.048 m long test combustor was used to test the results of the.2.54 cm. reactor in a distributed combustor application. A 2.54 cm outer diameter fuel gas line was provided within a 5.08 cm internal diameter combustion line. The fuel injection line provided a conduit for fuel to a fuel injection port located near an inlet end of the combustion line. The 5.08 cm internal diameter combustion line was placed within an insulated pipe, and thermocouples were placed along the fuel supply line.
Two different combustion lines were utilized. One combustion line was fabricated from a strip of "HAYNES
120" alloy. The strip was electro brush plated on one side with palladium to an average thickness of 0.0_00254 cm. The strip was then break formed, swedged and welded into a 3.048 m long pipe with the palladium coating on the inside surface. The other combustion line was a standard 7.62 cm pipe of "HAYNES 120" alloy. A
"MAXON" burner was used to supply combustion gases to the 3.048 m long combustion pipe, and varying amounts of air and/or other additives are mixed with the exhaust from the "MAXON" burner in a mixing section between the burner and the combustion line. To maintain a uniform temperature within the combustion line, three electric heaters, each with its own controller, were placed outside and along the length of the combustion line.
A series of tests were run, one with the palladium coated combustion line and one with the combustion line that was not palladium coated. Fuel gas was injected through the fuel gas injection port at a rate, when *Trade-mark measured at a temperature of 15.5 °C and at atmospheric pressure, of about 0.635 m3/hour, and, when measured at the same conditions, about 374 m3/hour of air was injected, including the burner air and the secondary air. ' Enough fuel gas was provided to the burner to provide a target temperature at the inlet of the combustion line.
Percentage of the injected methane that was burned is shown as a function of the combustion line inlet temperature in FIG. 2 for catalyzed configuration (line A) and noncatalyzed configuration (line B). From FIG. 2 it can be seen that at the lowest temperatures at which the apparatus can be operated is about 260 °C, 55a of the methane was oxidized with the palladium coated combustion line. The lowest temperature of operation might be somewhat below 260 °C but the equipment available was not capable of operation at a lower temperature. When the combustion line without the palladium coating was used, some oxidation of methane occurred at about 704 °C, and oxidation of methane occurs rapidly at temperatures of about 816 °C. At temperatures of 871 °C and above, the presence of the palladium surface has no effect because oxidation of methane is rapid and complete either with or without the palladium surface .
The temperature independence of the methane oxidized below 704 °C tends to verify that the methane within the boundary layer at the surface of the palladium surface oxidizes rapidly, and that transportation of methane to this boundary layer, and not kinetics, dictates the extent to which methane is oxidized. At temperatures of about 704 °C and greater, thermal oxidation becomes prevalent, and a temperature dependence is due to this thermal oxidation.
This invention relates to a flameless combustion ' apparatus and method.
U.S. Patent Nos. 4,640,352 and 4,886,118 disclose conductive heating of subterranean formations of low permeability that contain oil to recover oil therefrom.
Low permeability formations include diatomites, lipid , coals, and oil shales. Formations of low permeability are not amiable to secondary oil recovery methods such as steam, carbon dioxide, or fire flooding. Flooding materials tend to penetrate formations that have low permeabilities preferentially through fractures. The injected materials bypass most of the formation hydro-carbons. In contrast, conductive heating does not require fluid transport into the formation. Oil within the formation is therefore not bypassed as in a flooding process. When the temperature of a formation is increased by conductive heating, vertical temperature profiles will tend to be relatively uniform because formations generally have relatively uniform thermal conductivities and specific heats. Transportation of hydrocarbons in a thermal conduction process is by pressure drive, vaporization, and thermal expansion of oil and water trapped within the pores of the formation rock. Hydrocarbons migrate through small fractures created by the expansion and vaporization of the oil and water.
U.S. Patent No. 5,255,742 discloses a flameless combustor useful for heating subterranean formations that utilizes preheated fuel gas and/or combustion air wherein the fuel gas is combined with the combustion air in increments that are sufficiently small that flames are avoided. Creation of NOx is almost eliminated, and cost of the heaters can be significantly reduced because of less expensive materials of construction. Preheating the fuel gas in accordance with the method disclosed in this prior art reference may result in coke formation unless C02, H2, or steam is added to the fuel gas. Further, start-up of the known heater is a time consuming process because it must operate at temperatures above the uncatalyzed autoignition temperature of the fuel gas mixture.
Catalytic combustors are also known. For example, U.S. Patent No. 3,928,961 discloses a catalytically-sup-ported thermal combustion apparatus wherein formation of NOx is eliminated by combustion at temperatures above auto-ignition temperatures of the fuel, but less than those temperatures at which result in substantial formation of oxides of nitrogen.
Metal surfaces coated with oxidation catalyst are disclosed in, for example, U.S. Patent Nos. 5,355,668 and 4,065,917. These patents suggests catalytic coated surfaces on components of a gas turbine engine. Said US
Patent 4,065,917 suggests use of catalytic coated surfaces for start-up of the turbine, and suggests a mass transfer control limited phase of the start-up operation.
The combustor and flameless combustion method in accordance with the preamble of claims 1 and 16 are disclosed in U.S. Patent No. 3,817,332. In the known method fuel and oxidant are fed to the combustion chamber via separate supply conduits which is expensive but necessary to avoid premature combustion of the fuel in the supply conduit.
It is an object of the present invention to provide a flameless combustor wherein fuel and oxidant can be AMEt'~~D SHEET
fPE~P
- 2a -combined initially, and distribution of combustion determined by distribution of catalytic surfaces within a combustion chamber.
It is also an object of the present invention to provide a combustion method and apparatus which is flameless, and does not require additives in a fuel gas stream to prevent formation of coke. In another aspect of the present invention, it is an object to provide a combustion method and apparatus wherein formation of NOX is minimal.
A~~~i~~'~ ~~~ t v ~n~~~r:
WO 97/24510 PCTlEP96/05754 These and other objects are accomplished by a flameless combustor for combustion of a fuel and oxidant mixture, the combustor comprising:
a combustion chamber in communication with an inlet and with a combustion product outlet;
a mixed fuel and oxidant supply in communication with the inlet; and a catalyst surface within the combustion chamber wherein the catalyst surface is effective to cause oxidization of an amount of fuel wherein the oxidization of the amount of fuel does not result in a temperature above an uncatalyzed autoignition temperature of the fuel and oxidant mixture.
The flameless combustor of the present invention results in minimal production of nitrous oxides because temperatures that would result from adiabatic combustion of the fuel-oxidant mixture are avoided. Other measures to remove or prevent the formation of nitrous oxides are therefore not required. Relatively even heat distribu-tion over a large area and long lengths are possible, and relatively inexpensive materials of construction for the combustor of the present invention can be used because of lower combustion temperatures.
Acceptable catalyst materials include noble metals, semi-precious metals, and transition metal oxides.
Generally, known oxidation catalysts are useful in the present invention. Mixtures of such metals or metal oxides could also be useful.
The flameless combustor of the present invention is particularly useful as a heat injector for heating subterranean formations for recovery of hydrocarbons.
The catalytic surfaces also improve operability and start-up operations of such heat injectors. The present invention eliminates a need to transport fuels and oxidants in separate conduits to the combustion zone in such heat injectors. This results in significant cost savings.
Tn accordance with the invention there is also provided a method of heating a subterranean formation by ' flameless combustion. The method according to the invention comprises:
installing a combustion tubular which defines a downhole combustion chamber in a wellbore within the formation to be heated;
feeding fuel and oxidant to the chamber via an inlet;
inducing the fuel and oxidant mixture to flow along a catalyst surface within the combustion chamber wherein the catalyst surface is effective to cause oxidization of an amount of fuel at such a rate that the average temperature in the combustion chamber remains below the uncatalyzed autoignition temperature of the fuel and oxidant mixture; and allowing combustion products to flow to the surface via a combustion product outlet conduit within the wellbore.
Preferably the combustion chamber is defined by a lower portion of a well casing and a plug near the bottom of the well casing and the catalyst surface is provided by a catalyst coating on the inner and/or outer surface of a tubular which is co-axially suspended within the well casing such that an axial spacing is maintained between a lower end of the suspended tubular and the plug.
It is also preferred that the suspended tubular is used as a mixed fuel and air inlet conduit and the annular space between the suspended tubular and the well casing is used as a combustion product outlet conduit or , vice versa.
These and other features, objects and advantages of the combustor and method according to the present invention will become apparent from the accompanying drawings, in which:
FIG. 1 shows a combustor according to the present ' invention; and FIG. 2 is a plot of methane consumption vs.
' temperature in a test apparatus demonstrating the present invention.
Generally, flameless combustion is accomplished by preheating combustion air and fuel gas sufficiently that when the two streams are combined the temperature of the mixture exceeds the autoignition temperature of the mixture, but to a temperature less than that which would result in the oxidation upon mixing being limited by the rate of mixing. Without a catalyst surface present, preheating of the streams to a temperature between about 815 C and about 1260 C and then mixing the fuel gas into the combustion air in relatively small increments will result in flameless combustion.
With an effective catalytic surface present, the temperature at which oxidation reactions occur in a region affected by the catalytic surface is significantly lowered. This reduced temperature is referred to herein as a catalyzed autoignition temperature. In turbulent flow, fluid-in a boundary layer that contacts the catalytic surface will be oxidized almost quantitatively, but almost no oxidation will occur outside of the boundary layer if the bulk temperatures remain below the non-catalyzed autoignition temperatures of the mixture.
Thus, reaction in the temperature range between the catalyzed autoignition temperature and the noncatalyzed autoignition temperature is mass-transfer limited, at a rate that is relatively independent of temperature. This is suggested in references such as U.S. Patent No. 4,065,917. This mass transfer limited reaction mechanism is utilized in the present invention to control distribution of heat generation within the combustion chamber of the flameless combustor. Heat generation and heat removal can be balanced so that the average stream temperature of the mixed oxidant, fuel, and combustion ' products remains between the catalyzed autoignition temperature and the noncatalyzed autoignition temper- "
ature.
The heater of the present invention can be controlled by such variables as fuel-oxidant ratio, fuel-oxidant flowrate. Depending on the particular application, the heat load~may be subject to controls.
An important feature of the flameless combustor of the present invention is that heat is removed along the axis of the combustion chamber so that a temperature is maintained that is significantly below the adiabatic combustion temperature. This almost eliminates formation of NOxs, and also significantly reduces metallurgical requirements resulting in a relatively inexpensive combustor.
Referring to FIG. 1, a combustor within a heat injection well capable of carrying out the present invention is shown. A formation to be heated, 1, is below an overburden, 2. A wellbore, 3, extends through the overburden and to a position that is preferably near the bottom of the formation to be heated. A vertical well is shown, but the wellbore could be deviated or horizontal.
Horizontal heat injector wells may be provided in formations that fracture horizontally to recover hydrocarbons by a parallel drive process. Shallow oil shale formations are examples of formations where horizontal heaters may be useful. Horizontal heaters may also be effectively used when thin layers are to be , heated to limit heat loss to overburden and base rock.
In the embodiment shown in Figure 1, the wellbore-is cased with a casing, 4. The lower portion of the wellbore WO 97/24510 PCTlEP96/05754 _ 7 _ may be cemented with a cement, 7, having characteristics suitable for withstanding elevated temperatures and transferring heat. A cement which is a good thermal ' insulator, 8, is preferred for the upper portion of the wellbore to prevent heat loss from the system. A
combustion mixture conduit, 10, extends from the wellhead (not shown) to the lower portion of the wellbore.
High temperature cements suitablefor cementing casing and conduits within the high temperature portions of the wellbore are available. Examples are disclosed in U.S. Patent Nos. 3,507,332 and 3,180,748. Alumina contents above about 50 percent by weight based on cements slurry solids are preferred.
In shallow formations, it may be advantageous to hammer-drill the heater directly into the formation.
When the heater is hammer-drilled directly into the formation, cementing of the heater in the formation may not be required, but an upper portion of the heater may be cemented to prevent fluid loss to the surface.
Choice of a diameter of the casing, 4, in the embodiment of FIG. 1 is a trade-off between the expense of the casing, and the rate at which heat may be transferred into the formation. The casing, due to the metallurgy required, is generally the most expensive component of the injection well. The heat that can be transferred into the formation increases significantly with increasing casing diameter. A casing of between about l0 and about 20 cm in internal diameter will typically provide an optimum trade-off between initial cost and capability to transferheat from the wellbore.
A cement plug 23 is shown at the bottom of the . casing, the cement plug being forced down the casing during the cementing operation to force cement out the bottom of the casing.
WO 97!24510 PCT/EP96/05754 _ g _ Catalyst surfaces 20 are provided within the combustion chamber 14 to provide a limited region~where.in the oxidation reaction temperature is lowered.
Distribution of these catalyst surfaces 20 as a coating which covers at least part ofthe inner and/or outer surface of a lower portion of the conduit 10 provide for "
distribution of heat release within the combustion chamber. The catalyst surfaces are sized to accomplish a nearly even temperature distribution along the casing. A
nearly even temperature profile within the casing results in more uniform heat distribution within the formation to be heated. A nearly uniform heat distribution within the formation will result in more efficient utilization of heat in a conductive heating hydrocarbon recovery process. A more even temperature profile will also result in the lower maximum temperatures for the same heat release. Because the materials of construction of the burner and well system dictate the maximum temper-atures, even temperature profiles will increase the heat release possible for the same materials of construction.
As the combustion products rise in the wellbore above the formation being heated, heat is exchanged between the combustion air and the fuel gas travelling down the flow conduits and the rising combustion products. This heat exchange not only conserves energy, but permits the desirable flameless combustion of the present invention.
The fuel gas and the combustion air are preheated as they travel down the respective flow conduits sufficiently that the mixture of the two streams at the ultimate mixing point is at a temperature above the catalyzed autoignition temperature of the mixture, but below the noncatalyzed autoignition temperature. Combustion on the , catalyst surface and flameless combustion within boundary layers adjacent to effective catalyst surfaces results, , avoiding a flame as a radiant heat source_ Heat is therefore transferred from the wellbore in an essentially uniform fashion.
It is important in the operation of a combustor of the present invention that heat be removed from the combustion chamber along the length of the combustion chamber. In the application of the present invention to a wellbore heat injector, heat is transferred to the formation around the wellbore. The heater of the present invention could also be used in other applications, such as steam generation and chemical industry process heaters and reactors.
Fuel gas and combustion air transported to the bottom of the wellbore through a mixed fuel and oxidant supply (22) which is shown as an annular volume surrounding the combustion product conduit. The mixed fuel and air react within the wellbore volume adjacent to the catalyst surfaces 14 forming combustion products. The combustion products travel up the wellbore and out an exhaust vent (not shown) at the wellhead through the combustion product conduit 10. From the exhaust vent, the combustion products may be routed to atmosphere through an exhaust stack (not shown). Alternatively, the combustion gases may be treated to remove pollutants, although nitrous oxides would not be present and would not therefore need to be removed. Additional energy recovery from the combustion products by an expander turbine or heat exchanger may also be desirable.
Preheating of the fuel gases to obtain flameless combustion without a catalyst would result in significant generation of carbon unless a carbon formation suppressant is included in the fuel gas stream. The need to provide such a carbon formation suppressant is therefore avoided by operating the heater at a temperature that is less than the carbon formation temperature. This is another significant advantage of AMEf~GED SHEE'!' IPE~P
WO 97/24510 PCT/EP9b/05754 - to -the present invention because the carbon suppressant increases the volume of gases to be passed through the heater and therefore increases the size of conduits required.
Cold start-up of a well heater of the present -invention may utilize combustion with a flame. Initial ignition may be accomplished by injecting pyrophoric material, an el-ectrical igniter, a spark igniter, temporally lowering an igniter into the wellbore, or an electrical resistance heater. The burner is preferably rapidly brought to a temperature at which a flameless combustion is sustained to minimize the time period at which a flame exists within the wellbore. The rate of heating up the burner will typically be limited by the thermal gradients the burner can tolerate.
The combustion mixture conduit can be utilized as a resistance heater to bring the combustor up to an operating temperature. To utilize this conduit as a resistance heater, an electrical lead 15 can be connected with a clamp 16 or other connection to the combustion mixture conduit 10 near the wellhead below an electrically insulating coupling to supply electrical energy. Electrical ground can be provided near the bottom of the borehole with one or more electrically conducting centralizers 17 around the combustion mixture conduit 10. Centralizers on the combustion mixture conduit above the electrically grounding centralizers are electrically insulating centralizers. Sufficient heat is preferably applied to result in the combustion mixture being, at the location of the initial catalyst surface, at a temperature that is above the catalyzed autoignition temperature but below the noncatalyzed auto ignition , temperature.
Thickness of the combustion mixture conduit can be varied to result is release of heat at preselected WO 97I245I0 PCTlEP96/05754 segments of the length of the fuel conduit. For example, in a well heat injector application, it may be desirably to electrically heat the lowermost portion of the wellbore in order to ignite the mixed gas stream at the highest concentration of fuel, and to burn the fuel before exhaust gasses are passed back up through the wellbore. Thin section 21 is shown in the combustion mixture conduit to provide a surface of elevated temperature for start-up of the combustor.
Oxidation reaction temperature of the fuel gas-oxidant mixture is lowered by provision of a noble metal surface, or another effective catalyst surface.
Catalytic surface is preferably provided on the either the inside, outside, or both inside and outside surface of the combustion products conduit 10. Alternatively, a surface, or a tubular or other noble metal containing surface, could be separately placed within the combustion chamber. Other noble metal coated surfaces could be provided, for example, in the combustion product annulus outside of the combustion gas conduit. This additional catalyst surface could ensure that complete combustion occurred within the wellbore, where generation of heat is desired.
Start-up of the flameless combustor of the present invention can be further enhanced by provision of supplemental oxidants during the start-up phase, or by use of a fuel that has a lower autoignition temperature such as hydrogen. Preferred supplemental oxidants include supplemental oxygen and nitrous oxide. Hydrogen could be provided along with a natural gas stream, and could be provided as shift gas, with carbon monoxide present and carbon dioxide present.
Start-up oxidants and/or fuels are preferably only used until the combustor has been heated to a temperature sufficient to enable operation with methane (natural gas) as fuel and air as the oxidant (i.e., the combustor has heated to a temperature above the catalyzed autoignition temperature of methane in air).
US patent 5,255,742 disclosed using an electrical ' resistance nicrome heater to generate heat for start-up of the flameless combustor. Such an electrical heater may be used in the practice of the present invention.
Noble metals such as palladium or platinum, or semi-precious metal, base metal or transition metal can l0 be coated, preferably by electroplating, onto a surface within the combustion chamber to enhance oxidation of the fuel at lower temperatures. The metal could then be oxidized as necessary to provide a catalytically effective surface. Such catalytic surface has been found to be extremely effective in-promoting oxidation of methane in air at temperatures as~low as 260 °C. This reaction rapidly occurs on the catalytic surface and in the adjacent boundary layer. An advantage of having a significant catalytic surface within the combustion chamber is that the temperature range within which the flameless combustor can operate can be significantly increased.
FXAMPT~F~
A thermal reactor was used to establish temperatures at which oxidation reactions would occur with various combinations of fuels, oxidants and catalyst surfaces.
The reactor was a 2.54 cm stainless steel pipe wrapped with an electrical resistance heating coil, and covered with insulation. A thermocouple for temperature control was placed underneath the insulation adjacent to the outer surface of the pipe. Thermocouples were also provided inside the pipe at the inlet, at the middle, and , at the outlet. Test ribbons of noble metals or stainless steel strips with noble metal coatings were hung in the pipe to test catalytic activity. Air preheated to a temperature somewhat below the desired temperature of the test was injected into the electrically heated test section of the pipe. Electrical power to the electrical resistance heater was varied until the desired temperature in the test section was obtained and a steady state, as measured by the thermocouples mounted inside the pipe, was achieved. Fuel was then injected through a mixing tee into the stream of preheated air and allowed to flow into the electrically heated test section. Four platinum ribbons one eighth of an inch (= 0.32 cm) wide and about sixteen inches (= 40 cm) long or a stainless steal strip three eighths of an inch (= 0.95 cm) wide and about one sixteenth of an inch (= 0.16 cm) thick and about sixteen inches (= 40 cm) long coated on both sides with either platinum or palladium were suspended within the pipe to test catalytic activity. When the test section contained a catalyst coated strep or ribbon of noble metal and was at or above the catalyzed autoignition temperature, the addition of fuel caused a temperature increase at the inside middle and outlet thermocouples.
Below the catalyzed autoignition temperature, such a temperature was not observed. When no catalytic coated strips or noble metal ribbons were present, the test section had to be heated to the autoignition temperature of the fuel before a temperature increase was observed. The non-catalyzed and catalyzed autoignition temperatures as measured are summarized in the TABLE, with the measured non-catalyzed or catalyzed autoignition temperature referred to as the measured autoignition temperature.
- AME1~ ~~~ ~~~
WO 97/24510 PCTlEP96/05754 TABLE
FUEL MEASURED AIR FLOW FUEL ACCEL. CATALYST
AUTO- RATE CONC. o OF AIR
IGNITION CC/MIN o OF AIR VOLo TEMP. C VOL. o NAT. GAS 788 380 10.5 NAT. GAS 732 380 2.6 N20/21 NAT. GAS 677 380 2.6 02/40 DIMETHYL 510 380 2.6 , ETHER
DIMETHYL 316 380 2.6 N20/21 ETHER
H2 49 380 13 pt 66.6%H2 676 380 13 33.3~C0 66.6~H2 213 380 13 pt 33.3~C0 66.6~H2 211 380 13 N20/44.7 Pt 33.3~C0 66.6~H2 149 0 13 380CC/MIN Pt 33.3~C0 1000 N20-Methane 310 380 13 - pd H2 149 380 13 - pd 66.6~H2 154 380 13 - Pd 33.3~C0 . . ._ ._-._.~..f~-~:'~.-~%
From the TABLE it can be seen that addition of N20 to the fuel stream greatly reduces the measured autoignitic~n temperature of the mixtures. Further, inclusion of hydrogen as a fuel and presence of the catalytic surface also significantly reduces the dynamic auto-ignition temperatures.
A 3.048 m long test combustor was used to test the results of the.2.54 cm. reactor in a distributed combustor application. A 2.54 cm outer diameter fuel gas line was provided within a 5.08 cm internal diameter combustion line. The fuel injection line provided a conduit for fuel to a fuel injection port located near an inlet end of the combustion line. The 5.08 cm internal diameter combustion line was placed within an insulated pipe, and thermocouples were placed along the fuel supply line.
Two different combustion lines were utilized. One combustion line was fabricated from a strip of "HAYNES
120" alloy. The strip was electro brush plated on one side with palladium to an average thickness of 0.0_00254 cm. The strip was then break formed, swedged and welded into a 3.048 m long pipe with the palladium coating on the inside surface. The other combustion line was a standard 7.62 cm pipe of "HAYNES 120" alloy. A
"MAXON" burner was used to supply combustion gases to the 3.048 m long combustion pipe, and varying amounts of air and/or other additives are mixed with the exhaust from the "MAXON" burner in a mixing section between the burner and the combustion line. To maintain a uniform temperature within the combustion line, three electric heaters, each with its own controller, were placed outside and along the length of the combustion line.
A series of tests were run, one with the palladium coated combustion line and one with the combustion line that was not palladium coated. Fuel gas was injected through the fuel gas injection port at a rate, when *Trade-mark measured at a temperature of 15.5 °C and at atmospheric pressure, of about 0.635 m3/hour, and, when measured at the same conditions, about 374 m3/hour of air was injected, including the burner air and the secondary air. ' Enough fuel gas was provided to the burner to provide a target temperature at the inlet of the combustion line.
Percentage of the injected methane that was burned is shown as a function of the combustion line inlet temperature in FIG. 2 for catalyzed configuration (line A) and noncatalyzed configuration (line B). From FIG. 2 it can be seen that at the lowest temperatures at which the apparatus can be operated is about 260 °C, 55a of the methane was oxidized with the palladium coated combustion line. The lowest temperature of operation might be somewhat below 260 °C but the equipment available was not capable of operation at a lower temperature. When the combustion line without the palladium coating was used, some oxidation of methane occurred at about 704 °C, and oxidation of methane occurs rapidly at temperatures of about 816 °C. At temperatures of 871 °C and above, the presence of the palladium surface has no effect because oxidation of methane is rapid and complete either with or without the palladium surface .
The temperature independence of the methane oxidized below 704 °C tends to verify that the methane within the boundary layer at the surface of the palladium surface oxidizes rapidly, and that transportation of methane to this boundary layer, and not kinetics, dictates the extent to which methane is oxidized. At temperatures of about 704 °C and greater, thermal oxidation becomes prevalent, and a temperature dependence is due to this thermal oxidation.
Claims (19)
1. A flameless combustor for combustion of a fuel and oxidant mixture, the combustor comprising:
a combustion chamber in communication with an inlet and with a combustion product outlet; and a catalyst surface within the combustion chamber;
characterized in that the combustor further comprises a mixed fuel and oxidant supply in communication with the inlet; and that the catalyst surface is effective to cause oxidization of an amount of fuel wherein the oxidization of the amount of fuel does not result in a temperature above an uncatalyzed autoignition temperature of the fuel and oxidant mixture.
a combustion chamber in communication with an inlet and with a combustion product outlet; and a catalyst surface within the combustion chamber;
characterized in that the combustor further comprises a mixed fuel and oxidant supply in communication with the inlet; and that the catalyst surface is effective to cause oxidization of an amount of fuel wherein the oxidization of the amount of fuel does not result in a temperature above an uncatalyzed autoignition temperature of the fuel and oxidant mixture.
2. The combustor of claim 1 wherein the catalyst surface comprises a component selected from the group consisting of noble metals, semi-precious metals, transition metal oxides and mixtures thereof.
3. The combustor of claim 1 wherein the catalyst surface comprises palladium.
4. The combustor of claim 1 wherein the catalyst surface comprises platinum.
5. The combustor of claim 1 further comprising a preheat section wherein in the preheat section heat can be exchanged between the fuel and oxidant mixture and the combustion products.
6. The combustor of any one of claims 1 to 5 wherein the combustor is designed for heating a subterranean formation by combustion of a fuel and oxidant mixture; the combustion chamber is defined by at least one combustion tubular which is located in a wellbore within the formation to be heated; and the combustor comprises a combustion gas outlet within the wellbore for allowing combustion products to flow to the surface.
7. The combustor of claim 6 wherein the catalyst surface area is distributed within the combustion chamber to result in an essentially constant temperature within the combustion chamber.
8. The combustor of claim 6 wherein the combustion chamber is defined by one or more tubular pipes placed within the wellbore.
9. The combustor of claim 6 wherein the combustion gas outlet is an annular space surrounding the combustion tubular.
10. The combustor of claim 6 wherein the combustion gas outlet is a tubular within the combustion chamber.
11. The combustor of claim 6 wherein the combustion chamber comprises an annular volume between a tubular and a casing.
12. The combustor of claim 11 wherein the tubular is a conduit for return of combustion products to a wellhead.
13. The combustor of claim 6 wherein the tubular is a conduit containing another portion of the combustion chamber.
14. The combustor of any one of claims 1 to 13 wherein the catalyst surface is provided by a catalyst coating which covers at least part of the inner or outer surface of a tubular within the combustion chamber.
15. The combustor of any one of claims 1 to 14 wherein the inlet is located at one end of the combustion chamber and the outlet is located at the other end of the combustion chamber.
16. A method of heating a subterranean formation by flameless combustion, the method comprising:
installing a combustion tubular which defines a downhole combustion chamber in a wellbore within the formation to be heated and inducing fuel and oxidant to flow along a catalyst surface within the combustion chamber;
characterized in that the method further comprises feeding a fuel and oxidant mixture to the chamber via an inlet;
wherein the catalyst surface is effective to cause oxidization of an amount of fuel at such a rate that the average temperature in the combustion chamber remains below the uncatalyzed autoignition temperature of the fuel and oxidant mixture; and allowing combustion products to flow to the surface via a combustion product outlet conduit within the wellbore.
installing a combustion tubular which defines a downhole combustion chamber in a wellbore within the formation to be heated and inducing fuel and oxidant to flow along a catalyst surface within the combustion chamber;
characterized in that the method further comprises feeding a fuel and oxidant mixture to the chamber via an inlet;
wherein the catalyst surface is effective to cause oxidization of an amount of fuel at such a rate that the average temperature in the combustion chamber remains below the uncatalyzed autoignition temperature of the fuel and oxidant mixture; and allowing combustion products to flow to the surface via a combustion product outlet conduit within the wellbore.
17. The method of claim 16 wherein the combustion chamber is defined by a lower portion of a well casing and a plug near the bottom of the well casing and the catalyst surface is provided by a catalyst coating on the inner or outer surface of a tubular which is co-axially suspended within the well casing such that an axial spacing is maintained between a lower end of the suspended tubular and the plug.
18. The method of claim 17 wherein the suspended tubular is used as a mixed fuel and air inlet conduit and the annular space between the tubular and the well casing is used as a combustion product outlet conduit or vice versa.
19. The method of claim 16, 17 or 18 wherein the method is used for heating a subterranean oil shale formation of low permeability.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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US934495P | 1995-12-27 | 1995-12-27 | |
US60/009,344 | 1995-12-27 | ||
PCT/EP1996/005754 WO1997024510A1 (en) | 1995-12-27 | 1996-12-17 | Flameless combustor |
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CA2240646A1 CA2240646A1 (en) | 1997-07-10 |
CA2240646C true CA2240646C (en) | 2005-03-08 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CA002240646A Expired - Lifetime CA2240646C (en) | 1995-12-27 | 1996-12-17 | Flameless combustor |
Country Status (19)
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EP (1) | EP0870101B1 (en) |
JP (1) | JP3825807B2 (en) |
KR (1) | KR100440993B1 (en) |
CN (1) | CN1079884C (en) |
AT (1) | ATE183810T1 (en) |
AU (1) | AU713893B2 (en) |
BR (1) | BR9612695A (en) |
CA (1) | CA2240646C (en) |
DE (1) | DE69603979T2 (en) |
DK (1) | DK0870101T3 (en) |
EA (1) | EA000250B1 (en) |
EG (1) | EG20999A (en) |
ES (1) | ES2138842T3 (en) |
GR (1) | GR3031660T3 (en) |
IL (1) | IL124805A (en) |
JO (1) | JO1947B1 (en) |
MA (1) | MA24041A1 (en) |
TR (1) | TR199801221T2 (en) |
WO (1) | WO1997024510A1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2563583C (en) * | 2004-04-23 | 2013-06-18 | Shell Internationale Research Maatschappij B.V. | Temperature limited heaters used to heat subsurface formations |
CN1614189B (en) * | 2004-10-18 | 2011-03-16 | 魏明 | Combustion heating apparatus for underground thermal production of petroleum |
CA2741861C (en) * | 2008-11-06 | 2013-08-27 | American Shale Oil, Llc | Heater and method for recovering hydrocarbons from underground deposits |
JP5445691B2 (en) * | 2010-11-04 | 2014-03-19 | 株式会社Ihi | Combustion heating system |
US10273790B2 (en) * | 2014-01-14 | 2019-04-30 | Precision Combustion, Inc. | System and method of producing oil |
RU2750638C1 (en) * | 2020-02-28 | 2021-06-30 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала флота Советского Союза Н.Г. Кузнецова" | Device for flameless obtaining of thermal energy from hydrocarbon fuels |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3817332A (en) * | 1969-12-30 | 1974-06-18 | Sun Oil Co | Method and apparatus for catalytically heating wellbores |
MX3874E (en) * | 1975-12-29 | 1981-08-26 | Engelhard Min & Chem | IMPROVEMENTS IN METHOD TO INITIATE A COMBUSTION SYSTEM USING A CATALYST |
US4237973A (en) * | 1978-10-04 | 1980-12-09 | Todd John C | Method and apparatus for steam generation at the bottom of a well bore |
US4377205A (en) * | 1981-03-06 | 1983-03-22 | Retallick William B | Low pressure combustor for generating steam downhole |
US4930454A (en) * | 1981-08-14 | 1990-06-05 | Dresser Industries, Inc. | Steam generating system |
US4706751A (en) * | 1986-01-31 | 1987-11-17 | S-Cal Research Corp. | Heavy oil recovery process |
-
1996
- 1996-12-17 TR TR1998/01221T patent/TR199801221T2/en unknown
- 1996-12-17 BR BR9612695A patent/BR9612695A/en not_active IP Right Cessation
- 1996-12-17 DK DK96944608T patent/DK0870101T3/en active
- 1996-12-17 EA EA199800601A patent/EA000250B1/en not_active IP Right Cessation
- 1996-12-17 EP EP96944608A patent/EP0870101B1/en not_active Expired - Lifetime
- 1996-12-17 AT AT96944608T patent/ATE183810T1/en not_active IP Right Cessation
- 1996-12-17 CN CN96199385A patent/CN1079884C/en not_active Expired - Lifetime
- 1996-12-17 JP JP52401197A patent/JP3825807B2/en not_active Expired - Lifetime
- 1996-12-17 KR KR10-1998-0704982A patent/KR100440993B1/en not_active IP Right Cessation
- 1996-12-17 AU AU13034/97A patent/AU713893B2/en not_active Ceased
- 1996-12-17 IL IL12480596A patent/IL124805A/en not_active IP Right Cessation
- 1996-12-17 CA CA002240646A patent/CA2240646C/en not_active Expired - Lifetime
- 1996-12-17 ES ES96944608T patent/ES2138842T3/en not_active Expired - Lifetime
- 1996-12-17 WO PCT/EP1996/005754 patent/WO1997024510A1/en active IP Right Grant
- 1996-12-17 DE DE69603979T patent/DE69603979T2/en not_active Expired - Lifetime
- 1996-12-25 MA MA24442A patent/MA24041A1/en unknown
- 1996-12-26 JO JO19961947A patent/JO1947B1/en active
- 1996-12-26 EG EG119196A patent/EG20999A/en active
-
1999
- 1999-10-27 GR GR990402749T patent/GR3031660T3/en unknown
Also Published As
Publication number | Publication date |
---|---|
DK0870101T3 (en) | 2000-03-27 |
DE69603979D1 (en) | 1999-09-30 |
AU1303497A (en) | 1997-07-28 |
AU713893B2 (en) | 1999-12-16 |
EP0870101A1 (en) | 1998-10-14 |
CN1206446A (en) | 1999-01-27 |
KR19990076855A (en) | 1999-10-25 |
KR100440993B1 (en) | 2004-11-06 |
ATE183810T1 (en) | 1999-09-15 |
EG20999A (en) | 2000-09-30 |
MA24041A1 (en) | 1997-07-01 |
IL124805A (en) | 2001-01-28 |
IL124805A0 (en) | 1999-01-26 |
EP0870101B1 (en) | 1999-08-25 |
CN1079884C (en) | 2002-02-27 |
ES2138842T3 (en) | 2000-01-16 |
WO1997024510A1 (en) | 1997-07-10 |
EA000250B1 (en) | 1999-02-25 |
JO1947B1 (en) | 1997-12-15 |
DE69603979T2 (en) | 2000-04-06 |
TR199801221T2 (en) | 1998-10-21 |
JP3825807B2 (en) | 2006-09-27 |
CA2240646A1 (en) | 1997-07-10 |
BR9612695A (en) | 1999-08-24 |
JP2000503085A (en) | 2000-03-14 |
GR3031660T3 (en) | 2000-02-29 |
EA199800601A1 (en) | 1998-12-24 |
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