Multiphase burner
10288283 ยท 2019-05-14
Assignee
Inventors
- Roman Alexandrovich Skachkov (Novosibirsk, RU)
- Pavel Andreevich Golikov (St. Petersburgh, RU)
- Christian Menger (Recke, DE)
- Vladimir Konstantinovich Khan (Novosibirsk, RU)
Cpc classification
F23D14/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23G7/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23G7/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23G7/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A multiphase burner for flaring gaseous/liquid combustible mixtures is disclosed. The burner may include a hollow base with an inlet for receiving the combustible gas/liquid mixture as well as a distal end that may be coupled to or that forms a nozzle cap. The nozzle cap may form as first outlet. The base may be coupled to a central body and a hollow bushing that encircles at least part of the central body. The base may form a mouth disposed between the inlet and the central body. The mouth may be in communication with a first passage that extends from the mouth to the first outlet and between the bushing and the distal end of the base. The mouth may be in communication with a second passage that extends from the mouth to the second outlet and between the bushing and central body.
Claims
1. A multiphase burner comprising: a hollow base having a central axis and including an inlet for receiving a combustible fluid, the base further including a distal end that is coupled to a nozzle cap, the nozzle cap forming a first outlet that encircles the central axis, the base further being coupled coaxially to a central body that includes a proximal end disposed distally from the mouth and within the holder and a tapered distal end that extends through the second outlet, the proximal end of the central body being connected to a first frustoconical section that expands radially outward to a circumferential bulge, the circumferential bulge being connected to a second frustoconical section that extends radially inwardly before being connected to a third frustoconical section that extends radially inwardly before being coupled to the tapered distal end, the base also being coaxially coupled to a hollow holder that encircles at least part of the central body, the holder being coupled to a hollow bushing that encircles at least part of the central body, the bushing forming a second outlet that encircles the central axis and that is disposed within the first outlet, the base forming a mouth disposed along the central axis and between the inlet and the central body, the mouth in communication with a first passage that extends from the mouth to the first outlet and between the holder and the distal end of the base, the mouth in communication with a second passage that extends from the mouth to the second outlet and between the holder and the central body.
2. The burner of claim 1 wherein the base and nozzle cap are connected.
3. The burner of claim 1 wherein the base is tubular.
4. The burner of claim 1 wherein the holder and bushing are integrally connected.
5. The burner of claim 1 wherein the holder and bushing are threadably connected.
6. The burner of claim 1 wherein the central body includes a proximal end that includes a circumferential bulge that extends radially outwards towards, but spaced apart from the holder, the central body also including a tapered distal end that extends axially through the second outlet.
7. The burner of claim 1 further including a fourth frustoconical section disposed between the third frustoconical section and the tapered distal end, the fourth frustoconical section extending radially inwardly before being connected to the tapered distal end.
8. The burner of claim 1 wherein the bushing includes an inner surface that includes a plurality of radially inwardly extending segments before terminating at the second outlet.
9. The burner of claim 1 wherein the bushing includes an inner surface that includes a plurality of segments that extend radially inwardly towards the central body but that are spaced apart from the central body before terminating at the second outlet.
10. The burner of claim 6 wherein the proximal end of the central body is coupled to a support, the support being coupled to the base and including a shaft having a distal end connected to the proximal end of the central body and a proximal end disposed in the inlet of the base.
11. The burner of claim 10 wherein the shaft passes through the mouth.
12. The burner of claim 1 wherein the nozzle cap may be removed from the base and the bushing may be removed from the holder without disturbing the central body.
13. The burner of claim 1 wherein first outlet is serrated.
14. A method for flaring a wet gas flow, the method comprising: delivering the wet gas flow to an inlet of a hollow base, the base including a mouth that is in communication with a first annular passage and a second annular passage that is concentrically disposed within the first annular passage, the first annular passage being defined by a nozzle cap and a hollow bushing, the nozzle cap being coupled to the base, the hollow bushing being coupled to the base and concentrically within the nozzle cap, the nozzle cap forming a first outlet, the bushing forming a second outlet, the second annular passage being defined by the bushing and a central body disposed axially within the bushing, dividing the wet gas flow into a first flow that passes through the first annular passage and a second flow that passes through the second annular passage, compressing the first flow in the first passage and accelerating the first flow to sonic speed by forcing the first flow between the nozzle cap and the bushing before the first flow is ejected out through the first outlet, compressing the second flow in the second passage and accelerating the second flow to sonic velocity by forcing the second flow between the bushing and the central body before the second flow is ejected out through the second outlet, atomizing fluid in the second flow at the second outlet by engaging the second flow with ridges disposed on an inner surface of the bushing before the second flow is accelerated to sonic speed at the second outlet, and igniting the first and second flows downstream of the first and second outlets.
15. The method of claim 14 further including atomizing fluid in the first flow at the first outlet by engaging the first flow with serrations that encircle the first outlet.
16. The method of claim 14 wherein the first flow includes less liquid than the second flow.
17. A multiphase burner for flaring wet gas, the burner comprising: a hollow base having a central axis and including an inlet for receiving a flow of wet gas, the base further including a distal end that is coupled to a nozzle cap, the nozzle cap forming a first outlet with a serrated rim that encircles the central axis, the base further being coupled to a central body that is disposed along the central axis, the base also being coaxially coupled to a hollow holder that encircles at least part of the central body, the holder being coupled to a hollow bushing that encircles at least part of the central body, the bushing forming a second outlet that encircles the central axis and at least part of the central body and that is disposed concentrically within the first outlet, the base forming a mouth disposed along the central axis and between the inlet and the central body, the mouth in communication with a first passage that extends from the mouth to the first outlet and between both the holder and bushing and the distal end of the base, the mouth in communication with a second passage that extends from the mouth to the second outlet and between both the holder and bushing and the central body, the bushing having an inner surface and the central body having an outer surface, the inner surface of the bushing including a plurality of ridges, the outer surface of the central body including a plurality of steps.
18. The burner of claim 1 wherein the nozzle cap may be removed from the base and the bushing may be removed from the holder without disturbing the central body.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) For a more complete understanding of the disclosed methods and apparatuses, reference should be made to the embodiment illustrated in greater detail on the accompanying drawings, wherein:
(2)
(3)
(4)
(5)
(6) It should be understood that the drawings are not necessarily to scale and that the disclosed embodiments are sometimes illustrated diagrammatically and in partial views. In certain instances, details which are not necessary for an understanding of the disclosed methods and apparatuses or which render other details difficult to perceive may have been omitted. It should be understood, of course, that this disclosure is not limited to the particular embodiments illustrated herein.
DETAILED DESCRIPTION
(7) Disclosed herein is a flaring apparatus in the form of a multiphase burner that provides clean and smokeless combustion of a waste gas effluent or a waste gas-liquid fuel mixture (i.e., wet gas) at high inlet pressures through fine atomization of the liquid component of the wet gas, intensive mixing with ambient air and self-sustaining ignition. The disclosed multiphase burner also may provide improved burning efficiency at decreased noise levels and improved mechanical durability and reliability.
(8) In a typical well testing operation, a gas flare is used to burn the wet gas exiting a well test separator. The wet gas typically includes a fraction of liquid that remains in the gas flow and needs to be combusted. The liquid typically includes water and oil but some formations produce wet gas with a liquid fraction that includes water without oil, oil without water, or both at the same time. As disclosed herein, smoke-free and fallout-free flaring of the wet gas is possible even with a high fraction of liquid.
(9)
(10) As shown in
(11) In addition to supporting the central body 21 and support 25, the base 11 may also support a holder 38 by way of the strut 44. The holder 38 may be integrally connected to or coupled directly or indirectly to a bushing 41. As shown in
(12) As shown in
(13) The base 11 may also form a mouth 57 through which the support 25 passes. The strut 27 may be used to support the central body 21 and the support 25 in the axial position shown in
(14) The burner 10 may operate in the following manner. The inlet wet gas flow 13 for flaring may be supplied though pipelines (not shown) to the base 11. The inlet wet gas flow 13 may be a complex and unsteady combination different phases: gas flow (mainly methane); droplets of oil and water carried by high-velocity gas flow; liquid film on the inlet 12 (not shown), which may be transformed into liquid slugs; and, as a minor component, flow of particulates (e.g., sand from the formation and other debris from metal pipelines). This multiphase wet gas inlet flow 13 passes through the narrow mouth 57. At the sharp edge of mouth 57, the inlet flow 13 may be divided into two flows 61 and 63 as shown in
(15) The flow 61 may include gas carrying liquid droplets and liquid jets, which develop as a result of detachment of liquid film from the base 11 at or near the tapered surface 64 and/or the mouth 57. The gas, liquid droplets and liquid jets move through the central passage 58 between the central body 21 and the holder 38/bushing 41. Due to the converging inner surface 64 of the base 11 in the vicinity of the mouth 57 (see
(16) In contrast, the flow 63 includes gas and liquid droplets and passes through the outer passage 59 as shown. The flow 63 exits the burner 10 through the nozzle cap outlet 18, which as shown in
(17) The design of the burner 10 and its dual passage flows 61, 63 may provide an improved dispersion of big liquid droplets and liquid films. Specifically, big liquid droplets and any liquid films from the flow 61 may be dispersed into smaller droplets inside the burner 10 and between the central body 21 and holder 38/bushing 41. Further, another atomization of the flow 61 may take places downstream the sonic transition cross-section shown in phantom at 65 in
(18) For a high-pressure gas-liquid flow (when the absolute pressure at the inlet 12 of the base 11 exceeds about 0.2 MPa), transition of a flow through the narrowing central passage 58 may result in the sonic transition critical section 65 at a narrow point of the central passage 58. The critical section 65 may be defined as a section where the gas flow at a given temperature reaches the sonic level. As an example, an expected location for critical cross-section 65 in the gas flow 61 through the central passage 58 is shown just upstream of the outlet 55 in
(19) The smooth-shaped mouth 57 in combination with the control body 21 splits inlet gas-liquid flow 13 into two parts 61, 63 as shown in
(20) The serrations on the outlet 18 of the nozzle cap 15 may produce turbulisation of the exit flow and may improve aeration of the final mixture at the outlets 18, 55 of the burner 10 while suppressing jet noise while the flow 63 is ejected from the outer passage 59. The small size of the serrations may also act to disperse the liquid film (if a film has survived up to outlet 18) into small droplets that continue their flight in the near the central axis 66.
(21) The dual flows 61, 63 produced by the burner 10 may result in only a minor part of liquid (in the form of small droplets) that is dragged by the deviated gas flow 63 into the outer passage 59. Therefore, the gas flow 63 passing through outer passage 59 may have much lower liquid content than the flow 61 through the central passage 58.
(22) The smallest cross-sectional area for the central passage 58 may be at or near the outlet 55 and may also be in close proximity to the smallest cross-sectional area for the outer passage 59, which is at the outlet 18 and which may also be small enough to generate sonic velocities for the flow 63. Any surviving liquid droplets in the flow 63 may be dispersed into a fine mist along the central axis 66 as such droplets exit the outlet 18. Specifically, at the outlet 18 of the nozzle cap 15, the flow from the outer passage 59 ejects near the serrated outlet 18. The serrations on the outlet 18 facilitate dispersion of any liquid film present in the flow 63 along the axis 66, better mixing of gas with ambient air, and a reduction in the jet noise level.
(23) As a result of gas-liquid flow splitting into two flows 61, 63 and dispersion of liquid droplets inside the burner 10, the exit flow may consist of a core flow with a high concentration of liquid droplets (spray flow) and a turbulised sheath-shaped flow with a low concentration of entrained droplets. Mixed with ambient air and entrained by a highly turbulised jet flow, the mixture of combustible gas, liquid droplets, and air becomes a mixture that may be ignited for clean and smokeless combustion of wet gas with a high amount of entrained liquid. The mass fraction of liquid in the inlet flow can be up to 30% or more. However, the described gas burner device also operates as effective burner for fluids with low liquid content (dry gas) as well.
(24) The smallest cross-sectional area for the central passage 58 is about equal to the smallest cross-sectional area for the outer passage 59. However, the proportions between the minimal cross-sectional areas for two passages 58 and 59 can vary by 30-50% depending on the fluid composition and inlet pressure in the base 11. The serrations on the outlet 18 may be triangular-shaped with the height in the range from about 2 to about 6 mm. However, as will be apparent to those skilled in the art, other geometries and sizes can be chosen for liquid film atomization, effective gas-air mixing, and jet noise reduction. The bushing 41 and central body 21 may have axisymmetric shapes for defining the central passage 58. Since a minor fraction of solid particulate (sand) can be found in the burner inlet flow 13 and high-speed solid particles create an abrasive impact on target surfaces (sand-jetting), the bushing 41 and central body 21 may be fabricated from a wear-resistant alloy.
(25) In field conditions, due to high velocities of fluid flow and intensive heat radiation from the flame, the nozzle cap 15 and bushing 41 may degrade to a point of failure before other parts of burner 10. Therefore, the nozzle cap 15 and bushing 41 may be replaced in a quick process performed on-site due to the use of threaded distal surfaces 42, 43, 16, 17. Specifically, the nozzle cap 15 may be detached from the base 11 and the bushing 41 may be detached from the holder 38 without disturbing the central body 21. Durability of the burner 10 is achieved in part by using abrasion-resistant materials for the bushing 41 and nozzle cap 15 and providing the removable design for the bushing 41 and nozzle cap 15.
(26) In general, the disclosed high-pressure multiphase burner 10 with dual passages 58, 59 may be used to improve the dispersion of liquid components of wet gas and provide improved flaring over other burners known in the art.
(27) The wet gas inlet pressure may be greater than 1 barg. For input pressures above 1 barg, the critical section 65 at the outlet 55 and the critical section at the annular orifice defined by the outlet 18 and the outer surface 45 of the bushing 41 are formed inside the central passage 58 and outer passage 59 respectively, and this facilitates dispersion liquid components into a fine spray of gas-liquid fuel at the burner outlets 55, 18.
(28) Although the disclosed burner 10 is described as multiphase burner, it must be appreciated that the burner 10 as described herein can be used for combustion of dry combustible gas (dry gas) without any changes in design.
(29) The gas-liquid flow 13, 14 that is directed through the two passages 58, 59 within the burner 10 may pass through corresponding critical sections (shock waves) if the input pressure exceeds about 2 barg. Fluid mechanics may describe this situation as under-expanded flow. As the exit gas-liquid flow comes out from the outlets 55, 18 to surrounding air, shock waves may be developed, which creates zones of high and low pressure. At a stable input flow rate, the shock waves remain at certain distances from the nozzle outlets 55, 18. These zones may be a place of additional atomization of liquid droplets. As the flow (gas jet with atomized fuel) keeps expanding, the axial velocity of the jet becomes close to the flame propagation speed, so self-stabilization of flare flame takes place.
(30) The disclosed multiphase burner 10 may be used in many industries, including those where a separate liquid feed 14 is required. The liquid component (or liquid component with suspended solid particles like particles of micronized coal) may be fed through the inlet 14 into the base 11 and the gas (vapour) component of the feed may be supplied through the inlet 12 as shown in
(31) While only certain embodiments have been set forth, alternatives and modifications will be apparent from the above description to those skilled in the art. These and other alternatives are considered equivalents and within the spirit and scope of this disclosure and the appended claims.