Airfoil lance apparatus

Abstract: Apparatus for spraying an atomized mixture into a gas stream comprises a streamlined airfoil member having a large radius leading edge (3) and a small radius trailing edge (18). A nozzle assembly 4, 5, 6) pierces the trailing edge (18) of the airfoil member (7) and is concentrically surrounded by a nacelle (8) which directs shielding gas from the interior of the airfoil member around the nozzle assembly (4, 5, 6). Flowable medium to be atomized and atomizing gas for atomizing the medium are supplied in concentric conduits (2, 4) to the nozzle. A plurality of nozzles each surrounded by a respective nacelle (8) are spaced along the trailing edge (18) of the airfoil member (7).

Description: The invention relates to lance apparatus and has particular though not exclusive application to such apparatus for homogeneous humidification, and/or sorbent dispersion in a gas stream. There are many reasons for conditioning a process gas stream. These include: improving particulate collection capabilities (i.e. electrostatic precipitator performance enhancement); quenching or cooling of a gas stream to meet process requirements or to accommodate process equipment limitations (i.e. gas volume reduction); and facilitating process chemical reactions where a gas/liquid/solid phase interaction is required (e.g. sorbent injection for sulphur dioxide capture). It has been previously proposed to use sulphur trioxide injection into a particulate laden flue gas steam to reduce the resistivity of fly ash particulate. This results in an electrostatic precipitator collection efficiency improvement. Sulphur trioxide injection is typically carried out by conversion of liquid sulphur dioxide or elemental sulphur to sulphur trioxide prior to injection upstream of the electrostatic precipitator. Quenching or cooling of a process gas stream (e.g. flue gas) via humidification has also been proposed and can be carried out by spraying a fine mist of water droplets into a process gas stream, giving rise to evaporation of the water droplets and an increase in moisture content of the gas. Humidification to high 27°C to 38°C (80°F to 100°F) approaches to saturation temperature (i.e. low to moderate increases in gas humidity) can be easily achieved via installation of a simple spray nozzle in the gas duct. This is particularly true for a particulate free process gas. A typical problem arising in a particulate laden process gas application is the build-up of solids on the spray nozzle. If the deposit grows large enough, it can interfere with atomization spray quality, resulting in large droplets and greater evaporation time requirements. However, at a high approach to saturation temperature, the large temperature driving force for evaporation compensates, to a point, for poor droplet size distribution. Hence, quenching or cooling to high approaches to saturation temperature by means of spray evaporation is carried out frequently in many applications that require an immediate reduction in process gas temperature. Dry scrubbing technology which depends on the presence of moisture to achieve reaction of sulphur dioxide with sorbent is commercially available for sulphur dioxide removal from flue gases. Babcock & Wilcox, Flakt, Joy Niro and Research Cottrell are the major manufacturers of dry scrubbers. Treatment of flue gas with moisture and with sorbents injected dry or as slurries via the Linear VGA Nozzle is also know from Patent Specification US-A-4,314,670 to Walsh, Jr. which discloses a linear variable gas atomising nozzle best illustrated in Figures 12 and 13 of that specification. The specification does not disclose a low gas stream side pressure drop housing which solves the problem of deposition on the nozzle, however. An article by William A. Walsh, Jr. "A General Disclosure of Major Improvements in the Design of Liquid-Spray Gas Treating Processes though Commercial Development of Linear VGA Nozzle,", distributed by the author to solicit interest in this technology, describes improvements in a liquid-spray flue gas treating process which utilises the Linear VGA Nozzle design. Figure 3 of this article discloses the nozzle. This reference lacks both an airfoil geometry and shield air provision, resulting in increased process gas side pressure losses and deposition of solids on the nozzle, respectively. An airfoil lance assembly is discussed in very general terms on page 11 in a technical paper presented to the Energy Technology Conference & Exposition in Washington, D.C. on February 18, 1988. This technical paper mentions a shield air system. There are no drawings depicted in the article, or any details concerning the structure of the airfoil lance apparatus. A technical article by P.S. Nolan and R.V. Hendricks, "EPA's LIMB Development and Demonstration Program," Journal of the Air Pollution Control Association, Vol. 36, No. 4, April 1986 describes features of a limestone injection multistage burner (LIMB) system at Ohio Edison's Edgewater Station. The arrangement of injectors for sorbent injection is discussed on pages 435-436 thereof. A technical presentation by G.T. Amrhein and P.V. Smith, "In-Duct Humidification System Development for the LIMB Demonstration Project," presented at the 81st Annual Meeting of the Air Pollution Control Association, Dallas Texas, June 20-24, 1988, describes the development of an in-duct humidifier with optimum arrangement of atomizers. A technical presentation by P.S. Nolan and R.V. Hendricks, "Initial Test Results of the Limestone Injection Multistage Burner (LIMB) Demonstration Project," presented at the 81st Annual Meeting of the Air Pollution Control Association, Dallas Texas, June 20-24, 1988, describes the Edgewater LIMB design and operating conditions with the concept of humidification. Additional references which are relevant to the present invention are Patent Specifications:- US-A-4,285,838 to Ishida, et al.; US-A-4,019,896 to Appleby; US-A-4,180,455 to Taciuk; US-A-4,455,281 to Ishida, et al.; and US-A-4,285,773 to Taciuk. Patent Specification US-A-4 891 170 discloses lance apparatus wherein a member with a large radius leading edge faces an oncoming flow of gas into which an atomized mixture is to be sprayed. The member has a small radius trailing edge facing oppositely to the leading edge and a flowable medium conduit extending in the member with an inlet and an outlet to supply flowable medium. The member further has an atomizing gas conduit therein with an inlet and an outlet to supply atomizing gas and a nozzle means to spray the atomized mixture in a downstream direction into the gas stream. According to the invention there is provided lance apparatus comprising: a member having a large radius leading edge to face an oncoming flow of gas into which an atomized mixture is to be sprayed, and a small radius trailing edge to face oppositely to the leading edge; a flowable medium conduit extending in the member and having an inlet and an outlet, to supply flowable medium; an atomizing gas conduit extending in the member and having an inlet and an outlet, to supply atomizing gas; and nozzle means to spray the atomized mixture in a downstream direction into the gas stream; characterised in that the member is an airfoil member; at least one mixing chamber is provided in the airfoil member connected to the outlets of the flowable medium conduit and the atomizing gas conduit to mix the medium with the atomizing gas to form an atomized mixture; the nozzle means are connected to the mixing chamber and extend from the trailing edge; a nacelle is connected to the trailing edge and extends over the nozzle means, the nacelle defining a shielding gas discharge space to discharge shielding gas from the airfoil member around the nozzle means and in the downstream direction into the gas stream; and shielding gas supply means are connected to the airfoil member to supply shielding gas to the discharge space. Such airfoil lance apparatus can be used for homogeneous humidification and sorbent dispersion in a gas stream and can provide an aerodynamically efficient shape for a removable lance assembly containing a multiple number of atomizers and all related supply piping and hardware for in-duct installation in a process gas stream. Such airfoil lance apparatus, by minimising turbulence in the gas stream, can avoid the deposition of particles onto surfaces of the apparatus, in particular surfaces around and under the nozzle. It can also reduce pressure drop across the apparatus and can eliminate the likelihood of liquid or sorbent leakage to the exterior surfaces of the airfoil. The invention is diagrammatically illustrated by way of example in the accompanying drawings, in which:- Figure 1 is a partial perspective view of a duct for receiving a gas stream, in which a multiplicity of lance apparatus according to the invention have been installed; Figure 2 is a sectional view taken on line 2-2 of Figure 3 showing the construction of lance apparatus according to invention; and Figure 3 is a partial perspective view of lance apparatus according to the invention with portions cut away for clarity. Referring to the drawings, Figure 1 shows an arrangement for spraying an atomized mixture in a downstream direction into a flow of gas which is contained within a conduit 30. A multiplicity of airfoil lance apparatus generally designated 100 are positioned within the conduit 30. Each apparatus 100 includes a plurality of rearwardly directed nozzle assemblies for spraying the atomized mixture. Referring to Figures 2 and 3, in the apparatus 100, water or sorbent to be atomized enters an inner header manifold 1, at a port 21. The inner header manifold 1 supplies the water or sorbent to an atomizer mix chamber 5, via an inner barrel 2. The inner header manifold 1, is positioned by spacers 34 concentrically within an outer header manifold 3, which forms the leading edge of the airfoil lance apparatus. Atomizing gas enters a service supply lateral 12, through an atomizing gas inlet port 22, which directs the air to an annulus 14 formed between the inner header manifold 1 and the outer header manifold 3. The gas flows through this annulus and subsequently to the atomizer mix chamber 5, by entering, through an inlet port 19, an annulus 32 formed between the inner barrel 2, and an outer barrel 4 held by alignment spacers 20. The homogenized mixture of gas, liquid and/or solids exits the atomizer mix chamber 5, and subsequently nozzle openings 16 of an atomizer end cap 6. The outer barrel 4 is held to the manifold 3 by a packing gland 9, an O-ring 10 and a packing gland nut 11. Atomizer shield gas enters though a shield gas port 23 in a mounting plate 13 and is ducted through the passageway bounded in part by the outer header manifold 3, and an airfoil skin 7 which is fixed to the manifold 3. Subsequently the shield gas flows over the atomizer end cap 6, by entering an annulus 24 formed between the outer barrel 4 and a nacelle housing 8 extending from the trailing edge 18 of the airfoil skin 7. Uniform distribution of shield gas flow among the plurality of atomizers is accomplished through the use of a uniquely sized flow distributing orifice 33 fixed to the interior wall of each nacelle housing 8. Superficial gas flow first contacts the airfoil at the leading edge, i.e. the outer header 3, forming a stagnation point on the body's leading edge where flow is stopped. Symmetrically from the stagnation point, a laminar boundary layer is formed as gas starts to move around the body. The boundary layer comprises a thin sheet of gas immediately adjacent to the body surface. Gas velocity within the boundary layer is low due to friction between the gas and the surface of the body and a laminar or smooth flow distribution results. As the flow continues over the leading edge of the manifold 3, and over the airfoil skin 7, the boundary layer thickens and becomes unstable, forming a turbulent boundary layer which continues to the trailing edge 18 of the airfoil skin 7. If the body were not a streamlined airfoil shape, the turbulent boundary layer would become more unstable as it moved along the body and would separate from the body surface. The separated flow would form a turbulent wake which would result in an aerodynamic force resisting movement of gas past the non-airfoil body. The flow separation would increase the drag experienced on a body as gas moves past it. The airfoil design which entails the leading edge of the manifold 3, and the airfoil shaped skin 7, minimises flow separation and hence aerodynamic drag on the body. The drag co-efficient, C D for the airfoil shape is approximately 0.27 against 1.2 for a round pipe which is not streamlined. The nacelle enclosure 8 around each atomizer isolates the atomizer from any turbulence created at the trailing edge 18 of the airfoil. The skin 7 is closed at one end by the plate 13 and at its opposite end by a register plate 15 that carries an alignment pin 17 which is seated in a support 31 of the duct 30 shown in Figure 1. As shown in Figures 1 and 3, a plurality of the nozzle assemblies 4,5,6 extend from the trailing edge 18 of the airfoil member which is composed of the manifold 3 forming a large radius leading edge of the airfoil member facing the oncoming flow of gas and the airfoil skin 7 forming the small radius trailing edge 18 facing in the opposite direction. The manifolds 1 and 3 with their inlets 21 and 22 form a flowable medium conduit and an atomizing gas conduit, respectively. The shielding gas inlet port 23 and the interior space of the airfoil skin 7 together form shielding gas supply means to supply the shielding gas to the annular spaces 24 formed by the nacelles 8. Significant features of the design include: 1. The airfoil shape of the apparatus minimises the generation of separation turbulence associated with placement of a body in a gas stream with superficial velocity. This turbulence would otherwise result in gas recirculation patterns which provide the vehicle for particulate deposition on surfaces in contact with the gas stream. This problem is further compounded by recirculation patterns generated by aspiration mechanisms produced from the operation of an atomizer (i.e. entrainment of surrounding gas by each individual atomizer jet). 2. The shield gas supply provision is accomplished by the attachment of the nacelle enclosures around each atomizer nozzle assembly 4, 5, 6 positioned along the trailing edge 18 of the airfoil. This enclosure provides an annular flow path for the uniform distribution of shield gas to the atomizer nozzle end cap. 3. The concentric arrangement of the service supply piping can totally eliminate the possibility of a liquid or sorbent leakage to the exterior surfaces of the airfoil lance apparatus. 4. The design of the airfoil lance apparatus can be adapted to house any known atomizer type currently manufactured (i.e. dual fluid, pressure, rotary cup, vibratory and electrostatic types). The concentric header design of the apparatus of the invention has an advantage in that a water or slurry supply header housed inside the atomizing gas header, which forms the leading edge, minimises the profile of the airfoil. The exposed surface area onto which solids can collect and form deposits will be reduced as a result. An additional benefit of the concentric header arrangement with the atomizing gas header in the outer position it to maintain the air at a higher temperature, as a result of heat transfer from the process gas through the leading edge of the airfoil into the atomization gas. The higher temperature will prevent the possibility of condensation of acidic components on the surface of the outer header and the resulting corrosion will be stopped. The extended life of the unit as a result of corrosion reduction is commercially significant. The airfoil lance apparatus provides for a supply of particulate free shielding gas to each atomizer to protect against deposition. The shield gas flow is directed uniformly around each atomizer by the nacelles which are hollow cylindrical shapes surrounding each atomizer. Each nacelle is attached to the trailing edge of the airfoil via a smooth tapering transition. The smooth transition ensures minimal turbulence generation. The nacelle, thereby, mechanically protects the atomizer and the shield gas flowing through the annular region between the nacelle interior and the atomizer by developing a blanket of clean gas around it. The shield gas can be clean air or an inert dust free gas should an inert gas be required by the process. The length of the nacelle extending beyond the trailing edge of the airfoil is important to ensure that any turbulence resulting from gas contact with the airfoil is dissipated prior to reaching the atomizer jet. The nacelle length is set at a minimum of one times its diameter to prevent an interaction between airfoil and jet turbulences. These interactions result in recirculation patterns leading to contact of particulate laden gas on the atomizer and airfoil surfaces with consequential ash deposition. The nacelle length and airfoil shape of the apparatus, therefore, contribute to the shield gas effectiveness. The width of the annular gap between the atomizer and inner wall of the nacelle is important for effective shield gas distribution. The shield gas is supplied through the internal structure of the airfoil to each nacelle. Uniform distribution of shield gas to the individual nacelles is accomplished by the addition of flow orifices at each nacelle inlet as required. No additional piping is necessary to supply shield gas to each atomizer. The airfoil lance apparatus is adaptable to application-specific process requirements. The nature of its design allows it to be lengthened or shortened to meet specific duct dimensions. Placement of individual nozzles along a single airfoil lance can be varied to address specific process or individual atomizer spacing requirements. Although the original design of the apparatus of the invention accommodated an internal mix atomizer, specifically the Babcock & Wilcox I-Jet, Y-Jet and T-Jet designs, any conceivable type of atomizer can be installed within the airfoil housing with minimal modification to the airfoil design. The airfoil lance apparatus can be easily installed or removed from the process for inspection and maintenance impacting overall process availability. With proper design of the airfoil lance apparatus support system within a gas duct, the apparatus could be removed while the process is on line, serviced and reinstalled without the necessity of an undesired shutdown.

Claims: Lance apparatus comprising: a member (7) having a large radius leading edge (3) to face an oncoming flow of gas into which an atomized mixture is to be sprayed, and a small radius trailing edge (18) to face oppositely to the leading edge; a flowable medium conduit (1, 2) extending in the member (7) and having an inlet (21) and an outlet, to supply flowable medium; an atomizing gas conduit (14, 32) extending in the member (7) and having an inlet (22) and an outlet, to supply atomizing gas; and nozzle means (6, 16) to spray the atomized mixture in a downstream direction into the gas stream; characterised in that the member (7) is an airfoil member; at least one mixing chamber (5) is provided in the airfoil member (7) connected to the outlets of the flowable medium conduit and the atomizing gas conduit (14) to mix the medium with the atomizing gas to form an atomized mixture; the nozzle means (6, 16) are connected to the mixing chamber (5) and extend from the trailing edge (18); a nacelle (8) is connected to the trailing edge (18) and extends over the nozzle means (6, 16), the nacelle defining a shielding gas discharge space to discharge shielding gas from the airfoil member (7) around the nozzle means (6, 16) and in the downstream direction into the gas stream; and shielding gas supply means are connected to the airfoil member (7) to supply shielding gas to the discharge space. Lance apparatus according to claim 1, wherein the flowable medium conduit comprises an inner header manifold (1) and the atomizing gas conduit comprises an outer header manifold (3) surrounding the inner header manifold (1) and defining an annulus (14) for the passage of atomizing gas, part of an exterior surface of the outer header manifold (3) forming the leading edge of the airfoil member. Lance apparatus according to claim 2, wherein the airfoil member includes an airfoil skin (7) connected to the outer header manifold (3) and forming a smooth aerodynamic surface terminating at the trailing edge (18), the nacelle (8) being connected in a smooth transition to the airfoil skin (7). Lance apparatus according to claim 3, wherein the nozzle means comprises an inner barrel (2) connected to the inner header manifold, an outer barrel (4) connected to the outer header manifold and defining an annular space (32) around the inner barrel (2), the mixing chamber (5) communicating with the annular space (32) and with the inner barrel (2), and a nozzle cap (6) with at least one orifice (16) connected to the chamber (5) to discharge the atomized mixture through the orifice (16). Lance apparatus according to claim 4, wherein the nacelle (8) extends around and defines an annulus (24) with the outer barrel (4) to form the discharge space. Lance apparatus according to claim 5, wherein the nacelle (8) includes an internal flow distributing orifice (33) uniformly to distribute the shielding gas. Lance apparatus according to claim 1, wherein the airfoil member comprises an airfoil skin (7) defining an interior space having opposite ends, a mounting plate (13) having an opening (23) therein closing one end of the skin and a register plate (15) closing the opposite end of the skin (7), the skin having an opening in the trailing edge of the airfoil member covered by the nacelle (8), with the interior space of the skin defining the shielding gas supply means. Lance apparatus according to claim 7, wherein the nacelle (8), extends by at least an amount equal to a diameter of the nacelle (8), beyond the trailing edge of the airfoil member with an aspect ratio of the nacelle internal diameter to atomizer outside diameter being not less than 1.5 nor greater than 6.0. Lance apparatus according to claim 8, including a plurality of nozzle means spaced along and extending from the trailing edge of the airfoil member, with the respective nacelle (8) connected to the trailing edge extending over each of the nozzle means. Lance apparatus according to claim 1, wherein the flowable medium conduit and the atomizing gas conduit comprise concentric inner (1) and outer (3) header manifolds, the inlet (22) of the atomizing gas conduit comprising a service supply lateral connected to the outer header manifold (3). Lance apparatus according to claim 10, including a mounting plate (13) connected to an end of the airfoil member (7) adjacent the service supply lateral (12) the mounting plate (13) having an opening (23) therein communicating with the interior of the airfoil member (7), the opening (23) in the mounting plate (13) and the interior of the airfoil member forming the shielding gas supply means, the airfoil member having an opening in the trailing edge (18) thereof covered by the nacelle (8) to receive shielding gas from the interior of the airfoil member to the discharge space defined by the nacelle (8).

Inventors: MYERS ROBERT B, YAGIELA ANTHONY S, MYERS, ROBERT B., YAGIELA, ANTHONY S.
Applicants: BABCOCK & WILCOX CO, THE BABCOCK & WILCOX COMPANY
Application year: 1991
Main classification: B05B7
IPC codes: B01D53, B01F3, F24F13, B03C3, B05B7, F24F6, B01F5