CN1626289A - Detonative cleaning apparatus nozzle - Google Patents
Detonative cleaning apparatus nozzle Download PDFInfo
- Publication number
- CN1626289A CN1626289A CNA2004101006410A CN200410100641A CN1626289A CN 1626289 A CN1626289 A CN 1626289A CN A2004101006410 A CNA2004101006410 A CN A2004101006410A CN 200410100641 A CN200410100641 A CN 200410100641A CN 1626289 A CN1626289 A CN 1626289A
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- Prior art keywords
- flange
- downstream
- upstream
- cooling fluid
- wall
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28G—CLEANING OF INTERNAL OR EXTERNAL SURFACES OF HEAT-EXCHANGE OR HEAT-TRANSFER CONDUITS, e.g. WATER TUBES OR BOILERS
- F28G7/00—Cleaning by vibration or pressure waves
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B7/00—Cleaning by methods not provided for in a single other subclass or a single group in this subclass
- B08B7/0007—Cleaning by methods not provided for in a single other subclass or a single group in this subclass by explosions
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B9/00—Cleaning hollow articles by methods or apparatus specially adapted thereto
- B08B9/08—Cleaning containers, e.g. tanks
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28G—CLEANING OF INTERNAL OR EXTERNAL SURFACES OF HEAT-EXCHANGE OR HEAT-TRANSFER CONDUITS, e.g. WATER TUBES OR BOILERS
- F28G7/00—Cleaning by vibration or pressure waves
- F28G7/005—Cleaning by vibration or pressure waves by explosions or detonations; by pressure waves generated by combustion processes
Abstract
An apparatus directs gas from an upstream conduit through a vessel wall for cleaning surfaces within the vessel. A mounting flange couples the apparatus to the upstream conduit delivering the gas. The flange has first and second faces, an inboard surface bounding a central aperture, an outboard perimeter, and an array of bolt holes between the first and second faces. A conduit extends downstream from the flange and has inner and outer walls along at least a portion of a length and a space between the inner and outer walls for carrying a cooling fluid. The apparatus has a cooling fluid inlet and a cooling fluid outlet.
Description
Technical field
The present invention relates to industrial equipment.More especially, the present invention relates to the pinking cleaning of industrial equipment.
Background technology
The surface dirt is the subject matter in the industrial equipment.This equipment comprises stove (coal stove, oil oven, waste furnace, or the like), boiler, gasifier, reactor, heat exchanger, or the like.Usually, this equipment comprises the container that comprises the internal heat transfer surface, and internal heat transfer surface has been owing to accumulated particle for example cigarette ash, ashes, mineral and other combustion product and byproduct, more one assemble as slag and/or dirt etc., and be easy to form dirt.This particle assembles obstruction equipment operation gradually, lower efficiency and output and may cause infringement.Therefore be starved of equipment is cleaned and the cleaning of equipment need be considered many correlative factors.Usually, be difficult to directly near the surface that has dirt.In addition, in order to keep income, the industrial equipment downtime need be minimized with the cost relevant with cleaning.Multiple technologies have been proposed.For instance, at United States Patent (USP) 5,494,004 and 6,438,191 and U.S. Patent application publication 2002/0112638 in multiple technologies have been proposed.Other technology is disclosed in document Huque, Z.Experimental Investigation of Slag Removal UsingPulse Detonation Wave Technique, DOE/HBCU/OMI AnnualSymposium, Miami FL., March 16-18 is in 1999.Detailed shock wave technology by
With
Below it, be described in the publication:
K.and
I., Further Experience Using Detonation Wavesfor Cleaning Boiler Heating Surfaces, International Journalof Energy Reseafch Vol.17,583-595 (1993) and
K.and
I., Detonation-Wave Technique for On-load DepoistRemoval from Surfaces Exposed to Fouling:Parts I and II, Journal of Engineering for Gas Turbines and Power, Transactions of the ASME, Vol.1,116 223-236, January 1994.This type systematic is also discussed in Yugoslavia patent publications P 1756/88 and P 1728/88.According to the exemplary application of this technology, this type systematic usually is known as " soot blower ".
Yet, in this field, still have many possibilities that require further improvement.
Summary of the invention
One aspect of the present invention relates to a kind of being used for gas is imported so that the equipment on the surface in the cleaning container by chamber wall from upstream line.Mounting flange is connected in equipment on the upstream line of carrying gas, and has first and second, defines inner surface, the outside circumference of centre bore and the bolt hole array of extending between first and second face.Pipeline extends downstream from flange, and has along the inner and outer wall of at least a portion length.Space between inwall and the outer wall is used to transport cooling fluid.Has the outlet of cooling fluid inlet and cooling fluid.
In various implementations, the space can be extended in wall at least in part downstream from the upstream extremity in the chamber wall outside.Cooling fluid outlet can be along pipeline and cooling fluid inlet can be along flange.Inner and outer wall can respectively have a downstream edge.The cooling fluid outlet can be between inwall and outer wall.Inwall can be formed by first pipe fitting basically, and this first pipe fitting is from upstream edge edge extension downstream and have inner surface and outer surface.Along upstream portion, inner surface can provide the flange inner surface.Equipment can with container combination together.Container can be for having the stove that furnace interior and stove outside is separated and have the furnace wall of cinclides.This combination can comprise the pinking source of gas.Flange can be positioned at the upstream of furnace wall outer surface.Pipeline can extend so that stretch out to the downstream of furnace wall inner surface by the furnace wall.
Another aspect of the present invention relates to a kind of sootblower nozzle.There is device that nozzle is installed on the soot blower gas pipeline of upstream.The surface imports gas the inside of container from the soot blower gas pipeline.The device cooling jet is arranged.
Another aspect of the present invention relates to a kind of method that cleanliness of operation has the inner surface device therefor in the container of chamber wall that is used for.In combustion pipe, produce the burning pulse.Burning gases are passed through chamber wall along the combustion pipe guiding, so that spray from the outlet of combustion pipe.Refrigerating gas transmits along the part that is subjected to from the combustion pipe of the heat effects of container.
In various implementations, this load mode may continue to exist between a plurality of burning pulses basically.This load mode can comprise along the transmission of the path to small part round the part of burning gases stream cooling fluid.This load mode can comprise along the path sends cooling fluid into internal tank.
The details of one or more embodiment of the present invention is illustrated in accompanying drawing and following detailed description.By reading the following description and drawings and claim, can know and understand other features, objects and advantages of the present invention.
Description of drawings
Fig. 1 is the view of industrial furnace, and it is associated with some soot blowers that are positioned to the aspect that is used to clean stove.
Fig. 2 is the side view of one of soot blower of Fig. 1.
The side view that Fig. 3 cuts open for the part of the upstream extremity of the soot blower of Fig. 2.
Fig. 4 is the longitudinal sectional view of main burner portion section of the soot blower of Fig. 2.
Fig. 5 is the end-view of portion's section of Fig. 4.
Fig. 6 is the side view of the substituted type discharge end part of combustion tube assembly.
Fig. 7 is the view of gas curtain flange of the assembly of Fig. 6.
Fig. 8 is the downstream end view of the flange of Fig. 7.
Fig. 9 is the downstream end view of heat insulation flange assembly.
Figure 10 is the exploded view of the assembly of Fig. 9.
Figure 11 is the view of nozzle assembly.
Figure 12 is the downstream end view of the nozzle assembly of Figure 11.
Figure 13 is the longitudinal sectional view that the nozzle assembly 13-13 along the line of Figure 12 cuts open.
Figure 14 is the zoomed-in view of flange section of the nozzle assembly of Figure 13.
Figure 15 is the local longitudinal sectional view of downstream end portion of the nozzle assembly of Figure 11.
Figure 16 is the local longitudinal sectional view of substituted type gas curtain flange.
In each figure, identical reference number and label indication components identical.
The specific embodiment
Fig. 1 shows the stove 20 with three exemplary relevant soot blowers 22.In the embodiment shown, shaft forms the form of positive parallelepiped, and soot blower all is associated with the single common wall 24 of body of heater and is placed on the identical height along wall.Also can adopt other configuration (for example have one or more soot blowers on each aspect in individual sootblower, a plurality of aspect, or the like).
Each soot blower 22 comprises the long combustion pipe 26 that extends to the proximal downstream end 30 of abuts wall 24 from the upstream far-end 28 away from furnace wall 24.Yet randomly, end 30 can suitably be positioned at stove.When each soot blower of operation, the burning of fuel/oxidant mixture that is positioned at pipeline 26 is in that beginning is so that produce detonation wave near upstream extremity (for example the upstream of duct length 10%), and this detonation wave penetrates so that the surface in the internal volume of stove is cleaned from downstream as shock wave with relative combustion gas.Each soot blower can be associated with fuel/oxidant source 32.This provenance or its one or more parts can be shared by each soot blower.An exemplary source comprises liquefaction or compressed fuel gas cylinder 34 and the oxygen cylinder 36 that is arranged in corresponding container structure 38 and 40.In the exemplary embodiment, oxidant is for example oxygen of substantially pure of first oxidant.Second oxidant can be the form of 42 shop airs of carrying from the center air source.In the exemplary embodiment, air is stored in the air receiver 44.The fuel that is got by the fuel volumetric growth in the cylinder 34 generally is stored in the fuel accumulator 46.Each exemplary source 32 is connected on the associated conduit 26 by the suitable waveguide that is positioned at the below.Similarly, each soot blower comprises spark case 50, and it is used for the fire fuel oxidant mixture, and it is controlled by control and monitoring system (not shown) with source 32.Also illustrate among Fig. 1, wall 24 comprises a plurality of mouths of checking and/or measuring of being used to.Exemplary mouth comprises optical monitoring mouth 54 and the monitoring temperature mouth 56 that is associated with each soot blower 22, is used for putting respectively infrared ray and/or visible light camera and thermocouple probe, so that observe surface to be cleaned and monitoring internal temperature.Also can use other probe/monitoring/sampling apparatus, comprise pressure monitor, composition sampling apparatus, or the like.
Fig. 2 shows the more details of exemplary soot blower 22.Exemplary pinking pipeline 26 has by the pipe sections or the part 60 of the two flanges of a series of bands that are from upstream to arranged downstream and has the downstream nozzle pipe sections of downstream part 64 or the main part that part 62 forms, and downstream part 64 extends through the hole that is arranged in wall and ends at the downstream that is exposed at furnace interior 68 or export 30 places.The term nozzle is the meaning of summarizing this usefulness, thereby does not require contraction, expansion or its combination that exists on any aerodynamics.Illustrative conduit portion section material is metal (a for example stainless steel).If provide suitable supporting and cooling device, outlet 30 can be positioned at stove position more inward.Fig. 2 also shows tube bank 70 in the stove, and often there is dirt in their outer surface.In the exemplary embodiment, each pipe sections 60 is supported on the relevant chassis 72, and the wheel of chassis 72 engages with rail system 74 along equipment bay 76.Exemplary rail system comprises the closed slide that spill outer surface a pair of and the chassis wheel engages.Each exemplary section 60 has similar length L
1, and the associated bolt array of the bolt hole by being arranged in its respective flange and bolt end-to-end.Similarly, the downstream flange of the downstream portion section in each section 60 is bolted on the upstream flange of nozzle 62.In the exemplary embodiment, the reaction band 80 (for example firm synthetic material on cotton or the calorifics/structure) that is connected in series with one or more metal spiral antagonistic springs 82 is connected in this most last flange that matches to last, and combustion pipe is connected on environmental structure such as the furnace wall, so that flexibly absorb the reaction force relevant and the assurance combustion pipe is correctly placed to light subsequently with the emissions operation of soot blower.Randomly, can provide other damping (not shown).Reaction band/spring assembly can form single length or ring.In the exemplary embodiment, the downstream portion section of this combination has total length L
2Substituting elastic recoil absorption plant can comprise nonmetal or non-helical spring or rubber or other under tension force, compression and/or shear action advantageously to the elastomer element of small part strain, air pressure recoil absorber, or the like.
Pre-detonating agent pipe sections 84 is extended downstream from upstream extremity 28, and it also can be with two flanges and have length L
3The feature internal cross-sectional area (perpendicular to the axis/center line 500 of pipeline) of pre-detonating agent pipe sections 84 is less than the feature internal cross-sectional area of the downstream part (60,62) of combustion pipe (for example average, intermediate value, mode, or the like).In the exemplary embodiment that relates to circular cross section pipeline portion section, pre-detonating agent cross-sectional area is characterised in that diameter between between the 8cm to 12cm, and the downstream part is characterised in that diameter is between between the 20cm to 40cm.Correspondingly, the example transverse cross-sectional ratio of downstream part and pre-detonating agent portion section is between 1: 1 to 10: 1, and is narrower, between 2: 1 to 10: 1.Total length L between the end 28 and 30 can be 1-15m, and is narrower, is 5-15m.In the exemplary embodiment, transition conduit portion section 86 extension between pre-detonating agent portion section 84 and upstream portion section 60.Portion's section 86 has size and is suitable for the upstream and downstream flange that matches with the respective flange of portion section 84 and 60, and has the inner surface that seamlessly transits is provided between the internal cross section of portion's section 84 and 60.Exemplary section 86 has length L
4Exemplary half-angle≤12 of dispersing of the inner surface of portion's section 86 °, narrower, be 5-10 °.
The fuel/oxidant charging can be introduced the pinking pipe interior according to variety of way.One or more different fuel/oxidant mixtures can be arranged.This mixture can carry out premixed in pinking pipeline outside, perhaps can introduce the pipeline place or introduce the laggard row mixing of pipeline.Fig. 3 shows portion's section 84 and 86 and is configured to and is used for introducing respectively two kinds of different fuel/oxidant combinations: pre-detonating agent combination; With main combination.In the exemplary embodiment, in the upstream portion of portion's section 84, a pair of pre-detonating agent fuel injection pipe road 90 is connected on the mouth 92 of the Duan Bizhong of portion that defines fuel injection orifice.Similarly, a pair of pre-detonating agent oxidant conduit 94 is connected on the oxidant inlet 96.In the exemplary embodiment, these mouthfuls are arranged in the upstream half section on the length of portion's section 84.In the exemplary embodiment, each all (is depicted as exemplary 90 ° in that identical axial positions is angled in the fuel injection orifice 92, but also can be for comprising other angle of 180 °) with relevant oxidant mouth 96 pairings so that mix for fuel and oxidant provide relative jet.Will further discuss hereinafter, purge gas pipeline 98 is connected on the purge gas mouth 100 similarly at upstream end more.The end plate 102 that is bolted on the upstream flange of portion's section 84 is sealing the upstream extremity of combustion pipe and is passing the igniter/trigger 106 (for example spark plug) with the operation end 108 that is positioned at portion's section 84 inside.
In the exemplary embodiment, main fuel and oxidant are introduced in portion's section 86.In the embodiment shown, main fuel is transported by a plurality of main fuel pipelines 112 and primary oxidant is transported by a plurality of primary oxidant pipelines 110, wherein each primary oxidant pipeline 110 has with one heart the port around associated fuel pipeline 112, so that at relevant inlet 114 places mixing main fuel and oxidant.In the exemplary embodiment, fuel is hydrocarbon.In special exemplary embodiment, two kinds of fuel are identical, and but they are drawn from single fuels sources mix with different oxidant: mix so that obtain pre-detonating agent mixture with pure basically oxygen; Mix so that obtain main mixture with air.Available in this case exemplary fuel has propane, MAPP gas or its mixture.Also other fuel be can use, ethene and liquid fuel (for example diesel oil, kerosene and jet aviation fuel) comprised.Oxidant can comprise mixture, and the air/oxygen mixture of proper proportion for example is so that obtain required master and/or pre-detonating agent charging chemical property.In addition, have the fuel of molecular combinations and the monopropellant fuel of oxidant constituents and also can be used as selection.
When operation, begin the place in life cycle, except having air (or other purge gas), when beginning, be sky in the combustion pipe.Pre-detonating agent fuel and oxidant are introduced by critical point mutually subsequently, charge into portion's section 84 and extend partially in portion's section 86 (for example near midpoint), and advantageously just surpassed main fuel/oxidant mouth.Cut off pre-detonating agent fuel and oxidant stream then.The pre-detonating agent fuel that charges into and the exemplary volume of oxidant account for the 1-40% of combustion pipe volume, and be narrower, accounts for 1-20%.Introduce main fuel and oxidant then so that charge into the combustion pipe residual volume of definite part (for example 20-100%) basically.Cut off main fuel and oxidant stream then.Introduce pre-detonating agent fuel and oxidant through main fuel/oxidant mouth before this, just eliminated between pre-detonating agent and main charging, forming air or other does not fire the danger of piece greatly.This can prevent that combustion front from moving between two chargings.
After introducing charging, with regard to the pilot spark case so that the spark discharge of trigger is provided, thereby light pre-detonating agent charging.Pre-detonating agent charging is chosen to have the chemical property of very fast burning, and therefore in portion's section 84, initial detonation changes pinking apace into, and produces detonation wave.In case produced this detonation wave, just can pass through main charging effectively, and main charging may have enough slow chemical property in addition so that can pinking in pipeline automatically.Ripple longitudinally passes through downstream and occurs from the form of downstream 30 as the shock wave in the stove, thereby bombards on surface to be cleaned and generation calorifics and impact mechanically, so that dirt is fluffed.The pressure combustion product that to and then discharge from the pinking pipeline after the ripple, the product that row comes occurs as the form of jet and further finishes cleaning course (for example removing the material that has come loose) from downstream 30.After discharging combustion product, perhaps carry out simultaneously with the discharge combustion product, by (for example purging mouthful 100 introducing purge gas, air and/or nitrogen from the same source that is used to provide primary oxidant) (carry out immediately, perhaps carrying out (it can manually be determined or be automatically definite by control and monitoring system) according to regular or irregular interval subsequently so that repeat following one-period so that displace and make the pinking pipeline to be full of purge gas final combustion product.Randomly, can keep the baseline stream of purge gas between the cycle, so that prevent from upstream to permeate and be convenient to help the pinking pipeline is cooled off from the gas in the stove and particle in feed/drain.
In various implementations, internal surface area significantly can be increased to and exceed by for outside cylindrical and Frusto-conical the surface area that the section inner surface provides nominally inner surface increases device.Increase device and can help effectively to realize that detonation to detonation transition or help keeps detonation wave.The inner surface that Fig. 4 shows on the inner surface that is applied to one of principal part section 60 increases device.Nominally exemplary increase device is the Chin spiral, but also can use other to increase device, for example Shchelkin spiral and Smirnov chamber.Spiral is formed by helical form member 120.Exemplary member 120 forms the form of the hardware (for example stainless steel metal line) with circular cross section, and its diameter of section is approximately 8-20mm.Alternatively, also can use other cross section.Exemplary member 120 keeps being separated by by a plurality of staves 122 and portion's section inner surface.Exemplary stave be cross section and materials similar in member 120 and welding thereon with the inner surface of dependent part section 60 on bar.This increase device also can be used to provide in advance detonate, to replace relating to the aforementioned techniques of different feeds and different burner cross sections or replenishing as aforementioned techniques.
This equipment has widely to be used.For instance, just in typical coal furnace, equipment can be applied to: suspension or two-stage superheater, convection channel (primary superheater and economizer bundle); Air preheater; Selecting catalyst remover (SCR) washer; Dust storage chamber or electrostatic precipitator; Economizer hopper; No matter be to be positioned at heating surface or other local lime-ash or other heat/gather, or the like.Similarly possibility is present in other application, comprises that oil burner, black liquor recovery boilers, biological fuel boiler, waste recovery utilize stove (refuse furnace), or the like.
Can take other step that combustion pipe (or its major part) and chemical contamination and thermal stress are broken away from.
Fig. 6 shows the outlet/discharge end assembly 140 that extends to outlet 30 '.Port of export assembly 140 can be used as downstream nozzle/outlet conduit portion section and replace the portion's section 62 among Fig. 2.Although be known as nozzle, this does not also require and has any specific convergence in nozzle, disperse or its combination.Exemplary assembly 140 provides the device that is used for the upstream portion of combustion pipe is carried out heat and chemical isolation.To the downstream, assembly 140 comprises the pipe sections 142 of the two flanges of band from the upstream, and it has upstream and downstream screw flange 144 and 146.The main body of pipe sections 142 can have a plurality of instrumentation mouths and/or sample tap 148, on they can be blocked when not using.Flange 144 has upstream face, so that be installed on the downstream face of downstream flange of penult pipe sections.This connection also can be used for connecting reaction band or other device.Flange 146 has and is used for the downstream face that matches with the upstream face of gas curtain flange 150, and is as described below, and this gas curtain flange 150 provides chemical isolation for the part of the combustion pipe that is positioned at its upstream.Gas curtain flange 150 has and is used for the downstream face that matches with the upstream face of hot isolation flange 152, and this flange 152 is subjected to cooling off for use in the upstream portion of combustion pipe is isolated with the heat effect (heat is returned and soaked) from stove.Hot isolation flange 152 has and is used for the downstream face that matches with the upstream face of the flange 154 of nozzle assembly 156, and this nozzle assembly 156 has the nozzle body 148 of outlet of extending to 30 ' and also as mentioned belowly further cooled off.Nut and bolt combination 160 are passed the bolt hole of flange 146,150,152 and 154 so that on structure each parts is fixed together hermetically.
Exemplary gas curtain flange 150 (Fig. 7 and 8) comprises upstream face and downstream face, outer surface 170 and interior perimeter surface 172, and it defines the burning gases stream.Bolt hole array is extended between upstream face and downstream face.Inner surface 172 is basic identical apart from the radius of pinking pipe centerline, and is the same with the inner surface of adjacent channel portion section 142.Circular passage 174 is formed at (for example downstream face) in one of them face, and is communicated with external port 178 on being positioned at side face by connecting path 176.Passage inner edge 180 (be depicted as part and illustrated by the downstream face that passage and other section separate) along inner surface is divided into the multi-section section or is divided into castellation by the array along the circumferential direction of slit 182.Under confined state, the mouth at edge is by adjacent surface (for example downstream face of the downstream flange 146 of the upstream face of hot isolation flange or the pipe sections 142) sealing of the flange that matches with it.Gas (for example, air, N
2, CO
2Perhaps other compares inert gasses) can be by being introduced into path and mouthful (it may have suitable connection fittings (not shown among Fig. 7 and 8)) passage 174.When such introducing, gas is full of passage and inwardly flows into combustion pipe inside by slit.Exemplary gas curtain flange can be formed by proper metal (for example, steel or Ni-based or cobalt-based super heat-resistant alloy) machined (for example, directly machined or by foundry goods or forging machined).
Figure 16 shows a kind of hot isolation flange 184 of substituted type that comprises passage 185 and path 186.Substituted type flange 184 can have with flange 150 similarly constructs.The difference of exemplary substituted type flange 184 is that its outlet is provided by the full hole in inboard/inner surface 188 but not provided by groove.And these holes tilt so that make discharge effluent Off-Radial (for example, angled θ is so that have the downstream longitudinal component).Tangential flow component if desired, the center line in hole also can be oriented and have tangential component.Downstream longitudinal stream component can help also to prevent that pollutant from passing upstream from stove.The example values of angle θ is between 5 ° and 60 °.
When operation, air-flow can replenish or replace the flow of purge gas that baseline continues.Locate because gas curtain flange 150 is positioned near outlet 30 ', therefore can improve to the upstream infiltration again of the burning gases of discharging with to the infiltration of common furnace gas and the resistance of particle pollution from equipment.Except pollution from the particle that is produced in the stove, gas curtain stream has prevented the accumulation from the particle reaction product of burning gases, especially can cool off and be settled out particle or liquid condensate because of this gas, and this may allow the formation or the sedimentary formation of particle.If according to the baseline mode operation, then the air-flow of Chi Xuing also can provide the additional cooling effect to pipeline (especially in the downstream of introducing point).
Fig. 9 and 10 shows the details of exemplary hot isolation flange 152.This flange comprises upstream face, downstream face and outer peripheral face 190.It also is included in the inner surface 192 that the radius substantially the same with the inner surface of adjacent component surrounds the burning gases stream.Bolt hole array is extended between upstream face and downstream face.The passage 194 that is formed on one of them face (for example downstream face) inwardly extends longitudinally thus.In the embodiment shown, passage has two general parts: less than the dark base part 196 of loopful with extend to correlation surface and be the notch portion 198 of loopful.Notch portion is wider than base part, by it not only radially inwardly but also extend radially outward, so that limit a pair of annular shoulder surface 200 and 202.In the exemplary embodiment, passage carries out machined in two steps.Notch portion can form in machined, and base part can carry out machined below the pedestal of notch portion then, stays the partitioned portion 204 of flange between the two ends of base part.Alternatively, base part can at first form loopful, and then separating element is inserted so that the pedestal passage is become the part annular.A pair of path 206 is connected in (for example, in the side face of flange) on relevant external port 210 and 212 with 208 associated end with the channel base part.External port can be equipped with suitable accessory.In the exemplary embodiment, the notch portion of passage is being held loopful sealing ring 214, and it is placed on the shoulder surface of residue main component of flange and can be welded in the appropriate location so that closed channel.Alternatively, under the situation that does not have notch portion and sealing ring, adjacent flanges self can closed and sealed passage.When operation, heat-transfer fluid is introduced by one of them mouthful, and is along the circumferential direction discharging by the mouth from other behind the passage.Exemplary heat-transfer fluid can be applicable to carrying out liquid that required heat transmits (for example, water-based (mixture of water or water/ethylene glycol) or oil base) or gas (for example, the CO of air or compression/cooling
2Or N
2).Similarly, the geometry of heat transfer stream (for example passage) and flowing velocity can be adapted to realize required heat transmission.Heat-transfer fluid can either help cooling jet, and the nozzle temperature and the upstream components that can help again to raise are isolated.This hot isolation flange can be used for other place of system, also can use in other soot blowers or in the different application that needs heat to isolate.Can use and gas curtain flange materials similar and manufacturing technology.
Figure 11-14 further shows the details of nozzle assembly 156.Nozzle assembly shown in Figure 13 comprises is responsible for 220, and it has inner surface 222 and outer surface 224, and extends to the downstream edge 230 that defines outlet 30 ' basically from upstream edge 226.But inner surface distance center line is positioned at the radius substantially the same with the inner surface of above-mentioned other parts.Flange 154 comprises that the Your Majesty swims part 232, and it has upstream face 234, downstream face 236, inner surface 237 and outer surface 238.Main part 232 is fixed on the person in charge 220 the upstream portion, and its inner surface contacts with the outer surface of pipe.Exemplary connected mode is welding.Ring-shaped air chamber can be in main flange part 232 machined form the notch of the inside part of downstream face (for example, as).The Outboard Sections of passage is by 242 sealings of second flange part, and this flange part 242 has upstream face 244, downstream face 246, inner surface 248 and periphery 250.Upstream face 244 can be in connection with first downstream face 236 and sealing thereon, for example O type circle 252 sealings of the passage by being arranged in one of them part or two parts at least in part.These two parts can keep together by identical bolt/nut or by independent bolt, welding or the like.Inner surface 248 is spaced apart a little with tube outer surface 224.Cover 254 has inner surface 256 and outer surface 258 and 260 extends to downstream/edge 262 (Figure 13) from upstream extremity/edge.Inner surface 256 is spaced apart with tube outer surface 224 similarly, and upstream end portion is fixed in second of flange and goes up (for example, be received in the annular notches and welding thereon).Measure ring 264 and define air chamber 240 so that radially separate its inside part and Outboard Sections and have a plurality of holes that are positioned at wherein.One or more feeding paths 270 (being depicted as two) are communicated with air chamber 240.Path 270 is connected with the mouth (for example, in first of flange) 272 that is carrying accessory 274.Cooling fluid (for example, with gas like the gas curtain gas) is introduced along the nozzle cooling flowing path downstream by accessory, path, and is introduced into the Outboard Sections of air chamber 240.Ring 264 and hole measurement thereof from the Outboard Sections of air chamber 240 to inside part flow and when discrete supply port negligible amounts, help dispense flow rate along the circumferential direction.Stream continues advanced downstream from the inboard/downstream part of air chamber 240 the space 276 that is essentially annular between cover 250 and pipe 220.In the exemplary embodiment, cooling blast is discharged from the outlet of the refrigerating gas between the adjacent part of cover downstream edge 262 and tube outer surface 224 278.In the exemplary embodiment, cover edge, upstream is recessed slightly with respect to the pipe downstream edge, so that alleviate detonation wave to the influence of cooling blast and alleviate ripple to the influence of thin and frangible cover.
Advantageously, provide the device that is used for the relation that along the circumferential direction separates between holding tube 220 and the cover 254.Exemplary device comprises one or more isolated components.Isolated component can be associated with being used to measure roughly by the pipe and the device of temperature parameter that is positioned at the nozzle body that cover limited in flange downstream.Figure 11 shows the first exemplary separator 280.The first exemplary separator is forked, has two and extends to the prong 282 and 284 of joint 286 from upstream extremity, and single leg 288 further extends downward leg downstream near the cover downstream from joint 286.Distance between the prong can be held the additional heat galvanic couple (not shown) of contiguous joint, and its line traces back to the upstream and passes thermocouple accessory mouth 290 in the main flange part 232.Figure 15 shows second separator 292, nominally it is the elongated band of rectangle that is, extends to the downstream that is positioned at pipe downstream 230 places from the upstream extremity that is positioned at the cover upstream extremity.Exemplary separator 292 has in outside it and the hole between the inner surface in its downstream end, and the similar blind hole of alignment extends internally from tube outer surface.Thermocouple 294 is installed in the blind hole, and its main body 296 stretches out and by the protective cover on the outer surface that is fixed in cover 298 (also being shown among Figure 11) round cover.Thermocouple 294 is used for the temperature at measuring tube downstream edge place.Flange material therefor and mounting technique can be similar with gas curtain and hot isolation flange material therefor and mounting technique.Pipe, cover and ring material therefor can be similar and can be adopted various known manufacturing technologies to make (for example, the rolling and welding or the machined of sheet material).
When operation, control is used first thermocouple 294 with monitoring system so that main monitoring is exposed to the temperature of the nozzle assembly part in the stove.When not wishing that hard stop is repaired, above-mentioned additional heat galvanic couple can be monitored as standby under the situation that first thermocouple lost efficacy.When the output according to two thermocouples decides shutdown, can use identical or different critical-temperature.
Get back to Fig. 6, nozzle assembly can have the interface plate 300 of the part of sealing the hole, furnace wall that is positioned at the nozzle body outside substantially.In when operation, plate 300 settle near the furnace wall outer surface usually or with its tight contact.Plate can have a plurality of holes that are used to hold various measurements, sampling, observation and other equipment.These holes can have lid when not using.A series of pillars 302 are connected on the flange 154 plate 300 so that keeping plate with respect to flange.Plate can have the hole that almost surrounds main body 158.Plate stops up cinclides usually so that limit gas at least in part and particle mobile (for example inflow in the negative pressure stove) between combustion tube and cinclides.When the equipment discharging, utilize the effect of reaction band/spring assembly, exemplary plate recoils with combustion pipe, and therewith is back to its home position.The used material of exemplary plate is steel or Ni-based or cobalt-based super heat-resistant alloy, randomly has insulating barrier (for example gummed property (cementaceous) material).
More than one or more embodiment of the present invention are described.Yet, should be appreciated that and under the situation that does not deviate from the spirit and scope of the present invention, can make various changes.For example, can make the present invention be applicable in the various industrial equipments and in the various soot blower technology.The aspect of existing device and technology may influence the aspect of any specific implementation mode.Combustion pipe may adopt other shape (for example, be used for by outside or internal block non-straight section).Correspondingly, other embodiment is also within the scope of following claim.
Claims (12)
1. one kind is used for importing gas so that the equipment on the surface in the cleaning container comprises from upstream line by chamber wall:
Mounting flange is used for being connected in equipment on the upstream line of carrying gas and having:
First and second;
Define the inner surface of centre bore;
Outside circumference; And
Bolt hole array between first and second;
Pipeline, extend downstream and have from flange:
At least along the inner and outer wall of a part of length; And
Between inwall and outer wall, be used to transport the space of cooling fluid;
Cooling fluid inlet; And
The cooling fluid outlet.
2. equipment according to claim 1, wherein:
Extend in wall at least in part downstream from the upstream extremity in the chamber wall outside in this space.
3. equipment according to claim 1, wherein:
The cooling fluid outlet is along pipeline; And
Cooling fluid inlet is along flange.
4. equipment according to claim 3, wherein:
Inner and outer wall respectively has downstream edge; And
The cooling fluid outlet is between inwall and outer wall.
5. equipment according to claim 1, wherein:
Inwall is formed by first pipe fitting basically, and this first pipe fitting extends and has inner surface and outer surface in the edge downstream from upstream edge, and along upstream portion, inner surface provides the flange inner surface.
6. equipment according to claim 1, its combination has:
Described container, this container is a stove, has the furnace wall that stove outside and furnace interior is separated and have cinclides; And
The pinking source of described gas.
7. combination according to claim 6, wherein:
Flange is positioned at the upstream of furnace wall outer surface; And
Pipeline extends so that stretch out to the downstream of furnace wall inner surface by the furnace wall.
8. sootblower nozzle comprises:
Be used for nozzle is installed on device on the soot blower gas pipeline of upstream;
Be used for gas is imported from the soot blower gas pipeline surface of internal tank; And
The device that is used for cooling jet.
9. one kind is used for the method that cleanliness of operation has the inner surface device therefor in the container of chamber wall, and this method comprises:
In combustion pipe, produce the burning pulse;
Burning gases are passed through chamber wall along the combustion pipe guiding, so that spray from the outlet of combustion pipe; And
Transmit refrigerating gas along the part that is subjected to from the combustion pipe of the heat effects of container.
10. method according to claim 9, wherein:
Described load mode continues to exist basically between a plurality of described burning pulses.
11. method according to claim 9, wherein:
Described load mode comprises along the transmission of the path to small part round the part of burning gases stream cooling fluid.
12. method according to claim 9, wherein:
Described load mode comprises along the path sends cooling fluid into internal tank.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/733,717 US20050125932A1 (en) | 2003-12-11 | 2003-12-11 | Detonative cleaning apparatus nozzle |
| US10/733717 | 2003-12-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1626289A true CN1626289A (en) | 2005-06-15 |
Family
ID=34653172
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2004101006410A Pending CN1626289A (en) | 2003-12-11 | 2004-12-10 | Detonative cleaning apparatus nozzle |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US20050125932A1 (en) |
| CN (1) | CN1626289A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8651066B2 (en) | 2010-09-28 | 2014-02-18 | Bha Altair, Llc | Pulse detonation cleaning system |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7360508B2 (en) * | 2004-06-14 | 2008-04-22 | Diamond Power International, Inc. | Detonation / deflagration sootblower |
| US8377232B2 (en) * | 2009-05-04 | 2013-02-19 | General Electric Company | On-line cleaning of turbine hot gas path deposits via pressure pulsations |
| US8246751B2 (en) | 2010-10-01 | 2012-08-21 | General Electric Company | Pulsed detonation cleaning systems and methods |
| WO2014124199A1 (en) | 2013-02-08 | 2014-08-14 | Diamond Power Internaitoanal, Inc. | Condensate removal sootblower nozzle |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2066014A (en) * | 1936-12-29 | Soot blower | ||
| US2772729A (en) * | 1951-05-03 | 1956-12-04 | Hydrocarbon Research Inc | Apparatus for combustion of hydrocarbons |
| US2904260A (en) * | 1955-06-09 | 1959-09-15 | Diamond Power Speciality | Air cooled blower-type cleaner |
| US3045997A (en) * | 1959-03-02 | 1962-07-24 | Armco Steel Corp | Porous oxygen lance |
| US3084373A (en) * | 1960-03-29 | 1963-04-09 | United Nuclear Corp | Transpiration cooled soot blower |
| US3074648A (en) * | 1961-04-12 | 1963-01-22 | Union Carbide Corp | Fluid discharge gun |
| US3216046A (en) * | 1963-06-05 | 1965-11-09 | Diamond Power Speciality | Long travel soot blower with telescopic feed tube |
| US3903912A (en) * | 1970-09-17 | 1975-09-09 | Hydro Vel Services Inc | Tube cleaning system |
| US4193158A (en) * | 1979-01-05 | 1980-03-18 | Combustion Engineering, Inc. | Soot blower for pressurized furnace |
| US4359800A (en) * | 1981-03-05 | 1982-11-23 | The Babcock & Wilcox Company | Sootblower feed and lance tube structure with improved turbulizer system |
| JPS58500725A (en) * | 1981-04-30 | 1983-05-06 | インフラソニク ア−ベ− | Structure of low sound wave generator |
| US4545329A (en) * | 1983-09-23 | 1985-10-08 | Pvi Industries, Inc. | Water heater |
| CH667521A5 (en) * | 1985-09-03 | 1988-10-14 | Sulzer Ag | SUSSBLAESER. |
| US5494004A (en) * | 1994-09-23 | 1996-02-27 | Lockheed Corporation | On line pulsed detonation/deflagration soot blower |
| US5950572A (en) * | 1995-09-13 | 1999-09-14 | Metallgesellschaft Aktiengesellschaft | Opening that allows a soot blower lance to be introduced through a tube cage |
| US5765510A (en) * | 1996-04-26 | 1998-06-16 | Dltk, Inc. | Retractable, sealed sootblower for high pressure, high temperature applications |
| US6321690B1 (en) * | 1997-01-17 | 2001-11-27 | North American Industrial Services, Inc. | Device, system and method for on-line explosive deslagging |
| US6438191B1 (en) * | 1998-03-31 | 2002-08-20 | Sandia Corporation | Explosive scabbling of structural materials |
| ES2235009T3 (en) * | 2001-04-12 | 2005-07-01 | BANG & CLEAN GMBH | PROCEDURE AND APPLIANCE TO CLEAN INCINERATORS. |
| US6684823B1 (en) * | 2003-04-11 | 2004-02-03 | Electric Power Research Institute, Inc. | Impulse ash deposit removal system and method |
-
2003
- 2003-12-11 US US10/733,717 patent/US20050125932A1/en not_active Abandoned
-
2004
- 2004-12-10 CN CNA2004101006410A patent/CN1626289A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8651066B2 (en) | 2010-09-28 | 2014-02-18 | Bha Altair, Llc | Pulse detonation cleaning system |
Also Published As
| Publication number | Publication date |
|---|---|
| US20050125932A1 (en) | 2005-06-16 |
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Open date: 20050615 |