CN108562179B - Spiral jet flow sleeve heat exchanger and working method thereof - Google Patents
Spiral jet flow sleeve heat exchanger and working method thereof Download PDFInfo
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- CN108562179B CN108562179B CN201810400390.XA CN201810400390A CN108562179B CN 108562179 B CN108562179 B CN 108562179B CN 201810400390 A CN201810400390 A CN 201810400390A CN 108562179 B CN108562179 B CN 108562179B
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/10—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically
- F28D7/106—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically consisting of two coaxial conduits or modules of two coaxial conduits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/34—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending obliquely
- F28F1/36—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending obliquely the means being helically wound fins or wire spirals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/24—Arrangements for promoting turbulent flow of heat-exchange media, e.g. by plates
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- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
Description
技术领域Technical Field
本发明涉及强化换热技术领域,尤其涉及一种螺旋射流套管换热器及其工作方法。The invention relates to the technical field of enhanced heat exchange, and in particular to a spiral jet shell and tube heat exchanger and a working method thereof.
背景技术Background technique
目前化工行业中,套管换热器因结构简单、可承载高压而被广泛应用。套管换热器包含内管和外管,高温介质与低温介质通过内管壁传热,达到换热的目的。但是常规的套管换热器的内管与外管均采用光滑直管,两者之间缺少扰流元件,流体稳定缓慢流动,难以破坏流动边界层,导致传热效率不高。At present, in the chemical industry, shell and tube heat exchangers are widely used due to their simple structure and ability to bear high pressure. Shell and tube heat exchangers consist of an inner tube and an outer tube. The high-temperature medium and the low-temperature medium transfer heat through the inner tube wall to achieve the purpose of heat exchange. However, the inner and outer tubes of conventional shell and tube heat exchangers are both smooth straight tubes, and there is a lack of turbulent elements between the two. The fluid flows steadily and slowly, and it is difficult to destroy the flow boundary layer, resulting in low heat transfer efficiency.
发明内容Summary of the invention
本发明提供了一种螺旋射流套管换热器及其工作方法,所述螺旋射流套管换热器的内管采用螺旋翅片管,通过螺旋翅片、扰流柱构成扰流元件,形成内管与外管之间的螺旋流道和不规则流动;螺旋翅片上还设有射流孔形成射流,破坏流动边界层,提高传热效果。The present invention provides a spiral jet shell and tube heat exchanger and a working method thereof. The inner tube of the spiral jet shell and tube heat exchanger adopts a spiral fin tube. The spiral fins and the spoiler column constitute a spoiler element to form a spiral flow channel and irregular flow between the inner tube and the outer tube. The spiral fins are also provided with jet holes to form a jet, destroy the flow boundary layer, and improve the heat transfer effect.
为了达到上述目的,本发明采用以下技术方案实现:In order to achieve the above object, the present invention adopts the following technical solutions:
一种螺旋射流套管换热器,包括由外管和内管同心套设在一起的换热器本体,外管与内管之间为壳程通道,内管中为管程通道;所述内管的两端延伸至外管对应端面之外,内管的上端为管程进口,内管的下端为管程出口;外管的上端设外管上端板,外管的下端设外管下端板,外管上端板和外管下端板将壳程通道的两端进行封闭;靠近外管上端板的外管一侧设壳程出口,靠近外管下端板的外管另一侧设壳程进口;所述内管为螺旋翅片管,其外围沿纵向设有螺旋翅片,螺旋翅片的外侧边缘紧贴外管的内壁,在壳程通道中形成螺旋流道;螺旋流道中的内管外壁上设有多个扰流柱,螺旋翅片上设有多个射流孔。A spiral jet shell and tube heat exchanger comprises a heat exchanger body which is concentrically sleeved with an outer tube and an inner tube, a shell-side channel is formed between the outer tube and the inner tube, and a tube-side channel is formed in the inner tube; both ends of the inner tube extend beyond the corresponding end face of the outer tube, the upper end of the inner tube is the tube-side inlet, and the lower end of the inner tube is the tube-side outlet; an outer tube upper end plate is provided at the upper end of the outer tube, and an outer tube lower end plate is provided at the lower end of the outer tube, and both ends of the shell-side channel are closed by the outer tube upper end plate and the outer tube lower end plate; a shell-side outlet is provided on one side of the outer tube close to the outer tube upper end plate, and a shell-side inlet is provided on the other side of the outer tube close to the outer tube lower end plate; the inner tube is a spiral fin tube, and a spiral fin is provided on its outer periphery in the longitudinal direction, and the outer edge of the spiral fin is in close contact with the inner wall of the outer tube to form a spiral flow channel in the shell-side channel; a plurality of spoiler columns are provided on the outer wall of the inner tube in the spiral flow channel, and a plurality of jet holes are provided on the spiral fin.
所述螺旋翅片为等螺距螺旋翅片,扰流柱沿相同的螺旋轨迹均匀设置在相邻螺旋翅片中间,且多个扰流柱沿螺旋方向均匀设置。The spiral fins are equal-pitch spiral fins, the spoiler columns are evenly arranged in the middle of adjacent spiral fins along the same spiral trajectory, and a plurality of spoiler columns are evenly arranged along the spiral direction.
所述射流孔在靠近内管一侧的螺旋翅片上开设,且多个射流孔沿螺旋翅片的螺旋方向均匀开设。The jet holes are opened on the spiral fins close to one side of the inner tube, and a plurality of jet holes are evenly opened along the spiral direction of the spiral fins.
所述射流孔为方形通孔、圆形通孔、椭圆形通孔或菱形通孔。The jet hole is a square through hole, a circular through hole, an elliptical through hole or a diamond through hole.
所述扰流柱的伸出端端面紧贴在外管的内壁上,对内管形成支撑。The extended end surface of the spoiler column is closely attached to the inner wall of the outer tube, so as to support the inner tube.
所述扰流柱与射流孔沿螺旋翅片的螺旋方向间隔设置。The spoiler column and the jet hole are arranged at intervals along the spiral direction of the spiral fin.
所述一种螺旋射流套管换热器的工作方法,包括:The working method of the spiral jet shell and tube heat exchanger comprises:
1)管程介质从内管上端的管程进口进入套管换热器,通过内管的管壁与壳程介质换热后,从内管下端的管程出口离开套管换热器;1) The tube-side medium enters the shell-and-tube heat exchanger from the tube-side inlet at the upper end of the inner tube, exchanges heat with the shell-side medium through the tube wall of the inner tube, and leaves the shell-and-tube heat exchanger from the tube-side outlet at the lower end of the inner tube;
2)壳程介质从壳程进口进入套管换热器,通过螺旋翅片增加了与内管的接触面积,壳程介质从螺旋翅片构成的螺旋流道湍流运动,经扰流柱的阻挡扰流作用,促进了壳程介质的湍动程度,壳程介质在扰流柱的阻挡下分开后重新汇合;与螺旋流道上方的射流孔中射流下来的壳程介质混合后,一部分再经螺旋流道的射流孔进行轴向射流运动;另一部分继续在螺旋流道中运动,在下一个扰流柱和射流孔处,重复上述流动过程;2) The shell-side medium enters the shell-and-tube heat exchanger from the shell-side inlet, and the contact area with the inner tube is increased by the spiral fins. The shell-side medium moves turbulently in the spiral flow channel formed by the spiral fins. The turbulence of the shell-side medium is promoted by the blocking and turbulent effect of the spoiler column. The shell-side medium is separated and reunited under the blocking of the spoiler column; after mixing with the shell-side medium ejected from the jet hole above the spiral flow channel, a part of it is axially ejected through the jet hole of the spiral flow channel; the other part continues to move in the spiral flow channel, and repeats the above flow process at the next spoiler column and jet hole;
3)螺旋、扰流与射流的混合运动构成多次不规则折流,进一步破坏流动边界层,减小传热阻力,强化传热效果;完成传热后的壳程介质从壳程出口离开套管换热器。3) The mixed motion of spiral, turbulence and jet forms multiple irregular deflections, which further destroys the flow boundary layer, reduces the heat transfer resistance and enhances the heat transfer effect; after completing the heat transfer, the shell side medium leaves the shell side heat exchanger from the shell side outlet.
与现有技术相比,本发明的有益效果是:Compared with the prior art, the present invention has the following beneficial effects:
1)采用螺旋翅片管作为内管,增加了套管换热器的传热面积,能够提高单位质量的传热面积,有效降低套管换热器成本;1) Using spiral finned tubes as inner tubes increases the heat transfer area of the shell-and-tube heat exchanger, which can increase the heat transfer area per unit mass and effectively reduce the cost of the shell-and-tube heat exchanger;
2)螺旋翅片在内管和外管之间构成矩形螺旋流道,扰流柱能够阻挡流体规则流动,促进流体强烈扰动,从而减小传热阻力,强化传热;2) The spiral fins form a rectangular spiral flow channel between the inner tube and the outer tube. The spoiler column can block the regular flow of the fluid and promote strong disturbance of the fluid, thereby reducing the heat transfer resistance and enhancing the heat transfer;
3)螺旋翅片上设射流孔,可改善流体流路,增加轴向射流,促进流体在螺旋通道中的螺旋与轴向不规则运动,破坏传热边界层,进一步强化传热效果;3) The spiral fins are provided with jet holes, which can improve the fluid flow path, increase the axial jet, promote the spiral and axial irregular movement of the fluid in the spiral channel, destroy the heat transfer boundary layer, and further enhance the heat transfer effect;
4)射流孔与扰流柱间隔布置,有利于流路顺畅运行,达到扰流和射流的作用。4) The jet holes and the spoiler columns are arranged at intervals, which is conducive to the smooth operation of the flow path and achieves the effects of spoiler and jet.
附图说明BRIEF DESCRIPTION OF THE DRAWINGS
图1是本发明所述一种螺旋射流套管换热器的透视图。FIG. 1 is a perspective view of a spiral jet shell and tube heat exchanger according to the present invention.
图2图1中的A-A视图。Fig. 2 View A-A in Fig. 1.
图3是本发明所述内管的结构示意图。FIG. 3 is a schematic diagram of the structure of the inner tube of the present invention.
图中:1.壳程进口 2.外管下端板 3.内管 4.螺旋翅片 5.扰流柱 6.外管 7.壳程出口 8.外管上端板 9.射流孔 10.管程进口 11.管程出口In the figure: 1. Shell inlet 2. Outer tube lower end plate 3. Inner tube 4. Spiral fin 5. Turbine 6. Outer tube 7. Shell outlet 8. Outer tube upper end plate 9. Jet hole 10. Tube inlet 11. Tube outlet
具体实施方式Detailed ways
下面结合附图对本发明的具体实施方式作进一步说明:The specific embodiments of the present invention will be further described below in conjunction with the accompanying drawings:
如图1-图3所示,本发明所述一种螺旋射流套管换热器,包括由外管6和内管3同心套设在一起的换热器本体,外管6与内管3之间为壳程通道,内管3中为管程通道;所述内管3的两端延伸至外管6对应端面之外,内管3的上端为管程进口10,内管3的下端为管程出口11;外管6的上端设外管上端板8,外管6的下端设外管下端板2,外管上端板8和外管下端板2将壳程通道的两端进行封闭;靠近外管上端板8的外管6一侧设壳程出口7,靠近外管下端板2的外管6另一侧设壳程进口1;所述内管3为螺旋翅片管,其外围沿纵向设有螺旋翅片4,螺旋翅片4的外侧边缘紧贴外管6的内壁,在壳程通道中形成螺旋流道;螺旋流道中的内管3外壁上设有多个扰流柱5,螺旋翅片4上设有多个射流孔9。As shown in Fig. 1 to Fig. 3, a spiral jet shell-and-tube heat exchanger of the present invention comprises a heat exchanger body in which an outer tube 6 and an inner tube 3 are concentrically sleeved together, a shell-side channel is formed between the outer tube 6 and the inner tube 3, and a tube-side channel is formed in the inner tube 3; both ends of the inner tube 3 extend beyond the corresponding end surface of the outer tube 6, the upper end of the inner tube 3 is a tube-side inlet 10, and the lower end of the inner tube 3 is a tube-side outlet 11; an outer tube upper end plate 8 is provided at the upper end of the outer tube 6, an outer tube lower end plate 2 is provided at the lower end of the outer tube 6, and an outer tube upper end plate 8 is provided at the upper end of the outer tube 6. 8 and the lower end plate 2 of the outer tube close the two ends of the shell-side channel; a shell-side outlet 7 is provided on one side of the outer tube 6 close to the upper end plate 8 of the outer tube, and a shell-side inlet 1 is provided on the other side of the outer tube 6 close to the lower end plate 2 of the outer tube; the inner tube 3 is a spiral finned tube, and a spiral fin 4 is provided on its outer periphery along the longitudinal direction, and the outer edge of the spiral fin 4 is close to the inner wall of the outer tube 6 to form a spiral flow channel in the shell-side channel; a plurality of spoiler columns 5 are provided on the outer wall of the inner tube 3 in the spiral flow channel, and a plurality of jet holes 9 are provided on the spiral fin 4.
所述螺旋翅片4为等螺距螺旋翅片,扰流柱5沿相同的螺旋轨迹均匀设置在相邻螺旋翅片4中间,且多个扰流柱5沿螺旋方向均匀设置。The spiral fins 4 are spiral fins with equal pitches, and the spoiler columns 5 are evenly arranged in the middle of adjacent spiral fins 4 along the same spiral trajectory, and a plurality of spoiler columns 5 are evenly arranged along the spiral direction.
所述射流孔9在靠近内管3一侧的螺旋翅片4上开设,且多个射流孔9沿螺旋翅片4的螺旋方向均匀开设。The jet holes 9 are opened on the spiral fin 4 at one side close to the inner tube 3 , and a plurality of jet holes 9 are evenly opened along the spiral direction of the spiral fin 4 .
所述射流孔9为方形通孔、圆形通孔、椭圆形通孔或菱形通孔。The jet hole 9 is a square through hole, a circular through hole, an elliptical through hole or a diamond through hole.
所述扰流柱5的伸出端端面紧贴在外管6的内壁上,对内管3形成支撑。The extended end surface of the spoiler column 5 is in close contact with the inner wall of the outer tube 6 to support the inner tube 3 .
所述扰流柱5与射流孔9沿螺旋翅片4的螺旋方向间隔设置。The spoiler column 5 and the jet hole 9 are arranged at intervals along the spiral direction of the spiral fin 4 .
所述一种螺旋射流套管换热器的工作方法,包括:The working method of the spiral jet shell and tube heat exchanger comprises:
1)管程介质从内管3上端的管程进口10进入套管换热器,通过内管3的管壁与壳程介质换热后,从内管3下端的管程出口11离开套管换热器;1) The tube-side medium enters the shell-and-tube heat exchanger from the tube-side inlet 10 at the upper end of the inner tube 3, exchanges heat with the shell-side medium through the tube wall of the inner tube 3, and leaves the shell-and-tube heat exchanger from the tube-side outlet 11 at the lower end of the inner tube 3;
2)壳程介质从壳程进口1进入套管换热器,通过螺旋翅片4增加了与内管3的接触面积,壳程介质从螺旋翅片4构成的螺旋流道湍流运动,经扰流柱5的阻挡扰流作用,促进了壳程介质的湍动程度,壳程介质在扰流柱5的阻挡下分开后重新汇合;与螺旋流道上方的射流孔9中射流下来的壳程介质混合后,一部分再经螺旋流道的射流孔9进行轴向射流运动;另一部分继续在螺旋流道中运动,在下一个扰流柱5和射流孔9处,重复上述流动过程;2) The shell-side medium enters the shell-and-tube heat exchanger from the shell-side inlet 1, and the contact area with the inner tube 3 is increased by the spiral fins 4. The shell-side medium moves turbulently from the spiral flow channel formed by the spiral fins 4, and the turbulence of the shell-side medium is promoted by the blocking and turbulent effect of the spoiler column 5. The shell-side medium is separated and reunited under the blocking of the spoiler column 5; after mixing with the shell-side medium ejected from the jet hole 9 above the spiral flow channel, a part of it is axially ejected through the jet hole 9 of the spiral flow channel; the other part continues to move in the spiral flow channel, and repeats the above flow process at the next spoiler column 5 and jet hole 9;
3)螺旋、扰流与射流的混合运动构成多次不规则折流,进一步破坏流动边界层,减小传热阻力,强化传热效果;完成传热后的壳程介质从壳程出口7离开套管换热器。3) The mixed motion of spiral, turbulent flow and jet forms multiple irregular deflections, which further destroys the flow boundary layer, reduces the heat transfer resistance and enhances the heat transfer effect; after completing the heat transfer, the shell side medium leaves the shell side heat exchanger from the shell side outlet 7.
以上所述,仅为本发明较佳的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,根据本发明的技术方案及其发明构思加以等同替换或改变,都应涵盖在本发明的保护范围之内。The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical scheme and inventive concept of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.
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