EP0926355A2 - Strömungsgleichrichter und Verfahren zu dessen Herstellung - Google Patents
Strömungsgleichrichter und Verfahren zu dessen Herstellung Download PDFInfo
- Publication number
- EP0926355A2 EP0926355A2 EP98123789A EP98123789A EP0926355A2 EP 0926355 A2 EP0926355 A2 EP 0926355A2 EP 98123789 A EP98123789 A EP 98123789A EP 98123789 A EP98123789 A EP 98123789A EP 0926355 A2 EP0926355 A2 EP 0926355A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- flow
- tube
- carrier element
- flow rectifier
- support
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/02—Influencing flow of fluids in pipes or conduits
- F15D1/06—Influencing flow of fluids in pipes or conduits by influencing the boundary layer
- F15D1/065—Whereby an element is dispersed in a pipe over the whole length or whereby several elements are regularly distributed in a pipe
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F25/00—Flow mixers; Mixers for falling materials, e.g. solid particles
- B01F25/40—Static mixers
- B01F25/42—Static mixers in which the mixing is affected by moving the components jointly in changing directions, e.g. in tubes provided with baffles or obstructions
- B01F25/43—Mixing tubes, e.g. wherein the material is moved in a radial or partly reversed direction
- B01F25/431—Straight mixing tubes with baffles or obstructions that do not cause substantial pressure drop; Baffles therefor
- B01F25/4316—Straight mixing tubes with baffles or obstructions that do not cause substantial pressure drop; Baffles therefor the baffles being flat pieces of material, e.g. intermeshing, fixed to the wall or fixed on a central rod
- B01F25/43161—Straight mixing tubes with baffles or obstructions that do not cause substantial pressure drop; Baffles therefor the baffles being flat pieces of material, e.g. intermeshing, fixed to the wall or fixed on a central rod composed of consecutive sections of flat pieces of material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F25/00—Flow mixers; Mixers for falling materials, e.g. solid particles
- B01F25/40—Static mixers
- B01F25/42—Static mixers in which the mixing is affected by moving the components jointly in changing directions, e.g. in tubes provided with baffles or obstructions
- B01F25/43—Mixing tubes, e.g. wherein the material is moved in a radial or partly reversed direction
- B01F25/431—Straight mixing tubes with baffles or obstructions that do not cause substantial pressure drop; Baffles therefor
- B01F25/43197—Straight mixing tubes with baffles or obstructions that do not cause substantial pressure drop; Baffles therefor characterised by the mounting of the baffles or obstructions
- B01F25/431971—Mounted on the wall
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F25/00—Flow mixers; Mixers for falling materials, e.g. solid particles
- B01F25/40—Static mixers
- B01F25/42—Static mixers in which the mixing is affected by moving the components jointly in changing directions, e.g. in tubes provided with baffles or obstructions
- B01F25/43—Mixing tubes, e.g. wherein the material is moved in a radial or partly reversed direction
- B01F25/431—Straight mixing tubes with baffles or obstructions that do not cause substantial pressure drop; Baffles therefor
- B01F25/43197—Straight mixing tubes with baffles or obstructions that do not cause substantial pressure drop; Baffles therefor characterised by the mounting of the baffles or obstructions
- B01F25/431972—Mounted on an axial support member, e.g. a rod or bar
Definitions
- the invention relates to a flow rectifier module Use for one of a liquid or gaseous medium flowable tube, with at least one support element and at least a baffle supported by the support member.
- the invention also relates to a flow straightener with a pipe made of a liquid or gaseous Medium can be flowed through and a method for its production.
- the publication WO 90/00929 discloses a device for Mixing a liquid that flows through a pipe. Next the mixing also rectifies the liquid flow achieved.
- the device comprises a tubular one Carrier element, at one longitudinal end baffles are spaced from each other. These baffles extend obliquely to the central axis of the support element inside, i.e. towards the central axis.
- baffles extend obliquely to the central axis of the support element inside, i.e. towards the central axis.
- One or more of these Devices are inserted into the tube so that the Baffles are downstream and attached by an adhesive attached to the inner tube wall.
- the sloping baffles cause a swirling of the liquid and thus for mixing and equalizing the flow.
- the disadvantage of this device is that that the flow rectifier effect is unsatisfactory, especially because an existing one in the flow Swirl is not eliminated. This leads to one of the devices subordinate measuring point to measurement results with regard are not meaningful for the overall flow.
- the device is complex and therefore expensive their manufacture and moreover inflexible in their application.
- the support element is made from a piece of pipe, wherein the baffles are cut out of the tube wall and be bent. This is a complex manufacturing process and in particular also requires expensive starting material.
- the diameter of the support member must be exactly on the Be adapted to the diameter of the tube. However, this means that a production on stock due to the large number of different variants is not profitable.
- the object of the invention is therefore a flow straightener module and to provide a flow straightener, each with a very good flow rectification is achievable and that or which is inexpensive to manufacture.
- a Flow rectifier module of the type mentioned at the outset which is characterized in that at least one elongated support element is plate-shaped and that the baffle held obliquely to the longitudinal direction of the carrier element is.
- this flow rectifier module is in particular in that it is very inexpensive to manufacture and flexible, i.e. in pipes with different cross-sectional shapes and diameters can be used. It also improves the flow rectification in that the carrier element due to its elongated plate shape a twist in the medium flowing through the pipe is eliminated. So that fulfills Carrier element not only the support function for the baffles, but also a flow rectification function. Swirl is in connection with the invention to understand a flow component that is a Axis rotates, which is parallel to the longitudinal axis of the tube.
- the carrier element Since the carrier element has a plate shape, it can be manufacture from an inexpensive plate material, so that on expensive tubular elements can be dispensed with.
- the carrier element at least has an open edge slot into which the baffle intervenes.
- the one intended to receive the baffle Slit is simple and inexpensive in the carrier element applicable. So it is no longer necessary to use the baffle cut out of a tubular support member.
- the flow straightener module are a carrier element several spaced apart Baffles associated with trained in appropriately Engage slots.
- the flow rectification can improve, but without the structural effort in the same Increase ratio.
- the staggered arrangement advantageous because the individual flow paths can be distributed gently by offset vertebrae.
- This training is particularly advantageous if one particularly large swirl component from the medium flowing through should be removed.
- the Peak is upstream and its downstream Edge is chamfered.
- the beveled edge causes a vortex break, which is the flow rectification very strongly supported.
- a negative pressure is created in the cavity of the flow distributor and, depending on the embodiment, a pulsation that corresponds to the Helps improve flow straightening.
- the Baffle plate essentially has a trapezoidal shape, the tube-facing side is arcuate, so that essentially its two outer end regions as a contact surface to serve.
- This configuration of the baffle has the advantage that a very stable support that can withstand high tipping moments is.
- the baffle essentially abuts the tube with its two outer end regions the radius of the arcuate side is chosen larger than the inside radius of the pipe.
- the Baffle on an open edge slot on the tube facing side is attached.
- the in the baffle plate and slots provided in the carrier element formed such that only at the longitudinal slots ends Support surfaces with the support element or with the Deflection plate result.
- baffle is defined Points supported on the support element, so that a very large support moment can be guaranteed.
- Assembly greatly simplified and therefore inexpensive.
- the longitudinal axis of the support element parallel runs to the longitudinal axis of the support tube and wherein the support tube into which a liquid or gaseous medium can flow Tube is designed to be insertable.
- Flow rectifier of the type mentioned solved the is characterized in that in at least one longitudinal section a flow straightener module as before explained, is firmly arranged.
- This flow straightener has - like the one mentioned before Flow rectifier module - particularly good flow rectification properties and is also inexpensive with few simple components can be manufactured.
- the tube points to its a connection device on both ends, one Connection to another pipe or a pipe system enables.
- connection device for example as a flange is formed, the advantage is achieved that the flow straightener is easy to connect to existing pipes.
- this Pipe in its wall an opening for the insertion of a measuring probe on, the opening in a the flow rectifier module downstream longitudinal section of the tube provided is.
- the object underlying the invention is furthermore by a method of manufacturing a flow straightener solved, which is characterized in that in the tube Through holes are introduced that with the baffles provided support elements are introduced into the tube, wherein the carrier elements are aligned with the through holes are, and that the support elements through the through holes be welded through to the pipe.
- This manufacturing process can be carried out extremely inexpensively and requires only a few manufacturing steps in particular complex material forming can be saved can. It is only necessary that at least one carrier element and a flow straightener module comprising a baffle to be inserted into the pipe and via hole welds to fix to this, for what through holes in the tube are provided. This will make it extremely stable and easy achievable connection enables.
- the baffles inserted into the slots of the carrier element and the Carrier elements to each other via at least one mounting star aligned and fixed, with the support elements in introduced this aligned position as a unit in the tube become. After the welding process, the assembly star is then turned off removed the pipe.
- the flow distributor as a non-removable mounting star for alignment and Fixation of the support elements used.
- the carrier element and / or the baffle plate is punched out.
- the flow straightener module 10 includes a tubular sleeve 12 the inner wall 14 attached a plurality of elongate support elements 16 are.
- the cross-sectional representation shows that in present embodiment, a total of eight support elements 16 are provided which in the circumferential direction of the sleeve 12 in even distances from each other.
- sleeve 12 instead of one in present embodiment used circular shape of For example, sleeve 12 also has a rectangular cross section or insert a square sleeve.
- Each of the carrier elements 16 which are configured identically to one another has a plate shape and is divided into two longitudinal sections 18a and 18b.
- the longitudinal section 18b has the shape a strip, during which also referred to as the guide wing 19
- Longitudinal section 18a has a trapezoidal shape with respect to the central axis M of the sleeve 12 obliquely extending longitudinal end edge 20.
- the length of the support member 16 at its the Inner wall 14 facing side is thus larger than that Length of the opposite side of the support element 16.
- the radial Length (width) of the guide vane 19 greater than the width of the Longitudinal section 18b.
- the cross-sectional view further shows that the Carrier elements 16 run in an imaginary plane in which also the central axis M of the sleeve 12 lies. Furthermore lie the guide vanes 19 on one designated by an arrow S. Flow facing side 22, i.e. upstream of the sleeve 12.
- each support element 16 On the support elements 16 are flat in the longitudinal section 18b plate-shaped deflector wing 24 attached. In the present embodiment are a total of three on each support element 16 Deflector blades 24 spaced apart in the longitudinal direction are provided, this number, of course, depending on the application is variable.
- the wings extend obliquely to Center axis M, the outer wall facing the inner wall 14 Page 26 faces the guide vane 19, i.e. that this side 26 with respect to the opposite inner side 28 of the Deflector 24 is upstream.
- the inner side 28 of each Deflection wing 24 protrudes from a radially inner one Edge 30 of the support member 16, the distance of the inner side 28 to the central axis M is greater than the distance the inner edge of the guide wing 19 to the central axis M.
- the outer one Page 26 is arcuate, as in the one in FIG. 2 shown top view is clearly visible.
- the outer side 26 and the inner Page 28 are each bevelled.
- the beveled Edges are indicated by dashed lines in the top view.
- the bevel of the outer side is chosen so that this Edge lies as well as possible on the inner wall 14.
- the bevel the inner side 28 serves as a tear-off edge, the Function will be explained.
- the deflecting wing 24 also has a slot 32, starting from the outer side 26 in the direction of the Axis of symmetry SA of the deflection wing approximately to its center extends.
- the slot 32 is open at the edge towards the outer side 26 educated.
- the distance D of the opposite one another Surfaces 34, i.e. the slot width D is in one middle slot longitudinal section 36 larger than at the two Longitudinal end sections 37. This creates so-called elaborations 38.
- elaborations 38 With the help of these elaborations 38 defined contact areas with one inserted into the slot Plate, in the present embodiment, a section of the support member 16, ensure.
- the contact areas lie on the two longitudinal end portions 37 of the Slot 32.
- the carrier elements 16 also have slots 40, as in one Detail view shown in Fig. 2. Have the slots 40 a minimum width B in the area of the longitudinal end sections 42, which corresponds to the thickness S of the deflecting vanes 24. As the Slots 32 of the deflector blades 24 are also slots 40 of the Carrier elements 16 provided with elaborations 44, each introduced in a central longitudinal section of the slots 40 are. This creates defined contact areas that are in the Area of the two longitudinal end portions 42 lie. The slots 40 take up deflector blades 24, as is shown schematically in FIG. 2 is shown.
- the slots 32 of the deflector 24 and the Slots 40 of the carrier elements 16 are matched to one another in such a way that the deflector 24 in the slots 40 of the support elements 16 can be inserted, the outer side 26 in essentially flush with the edge 30 opposite completes the outer edge of the carrier element 16.
- each support element 16 is provided that have no deflection wings. So it is not absolutely necessary, these carrier elements 16 with slots to provide.
- the individual support elements 16 each at an equal distance arranged for example to the side 22 of the sleeve 12. I.e. that the deflector 24 of adjacent support members 16 each lie on a circumference.
- FIG. 3 shows a second exemplary embodiment of a flow straightener module 10 'shown.
- the structure of this flow straightener module 10 ' corresponds essentially to that Structure of the flow straightener module 10 explained above, so that on a repeated description of the same reference numerals marked parts is dispensed with.
- the respective Deflection wing 24 of every second support element 16 lie on a circumference.
- the increase in the number of deflector blades 24 and the offset the carrier elements 16 has the advantage that individual flow paths what is distributed gently by offset vertebrae especially plays a major role when the flow straightener module 10 'control units are connected upstream.
- FIG. 4 shows a third exemplary embodiment of a flow straightener module 10 '', which is essentially the Flow rectifier module 10 'shown in FIG. 3 corresponds. On another explanation of the same Parts marked with reference numerals are therefore omitted.
- the flow straightener module 10 '' at the upstream end 22 of the sleeve 12 a flow distributor 50 on the vanes 19 of the Carrier elements 16 is attached. Because adjacent support elements 16 each offset in the longitudinal direction the flow distributor 50 is on every second support element 16 attached.
- the flow distributor 50 is a paraboloid of revolution, which is hollow and its closed Peak is upstream.
- the edge 52 of the flow distributor 50 bevelled with a bevel angle of 30 ° to the longitudinal axis is preferred. This bevel serves as a tear-off edge and ensures an improvement the flow rectification.
- the surface 54 of the flow distributor facing the flow S. 50 can be smooth; however, it is also possible to provide an artificial surface roughness. It is particularly advantageous to have a swirl-generating surface profile to provide. Furthermore, it is for flow optimization also possible pressure equalization holes in the flow distributor 50 to introduce, which is not shown in FIG. 4 is. To minimize the pressure loss reach, the flow distributor 50 is preferably one Get teardrop shape.
- the flow rectifier modules 10, 10 'and 10 '' can be inserted into corresponding pipes, for example Flow measurements are to be carried out, insert, the sleeve 12 then tightly with its outer wall abuts the inner wall of the tube.
- a flow straightener 60 to create, in which a pipe section 61, as in Fig. 5th shown, directly with the support elements 16 and the deflector wings 24 is provided.
- the sleeve 12 waived. Rather, the carrier elements 16 directly on the Inner wall 63 of the pipe section 61 attached.
- the structure of the Carrier elements 16 themselves and their arrangement within the Pipe section 61 corresponds to that of the flow straightener module 10 according to FIG. 1.
- the pipe section 61 is at its longitudinal ends 65 with one each Provided flange 67, the two flanges 67 each Allow connection to a commercially available pipe.
- the pipe section 61 is divided into a first longitudinal section 69a and a second longitudinal section 69b, the first Longitudinal section 69a, the support elements with the deflecting vanes 24 are provided.
- the second longitudinal section 69b serves as a calming section, within which the flow profile continues can equalize.
- a tubular connector 71 on the tubular jacket attached, with a bore 78 a connection between the fitting 71 and the inside of the tube 61 enables.
- the connector 71 serves as a measured value connection to for example a measured value sensor in the interior of the pipe section respectively.
- the carrier elements 16 and the deflecting vanes 24 made of a plate-shaped material, preferably of metal, punched out.
- the simple geometric shape of support member 16 and deflector 24 das inexpensive punching allowed.
- the oblique slots 40 in the support member 16 and the Slits 32 are made in the deflector blades 24. Since only two Parts similar to the rows of diameters of the tubes or sleeves large batch sizes are required, a smaller one is required Storage space required and in particular can Costs can be saved. For the rest is a prefabrication of the Carrier elements 16 and deflector 24 possible.
- the carrier elements 16 are provided with the deflection wings 24, the two parts being inserted into each other.
- the one in the support element 16 and slots provided in the deflector wing 24 ensure that the deflector wing 24 can be inserted so far, that its outer side 26 with the outer, i.e. the later Tube-facing side, essentially flush.
- the Deflector 24 only on the longitudinal end portions of the Slot 40 on.
- the carrier element 16 lies only at the longitudinal end portions of the slot 32 of the deflector wing 24 on. This enables defined contact areas, which on the one hand improves the connection quality, in particular the absorption of tilting moments increased, and on the other hand for one Relief when inserting the deflector 24 into the Carrier elements 16 provides.
- Assembly starters are, for example, as in FIG. 6 shown to have a ring on its outside in Has longitudinal grooves 76 into which the inner Edge 30 of the carrier elements 16 are inserted.
- the Grooves 76 are for this according to the desired position of the placed respective support member 16.
- This assembly consisting from several support elements 16 with attached deflector wings 24 and two mounting stars 74, is then in the sleeve 12 or the pipe section 61 inserted.
- This assembly consisting from several support elements 16 with attached deflector wings 24 and two mounting stars 74, is then in the sleeve 12 or the pipe section 61 inserted.
- bores 78 introduced beforehand in the Sleeve 12 or the pipe section 61 bores 78 introduced.
- the position of the individual bores 78 corresponds to one another Position of the radially outer intersection points of the support elements 16 with the deflector wings 24.
- the aforementioned assembly is inside the sleeve 12 or the pipe section 61 aligned so that the intersection with the holes 78 are aligned.
- After the alignment can be the support elements with the deflection wings via the assembly stars 24 against the inner wall of the sleeve 12 or the pipe section 61 press, whereby, as can be clearly seen in Fig. 6, the Choosing a larger diameter for the arcuate side 26 of the deflector 24 against the inner radius of the sleeve 12 therefor ensures that the side 26 only at its outer portions abuts the sleeve 12.
- the softened material pulls when the welding spot cools together and pulls the deflector wing against the inner wall 14 of the sleeve 12 or the inner wall 63 of the pipe section 61.
- By resting the deflector 24 on its outer Edge sections create a connection with a very high Overturning moment.
- the assembly starter then becomes the flow straightener pulled out, this being facilitated by the fact that the mounting star can relax.
- FIG. 4 shown flow rectifier module 10 ''.
- the flow distributor 50 takes over the exemplary embodiment Function of one of the two mounting stars 74. Since the flow distributor 50 an integral part of the flow straightener module can therefore remove a mounting star be waived at the end of the procedure.
- the bores 78 can also follow the introduction of the assembly of support elements and deflection wings be introduced.
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- Chemical & Material Sciences (AREA)
- Dispersion Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Measuring Volume Flow (AREA)
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Abstract
Description
- Fig. 1
- einen Längsschnitt und einen Querschnitt eines Strömungsgleichrichter-Moduls gemäß einem ersten Ausführungsbeispiel;
- Fig. 2
- eine schematische Darstellung eines Ablenkflügels in Draufsicht und in Seitenansicht, sowie eine Darstellung zur Erläuterung seiner Befestigung an einem Trägerelement;
- Fig. 3
- einen Längsschnitt und einen Querschnitt eines Strömungsgleichrichter-Moduls gemäß einem zweiten Ausführungsbeispiel der Erfindung;
- Fig. 4
- einen Längsschnitt und einen Querschnitt eines Strömungsgleichrichter-Moduls gemäß einem dritten Ausführungsbeispiel, sowie eine Detaildarstellung eines Bereichs des Strömungsverteilers;
- Fig. 5
- einen Längsschnitt eines Strömungsgleichrichters;
- Fig. 6
- mehrere schematische Darstellungen zur Erläuterung der Herstellung des Strömungsgleichrichter-Moduls, und
- Fig. 7
- eine schematische Darstellung des in Fig. 1 gezeigten Strömungsgleichrichter-Moduls zur Erläuterung seiner Funktionsweise.
Claims (20)
- Strömungsgleichrichter-Modul als Einsatz für ein von einem flüssigen oder gasförmigen Medium durchströmbares Rohr, mit zumindest einem Trägerelement (16) und zumindest einer durch das Trägerelement gestützten Ablenkplatte (24), dadurch gekennzeichnet, daß das zumindest eine längliche Trägerelement (16) plattenförmig ausgebildet ist und daß die Ablenkplatte (24) schräg zur Längsrichtung des Trägerelements (16) angeordnet ist.
- Strömungsgleichrichter-Modul nach Anspruch 1, dadurch gekennzeichnet, daß das Trägerelement (16) zumindest einen randoffenen Schlitz (40) aufweist, in den die Ablenkplatte (24) eingreift.
- Strömungsgleichrichter-Modul nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß einem Trägerelement (16) mehrere zueinander beabstandete Ablenkplatten (24) zugeordnet sind, die in entsprechend ausgebildete Schlitze (40) eingreifen.
- Strömungsgleichrichter-Modul nach Anspruch 1, 2 oder 3, dadurch gekennzeichnet, daß mehrere Trägerelemente (16) vorgesehen sind, die in Umfangsrichtung des Rohrs beabstandet zueinander angeordnet sind.
- Strömungsgleichrichter-Modul nach Anspruch 4, dadurch gekennzeichnet, daß jedem Trägerelement (16) mehrere Ablenkplatten (24) zugeordnet sind, wobei die Ablenkplatten (24) benachbarter Trägerelemente (16) in Längsrichtung versetzt zueinander angeordnet sind.
- Strömungsgleichrichter-Modul nach Anspruch 4, dadurch gekennzeichnet, daß in Umfangsrichtung gesehen jedem zweiten Trägerelement (16) Ablenkplatten (24) zugeordnet sind.
- Strömungsgleichrichter-Modul nach einem der vorhergehenden Ansprüche 3-5, dadurch gekennzeichnet, daß an den Trägerelementen (16) stromaufwärts ein Strömungsverteiler (50) angebracht ist.
- Strömungsgleichrichter-Modul nach Anspruch 7, dadurch gekennzeichnet, daß der Strömungsverteiler (50) als hohler Rotationsparaboloid ausgebildet ist, dessen Spitze stromaufwärts liegt und dessen stromabwärts liegender Rand (52) abgeschrägt ist.
- Strömungsgleichrichter-Modul nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß die Ablenkplatte (24) im wesentlichen eine Trapezform aufweist, wobei deren dem Rohr zugewandte Seite (26) bogenförmig ausgebildet ist, so daß im wesentlichen deren zwei äußeren Endbereiche als Kontaktflächen dienen.
- Strömungsgleichrichter-Modul nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß die Ablenkplatte (24) einen randoffenen Schlitz (32) aufweist, der an der dem Rohr zugewandten Seite (26) eingebracht ist.
- Strömungsgleichrichter-Modul nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß die in der Ablenkplatte (24) als auch im Trägerelement (16) vorgesehenen Schlitze (32, 40) derart ausgebildet sind, daß sich lediglich an den Schlitz-Längsenden Abstützflächen mit dem Trägerelement (16) bzw. mit der Ablenkplatte (24) ergeben.
- Strömungsgleichrichter-Modul nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß das zumindest eine Trägerelement (16) an einer Innenwand eines Stützrohrs (12) angebracht ist, wobei die Längsachse des Trägerelements (16) parallel zur Längsachse des Stützrohrs (12) verläuft und wobei das Stützrohr in das von einem flüssigen oder gasförmigen Medium durchströmbare Rohr einsteckbar ausgebildet ist.
- Strömungsgleichrichter (60) mit einem Rohr (61), das von einem flüssigen oder gasförmigen Medium durchströmbar ist, dadurch gekennzeichnet, daß in zumindest einem Längsabschnitt (69a) des Rohrs (61) ein StrömungsgleichrichterModul (10; 10'; 10'') nach einem der Ansprüche 1- 10 fest angeordnet ist.
- Strömungsgleichrichter nach Anspruch 13, dadurch gekennzeichnet, daß das Rohr (61) einen kreisförmigen Querschnitt aufweist.
- Strömungsgleichrichter nach Anspruch 13 oder 14, dadurch gekennzeichnet, daß das Rohr (61) an seinen beiden Enden jeweils eine Anschlußvorrichtung (67) aufweist, die einen Anschluß an ein weiteres Rohr ermöglicht.
- Strömungsgleichrichter nach einem der Ansprüche 13 bis 15, dadurch gekennzeichnet, daß das Rohr (61) in seiner Wandung (63) eine Öffnung (73) zum Einbringen einer Meßsonde aufweist, wobei die Öffnung (73) in einem dem Strömungsgleichrichter-Modul nachgeordneten Längsabschnitt (69b) des Rohrs (61) vorgesehen ist.
- Verfahren zur Herstellung eines Strömungsgleichrichters nach einem der Ansprüche 13 bis 16 oder eines Strömungsgleichrichter-Moduls nach Anspruch 12, dadurch gekennzeichnet, daßin das Rohr (61; 12) Durchgangsbohrungen (78) eingebracht werden; die mit den Ablenkplatten (24) versehenen Trägerelemente (16) in das Rohr (61; 12) eingebracht werden, wobei die Trägerelemente (16) zu den Durchgangsbohrungen (78) ausgerichtet sind, unddie Trägerelemente (16) durch die Durchgangsbohrungen (78) hindurch mit dem Rohr (61; 12) verschweißt werden.
- Verfahren nach Anspruch 17, dadurch gekennzeichnet, daß die Ablenkplatten (24) in die Schlitze (40) der Trägerelemente (16) eingesteckt werden, und daß die Trägerelemente (16) über zumindest einen Montagestern (76) zueinander ausgerichtet und fixiert werden, wobei dann die Trägerelemente (16) in dieser ausgerichteten Lage als Einheit in das Rohr (61; 12) eingebracht werden, und daß nach dem Schweißvorgang der Montagestern (76) aus dem Rohr (61; 12) entfernt wird.
- Verfahren nach Anspruch 18, dadurch gekennzeichnet, daß der Strömungsverteiler (50) als nicht-entfernbarer Montagestern (76) zur Ausrichtung und Fixierung der Trägerelemente (16) verwendet wird.
- Verfahren nach einem der Ansprüche 17 bis 19, dadurch gekennzeichnet, daß das Trägerelement (16) und/oder die Ablenkplatte (24) ausgestanzt werden.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19755905A DE19755905C1 (de) | 1997-12-16 | 1997-12-16 | Strömungsgleichrichter-Modul, Strömungsgleichrichter und Verfahren zu dessen Herstellung |
DE19755905 | 1997-12-16 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0926355A2 true EP0926355A2 (de) | 1999-06-30 |
EP0926355A3 EP0926355A3 (de) | 2003-05-28 |
Family
ID=7852112
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98123789A Withdrawn EP0926355A3 (de) | 1997-12-16 | 1998-12-15 | Strömungsgleichrichter und Verfahren zu dessen Herstellung |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0926355A3 (de) |
DE (1) | DE19755905C1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1318341A3 (de) * | 2001-12-04 | 2003-11-05 | SMC Kabushiki Kaisha | Durchflussregelvorrichtung |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1551539B1 (de) * | 2002-07-15 | 2007-11-14 | Sulzer Chemtech AG | Anordnung von kreuzungselementen und verfahren zu deren herstellung |
KR101170174B1 (ko) * | 2003-02-28 | 2012-07-31 | 오쿠타마 고교 가부시키가이샤 | 혼합장치 및 슬러리화장치 |
GB201100673D0 (en) | 2011-01-15 | 2011-03-02 | Statiflo Internat Ltd | Static mixer assembly |
CN112696550B (zh) * | 2020-12-28 | 2022-04-22 | 中国航空工业集团公司沈阳空气动力研究所 | 一种扩散整流的均流结构 |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1990000929A1 (en) | 1988-07-27 | 1990-02-08 | Vortab Corporation | Static fluid flow mixing apparatus |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2553141A (en) * | 1945-08-17 | 1951-05-15 | Elgin Rowland Parker | Baffle |
US3574914A (en) * | 1968-02-19 | 1971-04-13 | Cenco Instr Corp | Method of fabricating a baffle assembly |
US3827461A (en) * | 1972-11-21 | 1974-08-06 | Worthington Pump Int Inc | Stream filament mixer for pipe flow |
US4072296A (en) * | 1975-07-16 | 1978-02-07 | Doom Lewis G | Motionless mixer |
DE3535680A1 (de) * | 1985-10-05 | 1987-04-16 | Bopp & Reuther Gmbh | Turbinenzaehler zur messung der durchflussmenge von fluessigkeiten |
JPS62132007A (ja) * | 1985-12-02 | 1987-06-15 | Nec Corp | 整流格子 |
DE8711604U1 (de) * | 1987-08-27 | 1987-12-23 | terracon Gesellschaft für Anlagenbau mbH, 3340 Wolfenbüttel | Durchströmungskörper |
US5099879A (en) * | 1991-05-16 | 1992-03-31 | Coen Company, Inc. | Combustion air flow stabilizer |
JPH10109756A (ja) * | 1996-10-08 | 1998-04-28 | Tsukishima Kikai Co Ltd | 固気二相流輸送管 |
-
1997
- 1997-12-16 DE DE19755905A patent/DE19755905C1/de not_active Expired - Fee Related
-
1998
- 1998-12-15 EP EP98123789A patent/EP0926355A3/de not_active Withdrawn
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1990000929A1 (en) | 1988-07-27 | 1990-02-08 | Vortab Corporation | Static fluid flow mixing apparatus |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1318341A3 (de) * | 2001-12-04 | 2003-11-05 | SMC Kabushiki Kaisha | Durchflussregelvorrichtung |
US6889706B2 (en) | 2001-12-04 | 2005-05-10 | Smc Kabushiki Kaisha | Flow rate control apparatus |
EP1672264A1 (de) * | 2001-12-04 | 2006-06-21 | Smc Kabushiki Kaisha | Durchflussregelvorrichtung |
Also Published As
Publication number | Publication date |
---|---|
DE19755905C1 (de) | 1999-05-12 |
EP0926355A3 (de) | 2003-05-28 |
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