WO2001051777A2 - Strömungsschalter - Google Patents
Strömungsschalter Download PDFInfo
- Publication number
- WO2001051777A2 WO2001051777A2 PCT/EP2000/013261 EP0013261W WO0151777A2 WO 2001051777 A2 WO2001051777 A2 WO 2001051777A2 EP 0013261 W EP0013261 W EP 0013261W WO 0151777 A2 WO0151777 A2 WO 0151777A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- flow switch
- switch according
- flow
- inflow surface
- displacer
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/08—Other arrangements or adaptations of exhaust conduits
- F01N13/087—Other arrangements or adaptations of exhaust conduits having valves upstream of silencing apparatus for by-passing at least part of exhaust directly to atmosphere
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N1/00—Silencing apparatus characterised by method of silencing
- F01N1/16—Silencing apparatus characterised by method of silencing by using movable parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15C—FLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
- F15C1/00—Circuit elements having no moving parts
- F15C1/08—Boundary-layer devices, e.g. wall-attachment amplifiers coanda effect
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15C—FLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
- F15C3/00—Circuit elements having moving parts
- F15C3/002—Circuit elements having moving parts using fluid droplets or similar deformable bodies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2410/00—By-passing, at least partially, exhaust from inlet to outlet of apparatus, to atmosphere or to other device
Definitions
- the object of the present invention is to develop a flow switch which is particularly suitable for exhaust systems of motor vehicles and which does not require any closure elements actuated by means of outwardly guided shafts and thus does not require any bearings to be sealed for such shafts which produces only comparatively low flow losses, enables bistable switching states with a switching point that is as precise as possible, causes a low mechanical production outlay and permits acceptable geometric dimensions in comparison to the overall system.
- the flow switch should be able to be designed either as an externally controlled device or as an autonomous switching element that works by itself.
- the flow switch according to the present invention thus comprises an inflow channel, a Coanda tulip, at least two outlet channels and a displacement body.
- the inflow channel can be designed as a simple cylindrical tube to which the Coanda tulip connects directly. However, it is particularly preferably designed as a cylindrical tube with an additional conical widening followed by a preferably cylindrical channel section. In this embodiment of the invention, the Coanda tulip expediently adjoins that cylindrical channel section.
- the casing of the displacer is preferably essentially cylindrical.
- the jacket can also have special shapes, for example in that it is conical or barrel-shaped.
- the displacement body is preferably dimensioned and arranged such that the inflow surface is arranged inside the Coanda tulip or in a cylindrical channel section located upstream thereof.
- the coat is preferably in the extension area of the Coanda tulip; in this case it extends completely or partially within the Coanda tulip.
- the outlet channels are preferably arranged concentrically and provided with catch spaces which are designed with a larger flow cross section than the actual outlet channels.
- the outer outlet duct expediently adjoins the Coanda tulip.
- the displacement body is designed as a full body or at least partially as a hollow body.
- the simplest and therefore most cost-effective structure is a flat inflow surface, which is followed by a cylindrical tube section as a jacket in the direction of flow. Not even a downstream termination is required to perform the simplest switching tasks.
- the inflow surface can be flat, concave or convex.
- the diameter of the inflow surface can optionally be chosen to be larger, smaller or equal to the outer circumference of the jacket.
- the outer circumference of the inflow surface can have a chamfer and / or an edge or a boundary layer fence, can be sharp-edged or rounded.
- the arrangement of interruptions, peaks or any irregularities are possible.
- the jacket can be designed as a cylinder, cone, barrel-like or wavy.
- the downstream end of the displacer can be omitted (see above), or can be designed as an essentially flat disc, as a hemisphere or as another suitable flow profile.
- the system of Coanda tulip, displacement body, inflow channel and outlet channels can deviate from the coaxial, axially symmetrical shape. In this sense, for example, in addition to the particularly flat design of the switching element,
- the flow is aligned axially.
- the undivided exhaust gas flow flows through the inflow channel to the flow switch.
- the inflow surface is, for example, in the plane that is formed from the attachment of the Coanda tulip to the cylindrical channel section.
- the flow divides, forms an annular flow, which detaches itself on the inside directly at the outer edge of the inflow plate, lies against the Coanda tulip in the outer area and is discharged into the outer outlet channel. Downstream of the displacement body there is a vortex zone which extends from the wake to the inner outlet channel and closes the inner outlet channel in terms of flow technology.
- the inflow surface is located upstream of the position of the first switching position, specifically in the cylindrical channel section of the inflow channel.
- the flow forms a detachment vortex immediately behind the outer edge of the inflow plate on the circumference of the lateral surface, but the flow is forced to rest on the lateral surface of the displacer.
- the flow is aligned axially and now separates from the Coanda tulip in the outer area.
- the flow is now guided by the displacer in such a way that it also engages in the wake of the displacer and is discharged through the inner outlet channel.
- a circumferential ring vortex is formed, which closes the outer outlet channel in terms of flow technology.
- a first autonomously acting solution uses the balance between the force of the dynamic pressure acting on the inflow surface and one on the movable inflow plate acting spring, which is preferably arranged in the interior of the displacer.
- the flat inflow surface m of a first switching position is located within the cylindrical channel section.
- the flow bears against the outer surface of the displacement body and is supplied to the internal outlet channel by the shape of the displacement body according to the invention.
- the dynamic pressure increases on the inflow surface.
- the inflow surface shifts in the direction of flow against the restoring force of the spring until the second switching point in the attachment area of the Coanda tulip is reached.
- the flow no longer lies against the cylindrical surface of the displacer, but against the Coanda tulip and passes through the outer outlet channel.
- a further switching area is located within the Coanda tulip. It is marked by the second border described above.
- the inflow surface is initially arranged in such a way that the flow along the Coanda tulip is derived from the outer flow channel. If one now increases the mass flow, the back pressure increases and the inflow surface moves downstream over the second boundary line. The flow changes. She puts on the displacer again.
- Another autonomously acting solution uses the thermal expansion of solid, liquid or gaseous agents, which are arranged, for example, in the interior of the displacement body for moving the inflow surface. This results in a temperature-dependent switching of the flow switch.
- an external pressure or vacuum sensor is connected to the interior of the displacer.
- an optional spring element and external pressure sensor can be used to position the inflow surface as required.
- the displacement of the complete displacement body is also possible.
- Autonomous solutions are of particular interest for use in semi-active silencers if a first flow path is preferred for a low exhaust gas mass flow and a second flow path or both flow paths are preferred for a higher exhaust gas mass flow.
- Figure 1 shows a first preferred embodiment of a
- Switching state 2 and Figure 3 shows a second preferred embodiment of a
- FIGS. 1 and 2 show the flow switch designed as a hybrid switching element, consisting of an inflow channel 1 with a conical extension 2 and a cylindrical channel section 3, to which the Coanda tulip 5 and an outer outlet channel 11 with a collecting space 13 are connected.
- the inner outlet duct 12 with the catch chamber 14 is located downstream behind the displacer body 6.
- Coanda tulip 5 replaces the exhaust gas mass flow 20 and forms an encircling vortex region 17, which stabilizes the flow and leads to the inner collecting space 14 and to the inner outlet channel 12.
- the back pressure increased to 7, the planar flow surface
- the planar flow surface 7 moves axially in the flow direction.
- the flat inflow surface 7 is located in the area of the attachment 4 of the Coanda tulip 5.
- the shape of the flow changes and now forms according to FIG. 1.
- the exhaust gas mass flow 20 no longer lies against the outer surface 8 of the displacer 6.
- a large swirl region 18 is formed behind the wake 9, which extends from the edge 15 to the inner catch chamber 14 and closes the internal outlet channel 12 in terms of flow technology.
- the exhaust gas mass flow 20 contacts the Coanda tulip 5, forms a stable ring flow 19, which is discharged via the outer collecting space 13 and the outer outlet duct 11.
- the inner catch chamber 14 is expanded so that part of the annular flow 19 is also diverted through the inner outlet duct 12.
- a corrugated tube compensator 22 is arranged between the inflow surface 7 and the outer surface 8 instead of the spring element 10.
- the complete displacement body 6 forms a closed hollow body which is filled with a fluid.
- the thermal expansion of the enclosed fluid causes the flat inflow surface 7 to shift.
- the magnitude of the dynamic pressure on the inflow surface 7 and the spring stiffness of the corrugated tube compensator 22 can be generated in this way. There are no limits to the variation options for changing the position of the inflow surface 7.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Theoretical Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Exhaust Silencers (AREA)
- Exhaust Gas After Treatment (AREA)
- Switches Operated By Changes In Physical Conditions (AREA)
Abstract
Description
Claims
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE50009679T DE50009679D1 (de) | 2000-01-07 | 2000-12-23 | Strömungsschalter |
| EP00985258A EP1244867B1 (de) | 2000-01-07 | 2000-12-23 | Strömungsschalter |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10000464A DE10000464B4 (de) | 2000-01-07 | 2000-01-07 | Fluidisches Schaltelement |
| DE10000464.4 | 2000-01-07 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2001051777A2 true WO2001051777A2 (de) | 2001-07-19 |
| WO2001051777A3 WO2001051777A3 (de) | 2001-12-20 |
Family
ID=7626949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/EP2000/013261 Ceased WO2001051777A2 (de) | 2000-01-07 | 2000-12-23 | Strömungsschalter |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP1244867B1 (de) |
| DE (2) | DE10000464B4 (de) |
| WO (1) | WO2001051777A2 (de) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CZ306551B6 (cs) * | 2012-05-25 | 2017-03-08 | Ăšstav termomechaniky AV ÄŚR , v.v.i. | Způsob dvourežimového řízení průtoku tekutin a zařízení pro provádění tohoto způsobu |
Citations (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5435489A (en) | 1994-01-13 | 1995-07-25 | Bell Helicopter Textron Inc. | Engine exhaust gas deflection system |
| US5438429A (en) | 1991-08-28 | 1995-08-01 | Silicon Graphics, Inc. | Digital filtering for lenticular printing |
| US5577294A (en) | 1993-10-01 | 1996-11-26 | James River Paper Company, Inc. | Web cleaner apparatus and method |
| US5658141A (en) | 1994-09-07 | 1997-08-19 | L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | Device for spreading a flame by the Coanda effect |
| DE19709432A1 (de) | 1996-03-13 | 1997-10-30 | Volkswagen Ag | Vorrichtung zur Behandlung von Abgasen aus Brennkraftmaschinen |
| DE19729666A1 (de) | 1996-07-20 | 1998-01-22 | Gillet Heinrich Gmbh | Schalldämpfer mit variabler Dämpfungscharakteristik |
| DE19637078A1 (de) | 1996-09-12 | 1998-03-19 | Pierburg Ag | Elektromagnetisches Steuerventil für Abgasrückführung |
| US5739483A (en) | 1994-05-09 | 1998-04-14 | Nissan Motor Co., Ltd. | Automobile exhaust noise suppressor |
| US5744762A (en) | 1995-02-24 | 1998-04-28 | Calsonic Corporation | Muffler controller for use in controllable exhaust system of internal combustion engine |
| US5801343A (en) | 1993-11-09 | 1998-09-01 | Futaba Industrial Co., Ltd. | Muffler for internal combustion engine |
| US5821474A (en) | 1995-11-02 | 1998-10-13 | Heinrich Gillet Gmbh & Co. Kg | Muffler with variable damping characteristics |
| DE19817340A1 (de) | 1997-05-02 | 1998-11-05 | Volkswagen Ag | Verfahren zur Erwärmung der Kühlflüssigkeit bei einem Kraftfahrzeug und Abgasanlage |
| DE19715939C1 (de) | 1997-04-17 | 1998-12-03 | Daimler Benz Ag | Abgasanlage für eine Brennkraftmaschine |
| DE19729563A1 (de) | 1997-07-10 | 1999-01-14 | Volkswagen Ag | Fluidisches Verteilerventil |
| EP0902171A2 (de) | 1997-09-12 | 1999-03-17 | Sango Co., Ltd. | Schalldämpfer |
| US5957413A (en) | 1995-06-12 | 1999-09-28 | Georgia Tech Research Corporation | Modifications of fluid flow about bodies and surfaces with synthetic jet actuators |
| DE19817391A1 (de) | 1998-04-20 | 1999-10-21 | Daimler Chrysler Ag | Zündkerze für eine Brennkraftmaschine bzw. Sensorelement für Entflammungs- und Verbrennungsvorgang |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3643693A (en) * | 1969-09-08 | 1972-02-22 | Raymond N Auger | Multistable wake deflection amplifier |
-
2000
- 2000-01-07 DE DE10000464A patent/DE10000464B4/de not_active Expired - Fee Related
- 2000-12-23 DE DE50009679T patent/DE50009679D1/de not_active Expired - Fee Related
- 2000-12-23 WO PCT/EP2000/013261 patent/WO2001051777A2/de not_active Ceased
- 2000-12-23 EP EP00985258A patent/EP1244867B1/de not_active Expired - Lifetime
Patent Citations (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5438429A (en) | 1991-08-28 | 1995-08-01 | Silicon Graphics, Inc. | Digital filtering for lenticular printing |
| US5577294A (en) | 1993-10-01 | 1996-11-26 | James River Paper Company, Inc. | Web cleaner apparatus and method |
| US5801343A (en) | 1993-11-09 | 1998-09-01 | Futaba Industrial Co., Ltd. | Muffler for internal combustion engine |
| US5435489A (en) | 1994-01-13 | 1995-07-25 | Bell Helicopter Textron Inc. | Engine exhaust gas deflection system |
| US5739483A (en) | 1994-05-09 | 1998-04-14 | Nissan Motor Co., Ltd. | Automobile exhaust noise suppressor |
| US5658141A (en) | 1994-09-07 | 1997-08-19 | L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | Device for spreading a flame by the Coanda effect |
| US5744762A (en) | 1995-02-24 | 1998-04-28 | Calsonic Corporation | Muffler controller for use in controllable exhaust system of internal combustion engine |
| US5957413A (en) | 1995-06-12 | 1999-09-28 | Georgia Tech Research Corporation | Modifications of fluid flow about bodies and surfaces with synthetic jet actuators |
| US5821474A (en) | 1995-11-02 | 1998-10-13 | Heinrich Gillet Gmbh & Co. Kg | Muffler with variable damping characteristics |
| DE19709432A1 (de) | 1996-03-13 | 1997-10-30 | Volkswagen Ag | Vorrichtung zur Behandlung von Abgasen aus Brennkraftmaschinen |
| DE19729666A1 (de) | 1996-07-20 | 1998-01-22 | Gillet Heinrich Gmbh | Schalldämpfer mit variabler Dämpfungscharakteristik |
| DE19637078A1 (de) | 1996-09-12 | 1998-03-19 | Pierburg Ag | Elektromagnetisches Steuerventil für Abgasrückführung |
| DE19715939C1 (de) | 1997-04-17 | 1998-12-03 | Daimler Benz Ag | Abgasanlage für eine Brennkraftmaschine |
| DE19817340A1 (de) | 1997-05-02 | 1998-11-05 | Volkswagen Ag | Verfahren zur Erwärmung der Kühlflüssigkeit bei einem Kraftfahrzeug und Abgasanlage |
| DE19729563A1 (de) | 1997-07-10 | 1999-01-14 | Volkswagen Ag | Fluidisches Verteilerventil |
| EP0902171A2 (de) | 1997-09-12 | 1999-03-17 | Sango Co., Ltd. | Schalldämpfer |
| DE19817391A1 (de) | 1998-04-20 | 1999-10-21 | Daimler Chrysler Ag | Zündkerze für eine Brennkraftmaschine bzw. Sensorelement für Entflammungs- und Verbrennungsvorgang |
Non-Patent Citations (1)
| Title |
|---|
| ""Grossmassstabliche fluidische Ventile für die Durchflusssteuerung"", 1 January 1983, J. LOLL UND K. THOMAS |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1244867B1 (de) | 2005-03-02 |
| EP1244867A2 (de) | 2002-10-02 |
| DE10000464A1 (de) | 2001-07-26 |
| WO2001051777A3 (de) | 2001-12-20 |
| DE50009679D1 (de) | 2005-04-07 |
| DE10000464B4 (de) | 2004-02-05 |
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