DE2747655A1 - Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas - Google Patents

Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas

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Publication number
DE2747655A1
DE2747655A1 DE19772747655 DE2747655A DE2747655A1 DE 2747655 A1 DE2747655 A1 DE 2747655A1 DE 19772747655 DE19772747655 DE 19772747655 DE 2747655 A DE2747655 A DE 2747655A DE 2747655 A1 DE2747655 A1 DE 2747655A1
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DE
Germany
Prior art keywords
exhaust gas
aluminum
partial flow
central line
extruded part
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
Application number
DE19772747655
Other languages
German (de)
Inventor
Hans Karl Dr Leistritz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from DE19772733443 external-priority patent/DE2733443A1/en
Application filed by Individual filed Critical Individual
Priority to DE19772747655 priority Critical patent/DE2747655A1/en
Priority to JP4868178A priority patent/JPS5416041A/en
Priority to IT22649/78A priority patent/IT1095302B/en
Priority to US05/900,247 priority patent/US4233812A/en
Priority to GB16521/78A priority patent/GB1603962A/en
Priority to BE187201A priority patent/BE866483A/en
Priority to FR7812561A priority patent/FR2388993A1/en
Publication of DE2747655A1 publication Critical patent/DE2747655A1/en
Ceased legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/18Construction facilitating manufacture, assembly, or disassembly
    • F01N13/1838Construction facilitating manufacture, assembly, or disassembly characterised by the type of connection between parts of exhaust or silencing apparatus, e.g. between housing and tubes, between tubes and baffles
    • F01N13/1844Mechanical joints
    • F01N13/1855Mechanical joints the connection being realised by using bolts, screws, rivets or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/02Silencing apparatus characterised by method of silencing by using resonance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/02Silencing apparatus characterised by method of silencing by using resonance
    • F01N1/023Helmholtz resonators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/16Selection of particular materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/02Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2260/00Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/02Exhaust treating devices having provisions not otherwise provided for for cooling the device
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2450/00Methods or apparatus for fitting, inserting or repairing different elements
    • F01N2450/24Methods or apparatus for fitting, inserting or repairing different elements by bolts, screws, rivets or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/02Tubes being perforated
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/10Tubes having non-circular cross section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/18Structure or shape of gas passages, pipes or tubes the axis of inlet or outlet tubes being other than the longitudinal axis of apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/26Tubes being formed by extrusion, drawing or rolling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/15Plurality of resonance or dead chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/15Plurality of resonance or dead chambers
    • F01N2490/155Plurality of resonance or dead chambers being disposed one after the other in flow direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Exhaust Silencers (AREA)

Abstract

A silencer forming part of the exhaust system of an internal combustion engine consists of two concentric tubes (51, 52). These tubes are joined by radial walls (55) which extend longitudinally so that the annular space between the tubes is divided into a number of separate compartments (5). A cooling fluid flows in these compartments (5) in the opposite direction to the flow of gas in the central bore (50). The outer wall of the outer tube (52) has a number of radial fins (56) which also extend longitudinally. These fins help to dissipate the heat which has been transferred to the cooling medium by convection and radiation.

Description

Zusatzanmeldung zur Patentanmeldung P 27 33 443.6 (lei S 7710)Additional application to patent application P 27 33 443.6 (lei S 7710)

Bezeichnung der Zusatzanmeldung : "Thermische Abgasfünrng Zusatz 8".Designation of the additional application: "Thermal exhaust gas addition 8".

Beschreibung In der Patentanmeldung P 27 33 443.6 wurde ein in der Regel stranggepreßtes Hohlkommerringrohr beschrieben, das aus Aluminium gefertigt ist und unter Beachtung bestimmter thermischer Regeln für die Gas£59hPung in Schalldämpfer bzw. Kühlstrecken oder sonstige Schlußteile von Abgasanlagen integriert ist. Diese Regeln sehen zunächst eine bestimmte Konstruktion des langgestreckten Aluminiumkörpers vor : eine rohr- oder profilartige Innenleitung (sog.Zentralleitung) wird von einem Mantelraum umgeben, der durch Rippen in eine Mehrzahl langgestreckter Kanal unterteilt ist. Indem diese Rippen mit dem Innenrohr einen einheitlichen Strangpreßkörper darstellen, ist ein ständiger Wärmefluß zwischen dem Innenrohr und den Teilstromkanälen gesichert, für dessen Richtung die Konstruktion der Gesamtanlage maßgeblich ist und aus der sich beantwortet, ob im Innenrohr oder in allen oder einigen Teilkanälen eine relativ kuhlere Gasmenge (Abgas oder Luft oder ein flüssiges Medium) bewegt wird. Die Organisation der durchfließenden Medien hängt wiederum mit konstruktiven Eigenarten der beiden Schlißkörper ab, welche an beiden Sonden des Strangpreßteiles demontierbar vorgesehen sind und mit denen die Zufübrungs-, Verteiler- und Auslaufkonzepte in bezug auf die durchgesetzten Medien zusammenhängen. Der Patentanspruch von P 27 33 443.6 ging davon aus, daß die Außenwandung des Hohlkommermantels in die freie Atmosphäre abstrahlt und dem weiteren Merkmal, daß die Gasmenge, welche die ersten Aluminiumleitungen, welche mit ihren Wandungen in die freie Atmosphäre abstrahlen, verläl3t, vor dem erneuten Eintritt in aluminiumbegrenzte Kanäle eine thermische Zwischenzone passiert, in welcher ein weiterer Wärmeverlust, etwa durch eine Wärmetauschwandung, vorgesehen ist. Der spezielle technische G.sichtspunkt der mit P 27 33 443.6 vorgelegten Konstruktion besteht in seinem kennzeichnenden Teil nunmehr darin, "daB innerhalb der zwischen Motorauslaß und erster Beaufachlagung von Aluminiumvandungen gelegenen Abgaseinlaufzone Wärmetauschwandung zu einem stromabwärts der erstbeaufschlagten Aluminium-Gasführungsleitungen gelegenen Gerätaustrittsrohr oder dessen Zuführungsleitungen vorgesehen ist." Es entsteht durch diese Anordnung ein sog. Wärmekurzschlußweg zwischen der Heißgaszulaufzone des Gerätes und der Gerätaustrittsleitung und hierdurch die Wirkung, daß die auf diesem Wege herausgeführte Wärmemenge das Aluminiumbauteil überspringt und hierdurch einen weiteren technischen Gesichtspunkt hinzufügt, der es ermöglicht, das Gerät mit einem heißeren Abgas zu beladen, als es nach der Theorie der Warmfestigkeitsgrenzen dieses Werkstoffes geboten wäre. Description In the patent application P 27 33 443.6 was in the Usually extruded Hohlkommerringrohr described, which is made of aluminum is and in compliance with certain thermal rules for the gas £ 59hPung in muffler or cooling sections or other final parts of exhaust systems is integrated. These Rules initially see a certain construction of the elongated aluminum body before: a pipe-like or profile-like inner line (so-called central line) is led by a Surrounding shell space, which is divided into a plurality of elongated channels by ribs is. As these ribs and the inner tube represent a uniform extruded body, a constant flow of heat between the inner pipe and the partial flow channels is ensured, for whose direction the construction of the overall system is decisive and from the answered whether in the inner pipe or in all or some of the sub-channels a relative cooler amount of gas (exhaust gas or air or a liquid medium) is moved. The organization the media flowing through depends in turn on the constructive peculiarities of the two Shear body from, which can be dismantled on both probes of the extruded part are and with which the feed, distribution and discharge concepts in relation to the enforced media are related. The patent claim of P 27 33 443.6 went on the assumption that the outer wall of the Hohlkommermantels radiates into the open atmosphere and the further feature that the amount of gas which the first aluminum pipes, which radiate with their walls into the free atmosphere, extends in front of the re-entry into aluminum-limited channels passes a thermal intermediate zone, in which a further loss of heat, for example through a heat exchange wall, is provided is. The special technical point of view of the construction presented with P 27 33 443.6 consists in its characteristic part now in "that within the between Engine exhaust and first exposure of aluminum walls located exhaust gas inlet zone Heat exchange wall to a downstream of the first exposed one Aluminum gas ducts located device outlet pipe or its supply lines is provided. "Es This arrangement creates a so-called thermal short-circuit path between the hot gas inlet zone of the device and the device outlet line and thereby the effect that the on The amount of heat carried out in this way skips the aluminum component and thereby adds another technical aspect that enables the device to be loaded with a hotter exhaust gas than it is according to the theory of high-temperature strength limits this material would be required.

Die beigefügten Schemazeichnungen Figuren 1 und 2 zeigen beide die oben beschriebene Konstruktion des Wärmekurzschlußweges.The attached schematic drawings Figures 1 and 2 both show the construction of the thermal short-circuit path described above.

In beiden Fällen besitzt die Abgaseinlaufzone 2, an welche das Motorauslaßrohr 1 direkt oder indirekt angeschlossen ist, eine Wärmetauschwandung 5, welche Bestandteil der Zufiihrungsleitung, also des Raumes 21, ist, aus welchem das Abgas über die Rohre 11 der freien Atmosphäre zugeführt wird. Austrittsrohr ist in Figur 1 das Rohr 13, in Figur 2 das Teilstrombündel der Rohre 24. Während indessen in der Anmeldung P 27 33 443.6 auf diesem Wärmekurzschlußwege überhaupt keine Aluminiumwandungen mehr beriihrt wurden, durchilißt das Abgas nach Austritt aus den Rohren 11 in den Figuren 1 und 2 den alumniumbegrenzten Zentralrohrteil 10. Aus diesem Grunde insbesondere war es zweckmässig, neben der Wärmesenkung durch die umseitig beschriebene thermische Zwischenzone", also den Schließkörperraum 19 der Figuren 1 und 2, eine weitere Wärme senkung vorzusehen. Diese besteht in einer nochmaligen Hindurchführung der Abgasmenge durch einen oder mehrere Teilstromkanäle des im Mantelkörper vorgesehenen, in die freie Atmospäre abstrahlenden und in der Regel aussen verrippten EanalbUndels. Wie aus den Schemazeichnungen ersichtlich, tritt das Abgas aus dem ersten Entspannungsraum 2 in mehrere Kanäle 9 des Strangpreßteils ein, mündet alsdann in den Schließkörperraum 19 und betritt aus diesem durch die Öffnungen 17 nochmals eines oder eine weitere Gruppe von Teilstromaanälen 16, die - in der Regel wechselseitig - den Teilstromkanälen 9 benachbart sind. Die Kanäle 16 sind durch den Schließkörper 4 stromabwärts verschlossen und das Abgas tritt durch eine übertrittsöffnung 15, die sich in den Aluminiumwandungen 20 befindet über eine korrespondierende Öffnung 7 in eine Zusatzkanmer 21 Uber, die mit Einstecktiefe in den Raum 10 des Alumniumkörpers Bestandteil des stromaufwärtigen SchlieB-körpers ist. In der Mantelwandung des Aluminiumstrangpreßteils befinden sich auf diese Weise zvei zueinander im Gegenstrom angeordnete Gasstromgruppen, von denen die folgende (16) gegenüber der vorigen (9) kühler ist, und zwar einmal nach dem langen Weg durch die Aluminiumvandteile der Kanaäle 9 infolge ihrer Ab strahlverluste, zum anderen durch den Abstrahlverlust aus dem Sammelraum 19, bei dem es eine reine Auslegungafrage ist, wie groß seine Außenoberfläche gehalten wird. Hinzu kommt, daß hiermit zugleich der Wärmeabfuhrweg aus der Wandung 20 der Innenleitung 10 atimiert wurde, da nunmehr mit Hilfe der Gasströme 16 ein größeres Wärmegefälle Richtung Außenwandung 8 entstanden ist.In both cases, the exhaust gas inlet zone 2, to which the engine exhaust pipe 1 is connected directly or indirectly, a heat exchange wall 5, which is part of of the supply line, that is to say of the space 21, from which the exhaust gas via the Tubes 11 is fed to the free atmosphere. The outlet pipe is in Figure 1 Tube 13, in Figure 2 the partial flow bundle of tubes 24. Meanwhile, in the application P 27 33 443.6 no aluminum walls at all on this thermal short-circuit path more were touched, the exhaust gas passes through after exiting the pipes 11 into the Figures 1 and 2 the aluminum-limited central tube part 10. For this reason in particular it was useful, in addition to the heat reduction through the thermal energy described overleaf Intermediate zone ", that is to say the closing body space 19 of FIGS. 1 and 2, another heat to provide for lowering. This consists in a repeated passage of the amount of exhaust gas through one or more partial flow channels of the provided in the shell body, into the EanalbUndels radiating a free atmosphere and usually ribbed on the outside. As As can be seen from the schematic drawings, the exhaust gas emerges from the first expansion space 2 into several channels 9 of the extruded part, then opens into the closing body space 19 and enters from this through the openings 17 again one or another Group of partial flow channels 16 which - as a rule, alternately - the partial flow channels 9 are adjacent. The channels 16 are closed downstream by the closing body 4 and the exhaust gas passes through an overflow opening 15 which is located in the aluminum walls 20 is located via a corresponding opening 7 in an additional channel 21 over, the one with insertion depth in the space 10 of the aluminum body part of the upstream Closing body is. In the jacket wall of the extruded aluminum part in this way there are two gas flow groups arranged in countercurrent to one another, of which the following (16) is cooler compared to the previous (9), namely once after the long way through the aluminum wall parts of the channels 9 as a result of their Ab beam losses, on the other hand due to the radiation loss from the collecting space 19 for which it is a mere design question how large its outer surface is kept. In addition, at the same time the heat dissipation path from the wall 20 of the inner line 10 was atimated, since now with the help of the gas streams 16 a greater heat gradient Direction outer wall 8 has arisen.

Sollte sich trotz dieser Maßnahme die Aluminiumtemperatur bei bestimmten Motorenarten und -größen dem oberen Warmfestigkeitsbereich nähern, gibt die in Figur 2 dargestellte Verstärkung des Wärmekurzschlußweges hierfür den Ausgleich. Es wird ein Innenkishlrohr 22 angeordnet, wie es seitens des Anmelders in der Offenlegungsschriit 25 10 624 beschrieben wurde. Dieses, einen vom Abgasdurchlauf prinzipiell unterschiedenen Luftdurchsatz bezwekkende Rohr kann sich als Innenleitung alsdann in ein Austrittsrohr fortsetzen, und zwar in dessen Innenleitung 23, während der Abgasaustritt durch das Teilstrombündel 24 erfolgt. Für Leerlaufzustände, in denen keine Fahrwindbeaufschlagung gegeben ist, kann im Rohrteil 22 ein Abgasinjektor mit Richtung Gerätaustritt vorgesehen sein. Das Innenkühlrohr durchläuft in Figur 2 sowohl den ersten Heißgasraum 2 wie den Sammelraum 21; seine thermische Entlastung der Innenwandung 20 des Aluminium-Strangpreßteiles ist mithin nicht nur aus seinem Durchlauf des Raumes 10, sonaern insbesondere aus der primären Wärmeabfuhr aus dem Zulaufraum 2 zu beurteilen.Should, despite this measure, the aluminum temperature be at certain Motor types and sizes approach the upper heat resistance range, is shown in the figure 2 reinforcement of the thermal short-circuit path for this compensation. It will an Innenkishlrohr 22 arranged, as it is on the part of the applicant in the Offenlegungsschriit 25 10 624 has been described. This one, which is fundamentally different from the exhaust gas flow The air flow-aiming pipe can then be used as an inner line in an outlet pipe continue, in the inner line 23, while the exhaust gas outlet through the partial flow bundle 24 takes place. For idling conditions in which there is no driving wind is given, an exhaust gas injector with the direction of the device outlet can be provided in the pipe part 22 be. The inner cooling pipe runs through both the first hot gas space 2 and in FIG the collecting space 21; its thermal relief of the inner wall 20 of the aluminum extrusion is therefore not only from its passage through the room 10, but in particular from the primary heat dissipation from the inlet chamber 2 to be assessed.

LeerseiteBlank page

Claims (7)

Patentansprüche 9 Thermische AbgasiUhrung mit dem im Strangpreßverfahren hergestellten aluminiumgefertigten Bauelement eines Hohlkammerringrohres, das in Schalldämpfer oder ESihnstrecken der Abgasanlagen von Brennkraftmaschinen integriert ist und durch Rippen insbesondere hinsichtlich seines Mantelraumes in langgestreckte, um eine Zentralleitung angeordnete Teilstromführungsgruppen unterteilt ist, mit dem Merkmal, daß die Außenwandung des Hohlkammermantels in die freie Atmosphäre abstrahlt, dem Merkmal, daß die Abgasmenge, welche die erste Aluminium-Eanalfuhrung verläßt vor Eintritt in eine zweite Kanalführngsgruppe des Strangpreßteils eine thermische Zwischenzone passiert, in welcher sie einen weiteren Wärmeverlust erleidet, und dem weiteren iIerkmn1, daß innerhalb der zwischen Notorauslaß und erster Beaufchlabung von Aluminiumwandungen gelegenen Vorzone (2) Wärmetauschwandung (5) zu einer stromabwärts der ersten Aluminium-Leitung (9) gelegenen Zufuhrnngsleitung (21) zum Gerätaustrittsrohr (13, 24) vorgesehen st, dodurcli gekehnzeichnet, daß das 'Ogh9 aus einer ersten aluminiumbegrenzten Teilstromgruppe (9) in den durch einen Schließkörper (14) des Strangpreßteils (8/20) gebildeten Sammelraum (19) übertritt, aus dem es in eine weitere Teilstromgruppe bzw. mindestens in eine Gasführungsleitung (17/16) gelangt, welche sich ebenfalls innerhalb des Hohlksmmermanteltaumes des Strangpreßteiles befindet und in Gegenstromanordnung mindestens teilweise an Wandungen angrenzt,welche Jenseitig zu der erstbeaufschlagten Teilstromgruppe (9) bzw. zur Bildung der Zentralleitung (10) gehören. Claims 9 Thermal exhaust gas flow using the extrusion process manufactured aluminum-manufactured component of a hollow chamber ring tube, which is in Integrated silencers or sections of the exhaust systems of internal combustion engines is and by ribs in particular with regard to its shell space in elongated, is divided around a central line arranged partial flow routing groups, with the feature that the outer wall of the hollow chamber jacket into the free atmosphere emits, the feature that the amount of exhaust gas that the first aluminum Eanalfuhrung leaves one before entering a second channel guide group of the extruded part thermal intermediate zone, in which it suffers further heat loss, and the further iIerkmn1 that within the between the Notorauslaß and the first vent from aluminum walls located pre-zone (2) heat exchange wall (5) to a downstream the first aluminum line (9) located supply line (21) to the device outlet pipe (13, 24) st, dodurcli marked that the 'Ogh9 comes from a first aluminum-limited partial flow group (9) in the by a closing body (14) of the Extruded part (8/20) formed collecting space (19) passes from which it is in a another partial flow group or at least one gas duct (17/16) reaches, which is also within the Hohlksmmermanteltaumes of the extruded part is located and in a countercurrent arrangement at least partially adjoins walls, which On the other side to the partial flow group (9) to which the first act is applied or to form the central line (10) belong. 2. Vorrichtung gemäß vorigem Anspruch dadurch gekennzeichnet, daß die zweite Teilstromgruppe (16) in einen Sammelraum (21) übergeht, welcher Wärmetauschwandung (5) zur Heißgas-Eintrittszone (2) des Gerätes aufweist und mit Eindringtiefe in die Zentralleitung (10) des Strangpreßteils Bestandteil des stromaufwärtigen Schließkörpers des Aluminium-Strangpreßteiles ist.2. Device according to the previous claim, characterized in that the second partial flow group (16) merges into a collecting space (21), which heat exchange wall (5) to the hot gas inlet zone (2) of the device and with penetration depth in the central line (10) of the extruded part is part of the upstream closing body of the aluminum extrusion. 3. Vorrichtung gemäß einem der vorigen Ansprüche dadurch gekennzeichnet, daß die Zentralleitung (10) des Strangpreßteils durch ein Innenkühlrohr (22) durchquert wird, in dem ein vom Abgasdurchlauf unterschiedener Luftdurchsatz stattfindet.3. Device according to one of the preceding claims, characterized in that that the central line (10) of the extruded part passes through an internal cooling pipe (22) in which an air throughput that is different from the exhaust gas flow takes place. 4. Innenkühlrohr gemäß vorigem Anspruch dadurc'n gekennzeichnet, daß es auch die Heißgaseinlaufzone (2) und sonstige Zwischenvolumen (wie 21) durchdringt.4. inner cooling tube according to the previous claim dadurc'n characterized in that it also penetrates the hot gas inlet zone (2) and other intermediate volumes (such as 21). 5. Innenkhlrohr nach einem der vorigen Anspruche dadurch 2ekennzeichnet, daß es sich in die Zentralleitung (23) eines als Hohlkammermantelrohr ausgeführten Austrittsrohres fortsetzt, durch dessen äußere Teilstromgruppe (24) der Abgasaustritt stattfindet.5. Inner cooling tube according to one of the preceding claims, characterized in that that it is in the central line (23) designed as a hollow-chamber jacket tube Outlet pipe continues, through the outer partial flow group (24) of the exhaust gas outlet takes place. 6. Innenkishlrohr gemäß einem der vorigen Ansprüche dadurch gekennzeichnet, daß stromaufwärts ein Abgasinj ektor angeordnet ist, der das Abgas aus der Zentralleitung (10) des 3trangpreßteils abnimmt.6. Innenkishlrohr according to one of the preceding claims, characterized in that that an exhaust gas injector is arranged upstream, which extracts the exhaust gas from the central line (10) of the 3trangpreßteil decreases. 7. Vorrichtung gemäß einem der vorigen Ansprüche dadurch gekennzeichnet, daß die Schließkörper, welche beidseitig die Zulaufanordnung einschließlich der Verteiler- und Auslaufkonzete bestimmen, durch eine axial verlaufende Spannvorrichtung verbunden sind.7. Device according to one of the preceding claims, characterized in that that the closing body, which on both sides the inlet arrangement including the Determine distribution and discharge concepts by means of an axially extending clamping device are connected.
DE19772747655 1977-04-28 1977-10-24 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas Ceased DE2747655A1 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
DE19772747655 DE2747655A1 (en) 1977-07-25 1977-10-24 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
JP4868178A JPS5416041A (en) 1977-04-28 1978-04-24 Multipleewall hollow mold material with blockade body for guiding thermal gas
IT22649/78A IT1095302B (en) 1977-04-28 1978-04-24 CONDUCTION SYSTEM FOR GAS APPLIANCES WITH DISCHARGE IN THE FREE ATMOSPHERE, IN PARTICULAR FOR MOTOR DRIVE ELEMENTS
US05/900,247 US4233812A (en) 1977-04-28 1978-04-26 Gas discharge apparatus
GB16521/78A GB1603962A (en) 1977-04-28 1978-04-26 Gas discharge apparatus
BE187201A BE866483A (en) 1977-04-28 1978-04-27 GAS CONDUCTION DEVICE AND HOLLOW PROFILES FOR ITS REALIZATION
FR7812561A FR2388993A1 (en) 1977-04-28 1978-04-27 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19772733443 DE2733443A1 (en) 1977-05-03 1977-07-25 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
DE19772747655 DE2747655A1 (en) 1977-07-25 1977-10-24 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas

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DE2747655A1 true DE2747655A1 (en) 1979-04-26

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