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 gasInfo
- 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
- Authority
- 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
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 ; 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
- F01N13/18—Construction facilitating manufacture, assembly, or disassembly
- F01N13/1838—Construction 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
- F01N13/1844—Mechanical joints
- F01N13/1855—Mechanical joints the connection being realised by using bolts, screws, rivets or the like
-
- 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
- F01N1/02—Silencing apparatus characterised by method of silencing by using resonance
-
- 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
- F01N1/02—Silencing apparatus characterised by method of silencing by using resonance
- F01N1/023—Helmholtz resonators
-
- 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 ; 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
- F01N13/16—Selection of particular materials
-
- 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
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
-
- 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
- F01N2260/00—Exhaust treating devices having provisions not otherwise provided for
- F01N2260/02—Exhaust treating devices having provisions not otherwise provided for for cooling the device
-
- 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
- F01N2450/00—Methods or apparatus for fitting, inserting or repairing different elements
- F01N2450/24—Methods or apparatus for fitting, inserting or repairing different elements by bolts, screws, rivets or the like
-
- 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
- F01N2470/00—Structure or shape of gas passages, pipes or tubes
- F01N2470/02—Tubes being perforated
-
- 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
- F01N2470/00—Structure or shape of gas passages, pipes or tubes
- F01N2470/10—Tubes having non-circular cross section
-
- 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
- F01N2470/00—Structure or shape of gas passages, pipes or tubes
- F01N2470/18—Structure or shape of gas passages, pipes or tubes the axis of inlet or outlet tubes being other than the longitudinal axis of apparatus
-
- 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
- F01N2470/00—Structure or shape of gas passages, pipes or tubes
- F01N2470/26—Tubes being formed by extrusion, drawing or rolling
-
- 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
- F01N2490/00—Structure, disposition or shape of gas-chambers
- F01N2490/15—Plurality of resonance or dead chambers
-
- 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
- F01N2490/00—Structure, disposition or shape of gas-chambers
- F01N2490/15—Plurality of resonance or dead chambers
- F01N2490/155—Plurality of resonance or dead chambers being disposed one after the other in flow direction
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving 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
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)
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 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE2747655A1 true DE2747655A1 (en) | 1979-04-26 |
Family
ID=25772388
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19772747655 Ceased DE2747655A1 (en) | 1977-04-28 | 1977-10-24 | Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE2747655A1 (en) |
-
1977
- 1977-10-24 DE DE19772747655 patent/DE2747655A1/en not_active Ceased
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8131 | Rejection |