CH370281A - Soundproofing device for explosion engines - Google Patents
Soundproofing device for explosion enginesInfo
- Publication number
- CH370281A CH370281A CH7902659A CH7902659A CH370281A CH 370281 A CH370281 A CH 370281A CH 7902659 A CH7902659 A CH 7902659A CH 7902659 A CH7902659 A CH 7902659A CH 370281 A CH370281 A CH 370281A
- Authority
- CH
- Switzerland
- Prior art keywords
- chamber
- perforated
- pipe
- truncated cone
- jacket
- Prior art date
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
- F01N1/00—Silencing apparatus characterised by method of silencing
- F01N1/08—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
- F01N1/089—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling using two or more expansion chambers in series
-
- 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
- F01N1/08—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Description
Schalldämpfungseinrichtung für Explosionsmotoren Nach vorliegender Erfindung ist eine Schalldämp- fungseinrichtung für Explosionsmotoren dadurch ge kennzeichnet, dass im Abgasrohr ein gegenüber diesem Rohr erweitertes Schalldämpferrohr eingesetzt ist, welches durch mindestens zwei Lochwände in hinter einander angeordnete Kammern unterteilt ist, wobei in der ersten Kammer ein sich von der Eingangsseite her zur ersten Trennwand verengernder,
mit Wandungs- löchern versehener Kegelstumpfmantel und in der zweiten Kammer ein direkt an den genannten Kegel- stumpfmantel angeschlossenes, am Ausgangsende ver schlossenes Lochmantelrohr angeordnet ist, während in der dritten Kammer<B>je</B> den grössten Teil des Kam merquerschnittes absperrende, in ihrem Zusammen wirken eine mäandrige Hin- und Herströmung der Gase erzwingende Querwände eingebaut sind.
Ein Ausführungsbeispiel des Erfind,ungsgegen- standes ist als Axialschnitt in der Zeichnung dar gestellt.
Im Auspuffrohr<B>1</B> eines Explosionsmotors ist ein gegenüber diesem Rohr erweitertes Schall- dämpfu#ngsrohr 2 eingesetzt. Dieses ist durch zwei Lochwände<B>3,</B> 4 in drei hintereinander angeordnete Kammern<B><I>A,</I></B><I> B,<B>C</B></I> unterteilt. Die erste Kammer<B>A</B> enthält einen sich von der Eingangsseite her zur ersten Trennwand<B>3</B> verengenden, mit Wandungslöchern <B>50</B> versehenen Kegelstumpfmantel <B>5,</B> welcher einen we sentlichen Teil der Gase bereits an die Peripherie des Rohres 2 entweichen lässt.
Die mittlere Kammer B enthält ein verhältnis mässig enges, am Ende verschlossenes Lochmantel- rohr <B>6,</B> welches die Restgase aus dem Innem des Kegelstumpfmantels <B>5</B> übernimmt und sie austreten lässt.
Durch die Lochwand 4 treten die Gase aus der Kammer B in die Kammer<B>C</B> über, wo Querwände <B>81, 82, 83</B> angeordnet sind, welche<B>je</B> den grössten Teil des Querschnittes absperren und bezüglich der offenen Durchgänge gegeneinander so versetzt sind, dass den Gasen eine mäandrige Hin- und Herströmung aufgezwungen wird. Diese Querwände.<B>81, 82, 83</B> sind miteinander gegen die Lochwand 4 durch ein Lochmantelrohr <B>7</B> abgestützt.
Versuche mit einer solchen Einrichtung haben einen hohen Schal#ldämpfungsgrad bei kleiner Vermin derung des Motorwirkungsgrade-s bewiesen.
Sound-damping device for explosion engines According to the present invention, a sound-damping device for explosion engines is characterized in that a muffler pipe is inserted in the exhaust pipe which is enlarged compared to this pipe and which is divided into chambers arranged one behind the other by at least two perforated walls, with one in the first chamber the entrance side narrowing towards the first partition,
truncated cone jacket provided with wall holes and in the second chamber a perforated jacket tube connected directly to the said truncated cone jacket and closed at the outlet end, while in the third chamber <B> each </B> most of the chamber cross-section is shut off, A meandering back and forth flow of the gases work together, which enforce transverse walls.
An exemplary embodiment of the invention, object of the invention is shown as an axial section in the drawing.
In the exhaust pipe <B> 1 </B> of an explosion engine, a sound-absorbing pipe 2, which is widened compared to this pipe, is inserted. This is through two perforated walls <B> 3, </B> 4 in three chambers <B> <I> A, </I> </B> <I> B, <B> C </B> <arranged one behind the other / I> divided. The first chamber <B> A </B> contains a truncated cone jacket <B> 5 </B> which narrows from the entrance side to the first partition <B> 3 </B> and is provided with wall holes <B> 50 </B>. B> which allows a substantial part of the gases to escape to the periphery of the pipe 2.
The middle chamber B contains a relatively narrow, perforated jacket tube <B> 6 </B> closed at the end, which accepts the residual gases from the interior of the truncated cone jacket <B> 5 </B> and lets them escape.
The gases pass through the perforated wall 4 from the chamber B into the chamber <B> C </B>, where transverse walls <B> 81, 82, 83 </B> are arranged, which <B> each </B> Block off most of the cross-section and offset from one another with respect to the open passages in such a way that a meandering back and forth flow is forced upon the gases. These transverse walls 81, 82, 83 are supported against one another against the perforated wall 4 by a perforated casing tube 7.
Tests with such a device have proven a high degree of sound attenuation with a small reduction in the motor efficiency.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH7902659A CH370281A (en) | 1959-10-03 | 1959-10-03 | Soundproofing device for explosion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH7902659A CH370281A (en) | 1959-10-03 | 1959-10-03 | Soundproofing device for explosion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH370281A true CH370281A (en) | 1963-06-30 |
Family
ID=4536927
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH7902659A CH370281A (en) | 1959-10-03 | 1959-10-03 | Soundproofing device for explosion engines |
Country Status (1)
Country | Link |
---|---|
CH (1) | CH370281A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3491850A (en) * | 1967-07-12 | 1970-01-27 | Pullman Inc | Sound silencing apparatus |
-
1959
- 1959-10-03 CH CH7902659A patent/CH370281A/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3491850A (en) * | 1967-07-12 | 1970-01-27 | Pullman Inc | Sound silencing apparatus |
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