US2544284A - Muffler with plural perforated passages - Google Patents
Muffler with plural perforated passages Download PDFInfo
- Publication number
- US2544284A US2544284A US745978A US74597847A US2544284A US 2544284 A US2544284 A US 2544284A US 745978 A US745978 A US 745978A US 74597847 A US74597847 A US 74597847A US 2544284 A US2544284 A US 2544284A
- Authority
- US
- United States
- Prior art keywords
- shell
- channel
- muffler
- openings
- gas
- 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.)
- Expired - Lifetime
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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
-
- 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
- F01N1/084—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling the gases flowing through the silencer two or more times longitudinally in opposite directions, e.g. using parallel or concentric tubes
-
- 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
-
- 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
- F01N2260/18—Exhaust treating devices having provisions not otherwise provided for for improving rigidity, e.g. by wings, ribs
-
- 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
- F01N2450/22—Methods or apparatus for fitting, inserting or repairing different elements by welding or brazing
-
- 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
- F01N2470/30—Tubes with restrictions, i.e. venturi or the like, e.g. for sucking air or measuring mass flow
-
- 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
- F01N2490/12—Chambers having variable volumes
Definitions
- This invention has to do generally with the elimination or separation of gas stream undulations, inclusive of those within the audible and sub-audible ranges and is concerned particularly with improvements in acoustical filter type equipment, of which internal combustion engine mufflers may be regarded as typical.
- the invention has to do with improvements in that general type of muffler comprising a shell containing a pair of chambers, functioning essentially as acoustical capacitances, interconnected by conduits forming elongated passages in the nature of acoustical resistances or inductances.
- Our general object is to provide a muffler of the low pass filter type, characterized by its extreme simplicity of construction and assemblage, and the assured predictability of its operation from acoustical and pressure drop standpoints.
- the invention contemplates separating the capacitance chambers by a transverse partition in the mufller shell, and interconnecting the chambers by a plurality of channel shaped conduits opening toward and adjacent the shell,
- openings through which the gas enters or leaves the channel passage, as the case may be, transversely with relation to its longitudinal flow therethrough.
- openings may be utilized to permit lateral as well as longitudinal gas flow along the extents of the channel passages.
- the channel edges are spaced from the shell to provide slot-like openings through which gas enters the conduits from one chamber, to be released lengthwise of the conduit into the second chamber. Attachment of the conduits to the shell at intervals maintains the stated spaced relationship and gives the conduits the additional function of strong re-enforcements stabilizing the muflier shell against vibration.
- Fig. 1 is a view showing a muffler embodiment of the invention in longitudinal section
- Fig. 2 is an enlarged scale cross-section on line 2-2 of Fig. 1;
- Fig. 3 is a fragmentary section illustrating the mode of channel connection with the shell
- Fig. 4 is a view showing the inlet diffuser in elevation.
- Figs. 5 and 6 are fragmentary views illustrating variational features of the invention.
- the muffler is shown to comprise an elongated cylindrical shell 10 having an inlet I l and an outlet l2 through the flared mouth discharge pipe IS.
- the shell is divided by transverse partition l4 into a pair of chambers I5 and I6, which may be of substantially equal volume, forming the acoustical capacitances referred to above.
- the chambers I5 and iii are in communication only through a circular arrangement of channel members I! received within notches IS in the partition [4, the open sides of the channels facing and forming with the shell [0, elongated passages l9 through which the gas flows from chamber l5 into chamber l6. While the invention broadly contemplates use of channels having any desired cross-sectional configuration, we preferably use simple angle iron or substantially L-shaped members I1, by reason of their availability and low cost, and adaptability to the desired structural characteristics of the assembly.
- Members I! are attached to the shell I0 by terminal welds IN, the edges of the channel being narrowly spaced from the shell to form slot-like openings l9 extending substantially the full length of the channels.
- the latter also may be welded to the partition l4 so that the entire assembly is integrated into a muffler structure strongly re-enforced by the attached channels.
- the diffuser may consist of an elongated tapered shell 2
- the illustrated 3 type of diffuser 22 constitutes the particular subject matter of copending application Serial No. 748,961, now Patent Number 2,517,623, issued August 8, 1950, filed by Raymond C. Baird, on Acoustic Discontinuity Diffuser.
- the exhaust gas is subjected to progressively decreasing impedence in passing through the injector shell 2
- the injector acts as a filter causing the energy at any point along the pulse wave to be distributed longitudinally of the injector, so that the path difierences with respect to any point in the chamber 15 effect a phase shift.
- the gas After admission to the chamber 5, the gas enters the channel passages !9 through their open ends and along both sides of each channel through the openings ISI. Similarly at the opposite side of partition M, the gas escapes pro gressively through the side openings toward the open ends of the channels.
- Figs 5 and 6 illustrate variational aspects relating to the admission of exhaust gas to, and its exhaust from the channel passages, other than by the described openings along the channel edges.
- the channel 25 (corresponding to channel I1) is welded at 26 along its edges to the shell [0, and has a series 21 of perforations extending substantially throughout the length of the channel to afford substantially continuous restricted passages through which the gas may transversely enter and escape from the channel passage proper.
- the channel 28, welded along its edges at 29 to the shell has at its apex a longitudinal gas passing slot 33 extending substantially the length of the channel.
- An engine mufiler comprising an elongated shell containing a pair of chambers through which the gas has series flow, a partition separating said chambers, channel members extending through said. partition adjacent the shell and spaced therefrom to form narrow elongated openings through which the gas flows from one chamber into the channel members and passes therethrough into the other chamber, and means attaching the edges of said members to the shell at spaced intervals so that the members and shell are in mutually reenforoing relation.
- An engine mufiier comprising an elongated shell containing a pair of chambers through which the gas has series flow, a partition separating said chambers, circularly spaced channel members of substantially L-shaped cross-section extending through peripheral notches in said partition adjacent the shell and having their edges spaced therefrom to form narrow elongated openings along said edges and through which the gas flows from one chamber into the channel members and passes therethrough into the other chamber, and means attaching the edges of said members to the shell at spaced intervals so that the members and shell are in mutually reenforcing relation.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Description
March 6, 1951 F. M. STEPHENS ET AL MUFFLER WITH PLURAL PERFORATED PASSAGES Filed May 5, 1947 IN VEN TORS fllP/IGID 3027116 TIP/YJIIRHIMS BYMM .147 TOP/wry Patented Mar. 6, 1 951 MUFFLER WITH PLURAL PERFORATED PASSAGES Foster M. Stephens and Arnold Bartels, Los Angeles, Calif., assignors 'to The Fluor Corporation, Ltd., Los Angeles, Calif., a corporation of California Application May 5, 1947, Serial No. 745,978
2 Claims. 1
This invention has to do generally with the elimination or separation of gas stream undulations, inclusive of those within the audible and sub-audible ranges and is concerned particularly with improvements in acoustical filter type equipment, of which internal combustion engine mufflers may be regarded as typical.
Specifically the invention has to do with improvements in that general type of muffler comprising a shell containing a pair of chambers, functioning essentially as acoustical capacitances, interconnected by conduits forming elongated passages in the nature of acoustical resistances or inductances. Our general object is to provide a muffler of the low pass filter type, characterized by its extreme simplicity of construction and assemblage, and the assured predictability of its operation from acoustical and pressure drop standpoints. Of particular advantage is the structural association of inter-chamber conduits with the muffler shell in a manner resulting in re-enforcement of the shell (with consequent elimination of mechanical vibration and associated noises) and the formation lengthwise of the conduit, of gas entry and escape gaps which materially supplement the acoustical and filtering qualities of the mufller.
structurally the invention contemplates separating the capacitance chambers by a transverse partition in the mufller shell, and interconnecting the chambers by a plurality of channel shaped conduits opening toward and adjacent the shell,
and having openings through which the gas enters or leaves the channel passage, as the case may be, transversely with relation to its longitudinal flow therethrough. As will appear, different forms and arrangements of openings may be utilized to permit lateral as well as longitudinal gas flow along the extents of the channel passages.
Preferably the channel edges are spaced from the shell to provide slot-like openings through which gas enters the conduits from one chamber, to be released lengthwise of the conduit into the second chamber. Attachment of the conduits to the shell at intervals maintains the stated spaced relationship and gives the conduits the additional function of strong re-enforcements stabilizing the muflier shell against vibration.
Additional features of the invention, as well as the details of a typical embodiment thereof, will be understood from the following detailed description of the accompanying drawing, in which:
Fig. 1 is a view showing a muffler embodiment of the invention in longitudinal section;
Fig. 2 is an enlarged scale cross-section on line 2-2 of Fig. 1;
Fig. 3 is a fragmentary section illustrating the mode of channel connection with the shell;
Fig. 4 is a view showing the inlet diffuser in elevation; and
Figs. 5 and 6 are fragmentary views illustrating variational features of the invention.
Referring to Figs. 1 and 2, the muffler is shown to comprise an elongated cylindrical shell 10 having an inlet I l and an outlet l2 through the flared mouth discharge pipe IS. The shell is divided by transverse partition l4 into a pair of chambers I5 and I6, which may be of substantially equal volume, forming the acoustical capacitances referred to above.
The chambers I5 and iii are in communication only through a circular arrangement of channel members I! received within notches IS in the partition [4, the open sides of the channels facing and forming with the shell [0, elongated passages l9 through which the gas flows from chamber l5 into chamber l6. While the invention broadly contemplates use of channels having any desired cross-sectional configuration, we preferably use simple angle iron or substantially L-shaped members I1, by reason of their availability and low cost, and adaptability to the desired structural characteristics of the assembly.
Members I! are attached to the shell I0 by terminal welds IN, the edges of the channel being narrowly spaced from the shell to form slot-like openings l9 extending substantially the full length of the channels. The latter also may be welded to the partition l4 so that the entire assembly is integrated into a muffler structure strongly re-enforced by the attached channels.
Exhaust gas enters the chamber 15 at the inlet ll through a diffuser, generally indicated at 20 which, in the broad contemplation of the invention, may be of any suitable form capable of presenting to the inlet gas flow a passage of progressively decreasing cross-sectional area, from which the gas escapes through one or more slot-like openings of progressively increasing size or width in the direction of the gas flow. Typically the diffuser may consist of an elongated tapered shell 2| split longitudinally to form diametrically opposed openings 22 of progressively increasing width toward the end of the shell, the split portion of the latter being re-enforced by bridge pieces 23 extending across the openings. At this point it may be mentioned that the illustrated 3 type of diffuser 22 constitutes the particular subject matter of copending application Serial No. 748,961, now Patent Number 2,517,623, issued August 8, 1950, filed by Raymond C. Baird, on Acoustic Discontinuity Diffuser.
Entering the diffuser shell 2 l, the exhaust gas is subjected to progressively decreasing impedence in passing through the injector shell 2|, the relation between the dimension of the internal passage and escape openings being such that the quantity of exhaust gases leaving the injector along any interval is small as compared With the quantity remaining within and advancing beyond that interval. While this ratio approaches maximum at the open end of the body, the energy there reflected is so small relative to that of the incident stream as to create little tendency for pipe resonance. 'The incremental energy refiects along the openings 22 are shifted in phase relative to the course of flow, in a manner further tending to prevent resonance. In suppressing shock resonance of the muflier, the injector acts as a filter causing the energy at any point along the pulse wave to be distributed longitudinally of the injector, so that the path difierences with respect to any point in the chamber 15 effect a phase shift. After admission to the chamber 5, the gas enters the channel passages !9 through their open ends and along both sides of each channel through the openings ISI. Similarly at the opposite side of partition M, the gas escapes pro gressively through the side openings toward the open ends of the channels.
Figs 5 and 6 illustrate variational aspects relating to the admission of exhaust gas to, and its exhaust from the channel passages, other than by the described openings along the channel edges. In Fig. 5 the channel 25 (corresponding to channel I1) is welded at 26 along its edges to the shell [0, and has a series 21 of perforations extending substantially throughout the length of the channel to afford substantially continuous restricted passages through which the gas may transversely enter and escape from the channel passage proper. In the modification of Fig. 6, the channel 28, welded along its edges at 29 to the shell, has at its apex a longitudinal gas passing slot 33 extending substantially the length of the channel.
It will be understood that the drawing is to be regarded. as merely illustrative of the inven- 4 tion as embodied in a preferred form, and that various changes and modifications may be made without departure from the intended spirit and scope of the invention.
We claim:
1. An engine mufiler comprising an elongated shell containing a pair of chambers through which the gas has series flow, a partition separating said chambers, channel members extending through said. partition adjacent the shell and spaced therefrom to form narrow elongated openings through which the gas flows from one chamber into the channel members and passes therethrough into the other chamber, and means attaching the edges of said members to the shell at spaced intervals so that the members and shell are in mutually reenforoing relation.
2. An engine mufiier comprising an elongated shell containing a pair of chambers through which the gas has series flow, a partition separating said chambers, circularly spaced channel members of substantially L-shaped cross-section extending through peripheral notches in said partition adjacent the shell and having their edges spaced therefrom to form narrow elongated openings along said edges and through which the gas flows from one chamber into the channel members and passes therethrough into the other chamber, and means attaching the edges of said members to the shell at spaced intervals so that the members and shell are in mutually reenforcing relation.
FOSTER M. STEPHENS. ARNOLD BAR'IELS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,468,398 Reed Sept. 18, 1923 2,016,254 Noblitt Oct. 1, 1935 2,051,675 Blanchard Aug. 18, 1936 2,264,195 Bourne Nov. 25, 1941 2,397,208 Saco, Jr., et al. Mar. 26, 1946 2,445,045 Strachan July 13, 1948 FOREIGN PATENTS Number Country Date 342,364 Great Britain Feb. 5, 1931
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US745978A US2544284A (en) | 1947-05-05 | 1947-05-05 | Muffler with plural perforated passages |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US745978A US2544284A (en) | 1947-05-05 | 1947-05-05 | Muffler with plural perforated passages |
Publications (1)
Publication Number | Publication Date |
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US2544284A true US2544284A (en) | 1951-03-06 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US745978A Expired - Lifetime US2544284A (en) | 1947-05-05 | 1947-05-05 | Muffler with plural perforated passages |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2675088A (en) * | 1951-11-24 | 1954-04-13 | William B Mcleod | Muffler |
US3144913A (en) * | 1962-08-31 | 1964-08-18 | Garrett Corp | Method and apparatus for attenuating helical acoustic pressure waves |
US3276108A (en) * | 1964-02-21 | 1966-10-04 | Reynolds Metals Co | Method of making a muffler |
US3280903A (en) * | 1964-12-21 | 1966-10-25 | Universal Silencer Corp | Exhaust silencer and heat recovery unit |
FR2349730A1 (en) * | 1976-04-30 | 1977-11-25 | Nihon Radiator Co | EXHAUST |
US5016729A (en) * | 1987-06-18 | 1991-05-21 | Claes Linden | Exhaust system for combustion engine |
DE102005025288A1 (en) * | 2005-06-02 | 2006-12-07 | D'alessandro, Luigi | Exhaust gas silencer for e.g. exhaust gas system of water-craft has transverse wall, which is interspersed by two, preferably three pipe lead-through for parallel exhaust gas stream for creating reflection silencer |
US7159692B1 (en) * | 1999-10-11 | 2007-01-09 | Silentor Holding A/S | Silencer |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1468398A (en) * | 1921-05-06 | 1923-09-18 | Reed John | Intake silencer for internal-combustion engines |
GB342364A (en) * | 1930-04-30 | 1931-02-05 | Robert Walker | Improvements in or relating to exhaust silencers |
US2016254A (en) * | 1931-08-03 | 1935-10-01 | Noblitt Sparks Ind Inc | Muffler |
US2051675A (en) * | 1933-06-02 | 1936-08-18 | Cecil Gordon Vokes | Apparatus for silencing pulsating gaseous currents |
US2264195A (en) * | 1939-08-16 | 1941-11-25 | Maxim Silencer Co | Silencing device |
US2397208A (en) * | 1941-02-21 | 1946-03-26 | Maxim Silencer Co | Waste heat utilizer |
US2445045A (en) * | 1944-06-26 | 1948-07-13 | Strachan Christopher | Sound-trapping muffler construction |
-
1947
- 1947-05-05 US US745978A patent/US2544284A/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1468398A (en) * | 1921-05-06 | 1923-09-18 | Reed John | Intake silencer for internal-combustion engines |
GB342364A (en) * | 1930-04-30 | 1931-02-05 | Robert Walker | Improvements in or relating to exhaust silencers |
US2016254A (en) * | 1931-08-03 | 1935-10-01 | Noblitt Sparks Ind Inc | Muffler |
US2051675A (en) * | 1933-06-02 | 1936-08-18 | Cecil Gordon Vokes | Apparatus for silencing pulsating gaseous currents |
US2264195A (en) * | 1939-08-16 | 1941-11-25 | Maxim Silencer Co | Silencing device |
US2397208A (en) * | 1941-02-21 | 1946-03-26 | Maxim Silencer Co | Waste heat utilizer |
US2445045A (en) * | 1944-06-26 | 1948-07-13 | Strachan Christopher | Sound-trapping muffler construction |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2675088A (en) * | 1951-11-24 | 1954-04-13 | William B Mcleod | Muffler |
US3144913A (en) * | 1962-08-31 | 1964-08-18 | Garrett Corp | Method and apparatus for attenuating helical acoustic pressure waves |
US3276108A (en) * | 1964-02-21 | 1966-10-04 | Reynolds Metals Co | Method of making a muffler |
US3280903A (en) * | 1964-12-21 | 1966-10-25 | Universal Silencer Corp | Exhaust silencer and heat recovery unit |
FR2349730A1 (en) * | 1976-04-30 | 1977-11-25 | Nihon Radiator Co | EXHAUST |
US5016729A (en) * | 1987-06-18 | 1991-05-21 | Claes Linden | Exhaust system for combustion engine |
US7159692B1 (en) * | 1999-10-11 | 2007-01-09 | Silentor Holding A/S | Silencer |
DE102005025288A1 (en) * | 2005-06-02 | 2006-12-07 | D'alessandro, Luigi | Exhaust gas silencer for e.g. exhaust gas system of water-craft has transverse wall, which is interspersed by two, preferably three pipe lead-through for parallel exhaust gas stream for creating reflection silencer |
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