US2656005A - Retroverted passage type muffler with resonator chambers - Google Patents

Retroverted passage type muffler with resonator chambers Download PDF

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US2656005A
US2656005A US88799A US8879949A US2656005A US 2656005 A US2656005 A US 2656005A US 88799 A US88799 A US 88799A US 8879949 A US8879949 A US 8879949A US 2656005 A US2656005 A US 2656005A
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tube
conduit
section
resonator
casing
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US88799A
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Beecher B Cary
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HAYES IND
HAYES INDUSTRIES
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HAYES IND
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    • 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
    • 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
    • F01N1/08Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
    • F01N1/084Silencing 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
    • 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
    • F01N2450/20Methods or apparatus for fitting, inserting or repairing different elements by mechanical joints, e.g. by deforming housing, tube, baffle plate or parts thereof
    • 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
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/02Two or more expansion chambers in series connected by means of tubes
    • F01N2490/06Two or more expansion chambers in series connected by means of tubes the gases flowing longitudinally from inlet to outlet in opposite directions
    • 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

Definitions

  • This invention relates to retroverted passage type mu termers and more particularly to such as are used in connection with internal combustion engines for attenuating the sound of the exhaust.
  • An object of the invention is to provide an improved construction of retroverted type of mufiier which is of simplified yet efficient construction and gives desirable sound damping or attenuating possibilities for a wide range of operating conditions.
  • Another object of the invention is to provide an acoustically tuned muffler which incorporates a. tortuous gas conduit and associated wave filter and compounded resonator chambers in a novel and efficient assembly.
  • Fig. I is a longitudinal section of a mufiler construction in accordance with the invention
  • Fig. II is an end view of Fig. I, looking on the left end thereof,
  • Fig. III is an end view looking onthe right end of Fig. I,
  • Fig. IV is a transverse section on the line A-A of Fig. I,
  • Fig. V is an enlarged fragmentary cross section on the 1ine BB of Fig. VI and showing a preferred construction of the louvres provided on the gas conduits, and
  • Fig. VI is a section on the line C-C of Fig. V.
  • the mufiier comprises an outer and main casing l0, which is conveniently of oval shape in cross-section, as seen in Figs. II-IV, and has end header plates I2 and I4 and intermediate axially spaced partition plates I6, I8 and 20, these plates defining resonator chambers 22, 24 and 26'.
  • the end header plate I2 has an opening 28 in which a straight conduit section 30 is supported with its end extension 30a, while the other end header plate I4 has an opening 32 in which another straight conduit section 34 is supported with its end extension 34a.
  • Thend extension 30a can be employed to constitute the inlet end of the mufiler, with the latter so hooked-up to the engine exhaust system and with the end extension 3411 constituting the out let end of the mufller. It is possible, however, to reverse this connection and so employ the end extension 34a as inlet'and the end extension 30a as outlet.
  • the two conduit sections 34 and 36 are itnerconnected by an elbow section 38, whereas the opposite end of the conduit section 36 and also the corresponding end of the conduit section 30, open into the resonator chamber 24.
  • the latter is placed in compounding relationship with respect to the adjacent resonator chamber 26, as by the partition plate 20 being provided with a series of perforations 40, or alternatively with a tube section 42, while the elbow connection 38 is also placed in communication with the resonator chamber 22 by the tube section 44.
  • That portion 34b of the tube section 34 which extends between the partition plates I6 and I8 is enclosed within an encircling imperforate tube 46 secured at its ends, as by welding, to the said partition plates and defining an enclosed annular acoustic wave filter chamber 48 into which gases conveyed along the tube portion 3412 can pass through the louvre portion of this tube portion and indicated generally at 50 in Fig. I.
  • the tube section 36 and also the portion 30a of the tube section 30 are provided with louvre portions indicated generally at SI and 52 in Fig. I, and through which louvre portions these. tube are able to discharge into a pair of wave filter chambers 54 and 56 defined about the tubes section 36, andthe tube'portions 39a and 34b as seen in Fig. IV.
  • Such chambers 54 and 56 are of substantially semi-annular shape and are conveniently defined by elongated web portions 58 bent radially outwards from opposite.
  • the said louvre portions are preferablyformed by piercing the corresponding tube surfaces along.
  • the length and diameter of the tube section 44 can be varied to alter the acoustic characteristic of the resonator chamber 22, while a similar adjustment is possible with respect to the size and number of the perforations 40 in the common partition plate 22 of the compounded resonator assembly 2 and 23, or with respect to the length and diameter or the tube section 42, if employed.
  • the gas flow will take place along the tube section 30 and discharge into the resonator chamber E l, with an attendant filtering action through the louvre portion 5! int the chamber
  • the gases can surge bacl; and forth into the resonator chamber via the perforations 40, or the tube t2, and enter the tube section 36, from which the gases can filter through the louvre portion into the chamber 54.
  • tion provides a very compact and relatively plified mufiler construction which can be readily manufactured and assembled and which provides a number of acoustic tuning or adjustment possibilities, while at the same time making maximum use of the available casing space in the provision of a retroverted conduit and associated filter and resonator chambers.
  • the retroverted conduit is of substantially the same general cross sectional area throughout its length and the entire gas conducting assembly is such as provides for unrestricted flow and the elimination of any undue back pressure.
  • the proportions of the acustic wave attenuating structure will, of course, vary, depending upon particular requirements and practical considerations.
  • the filter chambers 54, E58 and :38 are proportioned to attenuate the higher frequency wave ranges or hands and the resonator chambers 22, 22 and 28 are proportioned and tuned to attenuate th lower frequency ranges or bands.
  • the compounding of the resonator chambers 24 and 26 materially increases the attenuating characteristics of the muffler and leads to increased efilciency and compactness of construction.
  • An acoustically tuned muflier construction comprising in combination, an outer elongated hollow casing, end header plates at opposite ends of said casing, each said header plate having an opening therein, a first partition plate within the casing in axially spaced adjacent relationship to one said header plate and defining with the latter an end resonator chamber, a second partition plate within the casing in axially spaced relationship both to the other header plate and to said first partition plate and defining with the latter the opposite end Walls of a compounded resonator chamber assembly, an intermediat partition plate in said compounded resonator chamber assembly and defining adjacent resonator chambers at the end of the casing remote from the end containing said first mentioned resonator chamber, means placing said adjacent resonator chambers in gas fiow compounding relationship, a first tube section extending within the casing interior from one end thereof and mounted in the header plate at such end and in said first and second partition plates, a second tube section extending within the casing from its opposite end and mounted
  • An acoustically tuned muffler construction comprising an elongated hollow casing, a gas flow conduit mounted in said casing with axial extending portions in r troverted arrangement within the latter, transverse interior partition plates in said casing defining an intermediate space surrounding portions of said conduit, axially extending acoustic wave attenuating structure embracing said conduit portions, and axially extending bafiie means disposed between the sides of said casing and constituting a partition between certain of said conduit portions for dividing said intermediate space into two separate compartments.

Description

B. B. CARY Oct. 20, 1953 RETROVERTED PASSAGE TYPE MUFFLER WITH RESONATOR CHAMBERS Filed April 21, 1949 55.5mm? 5. CARY 3 Patented Oct. 20, 1953 RETROVERTED PASSAGE TYPE MUFFLER WITH RESONATOR CHAMBERS Beecher B. Cary, Jackson, Mich., assignor to Hayes Industries, Jackson, Mich., a corporation.
of Michigan Application April 21, 1949, Serial N 0. 88,799
This invention relates to retroverted passage type muiilers and more particularly to such as are used in connection with internal combustion engines for attenuating the sound of the exhaust.
An object of the invention is to provide an improved construction of retroverted type of mufiier which is of simplified yet efficient construction and gives desirable sound damping or attenuating possibilities for a wide range of operating conditions.
Another object of the invention is to provide an acoustically tuned muffler which incorporates a. tortuous gas conduit and associated wave filter and compounded resonator chambers in a novel and efficient assembly.
Further objects and advantages, residing in the construction, arrangement and combination of features and structural parts of the muffler will become apparent and clear from a consideration of the following detailed description with reference to the accompanying drawings in which- Fig. I is a longitudinal section of a mufiler construction in accordance with the invention,
Fig. II is an end view of Fig. I, looking on the left end thereof,
Fig. III is an end view looking onthe right end of Fig. I,
Fig. IV is a transverse section on the line A-A of Fig. I,
Fig. V is an enlarged fragmentary cross section on the 1ine BB of Fig. VI and showing a preferred construction of the louvres provided on the gas conduits, and
Fig. VI is a section on the line C-C of Fig. V.
Referring to the drawings, the mufiier comprises an outer and main casing l0, which is conveniently of oval shape in cross-section, as seen in Figs. II-IV, and has end header plates I2 and I4 and intermediate axially spaced partition plates I6, I8 and 20, these plates defining resonator chambers 22, 24 and 26'.
The end header plate I2 has an opening 28 in which a straight conduit section 30 is supported with its end extension 30a, while the other end header plate I4 has an opening 32 in which another straight conduit section 34 is supported with its end extension 34a.
Thend extension 30a can be employed to constitute the inlet end of the mufiler, with the latter so hooked-up to the engine exhaust system and with the end extension 3411 constituting the out let end of the mufller. It is possible, however, to reverse this connection and so employ the end extension 34a as inlet'and the end extension 30a as outlet.
2 Claims. (01. 18154) The two conduit sections 30 and 34 extend in axial and parallel relationship into the casing interior and are supported therein by passage through suitable openings in the partition plates I6, I8 and 26. as is clearly seen in Fig. I, where the inner end portions of these conduit sections are shown in overlapped relationship and as extending in opposite directions between the partition plates I6 and I8, while the latter are also shown as supporting between them a third straight conduit section 36.
At one end, the two conduit sections 34 and 36 are itnerconnected by an elbow section 38, whereas the opposite end of the conduit section 36 and also the corresponding end of the conduit section 30, open into the resonator chamber 24. The latter is placed in compounding relationship with respect to the adjacent resonator chamber 26, as by the partition plate 20 being provided with a series of perforations 40, or alternatively with a tube section 42, while the elbow connection 38 is also placed in communication with the resonator chamber 22 by the tube section 44.
That portion 34b of the tube section 34 which extends between the partition plates I6 and I8 is enclosed within an encircling imperforate tube 46 secured at its ends, as by welding, to the said partition plates and defining an enclosed annular acoustic wave filter chamber 48 into which gases conveyed along the tube portion 3412 can pass through the louvre portion of this tube portion and indicated generally at 50 in Fig. I.
The tube section 36 and also the portion 30a of the tube section 30 are provided with louvre portions indicated generally at SI and 52 in Fig. I, and through which louvre portions these. tube are able to discharge into a pair of wave filter chambers 54 and 56 defined about the tubes section 36, andthe tube'portions 39a and 34b as seen in Fig. IV. Such chambers 54 and 56 are of substantially semi-annular shape and are conveniently defined by elongated web portions 58 bent radially outwards from opposite.
sides of the imperforate tube 46 in the formation of the latter from half sections of sheet metal and weld connected, for instance, at 80, to the inside of the outer casing. III, all as clearly shown in Fig. IV.
The said louvre portions are preferablyformed by piercing the corresponding tube surfaces along.
short parallel lines and deflecting the thus defined tube portion 52 outwardly to define an arch, as is clearlyseen in Figs. IV, V and VI, with side openings 64 between the curved anchored ends 66 of the portion 62, which ends 66 merge into the general contour of the corresponding tube surface. Such louvre construction is preferable to mere perforations since it does not create objectionable high frequency sounds and enables the acoustic wave attenuating characteristics to be varied simply by regulating the height of the arches defined by the outwardly bent tube portions 62.
The length and diameter of the tube section 44 can be varied to alter the acoustic characteristic of the resonator chamber 22, while a similar adjustment is possible with respect to the size and number of the perforations 40 in the common partition plate 22 of the compounded resonator assembly 2 and 23, or with respect to the length and diameter or the tube section 42, if employed.
In operation, and assuming that the mufiier is connected in the exhaust gas circuit of an internal combustion engin with the inlet end 30c, the gas flow will take place along the tube section 30 and discharge into the resonator chamber E l, with an attendant filtering action through the louvre portion 5! int the chamber In the resonator chamber 22 the gases can surge bacl; and forth into the resonator chamber via the perforations 40, or the tube t2, and enter the tube section 36, from which the gases can filter through the louvre portion into the chamber 54. From the tube section as the gases fiow the elbow 38, wherein there is a surging possicility through the tube 20 into the resonator chamber 22, and from this el ow connection the flow into the tube portion 34b for delivery along the tube section 34 to the outlet connection While in the tube portion 3472 the gases are permitted to filter through the louvre into the enclosed air space constituted by the ch? It will be appreciated therefore that tion provides a very compact and relatively plified mufiler construction which can be readily manufactured and assembled and which provides a number of acoustic tuning or adjustment possibilities, while at the same time making maximum use of the available casing space in the provision of a retroverted conduit and associated filter and resonator chambers. The retroverted conduit is of substantially the same general cross sectional area throughout its length and the entire gas conducting assembly is such as provides for unrestricted flow and the elimination of any undue back pressure.
The proportions of the acustic wave attenuating structure will, of course, vary, depending upon particular requirements and practical considerations. In general, with the acoustic range of the exhaust system determined by a Wave frequency analyzer, the filter chambers 54, E58 and :38 are proportioned to attenuate the higher frequency wave ranges or hands and the resonator chambers 22, 22 and 28 are proportioned and tuned to attenuate th lower frequency ranges or bands. The compounding of the resonator chambers 24 and 26 materially increases the attenuating characteristics of the muffler and leads to increased efilciency and compactness of construction.
Having thus described the invention, What it is desired to protect by Letters Patent and claim is:
1. An acoustically tuned muflier construction comprising in combination, an outer elongated hollow casing, end header plates at opposite ends of said casing, each said header plate having an opening therein, a first partition plate within the casing in axially spaced adjacent relationship to one said header plate and defining with the latter an end resonator chamber, a second partition plate within the casing in axially spaced relationship both to the other header plate and to said first partition plate and defining with the latter the opposite end Walls of a compounded resonator chamber assembly, an intermediat partition plate in said compounded resonator chamber assembly and defining adjacent resonator chambers at the end of the casing remote from the end containing said first mentioned resonator chamber, means placing said adjacent resonator chambers in gas fiow compounding relationship, a first tube section extending within the casing interior from one end thereof and mounted in the header plate at such end and in said first and second partition plates, a second tube section extending within the casing from its opposite end and mounted in the header plate at such end as well as in said first and second partition plates, said conduit sections having laterally spaced end portions extending in opposite directions between said first and second partition plates, one said conduit being in communication with said compounded resonator chamber assembly, a third conduit section extending between and mounted on said first and second partition plates in laterally spaced relationship to said first and second conduit sections, means connecting said second and third conduit sections in gas flow communication at the first said partition plate to define a re-...Verted conduit, said third conduit section bein in open communication with the compounded resonator chamber assembly at the end thereof adjacent said second partition plate, a tube enclosing the portion of said second conduit section extending between said first and second partition plates, means connecting said tube with opposite sides of the casing interior to define separate acoustic wave attenuating chamber portions embracing said third conduit section and the portion of the first said conduit section which extends between said partition plates.
2. An acoustically tuned muffler construction comprising an elongated hollow casing, a gas flow conduit mounted in said casing with axial extending portions in r troverted arrangement within the latter, transverse interior partition plates in said casing defining an intermediate space surrounding portions of said conduit, axially extending acoustic wave attenuating structure embracing said conduit portions, and axially extending bafiie means disposed between the sides of said casing and constituting a partition between certain of said conduit portions for dividing said intermediate space into two separate compartments.
BEECHER B. CARY.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,018,084 Oldberg ct. 22, 1935 2,022,099 Oldberg Dec. 3, 1935 2,109,220 i'ioblitt et a1 Feb. 22, 1938 2,182,945 Gunn Dec. 12, 1939 2,194,550 Hector et a1 Mar. 22, 1940 2,235,705 Haas Mar. 8, 1941 2,337,300 Noblitt Dec. 21, 1943 2,357,791 Powers Sept. 5, i944 FOREIGN PATENTS Number Country Date 109,785 Australia Feb. 22, 1940
US88799A 1949-04-21 1949-04-21 Retroverted passage type muffler with resonator chambers Expired - Lifetime US2656005A (en)

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2934161A (en) * 1955-11-28 1960-04-26 Walker Mfg Co Muffler
US2950777A (en) * 1956-08-01 1960-08-30 Oldberg Mfg Company Silencer or muffler
US3036654A (en) * 1957-09-18 1962-05-29 Walter Mfg Company Muffler construction
US3087580A (en) * 1959-10-12 1963-04-30 Walker Mfg Co Muffler
US3235244A (en) * 1963-09-13 1966-02-15 Gen Tire & Rubber Co Energy absorbing device for dock bumpers
US3841435A (en) * 1973-02-05 1974-10-15 Tenneco Inc Swaged tri-flow muffler
US20070051556A1 (en) * 2005-09-02 2007-03-08 Arvin Technologies, Inc. Exhaust system with external Helmholtz resonator and associated method
US20070062757A1 (en) * 2005-09-21 2007-03-22 Arvin Technologies, Inc. Pressed assembly for passive valve installation
EP1843018A1 (en) * 2006-04-04 2007-10-10 J. Eberspächer GmbH & Co. KG Silencer
CN106368783A (en) * 2016-09-26 2017-02-01 南京航空航天大学 Full-frequency-band large noise elimination quantity absolute silencer for automobile NVH experiment

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2018084A (en) * 1934-09-24 1935-10-22 Oldberg Sidney Silencer
US2022899A (en) * 1934-10-08 1935-12-03 Oldberg Sidney Silencer
US2109220A (en) * 1936-04-11 1938-02-22 Noblitt Sparks Ind Inc Muffler
US2182945A (en) * 1937-07-30 1939-12-12 Walker Mfg Co Exhaust silencer
US2194550A (en) * 1937-06-23 1940-03-26 Buffalo Pressed Steel Company Muffler
US2235705A (en) * 1939-08-29 1941-03-18 Mackenzie Muffler Company Inc Muffler
US2337300A (en) * 1941-09-02 1943-12-21 Noblitt Sparks Ind Inc Muffler
US2357791A (en) * 1941-03-24 1944-09-05 Walker Mfg Company Of Wisconsi Silencer

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2018084A (en) * 1934-09-24 1935-10-22 Oldberg Sidney Silencer
US2022899A (en) * 1934-10-08 1935-12-03 Oldberg Sidney Silencer
US2109220A (en) * 1936-04-11 1938-02-22 Noblitt Sparks Ind Inc Muffler
US2194550A (en) * 1937-06-23 1940-03-26 Buffalo Pressed Steel Company Muffler
US2182945A (en) * 1937-07-30 1939-12-12 Walker Mfg Co Exhaust silencer
US2235705A (en) * 1939-08-29 1941-03-18 Mackenzie Muffler Company Inc Muffler
US2357791A (en) * 1941-03-24 1944-09-05 Walker Mfg Company Of Wisconsi Silencer
US2337300A (en) * 1941-09-02 1943-12-21 Noblitt Sparks Ind Inc Muffler

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2934161A (en) * 1955-11-28 1960-04-26 Walker Mfg Co Muffler
US2950777A (en) * 1956-08-01 1960-08-30 Oldberg Mfg Company Silencer or muffler
US3036654A (en) * 1957-09-18 1962-05-29 Walter Mfg Company Muffler construction
US3087580A (en) * 1959-10-12 1963-04-30 Walker Mfg Co Muffler
US3235244A (en) * 1963-09-13 1966-02-15 Gen Tire & Rubber Co Energy absorbing device for dock bumpers
US3841435A (en) * 1973-02-05 1974-10-15 Tenneco Inc Swaged tri-flow muffler
US20070051556A1 (en) * 2005-09-02 2007-03-08 Arvin Technologies, Inc. Exhaust system with external Helmholtz resonator and associated method
US7870930B2 (en) * 2005-09-02 2011-01-18 Emcon Technologies Llc Exhaust system with external helmholtz resonator and associated method
US20070062757A1 (en) * 2005-09-21 2007-03-22 Arvin Technologies, Inc. Pressed assembly for passive valve installation
US7575096B2 (en) * 2005-09-21 2009-08-18 Emcon Technologies Llc Pressed assembly for passive valve installation
EP1843018A1 (en) * 2006-04-04 2007-10-10 J. Eberspächer GmbH & Co. KG Silencer
CN101050721B (en) * 2006-04-04 2010-12-01 J.埃贝斯佩歇合资公司 Silencer
CN106368783A (en) * 2016-09-26 2017-02-01 南京航空航天大学 Full-frequency-band large noise elimination quantity absolute silencer for automobile NVH experiment

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