US2708006A - Muffler assembly for internal combustion engines - Google Patents

Muffler assembly for internal combustion engines Download PDF

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US2708006A
US2708006A US390377A US39037753A US2708006A US 2708006 A US2708006 A US 2708006A US 390377 A US390377 A US 390377A US 39037753 A US39037753 A US 39037753A US 2708006 A US2708006 A US 2708006A
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rotor
section
muffler assembly
exhaust gases
internal combustion
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US390377A
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Backman Hans Fredrik
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    • 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
    • F01N1/16—Silencing apparatus characterised by method of silencing by using movable parts
    • F01N1/18—Silencing apparatus characterised by method of silencing by using movable parts having rotary movement
    • 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
    • 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
    • F01N13/1888—Construction facilitating manufacture, assembly, or disassembly the housing of the assembly consisting of two or more parts, e.g. two half-shells
    • F01N13/1894—Construction facilitating manufacture, assembly, or disassembly the housing of the assembly consisting of two or more parts, e.g. two half-shells the parts being assembled in longitudinal direction
    • 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

Definitions

  • innermost tubular element and the intermediate tubular element or elements is or are provided externally with a circumferential series of radial ribs arranged in uniformly spaced interrelation and longitudinally coextensive with said tubular elements, both said ribs and said intermediate tubular element or elements being made of perforated sheet-metal and said ribs dividing the annular interspaces into a plurality of longitudinally extending gas passages, secondly, the upstream or inlet section, which is connectable at its upstream end to the exhaust pipe of said engine, is provided at its downstream end adjacent to said intermediate section with an insert element comprising a plurality of radially inwardly extending webs provided at their radially outer ends with projections extending axially upstream along, and in contact with, the conically tapering internal casing wall of said inlet section, said insert element being adapted to cause uniform distribution of the exhaust gases into said longitudinal passages, and, thirdly, the rear or outlet section comprises a pluralit
  • the muffler assembly according to the present invention provides an excellent silencing effect, and at the same time the operating efiiciency of the engine will be improved which, in its turn, involves improved fuel economies.
  • muffler assembly may be obtained by resiliently axially displaceably and rotatably mounting an exhaust driven rotor element on a shaft coaxially secured within the innermost tubular element of the intermediate section and having its upstream end projecting into the upstream or inlet section for carrying said rotor at the upstream side of said insert element.
  • Such an arrangement entails, inter alia, a further improved distribution of the exhaust gases into the longitudinal passages, involving improved efficiency of the muffler assembly.
  • a spring is arranged to urge the rotor yieldingly toward the smaller diameter inlet end of the conically convergent inlet section against the flow direction of the exhaust gases. At low engine speeds substantially all of the exhaust gases are thus constrained to flow through the rotor blades. At high engine speeds the increased flow of exhaust gases forces the rotor in a downstream of the internal combustion engine.
  • the rotor thus provides a variable throttling action with respect to the exhaust gases which automatically accommodates itself to the flow rate of the exhaust gases through the muffler.
  • Fig. l is a longitudinal section through the muffler assembly according to this embodiment
  • Fig. 2 is a cross-sectional view thereof taken on line IIII in Fig. 1,
  • Fig. 3 is a cross-sectional view thereof taken on line IHIII in Fig. l, and
  • Fig. 4 is a cross-sectional view of the same taken on line IVIV in Fig. 1.
  • the muffler assembly illustrated therein consists of three sections A, B, and C arranged in series and of which the intermediate section B is composed by a plurality of, and in the present example five, tubular elements 1, 2, 3, 4, and 5 coaxially nested one within the other in radially spaced interrelation.
  • the innermost tubular element 1 and the intervening tubular elements 2, 3, and 4 are provided externally with a plurality of radial ribs 6 circumferentially spaced in uniform distribution and coextensive with the tubular elements 1 to 5, said ribs 6 being, as well as the intermediate tubular elements 2, 3, and 4, made of perforated sheet-metal.
  • the axially extending gas passages 7 formed by these tubular elements and the associated radial ribs 6 are open at both ends at which they communicate with the front or inlet section A and the rear or outlet section C, respectively.
  • the inlet section A the outer casing wall of which, 8, is, in the embodiment illustrated, a continuous extension of the outermost tubular element 5 of the intermediate section B, and consists of an outlet end portion tapering conically in the upstream direction and merging into a cylindrical inlet end portion 9 adapted, in any suitable manner, to be connected to the exhaust pipe (not shown)
  • the front or inlet section A is provided in its outlet end adjacent to the intermediate section B with an insert element consisting of a plurality of inwardly extending radial webs 10 having at their outer upstream ends axially directed extensions 11 which project upstream along, and in contact with, the inner walls of the tapering end portion 8, said webs 10 together with their extensions or projections 11 being made of perforated sheet-metal.
  • This insert element 10, 11 has for its purpose to cause an even distribution of the exhaust gases into the passages 7 of the intermediate section B.
  • a shaft 12 is coaxially secured, said shaft being extended into the inlet section A.
  • a socket member 13 having its upstream end closed and which, through the intermediary ot' a conically divergent portion 14, merges into a sleeve or skirt 15 of larger diameter, said sleeve or skirt being loosely slipped over the innermost tube 1 of the interd mediate section B and both axially slidably and rotatably supported on the shaft 12 by means of a ball bearing 16.
  • these parts 13, 14, 15 forming a hub a rotor 17 comprising a plurality of radial vanes is mounted to be rotated by the action of the engine exhaust gases.
  • a compression coil spring 19 is positioned and is arranged to urge the hub 1314l5 and rotor 17 yieldin ly towards the convergent inlet end of the muffler assembly.
  • the ribs 6 are cut away axially at their bases, adjacent the tubular element 1.
  • the rotor 17 has for its purpose, firstly, to provide a uniform distribution of the exhaust gases, and, secondly, in response to a reduction in the engine speed, to move 'in the upstream direction under the yielding influence of the helical compression spring 19 and thereby bring the periphery of the rotor 17 into closer proximity to the conically tapering inner wall surfaces of the outer casing 3 of the inlet section A.
  • the periphery of the rotor 17 acting in cooperation with the convergent casing 8 constrains a greater portion of the exhaust gases at low engine speeds to pass through the vanes of the rotor 17 than at higher engine speeds when the rotor is forced downstream against the action of spring 19 by the increased pressure of the exhaust gases.
  • the rear or outlet section C of the muflier assembly consists, in part, of a conical outer casing 20 having its end portion adiacent to and communicating with the intermediate mufiier section B, the casing 20 being slipped over the tubular element 5 thereof and secured thereto by bolts 21, and in part by an interiorly disposed cylin drical part 22 in the form of a rearward extension of the tubular member 1. Between these two parts 20 and 22 helically extending partitions 23 are interposed forming helical passages 24 which receive the gases discharged from the passages 7 of the intermediate section B and impart to said gases a vortex motion.
  • the outer casing 20 of the rear section C is provided externally with two diametrically disposed radially and longitudinally extending fins 25 serving as handles for use when assembling and dismantling the muffler assembly.
  • a mufller for silencing the exhaust of an internal combustion engine comprising: intercommunicating inlet, intermediate and outlet sections disposed in axially aligned series relationship, each of said sections comprising a hollow cylindrical casing portion for confining exhaust gases within said mufiier; said inlet section comprising an upstreamwardly disposed portion adapted for connection to the exhaust duct of an internal combustion engine; an insert element disposed within said casing portion of said inlet section and including a plurality of radially inwardly extending webs each provided at its radially outwardly disposed end portion with an axially upstreamwardly directed extension, said webs being arranged to cause effectively uniform distribution of exhaust gases flowing toward said intermediate section; a plurality of coaxially nested tubular members disposed in laterally spaced relationship within said casing portion of said intermediate section, each of said tubular members which is located intermediate said intermediate section casing portion and the innermost of said tubular members being formed of perforated sheet metal; a plurality of spaced
  • a muffler in which the inner surface of said inlet section casing portion tapers conically and convergently toward said upstreamwardly disposed portion thereof, and wherein said rotor is both axially movably and rotatably disposed on said shaft, said mufller further comprising resilient means acting on said rotor and yieldingly urging said rotor upstreamwardly along said shaft toward the reduced diameter portion of said inlet section casing portion for exerting a variable throttling action on exhaust gases passing through said mufiier, said throttling action being reduced with increasing engine speed.

Description

May 10, 1955 H. F. BACKMAN MUFFLER ASSEMBLY FOR INTERNAL COMBUSTION ENGINES Filed Nov. 5, 1953 Hsws Frecoam BAG-KHAN \N VENTo Q a- MY/WM United States Patent 0 MUFFLER ASSEMBLY FOR INTERNAL COMBUSTION ENGINES Hans Fredrik Backman, Alby, Sweden Application November 5, 1953, Serial No. 390,377
4 Claims. (Cl. 181--55) innermost tubular element and the intermediate tubular element or elements is or are provided externally with a circumferential series of radial ribs arranged in uniformly spaced interrelation and longitudinally coextensive with said tubular elements, both said ribs and said intermediate tubular element or elements being made of perforated sheet-metal and said ribs dividing the annular interspaces into a plurality of longitudinally extending gas passages, secondly, the upstream or inlet section, which is connectable at its upstream end to the exhaust pipe of said engine, is provided at its downstream end adjacent to said intermediate section with an insert element comprising a plurality of radially inwardly extending webs provided at their radially outer ends with projections extending axially upstream along, and in contact with, the conically tapering internal casing wall of said inlet section, said insert element being adapted to cause uniform distribution of the exhaust gases into said longitudinal passages, and, thirdly, the rear or outlet section comprises a plurality of axially but slightly helically extending gas passages connecting to said longitudinal passages and opening towards the outlet end of the muffler assembly.
It has been found that, in practice, the muffler assembly according to the present invention provides an excellent silencing effect, and at the same time the operating efiiciency of the engine will be improved which, in its turn, involves improved fuel economies.
According to a further feature of the invention,'a still better operation characteristic of the muffler assembly may be obtained by resiliently axially displaceably and rotatably mounting an exhaust driven rotor element on a shaft coaxially secured within the innermost tubular element of the intermediate section and having its upstream end projecting into the upstream or inlet section for carrying said rotor at the upstream side of said insert element.
Such an arrangement entails, inter alia, a further improved distribution of the exhaust gases into the longitudinal passages, involving improved efficiency of the muffler assembly.
A spring is arranged to urge the rotor yieldingly toward the smaller diameter inlet end of the conically convergent inlet section against the flow direction of the exhaust gases. At low engine speeds substantially all of the exhaust gases are thus constrained to flow through the rotor blades. At high engine speeds the increased flow of exhaust gases forces the rotor in a downstream of the internal combustion engine.
direction against the action of the spring and allows a substantial portion of the exhaust gases to flow past the peripheral edges of the rotor without passing through its blades. The rotor thus provides a variable throttling action with respect to the exhaust gases which automatically accommodates itself to the flow rate of the exhaust gases through the muffler.
The invention will now be described more fully in conjunction with the accompanying drawing illustrating by Way of example a muffler assembly according to a preferred embodiment of the invention, and in which:
Fig. l is a longitudinal section through the muffler assembly according to this embodiment,
Fig. 2 is a cross-sectional view thereof taken on line IIII in Fig. 1,
Fig. 3 is a cross-sectional view thereof taken on line IHIII in Fig. l, and
Fig. 4 is a cross-sectional view of the same taken on line IVIV in Fig. 1.
Referring now to the accompanying drawing, the muffler assembly illustrated therein consists of three sections A, B, and C arranged in series and of which the intermediate section B is composed by a plurality of, and in the present example five, tubular elements 1, 2, 3, 4, and 5 coaxially nested one within the other in radially spaced interrelation. For centering the tubular elements relative to each other the innermost tubular element 1 and the intervening tubular elements 2, 3, and 4 are provided externally with a plurality of radial ribs 6 circumferentially spaced in uniform distribution and coextensive with the tubular elements 1 to 5, said ribs 6 being, as well as the intermediate tubular elements 2, 3, and 4, made of perforated sheet-metal. The axially extending gas passages 7 formed by these tubular elements and the associated radial ribs 6 are open at both ends at which they communicate with the front or inlet section A and the rear or outlet section C, respectively.
The inlet section A, the outer casing wall of which, 8, is, in the embodiment illustrated, a continuous extension of the outermost tubular element 5 of the intermediate section B, and consists of an outlet end portion tapering conically in the upstream direction and merging into a cylindrical inlet end portion 9 adapted, in any suitable manner, to be connected to the exhaust pipe (not shown) The front or inlet section A is provided in its outlet end adjacent to the intermediate section B with an insert element consisting of a plurality of inwardly extending radial webs 10 having at their outer upstream ends axially directed extensions 11 which project upstream along, and in contact with, the inner walls of the tapering end portion 8, said webs 10 together with their extensions or projections 11 being made of perforated sheet-metal. This insert element 10, 11 has for its purpose to cause an even distribution of the exhaust gases into the passages 7 of the intermediate section B.
Within the innermost tubular element 1 of the intermediate section B a shaft 12 is coaxially secured, said shaft being extended into the inlet section A. Onto this shaft 12 is slipped a socket member 13 having its upstream end closed and which, through the intermediary ot' a conically divergent portion 14, merges into a sleeve or skirt 15 of larger diameter, said sleeve or skirt being loosely slipped over the innermost tube 1 of the interd mediate section B and both axially slidably and rotatably supported on the shaft 12 by means of a ball bearing 16. Gr. these parts 13, 14, 15 forming a hub a rotor 17 comprising a plurality of radial vanes is mounted to be rotated by the action of the engine exhaust gases. Between the axially slidable ball bearing 16 and a collar 18 on the shaft 12 a compression coil spring 19 is positioned and is arranged to urge the hub 1314l5 and rotor 17 yieldin ly towards the convergent inlet end of the muffler assembly. In order to enable the sleeve of the hub to move freely over and around the tubular element 1, as will appear from Fig. l, the ribs 6 are cut away axially at their bases, adjacent the tubular element 1.
The rotor 17 has for its purpose, firstly, to provide a uniform distribution of the exhaust gases, and, secondly, in response to a reduction in the engine speed, to move 'in the upstream direction under the yielding influence of the helical compression spring 19 and thereby bring the periphery of the rotor 17 into closer proximity to the conically tapering inner wall surfaces of the outer casing 3 of the inlet section A. The periphery of the rotor 17 acting in cooperation with the convergent casing 8 constrains a greater portion of the exhaust gases at low engine speeds to pass through the vanes of the rotor 17 than at higher engine speeds when the rotor is forced downstream against the action of spring 19 by the increased pressure of the exhaust gases. As the rotor 17 'moves downstream, a greater portion of the exhaust gases are permitted to flow past the periphery of rotor 17 as the diameter of the casing 8 progressively increases. An automatic variable throttling action is thus obtained. In order to take up axial thrust when the rotor 17 is in its extreme downstream position, as shown in Fig. 1, a ball 26 is disposed in the socket 13 between the upstream ends of shaft 12 and socket 13, the ball 26 serving to limit the downstream movement of the rotor 17.
- The rear or outlet section C of the muflier assembly consists, in part, of a conical outer casing 20 having its end portion adiacent to and communicating with the intermediate mufiier section B, the casing 20 being slipped over the tubular element 5 thereof and secured thereto by bolts 21, and in part by an interiorly disposed cylin drical part 22 in the form of a rearward extension of the tubular member 1. Between these two parts 20 and 22 helically extending partitions 23 are interposed forming helical passages 24 which receive the gases discharged from the passages 7 of the intermediate section B and impart to said gases a vortex motion. In the embodiment illustrated, the outer casing 20 of the rear section C is provided externally with two diametrically disposed radially and longitudinally extending fins 25 serving as handles for use when assembling and dismantling the muffler assembly.
It will be understood that the invention is not restricted to the embodiment specifically described in the foregoing and illustrated in the accompanying drawing since the same is susceptible of various modifications without departing from its scope as defined in the appended claims.
Having now particularly described the nature of my invention and the manner of its operation What I claim is:
1. A mufller for silencing the exhaust of an internal combustion engine, said muffler comprising: intercommunicating inlet, intermediate and outlet sections disposed in axially aligned series relationship, each of said sections comprising a hollow cylindrical casing portion for confining exhaust gases within said mufiier; said inlet section comprising an upstreamwardly disposed portion adapted for connection to the exhaust duct of an internal combustion engine; an insert element disposed within said casing portion of said inlet section and including a plurality of radially inwardly extending webs each provided at its radially outwardly disposed end portion with an axially upstreamwardly directed extension, said webs being arranged to cause effectively uniform distribution of exhaust gases flowing toward said intermediate section; a plurality of coaxially nested tubular members disposed in laterally spaced relationship within said casing portion of said intermediate section, each of said tubular members which is located intermediate said intermediate section casing portion and the innermost of said tubular members being formed of perforated sheet metal; a plurality of spaced substantially uniformly peripherally disposed spacing members formed of perforated sheet metal and interconnecting said intermediate section casing portion and adjacent ones of said tubular members for maintaining said tubular members and said casing portion in said spaced coaxial relationship, said spacing members being axially coextensive with said tubular members and defining with said tubular members and said casing portion a plurality of longitudinally extending gas passages extending through said intermediate section; and a plurality of slightly helic'ally disposed partition members comprised within said outlet section and defining with the casing portion thereof a plurality of gas passages communicating with said gas passages of said intermediate section and with the atmosphere.
2. A muffler as claimed in claim 1, in which said webs and their extensions of said insert element are formed of perforated sheet-metal.
3. A mufiier as claimed in claim 1, further comprising an exhaust driven rotor element, and a shaft coaxially secured within the innermost tubular member of said intermediate section and having its upstream end projecting into said inlet section, said rotor being rotatably disposed on said shaft at the upstream side of said insert element.
4. A muffler according to claim 3, in which the inner surface of said inlet section casing portion tapers conically and convergently toward said upstreamwardly disposed portion thereof, and wherein said rotor is both axially movably and rotatably disposed on said shaft, said mufller further comprising resilient means acting on said rotor and yieldingly urging said rotor upstreamwardly along said shaft toward the reduced diameter portion of said inlet section casing portion for exerting a variable throttling action on exhaust gases passing through said mufiier, said throttling action being reduced with increasing engine speed.
References Cited in the file of this patent UNITED STATES PATENTS 1,535,787 Ragany Apr. 28, 1925 1,840,082 Breer Jan. 5, 1932 2,348,706 Batchelor et al May 16, 1944 2,514,520 Sauer July 11, 1950 2,646,854 Walker July 28, 1953
US390377A 1953-11-05 1953-11-05 Muffler assembly for internal combustion engines Expired - Lifetime US2708006A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2214855A1 (en) * 1973-01-22 1974-08-19 Aerospatiale
FR2507736A1 (en) * 1981-06-11 1982-12-17 Fisher Controls Int DEVICE FOR ATTENUATING THE NOISE OF A NON-SYMMETRIC TURBULENT FLOWING FLUID IN RELATION TO AN AXIS
US6415887B1 (en) 1999-11-26 2002-07-09 Cr Patents, Inc. Refractive wave muffler
US20040163887A1 (en) * 2003-02-25 2004-08-26 Ziehl John C. Exhaust silencer system
US20050045418A1 (en) * 2003-08-25 2005-03-03 Michael Choi Noise attenuation device for a vehicle exhaust system
US20050155819A1 (en) * 2004-01-21 2005-07-21 Kelly Libby Anti-reversion apparatus
US20050194206A1 (en) * 2004-03-03 2005-09-08 Marco Rose Arrangement for the generation of sonic fields of a specific modal composition
US20060243336A1 (en) * 2005-04-13 2006-11-02 Ingenieria Equipos Y Control Ltda Anti-cavitation system in pipelines which avoids that the fluid reaches its vapour pressure at the output of a given contraction using a device that connects the output section of the contraction with its downstream pressure
US7131514B2 (en) * 2003-08-25 2006-11-07 Ford Global Technologies, Llc Noise attenuation device for a vehicle exhaust system
US20070128998A1 (en) * 2005-12-05 2007-06-07 Denso Corporation Air conditioner and air conditioner duct
US20190093791A1 (en) * 2017-09-27 2019-03-28 Fisher Controls International Llc Flow stabilizer for a control valve

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1535787A (en) * 1924-11-25 1925-04-28 Ragany John Muffler
US1840082A (en) * 1927-05-28 1932-01-05 Chrysler Corp Muffler
US2348706A (en) * 1943-06-09 1944-05-16 Frederick K Batchelor Muffler
US2514520A (en) * 1946-06-03 1950-07-11 Harry R Levy Muffler with divided flow passages
US2646854A (en) * 1948-09-22 1953-07-28 Walker George Bromhead Baffle type muffler having a plurality of helical passages

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1535787A (en) * 1924-11-25 1925-04-28 Ragany John Muffler
US1840082A (en) * 1927-05-28 1932-01-05 Chrysler Corp Muffler
US2348706A (en) * 1943-06-09 1944-05-16 Frederick K Batchelor Muffler
US2514520A (en) * 1946-06-03 1950-07-11 Harry R Levy Muffler with divided flow passages
US2646854A (en) * 1948-09-22 1953-07-28 Walker George Bromhead Baffle type muffler having a plurality of helical passages

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2214855A1 (en) * 1973-01-22 1974-08-19 Aerospatiale
FR2507736A1 (en) * 1981-06-11 1982-12-17 Fisher Controls Int DEVICE FOR ATTENUATING THE NOISE OF A NON-SYMMETRIC TURBULENT FLOWING FLUID IN RELATION TO AN AXIS
WO1982004470A1 (en) * 1981-06-11 1982-12-23 Fisher Controls Int Eccentrically nested tube gas line silencer
US4402485A (en) * 1981-06-11 1983-09-06 Fisher Controls Company, Inc. Eccentrically nested tube gas line silencer
US6415887B1 (en) 1999-11-26 2002-07-09 Cr Patents, Inc. Refractive wave muffler
US6868939B2 (en) * 2003-02-25 2005-03-22 Vicious Cycle Performance, Inc. Exhaust silencer system
US20040163887A1 (en) * 2003-02-25 2004-08-26 Ziehl John C. Exhaust silencer system
US7131514B2 (en) * 2003-08-25 2006-11-07 Ford Global Technologies, Llc Noise attenuation device for a vehicle exhaust system
US7086498B2 (en) * 2003-08-25 2006-08-08 Ford Global Technologies, Llc Noise attenuation device for a vehicle exhaust system
US20050045418A1 (en) * 2003-08-25 2005-03-03 Michael Choi Noise attenuation device for a vehicle exhaust system
US20050155819A1 (en) * 2004-01-21 2005-07-21 Kelly Libby Anti-reversion apparatus
US20050194206A1 (en) * 2004-03-03 2005-09-08 Marco Rose Arrangement for the generation of sonic fields of a specific modal composition
US7516815B2 (en) * 2004-03-03 2009-04-14 Roll-Royce Deutschland Ltd & Co Kg Arrangement for the generation of sonic fields of a specific modal composition
US20060243336A1 (en) * 2005-04-13 2006-11-02 Ingenieria Equipos Y Control Ltda Anti-cavitation system in pipelines which avoids that the fluid reaches its vapour pressure at the output of a given contraction using a device that connects the output section of the contraction with its downstream pressure
US20070128998A1 (en) * 2005-12-05 2007-06-07 Denso Corporation Air conditioner and air conditioner duct
US7654099B2 (en) * 2005-12-05 2010-02-02 Denso Corporation Air conditioner and air conditioner duct
US20190093791A1 (en) * 2017-09-27 2019-03-28 Fisher Controls International Llc Flow stabilizer for a control valve
US10495234B2 (en) * 2017-09-27 2019-12-03 Fisher Controls International Llc Flow stabilizer for a control valve

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