US2557687A - Baffle type exhaust silencer - Google Patents

Baffle type exhaust silencer Download PDF

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US2557687A
US2557687A US23413A US2341348A US2557687A US 2557687 A US2557687 A US 2557687A US 23413 A US23413 A US 23413A US 2341348 A US2341348 A US 2341348A US 2557687 A US2557687 A US 2557687A
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flutes
shell
dissipator
exhaust silencer
silencer
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Omer J Rainville
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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
    • F01N13/1838Construction 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
    • F01N13/1844Mechanical joints
    • 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
    • F01N1/085Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling using a central core throttling gas passage
    • 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
    • F01N1/086Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling having means to impart whirling motion to the gases
    • F01N1/088Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling having means to impart whirling motion to the gases using vanes arranged on gas flow path or gas flow tubes with tangentially directed apertures
    • 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
    • F01N2240/00Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being
    • F01N2240/20Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being a flow director or deflector
    • 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
    • F01N2260/00Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/18Exhaust treating devices having provisions not otherwise provided for for improving rigidity, e.g. by wings, ribs
    • 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
    • F01N2450/22Methods or apparatus for fitting, inserting or repairing different elements by welding or brazing
    • 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
    • F01N2450/24Methods or apparatus for fitting, inserting or repairing different elements by bolts, screws, rivets or the like
    • 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
    • F01N2470/02Tubes being perforated
    • F01N2470/04Tubes being perforated characterised by shape, disposition or dimensions of apertures
    • 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
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/20Dimensional characteristics of tubes, e.g. length, diameter
    • 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
    • F01N2470/24Concentric tubes or tubes being concentric to housing, e.g. telescopically assembled

Definitions

  • This invention relates to certain new and useful improvements in exhaust silencers of the type generally employed with internal combustion engines for silencing or muiiling the discharge of products of combustion from such engines, and also relates to certain new and useful component parts of said silencers.
  • a new form of exhaust silencer of the class described which is so constructed as to give a maximum of silencing effect while presenting a minimum of interference to the gases passing through it; the provision of a new form of exhaust silencer so arranged in its component parts as to effectively silence so-called back-fires from the engine; the provision of an exhaust silencer of the class described which is simple to construct and which because of its simplicity may be readily adapted to existing types of internal combustion engines; the provision of a component part for an exhaust silencer which may readily be inserted in the exhaust tubes of internal combustion engines which are ordinarily not equipped with silencers, thereby to muifie and silence effectively the exhaust noise of such engines; and the provision of an exhaust silencer, and its component parts, which is economical to construct and efficient its operation.
  • Figure l is a longitudinal sectional view of one form of the exhaust silencer of the present invention.
  • Figures 2, 3, and 4 are cross-sectional views taken on lines 2-2, 33, and 44 respectively of Figure 1;
  • Figure 5 is an end perspective view looking into the silencer of Figure 1 from line 22;
  • Figure 6 is a longitudinal sectional view of one of the flutes of the present invention.
  • Figure 7 is a fragmentary longitudinal crosssection of a. part of this invention, in order to show more clearly certain relationship of parts;
  • Figure 8 is an end view of Figure 1, to illustrate more clearly certain portions of the silencer
  • Figure 9- is a cross-sectional broken view to illustrate another embodiment of this invention
  • Figure 10 is a cross-sectional view taken. along lines l8l ll of Figure 9;
  • Figure 11 is a perspective view of a part of the Figure 9 embodiment, to show more clearly certain features of construction.
  • casing I is tubular, preferably cylindrical in shape, but may have other shapes in cross-section if desired, such as hexagonal, for example. It will be noted that casing I is open throughout its length, and that it has an inlet or forward end indicated generally by 2 and an exit end indicated generally by 3.
  • a gas dissipator element comprising a tubular shell indicated generallv by 4.
  • Shell 4 may be made of one piece, if desired, but for ease in stamping certain perforations in the shell (later to be described), I prefer to use a 3-piece construction as shown. by the cross-sectional views, Figures 2, 3 and 4.
  • shell 4 is made up of three elongated members 5, 6 and 1, each member being as shown and comprising approximately the circumference of the shell 4.
  • Members 5, 6 and l are formed with turned outward flanges 8 thereon, which flanges serve, by means of spot welding or riveting, as meansto fasten members 5, 6 and I together to form the complete tubular shell 4.
  • Flanges 8 extend outwardly from shell 4 a distance not greater than 2. the approximate diameter of shell 4, and these joined flanges thus form ribs 9, l0, and H, running the length of the shell and serving as spacing and mounting means for shell 4 with- 3 in casing I.
  • the inside diameter of casing I is such that the outer edges of ribs 9, Ii) and II bear snugly with a good friction fit against the inside wall of casing I, thus holding shell 4 firmly in place.
  • Shell 6 is provided at its entrance end with an outwardly-flared riin 28 which fits snugly casing I.
  • the shell 4 is provided with a series of openings I2 throughout its length, and said openings I2 are preferably arranged in groups, with the openings of each group successively increasing in size toward the exit end of the silencer.
  • the openings of each circular series are in staggered relation with respect to the openings in adjacent series.
  • each of said openings I2 Projecting inwardly toward the center of shell 4 are flutes I3, each of said openings I2 having one flute attached to that portion of its edge which is toward the exit end 3 of the silencer.
  • said flutes gradually increase in size in a adjacent the exit end of the shell 4. It will also be noted that said flutes incline forwardly, and
  • the flutes I3 may be formed separately and attached to the shell in their proper positions as by spot welding or riveting, if desired.
  • Figure 5 illustrates the perspective appearance of the silencer if looking into the entrance end, and illustrates the above-mentioned staggering of openings I 2 to provide overlapping of the flutes as to any gases flowing against the flutes.
  • Flutes I3 are spoon shaped and are so positioned as to be concaved inwardly as shown in Figure 6, which is an enlarged drawing for purposes of clarity.
  • the forward portion (indicated at I4) of each flute is narrower than the rearward portion (indicated at I5) attached to shell 4.
  • I have found that by making the flutes spoon shaped and concaved inwardly as shown, each flute scoops out of the exhaust gas flowing past it a portion and directs substantially all of that portion outward through the respective opening and to the inside wall of casing I. By doing this the sound energy of the gas is effectively dissipated.
  • the flutes adjacent the exit end of the dissipator preferably overlap as shown in Figure 4, thus offering the greatest impediment to the flow of gas. Since these lastmentioned flutes do not touch each other, being displaced axially, it is to be noted that the dissipato-r cannot be considered to be completely closed at its exit end, and thus very low-speed gases, having little or no noise value, can pass around those flutes to emerge from within the dissipator. However, this overlapping of said flutes will be spoken of hereafter as resulting in a closed end, in contrast to end flutes which do not overlap, and hence result in an open central passageway 2
  • dissipator shell 4 In the forward end of dissipator shell 4, either by welding or riveting or other suitable means,
  • each deflector tends to deflect a portion of the central gas stream outwardly toward the wall of the dissipator, where the stream at high pressure and low volume can be acted upon by the first series of flutes I3, which are purposely made small to silence high-pressure gases.
  • the height of the spacing and supporting ribs 9, Ii] and II is such that the spacing between the outside periphery of dissipator shell 4 and the inner periphery of outside casing I is not more than the diameter of shell 4.
  • this spacing is not more than specified, effective mufiling will be ensured with a minimum of back pressure.
  • the muffiing effect will increase as the said spacing is made smaller, but a point is eventually reached at which the back pressure begins to increase to a point which is objectionable. As the spacing is made larger, the back pressure will decrease, but the mufiling effect becomes less.
  • a silencer constructed so that the outer periphery of shell 4 is 1 inches in diameter and the inner diameter of casing I is 1% inches has been found to be very satisfactory.
  • an outside casing I is provided, and mounted within it in the manner aforesaid are two dissipator shells I8 and I9, and a gas expander indicated generally at 20.
  • Said dissipator shells l8 and I9 follow the construction already described for shell 4.
  • shell I9 is of the closed end type like shell 4
  • shell [8 is of the open end type. That is, as shown in Figure 10, the flutes adjacent the exit end of shell l8 do not overlap, and thus an open central bore or passageway 2! is provided throughout the length of shell l8.
  • the lower end 25 of each support 23 and 24 is bent over and attached to expander 20, as by spot welding, and th top 26 of the support is bent over to fit the inside of shell I 9, as shown. Ends 26 are then spot welded, brazed, or riveted to hold expander 29 in its proper place in the entrance end of shell 19.
  • shell [8 is inserted in casing i, and shell I8 is then inserted until its inner flared end 2'! comes in line, approximately as shown, with the exit end of shell 18.
  • Shells l8 and [9 are, as before, held tightly in place, by friction fit, in casing l.
  • the operation of the double silencer is as follows: Exhaust gases enter the right (as shown) end of casing I and are first deflected by deflectors l6 and !1. As the gases pass down the length of shell l 8, the aforesaid flutes l3 scoop out gases in progressively greater amounts and directively deflect these scooped-out portions to the wall of casing I. Any gases which escape this, as well as high-speed backfire gases, emerge centrally from dissipator 18 to strike expander 20. They are deflected outwardly toward the wall of the dissipator shell I9 and traverse its length, wherein they are further dissipated and silenced.
  • a dissipator shell similar to shell 4 may be constructed and inserted in the exhaust pipe of the motor cycle. If the proper spacing has been followed, it will be found that the usual noisy exhaust is effectively reduced.
  • a dissipator adapted for use in an exhaust silencer comprising a tubular shell having a series of apertures in the wall thereof, and forwardlyinclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each of said flutes being narrower than that portion of the flute attached to the edge of the aperture, and said apertures and their respective flutes increasing in size in a direction toward the outlet end of said shell.
  • a dissipator adapted for use in an exhaust silencer comprising a tubular shell having a series of apertures in the wall thereof, and forwardlyinclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each of said flutes being narrower than that portion of the flute attached to the edge of the aperture, said shell having external support means attached thereto for spacing said shell from the wall of said exhaust silencer a distance not greater than the diameter of said shell.
  • a dissipator adapted for use in an exhaust silencer comprising a tubular shell having a series of apertures in the wall thereof, and forwardlyinclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each of said flutes being narrower than that portion of the flute attached to the edge of the aperture, said shell having external support means attached thereto for spacing said shell from the Wall of said exhaust silencer, said support means comprising at least three outwardly projecting ribs mounted on said shell and adapted to support said shell centrally within the exhaust silencer in such manner that the spacing between the outside of said shell and the. inside of said silencer is not more than 3 of the diameter of said shell, each of said ribs comprising outwardly turned flanges integral with said shell.
  • An exhaust silencer of the character described comprising an outside casing and a dissipator mounted within said casing concentrically therewith, said dissipator comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flutes projecting from the edges of said openings with the forward portion of each flute being narrower than that portion of the flute attached to the edge of its respective opening, said flutes gradually increasing in size in a direction toward the exit end of said exhaust silencer, said casing and said dissipator being spaced apart, throughout their length, by a distance not substantially greater than A; the diameter of said dissipator.
  • An exhaust silencer of the character described comprising an outside casing and at least two dissipators mounted within said casing concentrically therewith and in alignment with each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each flute being narrower than that portion of the flute attached to the edge of the aperture, said flutes likewise increasing in size in a direction toward the exit end of said exhaust silencer, and said casing being spaced apart from each of said dissipators a distance substantially *not greater than /4 the diameter of the dissipawith each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flute
  • An exhaust silencer of the character described comprising an outside casing, a first dissipator, and a second dissipator, said first and second dissipators being mounted within said casing concentrically therewith and in alignment with each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardlyinclined, inwardly-directed flutes projecting from the edges of said openings, said flutes gradually increasing in size in a direction toward the exit end of said exhaust silencer and gradually approaching the axes of said dissipators, said flutes being spoon shaped and concaved inwardly, with the forward portion of each flute being narrower than that portion of the flute attached to the edge of the opening, said first dissipator being mounted nearest the entrance end of said exhaust silencer and having the central part of its bore open throughout its length, said second dissipator being mounted nearest the exit end of said exhaust silencer and having the central part of its
  • An exhaust silencer of the character described comprising an outside casing and a dissipator mounted within said casing concentrically therewith, said dissipator comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined, inwardly-directed flutes projecting from the edges of said openings, said flutes being spoon shaped and concaved inwardly, said casing and said dissipator being spaced apart throughout their length, by a distance substantially not greater than /4 the diameter of said dissipator, and means mounted adjacent the entrance end 8 of saiddissipator for deflecting gases, entering therein. toward the wall of said dissipator.
  • An exhaust silencer of the character described comprising an outside casing, at least two dissipators mounted within said casing concentrically therewith and in alignment with each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flutes projecting from the edges of said openings, said flutes being spoon shaped and concaved inwardly with the forward portion of each' of said flutes being narrower than that portion of the flute attached to the edge of the aperture, said flutes gradually increasing in size in a direction toward the exit end of said exhaust silencer and gradually approaching the axes of said dissipators, and a gas expander mounted between the exit end flutes of one of said dissipators and the entrance end flutes of another of said dissipators, for directing exhaust gases against the inside wall of said other dissipator said gas expander comprising a substantially cone-shaped element mounted in alignment with said dis
  • An exhaust silencer of the character described comprising an outside casing, a first dissipator, a second dissipator, said first and second dissipators being mounted within said casing concentrically therewith and in alignment with each other, a gas deflector and a gas expander, said dissipators each comprising tubular shells having openings in the walls thereof gradually increasing in size in a direction toward the exit ends of said dissipators, and forwardly-inclined inwardlydirected flutes projecting from the edges of said openings, said flutes gradually increasing in size in a direction toward the exit ends of said dissipators and gradually approaching the axes of said dissipators, said flutes being spoon shaped and concaved inwardly, said gas deflector comprising at least two spirally-twisted elongate members mounted in the entrance end of said first dissipator and lying fora portion of their lengths in the central bore of said first dissipator thereby to deflect gases entering said entrance end toward the

Description

BAFF'LE TYPE EXHAUST SILENCER Filed April 27, 1948 2 Sheets-Sheet 1 INVENTOR. Omer \T/Fa/n wY/t BY June 19, 1951 b. J. RAINVILLE 2,557,687 BAFFLE TYPE EXHAUST SILENCER Filed April 27, 1948 2 Sheets-Sheet Z INVENTOR. Omar f P invv'l/e BY ain 3 Patented June 19, 1951 UNITED STATES PATENT OFFICE BAFFLE TYPE EXHAUST SILENCER Omer J. Rainville, Attleboro, Mass.
Application April 27, 1948, Serial No. 23,413
10 Claims. 1 This invention relates to certain new and useful improvements in exhaust silencers of the type generally employed with internal combustion engines for silencing or muiiling the discharge of products of combustion from such engines, and also relates to certain new and useful component parts of said silencers.
Among the several objects of the invention may be noted the provision of a new form of exhaust silencer of the class described which is so constructed as to give a maximum of silencing effect while presenting a minimum of interference to the gases passing through it; the provision of a new form of exhaust silencer so arranged in its component parts as to effectively silence so-called back-fires from the engine; the provision of an exhaust silencer of the class described which is simple to construct and which because of its simplicity may be readily adapted to existing types of internal combustion engines; the provision of a component part for an exhaust silencer which may readily be inserted in the exhaust tubes of internal combustion engines which are ordinarily not equipped with silencers, thereby to muifie and silence effectively the exhaust noise of such engines; and the provision of an exhaust silencer, and its component parts, which is economical to construct and efficient its operation. Other objects will be in part obvious and in part pointed out hereinafter.
The invention accordingly comprises the elements and combinations of elements, features of construction, and arrangements of parts which will be exemplified in the structures hereinafter described, and the scope of the application of which will be indicated in the following claims.
In the accompanying drawings, in which are illustrated several of the various possible embodiments of the invention:
Figure l is a longitudinal sectional view of one form of the exhaust silencer of the present invention;
Figures 2, 3, and 4 are cross-sectional views taken on lines 2-2, 33, and 44 respectively of Figure 1;
Figure 5 is an end perspective view looking into the silencer of Figure 1 from line 22;
Figure 6 is a longitudinal sectional view of one of the flutes of the present invention;
Figure 7 is a fragmentary longitudinal crosssection of a. part of this invention, in order to show more clearly certain relationship of parts;
Figure 8 is an end view of Figure 1, to illustrate more clearly certain portions of the silencer;
Figure 9- is a cross-sectional broken view to illustrate another embodiment of this invention; Figure 10 is a cross-sectional view taken. along lines l8l ll of Figure 9; and
Figure 11 is a perspective view of a part of the Figure 9 embodiment, to show more clearly certain features of construction.
Similar reference characters throughout the drawing are used to designate similar elements. In hitherto designed exhaust silencers, there have been attempts made to accomplish the three main requirements of a silencer, via, (1) effective muffiing or silencing of the regular ex haust noise of the internal combustion engine, as well as that form of noise called a back-fire;
' (2) silencing without setting up any appreciable back pressure; and (3) long life, which life is shortened by, for example, condensation vapors remaining in the silencer and oorroding the material of which the silencer is made. An addi tional requirement is that the silencer be as simple as possible, with a minimum of parts to get out of order or to fail.
It is the general purpose of this invention to provide a silencer which meets these requirements to the extent required. The manner in which it does will now be explained by referring to the accompanying drawings, as follows:
Referring to Figure 1, there is shown at l the outside casing of the exhaust silencer. Casing I is tubular, preferably cylindrical in shape, but may have other shapes in cross-section if desired, such as hexagonal, for example. It will be noted that casing I is open throughout its length, and that it has an inlet or forward end indicated generally by 2 and an exit end indicated generally by 3.
Mounted within casing l is a gas dissipator element comprising a tubular shell indicated generallv by 4. Shell 4 may be made of one piece, if desired, but for ease in stamping certain perforations in the shell (later to be described), I prefer to use a 3-piece construction as shown. by the cross-sectional views, Figures 2, 3 and 4. As shown, shell 4 is made up of three elongated members 5, 6 and 1, each member being as shown and comprising approximately the circumference of the shell 4. Members 5, 6 and l are formed with turned outward flanges 8 thereon, which flanges serve, by means of spot welding or riveting, as meansto fasten members 5, 6 and I together to form the complete tubular shell 4. Flanges 8 extend outwardly from shell 4 a distance not greater than 2. the approximate diameter of shell 4, and these joined flanges thus form ribs 9, l0, and H, running the length of the shell and serving as spacing and mounting means for shell 4 with- 3 in casing I. The inside diameter of casing I is such that the outer edges of ribs 9, Ii) and II bear snugly with a good friction fit against the inside wall of casing I, thus holding shell 4 firmly in place. Shell 6 is provided at its entrance end with an outwardly-flared riin 28 which fits snugly casing I.
The shell 4 is provided with a series of openings I2 throughout its length, and said openings I2 are preferably arranged in groups, with the openings of each group successively increasing in size toward the exit end of the silencer. The openings of each circular series are in staggered relation with respect to the openings in adjacent series.
Projecting inwardly toward the center of shell 4 are flutes I3, each of said openings I2 having one flute attached to that portion of its edge which is toward the exit end 3 of the silencer.
It will be noted, as shownin Figures 2, S, 4, and '7,
that said flutes gradually increase in size in a adjacent the exit end of the shell 4. It will also be noted that said flutes incline forwardly, and
while I prefer to form the flutes I3 as an integral part of shell 4 by strikin the flutes inwardly in the production of said openings I2, nevertheless, the flutes may be formed separately and attached to the shell in their proper positions as by spot welding or riveting, if desired.
Figure 5 illustrates the perspective appearance of the silencer if looking into the entrance end, and illustrates the above-mentioned staggering of openings I 2 to provide overlapping of the flutes as to any gases flowing against the flutes.
Flutes I3 are spoon shaped and are so positioned as to be concaved inwardly as shown in Figure 6, which is an enlarged drawing for purposes of clarity. The forward portion (indicated at I4) of each flute is narrower than the rearward portion (indicated at I5) attached to shell 4. I have found that by making the flutes spoon shaped and concaved inwardly as shown, each flute scoops out of the exhaust gas flowing past it a portion and directs substantially all of that portion outward through the respective opening and to the inside wall of casing I. By doing this the sound energy of the gas is effectively dissipated. When the flutes are flat, not spoon shaped, not all of the gas hitting the flute comes out, and furthermore, the gas coming out is not completely directed so as to impinge on the wall of casing I. Ihus, the spoon-shaped flute is far more silencing than the flat flute. Furthermore, it will be noted that since the size of any open- 'ing I2 through which the scooped portion of gas must be expelled, increases in a backward direction, and since the back portion of the flute is wider than the front, then as the scooped gas is deflected outwardly, it meets with lesser and lesser resistance. As a result of this, the gas to be expelled has a very free passageway outward, and the net effect of this is to give a greater muflling effect with less back pressure than is experienced in prior silencers.
7 While I do not know exactly why the particular form of dissipator works, I am led to believe by my experiments that the smaller forward flutes collect the high-speed, and hence high-pitchm, exhaust gases and dissipate their energy outward,
while the larger flutes toward the rear collect the lower-speed, lower-pitched gases. Also, since the impediment offered by the flutes to the flow of gas increases (due to their increase in size and greater angularity) as the velocity of the gas decreases in going from entrance end to exit end of the dissipator II, all portions of the dissipator tend to operate at maximum efliciency and hence the muifiing effect is very pronounced even with a short dissipator.
It will be noted that the flutes adjacent the exit end of the dissipator preferably overlap as shown in Figure 4, thus offering the greatest impediment to the flow of gas. Since these lastmentioned flutes do not touch each other, being displaced axially, it is to be noted that the dissipato-r cannot be considered to be completely closed at its exit end, and thus very low-speed gases, having little or no noise value, can pass around those flutes to emerge from within the dissipator. However, this overlapping of said flutes will be spoken of hereafter as resulting in a closed end, in contrast to end flutes which do not overlap, and hence result in an open central passageway 2|, as shown in Figure 10, through the dissipator, which type will be called an open end. 7
In the forward end of dissipator shell 4, either by welding or riveting or other suitable means,
I prefer to mount two gas deflectors I6 and II,
made of sheet metal and formed, as shown in Figures 1 and 8, so as to have a longitudinally partially spiral shape. These deflectors approach each other at the center of the dissipator, and thus lie for a portion of their lengths in the stream of gases flowing into the dissipate-r. Because of their spiral forward twist, each deflector tends to deflect a portion of the central gas stream outwardly toward the wall of the dissipator, where the stream at high pressure and low volume can be acted upon by the first series of flutes I3, which are purposely made small to silence high-pressure gases.
As specified above, the height of the spacing and supporting ribs 9, Ii] and II is such that the spacing between the outside periphery of dissipator shell 4 and the inner periphery of outside casing I is not more than the diameter of shell 4. I have found that if this spacing is not more than specified, effective mufiling will be ensured with a minimum of back pressure. The muffiing effect will increase as the said spacing is made smaller, but a point is eventually reached at which the back pressure begins to increase to a point which is objectionable. As the spacing is made larger, the back pressure will decrease, but the mufiling effect becomes less. In practice, a silencer constructed so that the outer periphery of shell 4 is 1 inches in diameter and the inner diameter of casing I is 1% inches, has been found to be very satisfactory.
Since there are no transverse walls in the above described silencer, it is obvious that no pockets are formed to entrap condensation products resulting from the exhaust vapors. Any such condensation products are free to drain from casing I, and as a result this construction provides a long life with a less amount of corrosion than has hitherto been experienced in other types of mufflers.
Referring now to Figure 9, I' have shown another preferred embodiment of my invention which I have found useful in cases where the simpler form already described is not as effective as desired. As before, an outside casing I is provided, and mounted within it in the manner aforesaid are two dissipator shells I8 and I9, and a gas expander indicated generally at 20. Said dissipator shells l8 and I9 follow the construction already described for shell 4. However, it is to be noted that while shell I9 is of the closed end type like shell 4, shell [8 is of the open end type. That is, as shown in Figure 10, the flutes adjacent the exit end of shell l8 do not overlap, and thus an open central bore or passageway 2! is provided throughout the length of shell l8. The purpose of this is to permit the passage through shell l8 of the high-speed exhaust gases resulting from a back-fire in the exhaust manifold of the internal combustion engine. Upon emergence from the central bore of dissipator I8, these high-speed gases strike the apex of gas expander 20, and are deflected outward to the wall of dissipator 19. In this position said gases can be acted upon by the first series of flutes of shell l9. The gas expander 20 also serves to slow down these high-speed gases; and thus give the flutes of dissipator IS a longer time to act upon them. Gas expander 20 is preferably slightly smaller in diameter at its base than dissipator I8.
I have shown in perspective view in Figure 11 a preferred form of gas expander 20. A substantially conical shell 22, either hollow or solid, is formed. Attached to it near its base are two supports 23, and 24, preferably being thin in cross section so as to offer minimum impedance to gases flowing past them. Said supports 23 and 24 may preferably be made of sheet metal. The lower end 25 of each support 23 and 24 is bent over and attached to expander 20, as by spot welding, and th top 26 of the support is bent over to fit the inside of shell I 9, as shown. Ends 26 are then spot welded, brazed, or riveted to hold expander 29 in its proper place in the entrance end of shell 19.
In assembly, shell [8 is inserted in casing i, and shell I8 is then inserted until its inner flared end 2'! comes in line, approximately as shown, with the exit end of shell 18. Shells l8 and [9 are, as before, held tightly in place, by friction fit, in casing l.
The operation of the double silencer is as follows: Exhaust gases enter the right (as shown) end of casing I and are first deflected by deflectors l6 and !1. As the gases pass down the length of shell l 8, the aforesaid flutes l3 scoop out gases in progressively greater amounts and directively deflect these scooped-out portions to the wall of casing I. Any gases which escape this, as well as high-speed backfire gases, emerge centrally from dissipator 18 to strike expander 20. They are deflected outwardly toward the wall of the dissipator shell I9 and traverse its length, wherein they are further dissipated and silenced.
For silencing the exhausts of motor cycles or other engines, a dissipator shell similar to shell 4 may be constructed and inserted in the exhaust pipe of the motor cycle. If the proper spacing has been followed, it will be found that the usual noisy exhaust is effectively reduced.
t is to be understood that the principle of this Figure 9 embodiment may be extended by providing more than two dissipators concentrically aligned as shown. While two is generally satisfactory, further muflling eflects may be obtained by adding more dissipators.
Since many departures may be made from the embodiments shown herein without departing from the spirit and scope of the invention, it is 6 to be understood that all matter set forth herein or shown in the accompanying drawings is to be considered as illustrative and not in a limiting sense.
I claim:
1. A dissipator adapted for use in an exhaust silencer comprising a tubular shell having a series of apertures in the wall thereof, and forwardlyinclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each of said flutes being narrower than that portion of the flute attached to the edge of the aperture, and said apertures and their respective flutes increasing in size in a direction toward the outlet end of said shell.
'2. A dissipator adapted for use in an exhaust silencer, comprising a tubular shell having a series of apertures in the wall thereof, and forwardlyinclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each of said flutes being narrower than that portion of the flute attached to the edge of the aperture, said shell having external support means attached thereto for spacing said shell from the wall of said exhaust silencer a distance not greater than the diameter of said shell.
3. A dissipator adapted for use in an exhaust silencer, comprising a tubular shell having a series of apertures in the wall thereof, and forwardlyinclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each of said flutes being narrower than that portion of the flute attached to the edge of the aperture, said shell having external support means attached thereto for spacing said shell from the Wall of said exhaust silencer, said support means comprising at least three outwardly projecting ribs mounted on said shell and adapted to support said shell centrally within the exhaust silencer in such manner that the spacing between the outside of said shell and the. inside of said silencer is not more than 3 of the diameter of said shell, each of said ribs comprising outwardly turned flanges integral with said shell.
4. An exhaust silencer of the character described comprising an outside casing and a dissipator mounted within said casing concentrically therewith, said dissipator comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flutes projecting from the edges of said openings with the forward portion of each flute being narrower than that portion of the flute attached to the edge of its respective opening, said flutes gradually increasing in size in a direction toward the exit end of said exhaust silencer, said casing and said dissipator being spaced apart, throughout their length, by a distance not substantially greater than A; the diameter of said dissipator.
5. An exhaust silencer of the character described comprising an outside casing and at least two dissipators mounted within said casing concentrically therewith and in alignment with each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flutes projecting from the edges of said apertures, said flutes being spoon shaped and concaved inwardly with the forward portion of each flute being narrower than that portion of the flute attached to the edge of the aperture, said flutes likewise increasing in size in a direction toward the exit end of said exhaust silencer, and said casing being spaced apart from each of said dissipators a distance substantially *not greater than /4 the diameter of the dissipawith each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flutes projecting from the edges of said openings, said flutes gradually increasing in size in a direction toward the exit end of said exhaust silencer and gradually approaching the axes of said dissipators, said first dissipator being mounted nearest the entrance end of said exhaust silencer and having its central bore open throughout its length, said second dissipator being mounted nearest the exit end of said exhaust silencer and having its central bore substantially restricted by the overlapping, on the axis line, of those flutes adjacent said exit end, said last-named flutes being spaced apart, axially, in order to provide passage-way for low velocity gases.
7. An exhaust silencer of the character described comprising an outside casing, a first dissipator, and a second dissipator, said first and second dissipators being mounted within said casing concentrically therewith and in alignment with each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardlyinclined, inwardly-directed flutes projecting from the edges of said openings, said flutes gradually increasing in size in a direction toward the exit end of said exhaust silencer and gradually approaching the axes of said dissipators, said flutes being spoon shaped and concaved inwardly, with the forward portion of each flute being narrower than that portion of the flute attached to the edge of the opening, said first dissipator being mounted nearest the entrance end of said exhaust silencer and having the central part of its bore open throughout its length, said second dissipator being mounted nearest the exit end of said exhaust silencer and having the central part of its bore substantially restricted by the overlapping, on the axis line, of those flutes adjacent said exit end, said last-named flutes being spaced apart, axially, in order to provide passage-way for low velocity gases.
8. An exhaust silencer of the character described comprising an outside casing and a dissipator mounted within said casing concentrically therewith, said dissipator comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined, inwardly-directed flutes projecting from the edges of said openings, said flutes being spoon shaped and concaved inwardly, said casing and said dissipator being spaced apart throughout their length, by a distance substantially not greater than /4 the diameter of said dissipator, and means mounted adjacent the entrance end 8 of saiddissipator for deflecting gases, entering therein. toward the wall of said dissipator.
9. An exhaust silencer of the character described comprising an outside casing, at least two dissipators mounted within said casing concentrically therewith and in alignment with each other, each of said dissipators comprising a tubular shell having openings therein gradually increasing in size in a direction toward the exit end of said exhaust silencer, and forwardly-inclined inwardly-directed flutes projecting from the edges of said openings, said flutes being spoon shaped and concaved inwardly with the forward portion of each' of said flutes being narrower than that portion of the flute attached to the edge of the aperture, said flutes gradually increasing in size in a direction toward the exit end of said exhaust silencer and gradually approaching the axes of said dissipators, and a gas expander mounted between the exit end flutes of one of said dissipators and the entrance end flutes of another of said dissipators, for directing exhaust gases against the inside wall of said other dissipator said gas expander comprising a substantially cone-shaped element mounted in alignment with said dissipators and having itsapex pointed toward the entrance end of said exhaust silencer.
10. An exhaust silencer of the character described comprising an outside casing, a first dissipator, a second dissipator, said first and second dissipators being mounted within said casing concentrically therewith and in alignment with each other, a gas deflector and a gas expander, said dissipators each comprising tubular shells having openings in the walls thereof gradually increasing in size in a direction toward the exit ends of said dissipators, and forwardly-inclined inwardlydirected flutes projecting from the edges of said openings, said flutes gradually increasing in size in a direction toward the exit ends of said dissipators and gradually approaching the axes of said dissipators, said flutes being spoon shaped and concaved inwardly, said gas deflector comprising at least two spirally-twisted elongate members mounted in the entrance end of said first dissipator and lying fora portion of their lengths in the central bore of said first dissipator thereby to deflect gases entering said entrance end toward the wall of said first dissipator, said gas expander comprising a substantially cone-shaped element mounted in the entrance end of said second dissipator in aligmnent therewith with its apex pointed toward the exit end of said first dissipator, thereby to deflect gases emerging from said first dissipator toward the wall of said second dissipator.
OMER. J. RAINVILLE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 624,062 Mattews May 2, 1899 738,858 Swain Sept. 15, 1903 788,242 Broga Apr. 25, 1905 1,182,098 Mayer May 9, 1916 7 1,213,558 Turner Jan. 23, 1917 1,781,001 Eisele Nov. 11, 1930 1,991,014 Compo Feb. 12, 1935 1,991,748 Johnson Feb. 19, 1935 1,998,385 Powell Apr. 16, 1935 2,065,343 Moore Dec. 22, 1936 2,213,614 Scarritt Sept. 3, 1940 2,350,924 Rainville June 6, 1944
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Cited By (17)

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US2704133A (en) * 1951-01-26 1955-03-15 Telephonics Corp Acoustic filter
US2723723A (en) * 1952-06-23 1955-11-15 Halliday John Combined muffler and spark arrester
US3011584A (en) * 1957-12-16 1961-12-05 Koppers Co Inc Sound attenuating device
US3174583A (en) * 1960-11-30 1965-03-23 Giordano Michele Muffler for internal combustion engines
US3176790A (en) * 1962-06-13 1965-04-06 Ervin C Lentz Muffler
US3185252A (en) * 1957-07-29 1965-05-25 C W Lemmerman Inc Jet engine noise attenuator
US3219142A (en) * 1962-10-03 1965-11-23 Oldberg Mfg Company Method and apparatus for attenuating sound waves in gas streams
US3482648A (en) * 1968-10-09 1969-12-09 Curtis Terry Reeve Motorcycle muffler
US3589395A (en) * 1968-09-16 1971-06-29 Edward W Bottum Refrigeration component
US3770081A (en) * 1972-10-13 1973-11-06 Line Inc M Silencer for combustion engines
US3884655A (en) * 1974-04-22 1975-05-20 Jeffrey W Coop Spark arrester and silencer
US4050539A (en) * 1975-09-13 1977-09-27 Teruo Kashiwara Exhaust apparatus for internal combustion engine
US6398520B2 (en) * 1999-01-14 2002-06-04 Samsung Electronics Co., Ltd. Discharge muffler of a hermetic rotary compressor
GB2413362A (en) * 2004-04-20 2005-10-26 Daniel Coles Exhaust system insert
US20070289809A1 (en) * 2004-10-29 2007-12-20 Kim Soo W Exhaust Gas-Discharging Device of Vehicle
US20110061757A1 (en) * 2009-09-15 2011-03-17 Butler Boyd L Anti-Resonant Pulse Diffuser
CN102628392A (en) * 2012-04-11 2012-08-08 宁波市鄞州吉士汽配有限公司 Muffler

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US788242A (en) * 1904-04-25 1905-04-25 William W Broga Muffler.
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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2704133A (en) * 1951-01-26 1955-03-15 Telephonics Corp Acoustic filter
US2723723A (en) * 1952-06-23 1955-11-15 Halliday John Combined muffler and spark arrester
US3185252A (en) * 1957-07-29 1965-05-25 C W Lemmerman Inc Jet engine noise attenuator
US3011584A (en) * 1957-12-16 1961-12-05 Koppers Co Inc Sound attenuating device
US3174583A (en) * 1960-11-30 1965-03-23 Giordano Michele Muffler for internal combustion engines
US3176790A (en) * 1962-06-13 1965-04-06 Ervin C Lentz Muffler
US3219142A (en) * 1962-10-03 1965-11-23 Oldberg Mfg Company Method and apparatus for attenuating sound waves in gas streams
US3589395A (en) * 1968-09-16 1971-06-29 Edward W Bottum Refrigeration component
US3482648A (en) * 1968-10-09 1969-12-09 Curtis Terry Reeve Motorcycle muffler
US3770081A (en) * 1972-10-13 1973-11-06 Line Inc M Silencer for combustion engines
US3884655A (en) * 1974-04-22 1975-05-20 Jeffrey W Coop Spark arrester and silencer
US4050539A (en) * 1975-09-13 1977-09-27 Teruo Kashiwara Exhaust apparatus for internal combustion engine
US6398520B2 (en) * 1999-01-14 2002-06-04 Samsung Electronics Co., Ltd. Discharge muffler of a hermetic rotary compressor
CN1112518C (en) * 1999-01-14 2003-06-25 三星电子株式会社 Exhausting silencing apparatus for air-tight rotary compressor
GB2413362A (en) * 2004-04-20 2005-10-26 Daniel Coles Exhaust system insert
US20070289809A1 (en) * 2004-10-29 2007-12-20 Kim Soo W Exhaust Gas-Discharging Device of Vehicle
US20110061757A1 (en) * 2009-09-15 2011-03-17 Butler Boyd L Anti-Resonant Pulse Diffuser
US8181671B2 (en) 2009-09-15 2012-05-22 Butler Boyd L Anti-resonant pulse diffuser
CN102628392A (en) * 2012-04-11 2012-08-08 宁波市鄞州吉士汽配有限公司 Muffler

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