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US1857845A - Exhaust gas silencer - Google Patents

Exhaust gas silencer Download PDF

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US1857845A
US1857845A US455403A US45540330A US1857845A US 1857845 A US1857845 A US 1857845A US 455403 A US455403 A US 455403A US 45540330 A US45540330 A US 45540330A US 1857845 A US1857845 A US 1857845A
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shell
barrel
head
pipe
exhaust gas
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US455403A
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Francis F Hamilton
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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
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/08Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
    • F01N1/10Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling in combination with sound-absorbing materials

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  • This invention relates to the art of exthe innerside of the shell 10.
  • a plurality haust gas silencers as are commonly emof holes 15, here shown as radial slots, are ployed .Wltll gas engines, and relates particuprovided in the apron and the length of the larly to a new and novel structure, the pri-' pipe 12 between the head 11 and the forward mary ob ect of which is to eliminate all noise side of the apron 14 is wrapped with steel wlthout creating undue back pressure of the wool 16 preferably in such a manner that 5 stream of gases exhausting from such enan annular space 17 is left immediately bei gmes; hind the head 11.
  • the steel wool 16 com- 1 A further important object resides in the pressively contacts the inner side of the shell 10 unique combination of the elements permit- 10 and the forward side of the apron 14. ting a free flow of gases through the silencing I form a spool member 18 having a central device and at the same time causing the gases hollow cylindrical barrel 19 and the forflowing therethrou'gh tobe slowed up in part ward and rear conical flanges 20 and 21, and expanded and cooled at intervals so that the barrel 19 and the flanges 20 and 21 being 15 the sound waves in the gas stream issuing provided with a plurality of holes therefrom the engine are broken up to such an exthrough, here shown as slots.
  • the flange 21 is preferably fixed to the shell to deaden and prevent vibration of various 10 by welding to form the attaching juncmembers embodied within the silencer. tures 22 and 23, Fig. 4.
  • the other flange 20 6 These and other objects will become apis not attached to the shell so that the barrel parent in the following description of the in- 19 may expand longitudinally from the vention as illustrated by the accompanying flange 21 as the fixed member.
  • Fig. 1 is a fragmentary side elevation of Within the .shell 10 to have the plane of the a silencer embodying my invention; forward edge of the flange 20 substantially Fig. 2, a vertical transverse section on the at the plane of the end of the pipe 12 so that line 22 of Fig. 1; there is an appreciable space between the Fig. 3; a vertical transverse section on the flange 20 and the apron 14 bounded thereby li e 3-3 of Fig. 1; and fore and aft and by the shell 10 circumferig. 4, a vertical transverse section on the entially therearound.
  • the rear end of the shell 10 has a head 25
  • Like characters of reference indicate like as a closure 'thereacross through which the parts throughout the several views in the tail pipe 26 is supported to pro ect inwardly drawings. to carry the exhaust head 27 on its forward 40 I form a cylindrical shell 10 having the end toward the rear of the flange 21.
  • apron 28 is fixed to the pipe 26 behind the which is an intake pipe 12 to extend for an head 27 and flares outwardly and rearwardly appreciable distance axially .within the shell. toward and in substantial contact with the
  • the inner end of the intake pipe 12 is closed shell 10.
  • the space between the head 25 and and a plurality of openings 13 are spaced the rear of the apron 28 is filled with steel circumferentially around the pipe near the wool 29 with the exception of a small annuclosed end. Spaced forwardly a slight disla'r space around the inside of the shell 10 tance from the openings 13 is a conical apron at its juncture with the head 25.
  • the head 27 is here shown as being com- 12.
  • This apron 14 flares outwardly and rearprised of a forwardly and outwardly flarwardly to terminate substantially against ing wall 30 on the end of the pipe 26 having the slots 31 therethrough.
  • a cap 32 encloses the forward opening to within the wall 30 and a frusto-conical apron 33 extends from the base of this cap rearwardly and spaced outwardly from the wall 30 to have an annular opening between it and the pipe 26.
  • the exhaust head 27 is similar to the head as described in my previous application for patent, filed November 1, 1929, Serial No. 404,114.
  • gases flow from the pipe 12 out through the holes 13 where they may expand into the chamber there provided as above described. Some of this gas may escape forwardly through the holes 15 into the steel wool 16. Also gases may escape rearwardly through the holes in the flange into the steel wool 24 and through the holes in the barrel 19 or on back through the holes in the flange 21. There is no restriction in the barrel 19 so that gases may flow freely from the chamber around the I end of the pipe 12 therethrough. The gases discharging back of the flange 21 again may expand and come in contact with the cool wall 10 and may in part flow through the holes in theapron 28 into the steel wool therebehind. The main volume of the gases will however flow through the holes 31 in the wall 30 and turn and flow rearwardly out the tail pipe 26.
  • a shell an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a material formed into a porous mass and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe projecting within the shell to have its forward end near the rear end of said barrel and surge chambers at each end of the shell formed by porous material around the intake and tail pipes.
  • an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe projecting within the shell to have its forward end near the rear end of said barrel, said intake and tail pipes being closed across theirinner endsantthavingholes through side walls near the closed ends and surge chambers at each end of the shell formed by p0- rous material around the intake. and tail pipes.
  • a shell In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the for ward end of said barrel, and said tail pipe projecting within the shell to have its forward end near the rear end of said barrel, said intake and tail pipes being closed across their inner ends and having holes through side walls near the closed ends and surge chambers at each end of the shell formed by porous material around the intake and tail pipes and perforated flanges extending from each end of said barrel toward said shell confining said first-mentioned material therebetween.
  • a shell an intake pipe discharging into the shell, a tail pi pe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, both said intake and tail pipe having extensions within the shell directed toward said'sur e chamber, porous material between the inta e pipe extension and the shell, and
  • a shell an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe extending within the shell to have its forward end near the rear end of said barrel, a filling of porous material between a part of the length of both of the extensions and the shell, and perforate aprons extending from the pipes toward the shell to confine said material and define expansion chambers at each end' of said barrel.
  • a shell an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe extending within the shell to have its forward end near the rear end of said barrel, a filling ofporous material between a part of the length of both extensions and the shell, and perforate aprons extending from the pipes toward the shell to confine said material and define expansion chambers at each end of said barrel, the inner ends of both the intake and tail pipes being closed, said pipes having holes through side walls near said inner ends.
  • a shell In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the. shell toward and terminating near the forward end of said.
  • said tail pipe extending within the shell to have its forward end near the rear end of said barrel, a filling of porous material between a part of the length of both extensions and the shell, and perforate aprons extending from the pipes toward the shell to confine said material and define expansion chambers at each end of said barrel, a head in each end of said shell, said last mentioned filling of porous material terminating to leave an annular-open space therearound adjacent the juncture of said heads and said shell.
  • an exhaust gas silencer a shell, a head in each end of the shell, an intake pipe extended through one head, a tail pipe extended through the other head, a spool fixedin the central part of inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, means on the inner end of the tail pipe to deflect the gas and steel wool around the tail pipe.
  • an exhaust gas silencer a shell, a head in each end of the shell, an intake pipe extended through one head, a tail pipe extended through the other head, a spoolfixed in the central part of the shell spaced between the inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, said intake pipe having its inner end closed and having holes through its side wall near the end, an apron carried on the intake pipe spaced forwardly from its inner end, and steel wool wrapped around said intake pipe between said apron and said one head.
  • an exhaust gas silencer a shell, a head in each end of the shell, an intake pipe extended through one head, a tail pipe extended through the other head, a spool fixed in the central part of the shellspaeed between the inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, said tail pipe having a cap over its inner end and holes through a side wall near the end, an apron fixed on the tail ipe, and steel wool wrapped around the tail pipe lietween said apron and said other head.
  • an exhaust gas silencer a shell, a head in each end of the shell, an lntake pipe extended through one head, a tail pipe extended through the other head, a spool fixed in the central part of the shell spaced between the inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, and a perforate fiangeat each end of the barrel extending toward said shell and confining said steel wool therebetween, said tail pipe having a cap over its inner end and steel wool wrapped around the tail pipe between the cap and other head.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)

Description

May 10, 1932.
F. F. HAMILTON EXHAUST GAS SILENCER Filed May 24. 1950 m van roR, Francis 7 Ham/(fen I BJ mm mm Patented May 10,11932 1,857,845
UNITED STATES PATENT oFFncs FRANCIS HAMILTON, OF INDIANAPOLIS, INDIANA EXHAUST GAS SILENCER Application filed May 24, 1930. Serial No. 455,403.
This invention relates to the art of exthe innerside of the shell 10. A plurality haust gas silencers as are commonly emof holes 15, here shown as radial slots, are ployed .Wltll gas engines, and relates particuprovided in the apron and the length of the larly to a new and novel structure, the pri-' pipe 12 between the head 11 and the forward mary ob ect of which is to eliminate all noise side of the apron 14 is wrapped with steel wlthout creating undue back pressure of the wool 16 preferably in such a manner that 5 stream of gases exhausting from such enan annular space 17 is left immediately bei gmes; hind the head 11. The steel wool 16 com- 1 A further important object resides in the pressively contacts the inner side of the shell 10 unique combination of the elements permit- 10 and the forward side of the apron 14. ting a free flow of gases through the silencing I form a spool member 18 having a central device and at the same time causing the gases hollow cylindrical barrel 19 and the forflowing therethrou'gh tobe slowed up in part ward and rear conical flanges 20 and 21, and expanded and cooled at intervals so that the barrel 19 and the flanges 20 and 21 being 15 the sound waves in the gas stream issuing provided with a plurality of holes therefrom the engine are broken up to such an exthrough, here shown as slots. Both flanges tent that there are no metallic pings or other 20 and 21 have their outer peripheries subnoises audible. stantially in contact with the inner side of A still further object resides in the means the shell 10 and the entire space between the for resisting the flow of gases through parts two flanges is filled with the steel wool 24. of the silencer and at the same time serving The flange 21 is preferably fixed to the shell to deaden and prevent vibration of various 10 by welding to form the attaching juncmembers embodied within the silencer. tures 22 and 23, Fig. 4. The other flange 20 6 These and other objects will become apis not attached to the shell so that the barrel parent in the following description of the in- 19 may expand longitudinally from the vention as illustrated by the accompanying flange 21 as the fixed member.
drawings, in which 7 The spool 18 is positioned longitudinally Fig. 1 is a fragmentary side elevation of Within the .shell 10 to have the plane of the a silencer embodying my invention; forward edge of the flange 20 substantially Fig. 2, a vertical transverse section on the at the plane of the end of the pipe 12 so that line 22 of Fig. 1; there is an appreciable space between the Fig. 3; a vertical transverse section on the flange 20 and the apron 14 bounded thereby li e 3-3 of Fig. 1; and fore and aft and by the shell 10 circumferig. 4, a vertical transverse section on the entially therearound. V 35 line 4-4 of Fig. 1. The rear end of the shell 10 has a head 25 Like characters of reference indicate like as a closure 'thereacross through which the parts throughout the several views in the tail pipe 26 is supported to pro ect inwardly drawings. to carry the exhaust head 27 on its forward 40 I form a cylindrical shell 10 having the end toward the rear of the flange 21. The
forward enclosing head 11 passed through. apron 28 is fixed to the pipe 26 behind the which is an intake pipe 12 to extend for an head 27 and flares outwardly and rearwardly appreciable distance axially .within the shell. toward and in substantial contact with the The inner end of the intake pipe 12 is closed shell 10. The space between the head 25 and and a plurality of openings 13 are spaced the rear of the apron 28 is filled with steel circumferentially around the pipe near the wool 29 with the exception of a small annuclosed end. Spaced forwardly a slight disla'r space around the inside of the shell 10 tance from the openings 13 is a conical apron at its juncture with the head 25.
14 which is fixed to and carried by/the pipe The head 27 is here shown as being com- 12. This apron 14 flares outwardly and rearprised of a forwardly and outwardly flarwardly to terminate substantially against ing wall 30 on the end of the pipe 26 having the slots 31 therethrough. A cap 32 encloses the forward opening to within the wall 30 and a frusto-conical apron 33 extends from the base of this cap rearwardly and spaced outwardly from the wall 30 to have an annular opening between it and the pipe 26. The exhaust head 27 is similar to the head as described in my previous application for patent, filed November 1, 1929, Serial No. 404,114.
In operation, gases flow from the pipe 12 out through the holes 13 where they may expand into the chamber there provided as above described. Some of this gas may escape forwardly through the holes 15 into the steel wool 16. Also gases may escape rearwardly through the holes in the flange into the steel wool 24 and through the holes in the barrel 19 or on back through the holes in the flange 21. There is no restriction in the barrel 19 so that gases may flow freely from the chamber around the I end of the pipe 12 therethrough. The gases discharging back of the flange 21 again may expand and come in contact with the cool wall 10 and may in part flow through the holes in theapron 28 into the steel wool therebehind. The main volume of the gases will however flow through the holes 31 in the wall 30 and turn and flow rearwardly out the tail pipe 26. While I have here described the material around the spool 18 and back of the aprons 14 and 28 as steel. wool, it is entirely possible and practical to use other material such as asbestos, metal shavings, porous cinders, porous or sponge iron and the like. -The essential feature of such material to be employed is that it be noncombustible and maintain a cellular-like condition to permit gas to flow therethrough but only by following devious paths.
Due to the close proximity of the holes 13 to the holes in the flan e 20, gases will flow throughthe holes in the flange 20 and drift out slowly into the barrel 19 thus causing a high resistance path at low engine speeds. I find that by leaving the unfilled spaces at the forward and rear ends of the material 16 and 29 respectively that an additional absorption is obtaine It is to be noted that substantially all of the reflecting surfaces against, which high velocity gases may hit are deadened by contact of steel wool. The parts of the shell which are shown as being packed with the steel wool are preferably designated as surge chambers since they tend to break up pressure waves within the shell itself and provide for a smooth resultant flow from the tail pipe.
While I have here shown and described my invention in the one form as now best own to me, it is obvious that structural variations may be made from that form without departing from the spirit of the invention and I, therefore, do not desire to be limited to that precise form, nor any more than may be required by the following claims.
I claim:
1. In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a material formed into a porous mass and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe projecting within the shell to have its forward end near the rear end of said barrel and surge chambers at each end of the shell formed by porous material around the intake and tail pipes.
2. In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe projecting within the shell to have its forward end near the rear end of said barrel, said intake and tail pipes being closed across theirinner endsantthavingholes through side walls near the closed ends and surge chambers at each end of the shell formed by p0- rous material around the intake. and tail pipes.
3. In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the for ward end of said barrel, and said tail pipe projecting within the shell to have its forward end near the rear end of said barrel, said intake and tail pipes being closed across their inner ends and having holes through side walls near the closed ends and surge chambers at each end of the shell formed by porous material around the intake and tail pipes and perforated flanges extending from each end of said barrel toward said shell confining said first-mentioned material therebetween.
4. In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pi pe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, both said intake and tail pipe having extensions within the shell directed toward said'sur e chamber, porous material between the inta e pipe extension and the shell, and
porous material between the tail pipe extension and the shell.
5. In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe extending within the shell to have its forward end near the rear end of said barrel, a filling of porous material between a part of the length of both of the extensions and the shell, and perforate aprons extending from the pipes toward the shell to confine said material and define expansion chambers at each end' of said barrel.
6. In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the shell toward and terminating near the forward end of said barrel, and said tail pipe extending within the shell to have its forward end near the rear end of said barrel, a filling ofporous material between a part of the length of both extensions and the shell, and perforate aprons extending from the pipes toward the shell to confine said material and define expansion chambers at each end of said barrel, the inner ends of both the intake and tail pipes being closed, said pipes having holes through side walls near said inner ends.
7 In an exhaust gas silencer, a shell, an intake pipe discharging into the shell, a tail pipe discharging from the shell, a surge chamber formed by filling a length of the shell with a porous material, and a barrel through the material having openings through its side walls, said intake pipe extending within the. shell toward and terminating near the forward end of said. barrel, and said tail pipe extending within the shell to have its forward end near the rear end of said barrel, a filling of porous material between a part of the length of both extensions and the shell, and perforate aprons extending from the pipes toward the shell to confine said material and define expansion chambers at each end of said barrel, a head in each end of said shell, said last mentioned filling of porous material terminating to leave an annular-open space therearound adjacent the juncture of said heads and said shell.
8. In an exhaust gas silencer, a shell, a head in each end of the shell, an intake pipe extended through one head, a tail pipe extended through the other head, a spool fixedin the central part of inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, means on the inner end of the tail pipe to deflect the gas and steel wool around the tail pipe.
9. In an exhaust gas silencer, a shell, a head in each end of the shell, an intake pipe extended through one head, a tail pipe extended through the other head, a spoolfixed in the central part of the shell spaced between the inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, said intake pipe having its inner end closed and having holes through its side wall near the end, an apron carried on the intake pipe spaced forwardly from its inner end, and steel wool wrapped around said intake pipe between said apron and said one head.
10. In an exhaust gas silencer, a shell, a head in each end of the shell, an intake pipe extended through one head, a tail pipe extended through the other head, a spool fixed in the central part of the shellspaeed between the inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, said tail pipe having a cap over its inner end and holes through a side wall near the end, an apron fixed on the tail ipe, and steel wool wrapped around the tail pipe lietween said apron and said other head.
11. In an exhaust gas silencer a shell, a head in each end of the shell, an lntake pipe extended through one head, a tail pipe extended through the other head, a spool fixed in the central part of the shell spaced between the inner ends of said pipes, said spool having a central perforate barrel and steel wool wrapped around said barrel, and a perforate fiangeat each end of the barrel extending toward said shell and confining said steel wool therebetween, said tail pipe having a cap over its inner end and steel wool wrapped around the tail pipe between the cap and other head.
In testimony whereof I aflix my signature.
FRANCIS F. HAMILTON.
the shell spaced between the
US455403A 1930-05-24 1930-05-24 Exhaust gas silencer Expired - Lifetime US1857845A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563509A (en) * 1951-08-07 Valve controlled silencer
US2685936A (en) * 1950-08-08 1954-08-10 Lockheed Aircraft Corp Sound reduction equipment for use with jet-propulsion units
US2828830A (en) * 1956-10-08 1958-04-01 John C Clark Non-directional muffler
US3851727A (en) * 1974-04-19 1974-12-03 Caterpillar Tractor Co Muffler with insulated internal sound dispersing and absorbing chambers
US4134472A (en) * 1977-08-29 1979-01-16 Trainor John B Combination muffler and air filter
US5667367A (en) * 1994-04-08 1997-09-16 Kabushiki Kaisha Kobe Seiko Sho Air compressor
US6082487A (en) * 1998-02-13 2000-07-04 Donaldson Company, Inc. Mufflers for use with engine retarders; and methods
US6354398B1 (en) 1998-02-13 2002-03-12 Donaldson Company, Inc. Mufflers for use with engine retarders; and methods
WO2008006383A1 (en) * 2006-07-14 2008-01-17 Silentor Holding A/S Manufacture-friendly silencer

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563509A (en) * 1951-08-07 Valve controlled silencer
US2685936A (en) * 1950-08-08 1954-08-10 Lockheed Aircraft Corp Sound reduction equipment for use with jet-propulsion units
US2828830A (en) * 1956-10-08 1958-04-01 John C Clark Non-directional muffler
US3851727A (en) * 1974-04-19 1974-12-03 Caterpillar Tractor Co Muffler with insulated internal sound dispersing and absorbing chambers
US4134472A (en) * 1977-08-29 1979-01-16 Trainor John B Combination muffler and air filter
US5667367A (en) * 1994-04-08 1997-09-16 Kabushiki Kaisha Kobe Seiko Sho Air compressor
US6082487A (en) * 1998-02-13 2000-07-04 Donaldson Company, Inc. Mufflers for use with engine retarders; and methods
US6354398B1 (en) 1998-02-13 2002-03-12 Donaldson Company, Inc. Mufflers for use with engine retarders; and methods
WO2008006383A1 (en) * 2006-07-14 2008-01-17 Silentor Holding A/S Manufacture-friendly silencer

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