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US3016972A - Muffler for an internal combustion engine - Google Patents

Muffler for an internal combustion engine Download PDF

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Publication number
US3016972A
US3016972A US805571A US80557159A US3016972A US 3016972 A US3016972 A US 3016972A US 805571 A US805571 A US 805571A US 80557159 A US80557159 A US 80557159A US 3016972 A US3016972 A US 3016972A
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nipples
chamber
partition
internal combustion
partitions
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US805571A
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Rebert J Dugas
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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
    • F01N1/083Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling using transversal baffles defining a tortuous path for the gases or successively throttling gas flow

Definitions

  • the present invention relates to a muffler for an internal combustion engine. 1
  • An object of the present invention is to provide, in a mufiler for an internal combustion engine, means for suppressing then'oises of the explosions of fuel-air mix tures in the engine Without increasing back pressure gases flowing from the engine.
  • Another object of the present invention is to provide a mufller for an internal combustion engine which provides as short as possible a route or passage for the flow of exhaust gases from the engine to atmosphere, with efiicient suppression of noise of the gases emitted to atmosphere.
  • a further object of the present invention is to provide a muffler for an internal combustion engine which permits an engine to operate at a lower operating temperature by providing means for dissipating the heat to atmosphere rapidly and efliciently, with little or no condensation of water vapor in the mufiler, and with substantially total suppression of the noise of the exhaust gases omitted to atmosphere.
  • FIGURE 1 is an isometric view of the muffier of the present invention with a portion of the wall cut away to showthe interior of the muflier;
  • FIGURE 2 is a view taken on the line 2-2 of FIG- URE 1.
  • FIGURE 1 the reference numeral 10 designates the shell, constituting a tunnel member, of the muffler of the present invention.
  • the tunnel member or shell 10 has a plate 12 closing one of its ends and another plate 14 closing the other of its ends.
  • the end plate 12 is provided with a tubular inlet 16 for receiving exhaust gases from an internal combustion engine and for attachment to the exhaust pipe of such engine.
  • the plate 14 is provided with a tubular outlet 18 for attachment to a vehicle tail pipe or other means of discharging exhaust gases from the shell 10.
  • Partitions 2t] and 22, and partitions 24 and 26, subdivide the interior of the shell 10 into two constraining chambers 28 and 3% with the chamber 28 adjacent and inwardly of the end plate 12 and with the chamber 30 adjacent and inwardly of the end plate 14.
  • the chamber 28 has ingress means embodying a plu- 2 rality of nipples 32 arranged in a ring and supported intermediate their ends in the partition 20. Another nipple 34 is supported in the partition 20 centrally thereof. The ends of the nipples 32 and 34 within the chamber 28 are formed at an acute angle with the cut ends or angled ends of the nipples 32 disposed so as to face the nipple 34.
  • the partition 24' is similarly provided with a plurality of nipples 36 arranged in a ring and in spaced relation with each nipple 36 having a cut end within the chamber 30.
  • the cut ends of the nipples 36 face toward the center of the ring that they form and constitute ingress means for the chamber 30.
  • the nipples 36 are supported intermediate their ends in the partition 24.
  • the open ended nipples 32, 34, and 36 are supported in their respective partitions 20 and 24 by welding or other suitable means, not shown. It is to be noted that the nipples 32, 34 and 36 of their respective partitions 20 and 24 are disposed in spaced relation with the parts contiguous to the acute angles being adjacent the perimeter of the partitions and the acute angles being remote from the perimeter of the partitions.
  • Each of the chambers 28 and 30 has egress means.
  • This means, in the chamber 28, embodies spaced apertures 38 in the partition 22.
  • Apertures 40 in the partition 26 are arranged in spaced relation and constitute the egress means for the chamber 30.
  • the nipples 32 and 34 in the partition 20 are of a larger inside diameter than the nipples 36 of the partition 24.
  • the apertures 38 of the partition 22 are of a larger diameter than the apertures 40 of the partition 26.
  • the space between the partitions 22 and 24 constitutes a collection chamber, designated by the numeral 42, separating the constraining chambers 28 and 30.
  • the space between the end plate 12 and the partition 20 constitutes a receiving chamber 44 and the space between the partition 26 and the other end plate 14 constitutes an exit chamber 46.
  • the tunnel member or shell Ill is provided with annular grooves as at 48 in FIGURE 2 receiving the peripheral portions of the partitions 2%, 22, 24, and 26, and also other similar grooves receiving the peripheral portions of the end plates 12 and 14.
  • the transversely arranged partitions and end plates are fixedly secured by welding or other suitable means, not shown, to the inner wall of the shell 10.
  • the tubular inlet 16 is connected to the exhaust pipe of an internal combustion engine and the outlet 18 connected to a tail pipe or other means for venting exhaust gases to atmosphere at a suitable location.
  • Gases received into the tubular member or shell 10 through the inlet 16 pass into the receiving chamber 44 and then through the nip les 32 and 34 into the first constraining chamber 28.
  • the gases then pass through the apertures 38 in the partition 22 into the collection chamber 42 and then through the nipples 36 into the other constraining chamber 30.
  • the gases flow through the apertures 40 in the partition 26 and into the exit chamber 46 from whence they are discharged through the outlet 18 to atmosphere.
  • Sound waves entering the shell ltl from the inlet 16 are substantially canceled out by out of phase sound waves generated by the portions of the partitions 20 and 24 exteriorly of the nipples 32, 34, and 36, and by portions of the partitions 22 and 26 exteriorly of the apertures 38 and 40.
  • the internal diameters of the nipples 32 and 34 are larger than the internal diameters of the nipples 36. Also, the size of the apertures 38 and 40 bear the same relationship to each other as the nipples 32 and 34 bear to the nipples 36.
  • 9 B 26 may be secured within the elongated shell by Welding, crimping, or by pressed fitting it found to be practical.
  • the spacing of the partitions relative to each other and to the end plates is not to be limited to the spacing shown in FIGURES 1 and 2 but may be varied to any other spacingif desired and the size of the apertures 38 and 4t) and the size of the nipples 32, 34 and 36 may be altered to accommodate the gases of any type of internal a combustion engine with which the muflier of the present invention is to be employed.
  • an open-ended elongated tunnel member an end plate closing one end of said member and having an inlet for receiving exhaust gases from an internal combustion engine,- another end plate closing the other end of said member and having an outlet for dis charging the exhaust gases from said member, a pair of partitions extending transversely of said member inwardly of and adjacent each of said end plates and fixedly attached to said member, each of said partitions and the portions of said member therebetween forming a constraining chamber, one of the partitions of each'cham-- her being provided with ingress means embodying a plurality of open-ended nipples and the other of the partitions of said chamber being provided with egress means embodying a plurality of apertures, the nipples of each partition being disposed so that the intermediate portions are supported in said partition with one end within the adjacent chamber and facing toward the apertured partition of said chamber and the other end exteriorly of said chamber and facing toward the adjacent end plate of said member, said one end of each nipple being formed at
  • nipples in the partition of the chamber adjacent the inlet containing end plate are disposed so that one of the nipples is centrally of the partition with the remaining nipples being disposed in a ring and each having the acute angle facing toward said one nipple.

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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

Jan. 16, 1962 R. J. DUGAS MUFFLER FoR AN INTERNAL COMBUSTION ENGINE Filed April 10, 1959 lrf II [N V EN TOR.
wwwflm JQM'MAM ATTORNEYS.
Patented Jan. 16, IQSZ 3,016,972 MUFFLER F012 AN ENTERNAL C(BMBUSTION ENGENE Rebert .ll. Dugas, 608 Lewis St, New Iberia, La. Fiied Apr. 16, 11959, Ser. No. 895,571 3 Claims. (6i. 181-56) The present invention relates to a muffler for an internal combustion engine. 1
Presently in use and previously proposed 'are mufflers for internal combustion engines of various constructions. All the muffiers have for their main consideration the suppression of the noise created by the explosion of a fuelair mixture within the cylinders of the internal combus tion engine. Suppression of noise may be accomplished by absorption of the sound waves created by the explosions or by canceling out of the sound waves by producing identical sound waves in opposite phase and impinging the out of phase waves on each other. Such mufflers have not been wholly successful for the reason that generally the structures proposed or provided increase the back pressure of the combustion gases, resulting in a lowering of the horsepower available in the respective engine.
An object of the present invention is to provide, in a mufiler for an internal combustion engine, means for suppressing then'oises of the explosions of fuel-air mix tures in the engine Without increasing back pressure gases flowing from the engine.
Another object of the present invention is to provide a mufller for an internal combustion engine which provides as short as possible a route or passage for the flow of exhaust gases from the engine to atmosphere, with efiicient suppression of noise of the gases emitted to atmosphere.
A further object of the present invention is to provide a muffler for an internal combustion engine which permits an engine to operate at a lower operating temperature by providing means for dissipating the heat to atmosphere rapidly and efliciently, with little or no condensation of water vapor in the mufiler, and with substantially total suppression of the noise of the exhaust gases omitted to atmosphere.
These and other objects and advantages of the present invention will be fully apparent from the following description when taken in conjunction with the annexed drawing, in which:
FIGURE 1 is an isometric view of the muffier of the present invention with a portion of the wall cut away to showthe interior of the muflier; and
FIGURE 2 is a view taken on the line 2-2 of FIG- URE 1.
Referring in greater detail to the drawing in which like numerals indicate like parts throughout the several views, in FIGURE 1 the reference numeral 10 designates the shell, constituting a tunnel member, of the muffler of the present invention. The tunnel member or shell 10 has a plate 12 closing one of its ends and another plate 14 closing the other of its ends. The end plate 12 is provided with a tubular inlet 16 for receiving exhaust gases from an internal combustion engine and for attachment to the exhaust pipe of such engine. The plate 14 is provided with a tubular outlet 18 for attachment to a vehicle tail pipe or other means of discharging exhaust gases from the shell 10.
Partitions 2t] and 22, and partitions 24 and 26, subdivide the interior of the shell 10 into two constraining chambers 28 and 3% with the chamber 28 adjacent and inwardly of the end plate 12 and with the chamber 30 adjacent and inwardly of the end plate 14.
The chamber 28 has ingress means embodying a plu- 2 rality of nipples 32 arranged in a ring and supported intermediate their ends in the partition 20. Another nipple 34 is supported in the partition 20 centrally thereof. The ends of the nipples 32 and 34 within the chamber 28 are formed at an acute angle with the cut ends or angled ends of the nipples 32 disposed so as to face the nipple 34.
The partition 24' is similarly provided with a plurality of nipples 36 arranged in a ring and in spaced relation with each nipple 36 having a cut end within the chamber 30. The cut ends of the nipples 36 face toward the center of the ring that they form and constitute ingress means for the chamber 30. The nipples 36 are supported intermediate their ends in the partition 24.
The open ended nipples 32, 34, and 36, are supported in their respective partitions 20 and 24 by welding or other suitable means, not shown. It is to be noted that the nipples 32, 34 and 36 of their respective partitions 20 and 24 are disposed in spaced relation with the parts contiguous to the acute angles being adjacent the perimeter of the partitions and the acute angles being remote from the perimeter of the partitions.
Each of the chambers 28 and 30 has egress means. This means, in the chamber 28, embodies spaced apertures 38 in the partition 22. Apertures 40 in the partition 26 are arranged in spaced relation and constitute the egress means for the chamber 30. The nipples 32 and 34 in the partition 20 are of a larger inside diameter than the nipples 36 of the partition 24. Likewise, the apertures 38 of the partition 22 are of a larger diameter than the apertures 40 of the partition 26.
The space between the partitions 22 and 24 constitutes a collection chamber, designated by the numeral 42, separating the constraining chambers 28 and 30. The space between the end plate 12 and the partition 20 constitutes a receiving chamber 44 and the space between the partition 26 and the other end plate 14 constitutes an exit chamber 46.
The tunnel member or shell Ill is provided with annular grooves as at 48 in FIGURE 2 receiving the peripheral portions of the partitions 2%, 22, 24, and 26, and also other similar grooves receiving the peripheral portions of the end plates 12 and 14. The transversely arranged partitions and end plates are fixedly secured by welding or other suitable means, not shown, to the inner wall of the shell 10.
In use, the tubular inlet 16 is connected to the exhaust pipe of an internal combustion engine and the outlet 18 connected to a tail pipe or other means for venting exhaust gases to atmosphere at a suitable location. Gases received into the tubular member or shell 10 through the inlet 16 pass into the receiving chamber 44 and then through the nip les 32 and 34 into the first constraining chamber 28. The gases then pass through the apertures 38 in the partition 22 into the collection chamber 42 and then through the nipples 36 into the other constraining chamber 30. Finally, the gases flow through the apertures 40 in the partition 26 and into the exit chamber 46 from whence they are discharged through the outlet 18 to atmosphere. Sound waves entering the shell ltl from the inlet 16 are substantially canceled out by out of phase sound waves generated by the portions of the partitions 20 and 24 exteriorly of the nipples 32, 34, and 36, and by portions of the partitions 22 and 26 exteriorly of the apertures 38 and 40.
Although specific dimensions are not here included, it is to be noted that the internal diameters of the nipples 32 and 34 are larger than the internal diameters of the nipples 36. Also, the size of the apertures 38 and 40 bear the same relationship to each other as the nipples 32 and 34 bear to the nipples 36.
The end plates 12 and 14, and partitions 20, 22, 24, and
9 B 26 may be secured within the elongated shell by Welding, crimping, or by pressed fitting it found to be practical. The spacing of the partitions relative to each other and to the end plates is not to be limited to the spacing shown in FIGURES 1 and 2 but may be varied to any other spacingif desired and the size of the apertures 38 and 4t) and the size of the nipples 32, 34 and 36 may be altered to accommodate the gases of any type of internal a combustion engine with which the muflier of the present invention is to be employed.
What is claimed is:
1. In a muffler, an open-ended elongated tunnel member, an end plate closing one end of said member and having an inlet for receiving exhaust gases from an internal combustion engine,- another end plate closing the other end of said member and having an outlet for dis charging the exhaust gases from said member, a pair of partitions extending transversely of said member inwardly of and adjacent each of said end plates and fixedly attached to said member, each of said partitions and the portions of said member therebetween forming a constraining chamber, one of the partitions of each'cham-- her being provided with ingress means embodying a plurality of open-ended nipples and the other of the partitions of said chamber being provided with egress means embodying a plurality of apertures, the nipples of each partition being disposed so that the intermediate portions are supported in said partition with one end within the adjacent chamber and facing toward the apertured partition of said chamber and the other end exteriorly of said chamber and facing toward the adjacent end plate of said member, said one end of each nipple being formed at an acute angle, the nipples of each partition being arranged in spaced relation thereabout with the angles being adjacent the perimeter of said partition and the parts contiguous to the acute angles being remote from the perimeter of said partition, the apertures and nipples of the ingress and egress means of said one chamber being of a larger diameter than the apertures and nipples 0f the ingress and egress means of said other chamber.
2. The muffler according to claim 1, wherein the nipples in the partition of the chamber adjacent the outlet containing endplate are disposed in a ring and each having the acute angles facing toward the center of the ring.
3. The muffier according to claim 1, wherein the nipples in the partition of the chamber adjacent the inlet containing end plate are disposed so that one of the nipples is centrally of the partition with the remaining nipples being disposed in a ring and each having the acute angle facing toward said one nipple.
References Cited in the tile of this patent UNITED STATES PATENTS Porter Sept. 26, 1911
US805571A 1959-04-10 1959-04-10 Muffler for an internal combustion engine Expired - Lifetime US3016972A (en)

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Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3101811A (en) * 1960-10-19 1963-08-27 Aircraft Prec Products Inc Marine type muffler
US3220508A (en) * 1961-10-11 1965-11-30 Gen Motors Corp Muffler with interlocked casing and baffle members
DE1247749B (en) * 1961-11-16 1967-08-17 Berliet Automobiles Exhaust silencers for internal combustion engines
US3897853A (en) * 1971-11-24 1975-08-05 Silentor As Silencer
US4177875A (en) * 1977-08-15 1979-12-11 Toyota Jidosha Kogyo Kabushiki Kaisha Muffler for internal combustion engine
US4919710A (en) * 1987-02-20 1990-04-24 Mitsui Petrochemical Industries, Ltd. Condensate drainage apparatus
WO1994002718A1 (en) * 1992-07-20 1994-02-03 Alexandr Viktorovich Chistov Exhaust silencer for internal combustion engine
US6170528B1 (en) * 1999-07-26 2001-01-09 Tapco International, Inc. Assembly of orifice chambers progressively reducing operating pressure for large gas flows
US6302235B1 (en) * 2000-03-03 2001-10-16 Carson J. Matherne High-performance muffler
US6364054B1 (en) 2000-01-27 2002-04-02 Midas International Corporation High performance muffler
US20040216951A1 (en) * 2003-05-01 2004-11-04 Chao Cai High performance muffler
US20070240932A1 (en) * 2006-04-12 2007-10-18 Van De Flier Peter B Long fiber thermoplastic composite muffler system with integrated reflective chamber
US20070240934A1 (en) * 2006-04-12 2007-10-18 Van De Flier Peter Long fiber thermoplastic composite muffler system
US20080178583A1 (en) * 2007-01-12 2008-07-31 Yuguang Zhang Device with Trace Emission for Treatment of Exhaust Gas
US20080181830A1 (en) * 2007-01-30 2008-07-31 Yuguang Zhang Device with No Emission for Treatment of Exhaust Gas
US20080209898A1 (en) * 2006-02-17 2008-09-04 Saes Getters S.P.A. Fumes Treatment System
US20090014236A1 (en) * 2006-04-12 2009-01-15 Van De Flier Peter B Long fiber thermoplastic composite muffler system with integrated crash management
US20100307863A1 (en) * 2007-12-14 2010-12-09 Ocv Intellectual Capital, Llc Composite muffler system thermosetable polymers
US8016071B1 (en) * 2010-06-21 2011-09-13 Trane International Inc. Multi-stage low pressure drop muffler
US20120103719A1 (en) * 2009-03-23 2012-05-03 Vortex Performance Limited exhaust filter
US8307943B2 (en) * 2010-07-29 2012-11-13 General Electric Company High pressure drop muffling system
US8430202B1 (en) 2011-12-28 2013-04-30 General Electric Company Compact high-pressure exhaust muffling devices
US8511096B1 (en) 2012-04-17 2013-08-20 General Electric Company High bleed flow muffling system
US8550208B1 (en) 2012-04-23 2013-10-08 General Electric Company High pressure muffling devices
US20130280109A1 (en) * 2010-09-23 2013-10-24 Michael J. Lucas Modular discharge silencer for vehicle-mounted compressor
US9399951B2 (en) 2012-04-17 2016-07-26 General Electric Company Modular louver system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1004195A (en) * 1911-04-06 1911-09-26 Alden Walter Porter Exhaust-muffler.
US1539595A (en) * 1921-10-10 1925-05-26 Powell Herbert Spencer Muffler for explosive engines
US1810252A (en) * 1930-03-17 1931-06-16 Albert S Noonan Exhaust muffler for internal combustion engines
US2194550A (en) * 1937-06-23 1940-03-26 Buffalo Pressed Steel Company Muffler
US2624418A (en) * 1951-08-01 1953-01-06 Maxim Silencer Co Muffler with plural passages
US2919761A (en) * 1957-05-13 1960-01-05 Vernon N Holderman Mufflers

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1004195A (en) * 1911-04-06 1911-09-26 Alden Walter Porter Exhaust-muffler.
US1539595A (en) * 1921-10-10 1925-05-26 Powell Herbert Spencer Muffler for explosive engines
US1810252A (en) * 1930-03-17 1931-06-16 Albert S Noonan Exhaust muffler for internal combustion engines
US2194550A (en) * 1937-06-23 1940-03-26 Buffalo Pressed Steel Company Muffler
US2624418A (en) * 1951-08-01 1953-01-06 Maxim Silencer Co Muffler with plural passages
US2919761A (en) * 1957-05-13 1960-01-05 Vernon N Holderman Mufflers

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3101811A (en) * 1960-10-19 1963-08-27 Aircraft Prec Products Inc Marine type muffler
US3220508A (en) * 1961-10-11 1965-11-30 Gen Motors Corp Muffler with interlocked casing and baffle members
DE1247749B (en) * 1961-11-16 1967-08-17 Berliet Automobiles Exhaust silencers for internal combustion engines
US3897853A (en) * 1971-11-24 1975-08-05 Silentor As Silencer
US4177875A (en) * 1977-08-15 1979-12-11 Toyota Jidosha Kogyo Kabushiki Kaisha Muffler for internal combustion engine
US4919710A (en) * 1987-02-20 1990-04-24 Mitsui Petrochemical Industries, Ltd. Condensate drainage apparatus
WO1994002718A1 (en) * 1992-07-20 1994-02-03 Alexandr Viktorovich Chistov Exhaust silencer for internal combustion engine
US6170528B1 (en) * 1999-07-26 2001-01-09 Tapco International, Inc. Assembly of orifice chambers progressively reducing operating pressure for large gas flows
US6364054B1 (en) 2000-01-27 2002-04-02 Midas International Corporation High performance muffler
US6382349B2 (en) * 2000-03-03 2002-05-07 Carson J. Matherne High-performance muffler
US6302235B1 (en) * 2000-03-03 2001-10-16 Carson J. Matherne High-performance muffler
US20040216951A1 (en) * 2003-05-01 2004-11-04 Chao Cai High performance muffler
US6892853B2 (en) * 2003-05-01 2005-05-17 Agency For Science Technology And Research High performance muffler
US20080209898A1 (en) * 2006-02-17 2008-09-04 Saes Getters S.P.A. Fumes Treatment System
US7934580B2 (en) * 2006-04-12 2011-05-03 Ocv Intellectual Capital, Llc Long fiber thermoplastic composite muffler system
US20070240932A1 (en) * 2006-04-12 2007-10-18 Van De Flier Peter B Long fiber thermoplastic composite muffler system with integrated reflective chamber
US20070240934A1 (en) * 2006-04-12 2007-10-18 Van De Flier Peter Long fiber thermoplastic composite muffler system
US20090014236A1 (en) * 2006-04-12 2009-01-15 Van De Flier Peter B Long fiber thermoplastic composite muffler system with integrated crash management
US7730996B2 (en) 2006-04-12 2010-06-08 Ocv Intellectual Capital, Llc Long fiber thermoplastic composite muffler system with integrated crash management
US7942237B2 (en) 2006-04-12 2011-05-17 Ocv Intellectual Capital, Llc Long fiber thermoplastic composite muffler system with integrated reflective chamber
US20080178583A1 (en) * 2007-01-12 2008-07-31 Yuguang Zhang Device with Trace Emission for Treatment of Exhaust Gas
US7857095B2 (en) * 2007-01-12 2010-12-28 Yuguang Zhang Device with trace emission for treatment of exhaust gas
US20080181830A1 (en) * 2007-01-30 2008-07-31 Yuguang Zhang Device with No Emission for Treatment of Exhaust Gas
US7955408B2 (en) * 2007-01-30 2011-06-07 Yuguang Zhang Device with no emission for treatment of exhaust gas
US20100307863A1 (en) * 2007-12-14 2010-12-09 Ocv Intellectual Capital, Llc Composite muffler system thermosetable polymers
US20120103719A1 (en) * 2009-03-23 2012-05-03 Vortex Performance Limited exhaust filter
US8627921B2 (en) * 2009-03-23 2014-01-14 Barry Mead Exhaust filter
US8016071B1 (en) * 2010-06-21 2011-09-13 Trane International Inc. Multi-stage low pressure drop muffler
US8307943B2 (en) * 2010-07-29 2012-11-13 General Electric Company High pressure drop muffling system
US20130280109A1 (en) * 2010-09-23 2013-10-24 Michael J. Lucas Modular discharge silencer for vehicle-mounted compressor
US9657732B2 (en) * 2010-09-23 2017-05-23 Ingersoll-Rand Company Modular discharge silencer for vehicle-mounted compressor
US8430202B1 (en) 2011-12-28 2013-04-30 General Electric Company Compact high-pressure exhaust muffling devices
US8511096B1 (en) 2012-04-17 2013-08-20 General Electric Company High bleed flow muffling system
US9399951B2 (en) 2012-04-17 2016-07-26 General Electric Company Modular louver system
US8550208B1 (en) 2012-04-23 2013-10-08 General Electric Company High pressure muffling devices

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