US2624418A - Muffler with plural passages - Google Patents

Muffler with plural passages Download PDF

Info

Publication number
US2624418A
US2624418A US239674A US23967451A US2624418A US 2624418 A US2624418 A US 2624418A US 239674 A US239674 A US 239674A US 23967451 A US23967451 A US 23967451A US 2624418 A US2624418 A US 2624418A
Authority
US
United States
Prior art keywords
tubes
chamber
shell
series
muffler
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US239674A
Inventor
Roland B Bourne
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Maxim Silencer Co
Original Assignee
Maxim Silencer Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Maxim Silencer Co filed Critical Maxim Silencer Co
Priority to US239674A priority Critical patent/US2624418A/en
Application granted granted Critical
Publication of US2624418A publication Critical patent/US2624418A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/18Construction facilitating manufacture, assembly, or disassembly
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/08Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
    • F01N1/089Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling using two or more expansion chambers in series
    • 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
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/02Two or more expansion chambers in series connected by means of tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2510/00Surface coverings
    • F01N2510/04Surface coverings for sound absorption
    • 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
    • F01N2530/00Selection of materials for tubes, chambers or housings
    • F01N2530/26Multi-layered walls

Definitions

  • This invention relates to silencing devicesfor internal combustion engines, and in particular to silencers which are mounted in confined spaces: which require holding the diameter of the shellof the silencer to a minimum.
  • One object is to produce a silencer which comprises an expansion: chamber into and out of which the exhaust gas capable of withstanding high external hydraulic pressure and so constructed as to reduce greatly the transmission of sound from the silencerto the surrounding water.
  • Fig. l is a median section through the silencer, taken on line l-I of Figs. 2 to 6 inclusive;
  • Fig. 2 is a section on line 2-2 of Fig. 1;
  • Fig. 3 is a section on line 33 of Fig. 1;
  • Fig. 4 is a section on line 4-4 of Fig. 1;
  • Fig. 5 is a section on line 55 of Fig. 1;
  • Fig. 6 is a section on line 66 of Fig. 1'.
  • the silencer is enclosed primarily in a cylindrical pressure shell l0, preferably of circular cross-section and formed of stainless steel about one inch thick so that it will withstand a pressure of 700. p. s. i. g.
  • a cylindrical pressure shell l0 preferably of circular cross-section and formed of stainless steel about one inch thick so that it will withstand a pressure of 700.
  • p. s. i. g. Within the pressure shell are cylindrical laminations of sheet metal H and I2, here shown as two in number, but which may be varied in number in different chambers of the silencer if desired. These laminations are not relied on so much for strength as for deadening sound transmission through the outer shell, and in combination with a pressure shell which is relatively massive prove remarkably and unexpectedly eflicient in that regard.
  • An inlet conduit l3 passes through one end of the pressure shell into 'a chamber l4 defined by the shell and an intermediate transverse partition I5.
  • the inlet conduit terminates with an open end at approximately the midpoint of the chamber H.
  • 6 enters the other end of the pressure shell and terminates with an open end within and about halfway along a chamber l1 defined by the pressure shell and a second intermediate transverse partition 18.
  • the inlet and outlet conduits preferably have antiresonance slots l9 and respectively.
  • , preferably 2 having their entrance ends flared as at 22, are circumferentially spaced as best shown in Fig. 3 and extend from a point in chamber l4 adjacent the terminus of the inlet conduit through the partition l5 and open into the chamber 23 formed between partitions I5 and IS.
  • a second circular series of tubes 24 pass through the partition I8, and have open ends in both chamber 23 and chamber ll, terminating in the latter adjacent the entrance end of the outlet conduit.
  • the entrance ends of the tubes 24 are preferably flared at 25 and that of the outlet conduit flared at 26.
  • are located radially outwardly of the inlet conduit so that there can be no direct gas or sound passage from one to the other, and that a similar relationship exists between tubes 24 and the outlet conduit IB.
  • and tubes 24 are both arranged in sets adjacent the shell of the silencer, and in order to prevent direct transmission the ends of tubes 2! are bent inwardly towards the center of the chamber 23 as is shown in Figs. 1 and 4.
  • and 24 are preferably provided with anti-resonance holes 27 as described in my Patent 2,297,046, September 29, 1942.
  • a silencer having a substantially cylindrical shell, a pair of spaced partitions dividing the interior of the shell into three chambers, an inlet conduit leading into the first chamber and terminating with an open end near the center thereof, a circumferentially spaced series of tubes located radially outwardly of the inlet conduit each having open ends one substantially in the plane of the open end of the inlet conduit and the other near the center of the second chamber, said tubes passing through the first partition into the second chamber and slanting radially inwardly towards the axis thereof, a second circumferentially spaced series of tubes circumferentially staggered with relation to the tubes of the first series, said second series of tubes extending substantially straight through the second partition into the second and third chambers and having open ends at substantially the mid-points of said chambers, and an outlet conduit entering the third chamber through the shell and terminating with an open end substantially in the plane of the open ends of the second series of tubes but located radially inwardly thereof.
  • a silencer having a substantially cylindrical shell, a. pair of transverse partitions dividing the interior of the shell into three chambers, a pair of conduits coaxial with the shell and entering each end chamber respectively with an open end REFERENCES CITED at a point intermediate its length
  • the following references are of record in the circumferentially spaced tubes located adjacent file of this patent: the peripheries of said end chambers and sta gered circumferentially with respect to each other, 5 UNITED STATES PATENTS the tubes in each series terminating at substan- Number Name Date tially the midpoint of the middle chamber with 2,265,342 Bourne Dec. 9, 941

Description

Jan. 6, 1953 R. B. BOURNE 2,624,418
I MUFFLER WITH PLURAL PASSAGES Filed Aug. 1, 1951 Roland B. Bourne Inventor Patented Jan. 6, 1953 MUFFLER WITH PLURAL PAS SAGES Roland B. Bourne, West Hartford, 001111., asslgnor to The Maxim Silencer Company, Hartford, Conn., a corporation of Connecticut Application August 1, 1951, Serial No. 239,674
2 Claims.
This invention relates to silencing devicesfor internal combustion engines, and in particular to silencers which are mounted in confined spaces: which require holding the diameter of the shellof the silencer to a minimum. One object is to produce a silencer which comprises an expansion: chamber into and out of which the exhaust gas capable of withstanding high external hydraulic pressure and so constructed as to reduce greatly the transmission of sound from the silencerto the surrounding water.
The invention will now be described with ref: erence to the accompanying drawing, in which Fig. l is a median section through the silencer, taken on line l-I of Figs. 2 to 6 inclusive;
Fig. 2 is a section on line 2-2 of Fig. 1;
Fig. 3 is a section on line 33 of Fig. 1;
Fig. 4 is a section on line 4-4 of Fig. 1;
Fig. 5 is a section on line 55 of Fig. 1; and
Fig. 6 is a section on line 66 of Fig. 1'.
The silencer is enclosed primarily in a cylindrical pressure shell l0, preferably of circular cross-section and formed of stainless steel about one inch thick so that it will withstand a pressure of 700. p. s. i. g. Within the pressure shell are cylindrical laminations of sheet metal H and I2, here shown as two in number, but which may be varied in number in different chambers of the silencer if desired. These laminations are not relied on so much for strength as for deadening sound transmission through the outer shell, and in combination with a pressure shell which is relatively massive prove remarkably and unexpectedly eflicient in that regard. An inlet conduit l3 passes through one end of the pressure shell into 'a chamber l4 defined by the shell and an intermediate transverse partition I5. The inlet conduit terminates with an open end at approximately the midpoint of the chamber H. An outlet conduit |6 enters the other end of the pressure shell and terminates with an open end within and about halfway along a chamber l1 defined by the pressure shell and a second intermediate transverse partition 18. The inlet and outlet conduits preferably have antiresonance slots l9 and respectively.
A plurality of intermediate tubes 2|, preferably 2 having their entrance ends flared as at 22, are circumferentially spaced as best shown in Fig. 3 and extend from a point in chamber l4 adjacent the terminus of the inlet conduit through the partition l5 and open into the chamber 23 formed between partitions I5 and IS. A second circular series of tubes 24 pass through the partition I8, and have open ends in both chamber 23 and chamber ll, terminating in the latter adjacent the entrance end of the outlet conduit. The entrance ends of the tubes 24 are preferably flared at 25 and that of the outlet conduit flared at 26.
It will be noted that the series of tubes 2| are located radially outwardly of the inlet conduit so that there can be no direct gas or sound passage from one to the other, and that a similar relationship exists between tubes 24 and the outlet conduit IB. Tubes 2| and tubes 24 are both arranged in sets adjacent the shell of the silencer, and in order to prevent direct transmission the ends of tubes 2! are bent inwardly towards the center of the chamber 23 as is shown in Figs. 1 and 4. The two sets of tubes 2| and 24 are preferably provided with anti-resonance holes 27 as described in my Patent 2,297,046, September 29, 1942.
What I claim is:
l. A silencer having a substantially cylindrical shell, a pair of spaced partitions dividing the interior of the shell into three chambers, an inlet conduit leading into the first chamber and terminating with an open end near the center thereof, a circumferentially spaced series of tubes located radially outwardly of the inlet conduit each having open ends one substantially in the plane of the open end of the inlet conduit and the other near the center of the second chamber, said tubes passing through the first partition into the second chamber and slanting radially inwardly towards the axis thereof, a second circumferentially spaced series of tubes circumferentially staggered with relation to the tubes of the first series, said second series of tubes extending substantially straight through the second partition into the second and third chambers and having open ends at substantially the mid-points of said chambers, and an outlet conduit entering the third chamber through the shell and terminating with an open end substantially in the plane of the open ends of the second series of tubes but located radially inwardly thereof.
2. A silencer having a substantially cylindrical shell, a. pair of transverse partitions dividing the interior of the shell into three chambers, a pair of conduits coaxial with the shell and entering each end chamber respectively with an open end REFERENCES CITED at a point intermediate its length two series of The following references are of record in the circumferentially spaced tubes located adjacent file of this patent: the peripheries of said end chambers and sta gered circumferentially with respect to each other, 5 UNITED STATES PATENTS the tubes in each series terminating at substan- Number Name Date tially the midpoint of the middle chamber with 2,265,342 Bourne Dec. 9, 941
open ends, the tubes of one series being bent i inwardly at one end to open into the middle FOREIGNPATENTS chamber closer to the axis of the cylindrical shell 10 Number Country a than the tubes in the other series. 139,369 at Britain Mar- 4. 1920 882,317 France May 31, 194 3 ROLAND'B. BOURNE'. 1 24rz55- Australia Jan. 27,194
US239674A 1951-08-01 1951-08-01 Muffler with plural passages Expired - Lifetime US2624418A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US239674A US2624418A (en) 1951-08-01 1951-08-01 Muffler with plural passages

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US239674A US2624418A (en) 1951-08-01 1951-08-01 Muffler with plural passages

Publications (1)

Publication Number Publication Date
US2624418A true US2624418A (en) 1953-01-06

Family

ID=22903227

Family Applications (1)

Application Number Title Priority Date Filing Date
US239674A Expired - Lifetime US2624418A (en) 1951-08-01 1951-08-01 Muffler with plural passages

Country Status (1)

Country Link
US (1) US2624418A (en)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2707033A (en) * 1952-12-16 1955-04-26 Fluor Corp Pulsation dampeners
US2801705A (en) * 1955-01-26 1957-08-06 Air Maze Corp Silencer
US2872998A (en) * 1954-03-30 1959-02-10 American Radiator & Standard Acoustical silencer
US2912062A (en) * 1952-05-31 1959-11-10 Burgess Manning Co Exhaust snubber or the like
US3016972A (en) * 1959-04-10 1962-01-16 Rebert J Dugas Muffler for an internal combustion engine
US3122366A (en) * 1961-05-16 1964-02-25 Brunswick Corp Rotatable ring for elevating bowling pins
US3204723A (en) * 1962-05-08 1965-09-07 Natalie Payne Exhaust muffler with filling of porous ceramic cinders and method of making same
US3224088A (en) * 1961-11-15 1965-12-21 Inland Steel Co Process for producing multi-layer metallic material
US3337939A (en) * 1963-06-03 1967-08-29 United States Steel Corp Muffler body and method of manufacture
US3480105A (en) * 1968-12-13 1969-11-25 Us Industries Inc Device for silencing gas flow streams
US3523590A (en) * 1968-12-18 1970-08-11 Tenneco Inc Simplified muffler shell construction
US3754620A (en) * 1972-08-21 1973-08-28 S Foster Muffler
US3786896A (en) * 1972-08-21 1974-01-22 C Smith Muffler
US4222456A (en) * 1977-04-25 1980-09-16 Kasper Witold A Sound-suppressing and back pressure-reducing apparatus and method
US20050155819A1 (en) * 2004-01-21 2005-07-21 Kelly Libby Anti-reversion apparatus
US20100199651A1 (en) * 2009-02-09 2010-08-12 Callahan Joseph E Tube structure for exhaust component
US20120103719A1 (en) * 2009-03-23 2012-05-03 Vortex Performance Limited exhaust filter
US9243543B2 (en) 2012-12-07 2016-01-26 Hanon Systems Universal attenuation device for air-conditioning circuit
US9816412B1 (en) * 2016-06-13 2017-11-14 Edmond Bruce Strickland, Jr. Dual purpose muffler

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB139369A (en) * 1919-05-21 1920-03-04 W J Smith Ltd An improved motor exhaust silencer
US2265342A (en) * 1940-05-18 1941-12-09 Maxim Silencer Co Silencer
FR882317A (en) * 1941-06-03 1943-05-31 Eberspaecher J Mufflers for internal combustion engines

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB139369A (en) * 1919-05-21 1920-03-04 W J Smith Ltd An improved motor exhaust silencer
US2265342A (en) * 1940-05-18 1941-12-09 Maxim Silencer Co Silencer
FR882317A (en) * 1941-06-03 1943-05-31 Eberspaecher J Mufflers for internal combustion engines

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2912062A (en) * 1952-05-31 1959-11-10 Burgess Manning Co Exhaust snubber or the like
US2707033A (en) * 1952-12-16 1955-04-26 Fluor Corp Pulsation dampeners
US2872998A (en) * 1954-03-30 1959-02-10 American Radiator & Standard Acoustical silencer
US2801705A (en) * 1955-01-26 1957-08-06 Air Maze Corp Silencer
US3016972A (en) * 1959-04-10 1962-01-16 Rebert J Dugas Muffler for an internal combustion engine
US3122366A (en) * 1961-05-16 1964-02-25 Brunswick Corp Rotatable ring for elevating bowling pins
US3224088A (en) * 1961-11-15 1965-12-21 Inland Steel Co Process for producing multi-layer metallic material
US3204723A (en) * 1962-05-08 1965-09-07 Natalie Payne Exhaust muffler with filling of porous ceramic cinders and method of making same
US3337939A (en) * 1963-06-03 1967-08-29 United States Steel Corp Muffler body and method of manufacture
US3480105A (en) * 1968-12-13 1969-11-25 Us Industries Inc Device for silencing gas flow streams
US3523590A (en) * 1968-12-18 1970-08-11 Tenneco Inc Simplified muffler shell construction
US3754620A (en) * 1972-08-21 1973-08-28 S Foster Muffler
US3786896A (en) * 1972-08-21 1974-01-22 C Smith Muffler
US4222456A (en) * 1977-04-25 1980-09-16 Kasper Witold A Sound-suppressing and back pressure-reducing apparatus and method
US20050155819A1 (en) * 2004-01-21 2005-07-21 Kelly Libby Anti-reversion apparatus
US20100199651A1 (en) * 2009-02-09 2010-08-12 Callahan Joseph E Tube structure for exhaust component
US8025121B2 (en) * 2009-02-09 2011-09-27 Emcon Technologies Llc Tube structure for exhaust component
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
US9243543B2 (en) 2012-12-07 2016-01-26 Hanon Systems Universal attenuation device for air-conditioning circuit
US9816412B1 (en) * 2016-06-13 2017-11-14 Edmond Bruce Strickland, Jr. Dual purpose muffler

Similar Documents

Publication Publication Date Title
US2624418A (en) Muffler with plural passages
US2692025A (en) Heavy-duty silencer for restricted spaces
US1081348A (en) Exhaust-silencer.
US3913703A (en) Single inner assembly wave interference silencer
US4203503A (en) Exhaust silencer for a railway locomotive
US3212603A (en) Muffler with tuned silencing chambers
US3794139A (en) Muffler with plural inlets and outlets
US2513229A (en) Manifold silencer with plural lateral inlets and outlets
US2184891A (en) Silencer
US4172508A (en) Exhaust silencers
US2841237A (en) Muffler structure
US2016253A (en) Muffler
US2537203A (en) Manifold silencer
US3289785A (en) Silencer with outer housing contacting inner conduit to define resonance chambers
US2150811A (en) Muffler
USRE25384E (en) Exhaust muffler
US2960179A (en) Exhaust muffler
US3104734A (en) Sound attenuating gas pipe
US2841235A (en) Sound muffler
US2660257A (en) Silencer with low back pressure
US1991014A (en) Muffler
US2035500A (en) Silencer
US3447629A (en) Automotive exhaust system and muffler therefor
US2017748A (en) Sound attenuating device
US2100030A (en) Silencer