Nothing Special   »   [go: up one dir, main page]

GB989061A - Improvements in or relating to a sound attenuating gas conduit - Google Patents

Improvements in or relating to a sound attenuating gas conduit

Info

Publication number
GB989061A
GB989061A GB26727/61A GB2672761A GB989061A GB 989061 A GB989061 A GB 989061A GB 26727/61 A GB26727/61 A GB 26727/61A GB 2672761 A GB2672761 A GB 2672761A GB 989061 A GB989061 A GB 989061A
Authority
GB
United Kingdom
Prior art keywords
elements
pipe
cycles
silencing
cross
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
Application number
GB26727/61A
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.)
Meritor Inc
Original Assignee
Arvin Industries Inc
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 Arvin Industries Inc filed Critical Arvin Industries Inc
Publication of GB989061A publication Critical patent/GB989061A/en
Expired legal-status Critical Current

Links

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
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/02Silencing apparatus characterised by method of silencing by using resonance
    • 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
    • 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
    • F01N2490/20Chambers being formed inside the exhaust pipe without enlargement of the cross section of the pipe, e.g. resonance chambers

Landscapes

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

Abstract

989,061. Exhaust silencers. ARVIN INDUSTRIES Inc. July 24, 1961 [Feb. 13, 1961], No. 26727/61. Heading F1B. In a sound attenuating gas conduit, an openended pipe forming a gas-flow passage is free from substantial abrupt changes in its diameter and has an unrestricted flow at its ends, and mounted within the pipe is at least one silencing element comprising an elongated enclosed wall forming a sound attenuating cavity interconnected by throat-forming means with the interior of the pipe and having all or substantially all of its wall spaced from the pipe, the cross-sectional area of the gas passage within the axial extent of the element being smaller than the average cross-sectional area of the gas passage elsewhere. The cross-sectional area of the element is from about 25% to 75% of the cross-sectional area of the pipe within the axial extent of the element. The invention is described in connection with an exhaust system of an I.C. engine but it may be used on the intake side of an I.C. engine. An exhaust pipe 10, Fig. 1, is provided with low frequency (below 300 cycles/sec.) silencing elements 16 and high frequency (above 1500 cycles/sec.) silencing elements 18. Each element 16 has a tube 28 at each end interconnecting the gas stream with noise attenuating resonator volumes 26 separated by a baffle 24. Sheet metal support brackets 30 keep the elements clear of any condensed corrosive liquids. Alternatively, the elements may be suspended -from the pipe wall with one or more lines of contact therewith. In Fig. 9 (not shown) the elements are supported by two lines of contact with the wall of a pipe of elliptical cross-section. The pipe 10 may be in sections to facilitate replacement of corroded elements. Preferably the resonator volumes 26 are tuned to attenuate one of the objectionable harmonics and placed at or adjacent one of the maximum pressure points of that harmonic. If one of the maximum pressure points occurs at a bend a curved tube 27 may be provided. The elements 16 may be positioned closely adjacent one another so that the opposing tubes 28 thereof form a greater effective length and attenuate lower frequency waves. The elements 18 which are closed at their ends are perforated to render them at least 30% open. They contain a porous fibrous material, such as asbestos fibres or stainless steel wool, in the form of a wadding filling the cavity or a hollow sleeve lining the cavity walls. Another form of silencing element 42, Figs. 5 and 6 for frequencies of 300 to 1500 cycles/secs., is divided by baffle plates 45 into chambers 46 associated with openings 48 formed by shearing the tube to provide tongues 49. In another form of silencing element a plain cylinder closed at its ends has perforations in its side wall or in one end. In the latter case two such elements may be arranged perforated end to perforated end and suitably spaced to provide an effective throat length which will attenuate sound waves having frequencies of 100 to 700 cycles/sec. Alternatively, a perforated end may be arranged adjacent an unperforated one. The different forms of elements described may be used in combination and with conventional silencers.
GB26727/61A 1961-02-13 1961-07-24 Improvements in or relating to a sound attenuating gas conduit Expired GB989061A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US88977A US3119459A (en) 1961-02-13 1961-02-13 Sound attenuating gas conduit

Publications (1)

Publication Number Publication Date
GB989061A true GB989061A (en) 1965-04-14

Family

ID=22214619

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26727/61A Expired GB989061A (en) 1961-02-13 1961-07-24 Improvements in or relating to a sound attenuating gas conduit

Country Status (3)

Country Link
US (1) US3119459A (en)
DE (2) DE1299647B (en)
GB (1) GB989061A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3263772A (en) * 1964-06-17 1966-08-02 Arvin Ind Inc Sound attenuating gas conduit with one-quarter wave-length side branch chambers
SE461290B (en) * 1982-06-01 1990-01-29 Neil Lawrence Currie EXHAUST SYSTEM FOR MOTOR VEHICLE
US5123501A (en) * 1988-10-21 1992-06-23 Donaldson Company, Inc. In-line constricted sound-attenuating system
FR2642470A1 (en) * 1989-01-27 1990-08-03 Glaenzer Spicer Sa SILENCER FOR EXHAUST GASES AND EXHAUST LINE PART COMPRISING SUCH SILENCER
US4979587A (en) * 1989-08-01 1990-12-25 The Boeing Company Jet engine noise suppressor
SE502786C2 (en) * 1991-11-26 1996-01-15 Volvo Ab Noise damping arrangement for IC engine exhaust gas system
US20080190689A1 (en) * 2007-02-12 2008-08-14 Ballard Ebbin C Inserts for engine exhaust systems
US7984787B2 (en) * 2009-01-23 2011-07-26 Dresser-Rand Company Fluid-carrying conduit and method with noise attenuation
US20110108358A1 (en) * 2009-11-06 2011-05-12 Jason Michael Edgington Noise attenuator and resonator
US9121329B2 (en) * 2012-04-24 2015-09-01 Faurecia Emissions Control Technologies, Usa, Llc Tailpipe diffuser
CN107461231A (en) * 2017-09-29 2017-12-12 武汉理工大学 A kind of model muffler
CN112443433B (en) * 2019-09-05 2024-02-27 上海索菲玛汽车滤清器有限公司 Air filter

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE559326A (en) *
DE511490C (en) * 1930-10-31 Paul Barringhaus Silencer for motor vehicles and. Like. With one behind the other and directly abutting nozzles
AT124595B (en) * 1928-06-02 1931-09-25 Burgess Lab Inc C F Silencer.
US1947987A (en) * 1929-03-26 1934-02-20 Curtiss Aeroplane & Motor Co Combined exhaust manifold and muffler
US1811762A (en) * 1929-05-08 1931-06-23 Burgess Lab Inc C F Exhaust muffler
US1847830A (en) * 1929-08-10 1932-03-01 Hills Horace Gastineau Exhaust silencer
GB415446A (en) * 1931-11-25 1934-08-27 Daimler Benz Ag Method of and means for stabilising the flow of gas in pipes connected to reciprocating piston machines
DE650784C (en) * 1931-11-26 1937-10-01 Daimler Benz Akt Ges A device used to steady intermittently flowing gaseous fluids in pipelines
US1910672A (en) * 1932-05-13 1933-05-23 Maxim Silencer Co Acoustic wave filter
US2014666A (en) * 1932-10-31 1935-09-17 Halsey W Taylor Company Muffler
US2056608A (en) * 1933-12-22 1936-10-06 C F Burges Lab Inc Silencer
US2099887A (en) * 1934-05-26 1937-11-23 Buffalo Pressed Steel Company Muffler
US2038309A (en) * 1934-07-25 1936-04-21 Oldberg Sidney Silencer
US2184891A (en) * 1937-12-13 1939-12-26 Maxim Silencer Co Silencer
US2297046A (en) * 1939-08-25 1942-09-29 Maxim Silencer Co Means for preventing shock excitation of acoustic conduits or chambers
CH285576A (en) * 1949-12-12 1952-09-15 Wayth Cullum Douglas Jack Noise damping device, especially for jet engine testing.
US2671523A (en) * 1950-07-14 1954-03-09 Walker George Bromhead Silencer or muffler for engine exhausts or the like
GB678344A (en) * 1950-10-12 1952-09-03 Vokes Ltd Improvements in silencers
US2694462A (en) * 1951-09-19 1954-11-16 Robbins Frank Acoustic system for loud-speakers
US2748883A (en) * 1952-12-03 1956-06-05 Millard J Ralph Muffler unit
CH317630A (en) * 1953-04-17 1956-11-30 Dehais Lucien Clement Georges Silencer for internal combustion engine
US2795374A (en) * 1953-08-13 1957-06-11 Du Pont Fluid flow pulsation damping
DE1712462U (en) * 1954-06-02 1955-12-08 Auto Union Gmbh EXHAUST SYSTEM FOR TWO-STROKE COMBUSTION MACHINES.
FR1215262A (en) * 1958-11-13 1960-04-15 Device for attenuating the noise of a moving fluid

Also Published As

Publication number Publication date
DE1299647B (en) 1969-07-24
US3119459A (en) 1964-01-28
DE1856343U (en) 1962-08-09

Similar Documents

Publication Publication Date Title
US3263772A (en) Sound attenuating gas conduit with one-quarter wave-length side branch chambers
GB989061A (en) Improvements in or relating to a sound attenuating gas conduit
GB748053A (en) Improvements in or relating to exhaust silencers for internal combustion engines
GB1408030A (en) Silencer for exhaust gases
GB1466512A (en) Gas stream silencer
US3927731A (en) Muffler with spiral duct and double inlets
US3212603A (en) Muffler with tuned silencing chambers
US3752260A (en) Air rush silencer
US2041767A (en) Silencer
US2841237A (en) Muffler structure
US2078754A (en) Silencer
US3112007A (en) Silencing element for exhaust gas conduit
US2995199A (en) Muffler
US3469653A (en) Muffler
US2656005A (en) Retroverted passage type muffler with resonator chambers
US2718273A (en) Muffler construction
US3117650A (en) Silencing element for exhaust gas conduit
GB678344A (en) Improvements in silencers
JP2004519575A (en) Device for damping resonance in conduit
US2194550A (en) Muffler
GB1394605A (en) Sound muffler
US3495680A (en) Exhaust silencing system
US3780826A (en) Gas silencing structure
CA2629430A1 (en) Pulsation damper
US2857014A (en) Silencer for positive pressure gas streams subjected to high amplitude pulsations