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EP0704617A1 - Acoustic absorber - Google Patents

Acoustic absorber Download PDF

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Publication number
EP0704617A1
EP0704617A1 EP95202130A EP95202130A EP0704617A1 EP 0704617 A1 EP0704617 A1 EP 0704617A1 EP 95202130 A EP95202130 A EP 95202130A EP 95202130 A EP95202130 A EP 95202130A EP 0704617 A1 EP0704617 A1 EP 0704617A1
Authority
EP
European Patent Office
Prior art keywords
tuner
acoustical
duct
sound
frequency
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.)
Withdrawn
Application number
EP95202130A
Other languages
German (de)
French (fr)
Inventor
Donald Robert Demorest
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.)
Motors Liquidation Co
Original Assignee
General Motors Corp
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 General Motors Corp filed Critical General Motors Corp
Publication of EP0704617A1 publication Critical patent/EP0704617A1/en
Withdrawn legal-status Critical Current

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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
    • F01N1/16Silencing apparatus characterised by method of silencing by using movable parts
    • F01N1/22Silencing apparatus characterised by method of silencing by using movable parts the parts being resilient walls
    • 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
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/12Intake silencers ; Sound modulation, transmission or amplification
    • F02M35/1255Intake silencers ; Sound modulation, transmission or amplification using resonance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/12Intake silencers ; Sound modulation, transmission or amplification
    • F02M35/1272Intake silencers ; Sound modulation, transmission or amplification using absorbing, damping, insulating or reflecting materials, e.g. porous foams, fibres, rubbers, fabrics, coatings or membranes
    • 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
    • F01N2490/14Dead or resonance chambers connected to gas flow tube by relatively short side-tubes

Definitions

  • the invention relates to passive cancellation of noise generated in a gas carrying duct and, in particular, to an air induction system of an internal combustion engine having a modified acoustical tuner.
  • the air induction system of an automotive internal combustion engine can be a source of undesirable noise.
  • Passive noise cancellation techniques have employed resonators or tuners which are connected to the intake system and are operable to attenuate specific frequencies.
  • An example of such a tuner is a quarter-wave tuner which is typically a tube having a length which is roughly equal to one-fourth of the wave length of the sound energy to be attenuated.
  • Generation by the induction system of the tuners natural frequency will result in a reflected waveform of the same frequency and amplitude but of opposite phase.
  • the tuner generated waveform cancels the induction noise at that frequency.
  • the tuners are typically constructed of a tube having an open end in communication with the induction system and a closed end.
  • a tuner may comprise a cylindrical body with both ends closed and an opening midway between the two ends which communicates with the induction system.
  • Maximum sound pressure points are created along the length of the intake system with the locations of the points dependent upon the length and configuration of the specific intake.
  • the opening to the tuner communicates with the intake at the pressure point for the frequency to be attenuated and can, as a result, significantly attenuate the generated noise at that frequency.
  • the tuning in noise generated in the narrow band addressed by such tuners may come undesirable side frequency peaks on either side of the absorbed frequency peak. Although reduced significantly from the attenuated frequency peak, these side frequency peaks can be the source of additional generated noise.
  • the present invention is directed to an acoustical tuner for use in the attenuation of noise generated from a gas carrying duct such as is commonly used in the intake systems of internal combustion engines.
  • the tuner of the present invention may be constructed as a tube having a length corresponding to the wavelength of the sound energy to be attenuated.
  • the tube is placed in communication with the gas carrying duct at a location along the duct at which a high pressure point for the wavelength of the sound to be attenuated exists.
  • Such a location has to be determined for each configuration of gas carrying duct, as the location of the points will depend on the specific configuration.
  • the acoustical tuner may also include a second, closed end which is constructed of a moveable diaphragm.
  • a sound wave entering the tuner from the gas carrying intake duct will be reflected from the closed end and returned to the open end in phase-opposition to the duct carried sound wave of the same frequency.
  • the movable diaphragm moves outwardly as the sound wave impacts the closed second end. The outward movement, and subsequent return of the diaphragm to its original location, converts acoustical energy to mechanical energy while changing the effective tuned length of the tuner.
  • the resultant frequency attenuation of the disclosed tuner is operable over a larger frequency range and, more specifically, over a portion of the range of undesirable side frequency peaks which may be generated when using an acoustical tuner having ends of conventional design.
  • the quarter-wave tuner 12 shown in figure 1, includes a tubular body 14 which extends radially outwardly from the inlet duct 10 and is terminated at a closed, second end 18.
  • the total length of the tuner 12 approximates one quarter the wave length of the frequency producing the sound pressure point to be attenuated.
  • a sound wave enters the first end 16 of tuner 12 it traverses the length of the tube 14 and is reflected by the closed second end 18 of the tuner as a waveform with the same frequency and amplitude but opposite in phase so as to cancel the induction noise at that frequency.
  • the side frequency peaks of curve "B" which are generated using the quarter-wave tuner are further attenuated by the application of a movable, diaphragm 20 to the closed, second end 18 of tuner 12.
  • the diaphragm 20 is preferably constructed of an inelastic material such as metal or semi rigid plastic. The diaphragm closes the second end 18 of the tuner 12 in a "limp" fashion as opposed to being drawn taught, across the second end which could radiate additional sound energy in much the same way as a drum.
  • FIG. 2 illustrates a second embodiment of the present invention in which a tuner 12' is constructed of two lengths of tube 22,24 placed in series and coupled by a bend 26 in the tuner.
  • a first diaphragm 28 At the terminus of the first length of tube 22 and integral with the bend 26 in tuner 12' is a first diaphragm 28.
  • a second diaphragm 30 At the terminus of the second length of tube 24 and integral with the second end of tuner 12' is a second diaphragm 30.
  • the tuner 12' of Figure 2 operates on more than one frequency peak in inlet duct 10'.
  • the first length 22 of tuner 12' operable to attenuate frequency peaks associated with its length and, in addition, the first and second lengths 22 and 24, operable to attenuate frequency peaks associated with the cumulative lengths thereof.
  • the diaphragms 28 and 30 extend the effective attenuation of the tuner 12' through the conversion of acoustic energy to mechanical energy as the diaphragms are moved outwardly and, subsequently, returned to position to thereby vary the effective length of the tuner sections.
  • the second diaphragm 30 of the tuner 12' shown in Figure 3 is shown with an additional embodiment of the present invention. It may be desirable to add a mass 32 to the surface of the flexible diaphragm. Such a mass can add to the energy dissipating effect of the diaphragm which may be desirable in further attenuating noise frequencies in the duct 10'.

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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)

Abstract

An intake system for an internal combustion engine is disclosed having an intake air duct (10) for transferring intake air to the engine. The inlet air duct has an acoustical tuner (12,12') in operable communication with the intake air flow to attenuate sound frequencies in the duct. The tuner has a first, opened end (16) which communicates with the air flow in duct (10), a tubular body (14) and a second end (18) which is closed by a moveable diaphragm (20). The diaphragm is moveable under the force of a sound wave traversing the tuner and is operable to extend the attenuation range of the tuner.

Description

    TECHNICAL FIELD
  • The invention relates to passive cancellation of noise generated in a gas carrying duct and, in particular, to an air induction system of an internal combustion engine having a modified acoustical tuner.
  • BACKGROUND
  • The air induction system of an automotive internal combustion engine can be a source of undesirable noise. Passive noise cancellation techniques have employed resonators or tuners which are connected to the intake system and are operable to attenuate specific frequencies. An example of such a tuner is a quarter-wave tuner which is typically a tube having a length which is roughly equal to one-fourth of the wave length of the sound energy to be attenuated. Generation by the induction system of the tuners natural frequency will result in a reflected waveform of the same frequency and amplitude but of opposite phase. The tuner generated waveform cancels the induction noise at that frequency.
  • The tuners are typically constructed of a tube having an open end in communication with the induction system and a closed end. Alternatively, such a tuner may comprise a cylindrical body with both ends closed and an opening midway between the two ends which communicates with the induction system. Maximum sound pressure points are created along the length of the intake system with the locations of the points dependent upon the length and configuration of the specific intake. The opening to the tuner communicates with the intake at the pressure point for the frequency to be attenuated and can, as a result, significantly attenuate the generated noise at that frequency. Along with the reduction in noise generated in the narrow band addressed by such tuners may come undesirable side frequency peaks on either side of the absorbed frequency peak. Although reduced significantly from the attenuated frequency peak, these side frequency peaks can be the source of additional generated noise.
  • SUMMARY OF THE INVENTION
  • The present invention is directed to an acoustical tuner for use in the attenuation of noise generated from a gas carrying duct such as is commonly used in the intake systems of internal combustion engines. The tuner of the present invention may be constructed as a tube having a length corresponding to the wavelength of the sound energy to be attenuated. The tube is placed in communication with the gas carrying duct at a location along the duct at which a high pressure point for the wavelength of the sound to be attenuated exists. Such a location has to be determined for each configuration of gas carrying duct, as the location of the points will depend on the specific configuration.
  • The acoustical tuner, to which the present invention is directed, may also include a second, closed end which is constructed of a moveable diaphragm. A sound wave entering the tuner from the gas carrying intake duct will be reflected from the closed end and returned to the open end in phase-opposition to the duct carried sound wave of the same frequency. In addition, the movable diaphragm moves outwardly as the sound wave impacts the closed second end. The outward movement, and subsequent return of the diaphragm to its original location, converts acoustical energy to mechanical energy while changing the effective tuned length of the tuner. The resultant frequency attenuation of the disclosed tuner is operable over a larger frequency range and, more specifically, over a portion of the range of undesirable side frequency peaks which may be generated when using an acoustical tuner having ends of conventional design.
  • The present invention will now be described, by way of example, with reference to the accompanying, description and to the drawings, in which:
    • Figure 1 is a perspective view, partially in section, of an acoustic tuner embodying features of the present invention;
    • Figure 2 is a perspective view of a second embodiment of an acoustic tuner embodying features of the present invention; and
    • Figure 3 is a graphic representation of noise levels generated in a gas carrying tube having varying levels of sound attenuation.
       Referring to Figure 1, an inlet duct 10 for an internal combustion engine (not shown) is illustrated having a sound attenuating acoustical tuner 12 attached to the side thereof. The intake duct 10 will typically extend from a first opened end at which point engine air enters the duct to a second end at the inlet to each engine cylinder. The duct may comprise several different components and is rarely straight, due to packaging considerations. Noise sources from the engine radiate sound through the intake duct which, if unchecked, will exit the inlet duct in the form of undesirable external noise. The sound waves travelling through the duct 10 establish maximum sound pressure points along its length. Attenuation of the sound wave frequencies which produce the maximum pressure points is typically addressed by connecting the first,opened end 16 of an acoustical quarter-wave length tuner 12, to the inlet duct 10, at the location of the pressure points.
  • The quarter-wave tuner 12, shown in figure 1, includes a tubular body 14 which extends radially outwardly from the inlet duct 10 and is terminated at a closed, second end 18. The total length of the tuner 12 approximates one quarter the wave length of the frequency producing the sound pressure point to be attenuated. When a sound wave enters the first end 16 of tuner 12 it traverses the length of the tube 14 and is reflected by the closed second end 18 of the tuner as a waveform with the same frequency and amplitude but opposite in phase so as to cancel the induction noise at that frequency. The operation of the quarter-wave tuner described thus far is illustrated in Figure 3 in which line "A" illustrates the sound characteristics of an unattenuated system, and line "B" illustrates the attenuation achieved by application of a quarter-wave tuner as described thus far.
  • The side frequency peaks of curve "B" which are generated using the quarter-wave tuner are further attenuated by the application of a movable, diaphragm 20 to the closed, second end 18 of tuner 12. The diaphragm 20 is preferably constructed of an inelastic material such as metal or semi rigid plastic. The diaphragm closes the second end 18 of the tuner 12 in a "limp" fashion as opposed to being drawn taught, across the second end which could radiate additional sound energy in much the same way as a drum. As a sound wave moves through the tube 14 and impacts the diaphragm 20 at the second end 18, a pressure build-up at the second end moves the diaphragm outwardly resulting in a change in the effective length of the tuner 12 and a conversion of a portion of the sound energy to mechanical energy. Similarly as the sound wave is reflected back, towards the first end 16 of the tuner 12, the diaphragm 20 is pulled inwardly, expending further sound energy in the form of mechanical energy. The effect of the in and out movement of the diaphragm 20 is the conversion of acoustical energy to mechanical energy with a resultant broadening of the attenuated sound frequency to include the side frequency peaks which are present after attenuation by a standard quarter-wave tuner. Line "C" in Figure 3 illustrates the additional attenuation available through the used of the diaphragm 20 in the second end 18 of the tuner 12.
  • Figure 2 illustrates a second embodiment of the present invention in which a tuner 12' is constructed of two lengths of tube 22,24 placed in series and coupled by a bend 26 in the tuner. At the terminus of the first length of tube 22 and integral with the bend 26 in tuner 12' is a first diaphragm 28. Similarly at the terminus of the second length of tube 24 and integral with the second end of tuner 12' is a second diaphragm 30. The tuner 12' of Figure 2 operates on more than one frequency peak in inlet duct 10'. The first length 22 of tuner 12' operable to attenuate frequency peaks associated with its length and, in addition, the first and second lengths 22 and 24, operable to attenuate frequency peaks associated with the cumulative lengths thereof. As with the embodiment of Figure 1, described above, the diaphragms 28 and 30 extend the effective attenuation of the tuner 12' through the conversion of acoustic energy to mechanical energy as the diaphragms are moved outwardly and, subsequently, returned to position to thereby vary the effective length of the tuner sections.
  • The second diaphragm 30 of the tuner 12' shown in Figure 3 is shown with an additional embodiment of the present invention. It may be desirable to add a mass 32 to the surface of the flexible diaphragm. Such a mass can add to the energy dissipating effect of the diaphragm which may be desirable in further attenuating noise frequencies in the duct 10'.
  • While the preferred embodiments of the present invention have been disclosed in their application to the intake duct of an automotive internal combustion engine, the invention should not be limited to that specific application. It is contemplated that such an apparatus for the reduction of generated noise in a gas carrying duct has further applications in such areas as the engine exhaust system and other fluid carrying conduits.

Claims (6)

  1. An acoustical tuner for attenuation of a sound frequency within a gas carrying duct, said tuner comprising a tubular body having a length corresponding to the wavelength of the sound frequency to be attenuated, a first, open end for communication with said duct and a second end closed by a diaphragm member, said member moveable under the force of a sound wave traversing said tuner to extend the attenuation range of said tuner beyond the frequency associated with the length of said tuner.
  2. An acoustical tuner, as defined in claim 1, said tubular body having a length corresponding to one-quarter the wavelength of the sound frequency to be attenuated.
  3. An acoustical tuner, as defined in claim 1, said diaphragm member constructed of an inelastic material.
  4. An acoustical tuner, as defined in claim 1, said diaphragm member having a mass fixed thereto, operable to increase the energy dissipating effect of movement of said diaphragm.
  5. An air induction system for an internal combustion engine comprising an intake air duct for transferring intake air to said engine and an acoustical tuner for attenuation of a sound frequency within said intake air duct, said tuner comprising a tubular body having a length corresponding to the wavelength of the sound frequency to be attenuated, a first, opened end in communication with the interior of said intake air duct and a second end closed by a moveable diaphragm member, said member moveable under the force of a sound wave traversing said tuner to extend the attenuation range of said tuner beyond the frequency associated with the length of said tuner.
  6. An acoustical tuner, as defined in claim 5, said tubular body further comprising a bend therein, intermediate of said first end and said second end, and located a distance from said first end which corresponds to a wavelength of a second sound frequency to be attenuated, said bend defining a second quarter-wave acoustical tuner integral with said first tuner, and a second diaphragm member located at the apex of said bend and moveable under the force of a sound wave, of the frequency associated with said second tuner length, traversing said distance from said first end to said bend to extend the attenuation range of said second tuner beyond the frequency associated therewith.
EP95202130A 1994-09-02 1995-08-03 Acoustic absorber Withdrawn EP0704617A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US299979 1981-09-08
US29997994A 1994-09-02 1994-09-02

Publications (1)

Publication Number Publication Date
EP0704617A1 true EP0704617A1 (en) 1996-04-03

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ID=23157143

Family Applications (1)

Application Number Title Priority Date Filing Date
EP95202130A Withdrawn EP0704617A1 (en) 1994-09-02 1995-08-03 Acoustic absorber

Country Status (3)

Country Link
EP (1) EP0704617A1 (en)
JP (1) JPH0874690A (en)
CA (1) CA2153855A1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7111601B2 (en) * 2004-03-18 2006-09-26 Visteon Global Technologies, Inc. Air induction system having an environmentally resistant acoustic membrane
EP1808594A1 (en) * 2006-01-13 2007-07-18 Denso Corporation Intake muffler
EP1865187A3 (en) * 2006-06-05 2008-12-24 Nissan Motor Company Limited Improvements in or Relating to Vehicle Noise
US7717230B2 (en) 2006-06-05 2010-05-18 Nissan Motor Co., Ltd. Device and method for amplifying suction noise
DE102012208250A1 (en) * 2012-05-16 2013-11-21 Leica Microsystems Cms Gmbh Device for the insulation of sound in the optical beam path of a microscope and a microscope with a corresponding device
WO2024011964A1 (en) * 2022-07-12 2024-01-18 合肥美的电冰箱有限公司 Silencer

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003097371A (en) * 2001-09-26 2003-04-03 Toyota Motor Corp Intake device for internal combustion engine
JP3901483B2 (en) 2001-10-04 2007-04-04 ヤマハ発動機株式会社 Engine intake sound adjustment structure and exhaust sound adjustment structure

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1954516A (en) * 1931-10-19 1934-04-10 Maxim Silencer Co Sound attenuating device
JPS5332222A (en) * 1976-09-06 1978-03-27 Kawasaki Heavy Ind Ltd Intake air nozzle silencer for internal combustion engine
JPS58124057A (en) * 1982-01-19 1983-07-23 Toyota Motor Corp intake resonator
DE8607920U1 (en) * 1985-04-02 1986-07-31 Fiat Auto S.P.A., Turin/Torino Pulsation absorption damper for the intake manifold of an internal combustion engine
JPS61190158A (en) * 1985-02-18 1986-08-23 Honda Motor Co Ltd Intake system silencer for internal-combustion engine
EP0376299A1 (en) * 1988-12-28 1990-07-04 Mazda Motor Corporation Suction apparatus for engine
US5103931A (en) * 1987-07-20 1992-04-14 Sanshin Industries Co., Ltd. Exhaust silencing means for marine propulsion
JPH04246221A (en) * 1991-01-31 1992-09-02 Toyoda Gosei Co Ltd Noise suppressing device
GB2260574A (en) * 1991-10-16 1993-04-21 Hyundai Motor Co Ltd Engine intake silencer with variable resonator capacity
US5333576A (en) * 1993-03-31 1994-08-02 Ford Motor Company Noise attenuation device for air induction system for internal combustion engine

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1954516A (en) * 1931-10-19 1934-04-10 Maxim Silencer Co Sound attenuating device
JPS5332222A (en) * 1976-09-06 1978-03-27 Kawasaki Heavy Ind Ltd Intake air nozzle silencer for internal combustion engine
JPS58124057A (en) * 1982-01-19 1983-07-23 Toyota Motor Corp intake resonator
JPS61190158A (en) * 1985-02-18 1986-08-23 Honda Motor Co Ltd Intake system silencer for internal-combustion engine
DE8607920U1 (en) * 1985-04-02 1986-07-31 Fiat Auto S.P.A., Turin/Torino Pulsation absorption damper for the intake manifold of an internal combustion engine
US5103931A (en) * 1987-07-20 1992-04-14 Sanshin Industries Co., Ltd. Exhaust silencing means for marine propulsion
EP0376299A1 (en) * 1988-12-28 1990-07-04 Mazda Motor Corporation Suction apparatus for engine
JPH04246221A (en) * 1991-01-31 1992-09-02 Toyoda Gosei Co Ltd Noise suppressing device
GB2260574A (en) * 1991-10-16 1993-04-21 Hyundai Motor Co Ltd Engine intake silencer with variable resonator capacity
US5333576A (en) * 1993-03-31 1994-08-02 Ford Motor Company Noise attenuation device for air induction system for internal combustion engine

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 11, no. 14 (M - 553)<2461> 14 January 1987 (1987-01-14) *
PATENT ABSTRACTS OF JAPAN vol. 17, no. 21 (M - 1353) 14 January 1993 (1993-01-14) *
PATENT ABSTRACTS OF JAPAN vol. 2, no. 69 (M - 021) 25 May 1978 (1978-05-25) *
PATENT ABSTRACTS OF JAPAN vol. 7, no. 230 (M - 249)<1375> 12 October 1983 (1983-10-12) *

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7111601B2 (en) * 2004-03-18 2006-09-26 Visteon Global Technologies, Inc. Air induction system having an environmentally resistant acoustic membrane
EP1808594A1 (en) * 2006-01-13 2007-07-18 Denso Corporation Intake muffler
US7350496B2 (en) 2006-01-13 2008-04-01 Denso Corporation Intake muffler
EP1865187A3 (en) * 2006-06-05 2008-12-24 Nissan Motor Company Limited Improvements in or Relating to Vehicle Noise
US7717230B2 (en) 2006-06-05 2010-05-18 Nissan Motor Co., Ltd. Device and method for amplifying suction noise
USRE42490E1 (en) 2006-06-05 2011-06-28 Nissan Motor Co., Ltd. Device and method for amplifying suction noise
DE102012208250A1 (en) * 2012-05-16 2013-11-21 Leica Microsystems Cms Gmbh Device for the insulation of sound in the optical beam path of a microscope and a microscope with a corresponding device
US8844671B2 (en) 2012-05-16 2014-09-30 Leica Microsystems Cms Gmbh Apparatus for damping sound in the optical beam path of a microscope, and microscope having a corresponding apparatus
WO2024011964A1 (en) * 2022-07-12 2024-01-18 合肥美的电冰箱有限公司 Silencer

Also Published As

Publication number Publication date
CA2153855A1 (en) 1996-03-03
JPH0874690A (en) 1996-03-19

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