EP1253312A1 - Low-noise integrated air-filtering device - Google Patents

Low-noise integrated air-filtering device Download PDF

Info

Publication number
EP1253312A1
EP1253312A1 EP02008733A EP02008733A EP1253312A1 EP 1253312 A1 EP1253312 A1 EP 1253312A1 EP 02008733 A EP02008733 A EP 02008733A EP 02008733 A EP02008733 A EP 02008733A EP 1253312 A1 EP1253312 A1 EP 1253312A1
Authority
EP
European Patent Office
Prior art keywords
casing
resonator
damping
damping element
pipe
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.)
Granted
Application number
EP02008733A
Other languages
German (de)
French (fr)
Other versions
EP1253312B1 (en
Inventor
Umberto Cornaglia
Alessio Tarabocchia
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.)
Officine Metallurgiche G Cornaglia SpA
Original Assignee
Officine Metallurgiche G Cornaglia SpA
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 Officine Metallurgiche G Cornaglia SpA filed Critical Officine Metallurgiche G Cornaglia SpA
Publication of EP1253312A1 publication Critical patent/EP1253312A1/en
Application granted granted Critical
Publication of EP1253312B1 publication Critical patent/EP1253312B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02M35/14Combined air cleaners and silencers
    • 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
    • F02M35/1205Flow throttling or guiding
    • F02M35/1216Flow throttling or guiding by using a plurality of holes, slits, protrusions, perforations, ribs or the like; Surface structures; Turbulence generators
    • 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
    • F02M35/1205Flow throttling or guiding
    • F02M35/1222Flow throttling or guiding by using adjustable or movable elements, e.g. valves, membranes, bellows, expanding or shrinking elements
    • 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
    • F02M35/1261Helmholtz resonators

Definitions

  • the present invention relates to a low-noise integrated air-filtering device.
  • noise reduction in reciprocating-type engines is a requirement that is assuming an ever-increasing importance.
  • the said noise is mainly caused by pressure waves that are generated on account of the reciprocating motion of the pistons in the cylinders and that propagate along the air-intake and exhaust-gas pipes.
  • silencer devices such as perforated-plug elements, are currently employed, which enable conversion of part of the energy associated to the pressure waves into heat.
  • the silencer devices are set along the exhaust pipe and contribute to reducing considerably the overall noise level of the engine.
  • the purpose of the present invention is to provide a low-noise integrated air-filtering device which enables the above-mentioned drawbacks to be overcome and which, moreover, is of simple and inexpensive implementation.
  • a low-noise integrated air-filtering device comprising a casing, which has an inlet pipe and an outlet pipe, and a filter element, which set inside said casing, characterized in that it comprises a silencer device including at least one resonator element and one first damping element, which are set in series together and are contained inside said casing .
  • the device is not only compact and of reduced overall dimensions, but can also be built with an optimal geometry which enables noise abatement in an extremely efficient way.
  • the use of a resonator element and a damping element, which substantially operate in contiguous frequency bands, makes it possible to achieve a high damping effect over a wide spectrum of frequencies.
  • the device forms a single body which can be conveniently mounted on different engines as a replacement for the traditional air-intake filter.
  • said resonator element, said first damping element, and said filter element form an axial sequence.
  • the device has a centroidal axis of symmetry, and said resonator element, said first damping element and said filter element define a linear pipe which is coaxial with said centroidal axis of symmetry.
  • linear geometry and the symmetry of the pipe with respect to a centroidal axis of symmetry enable effective reduction of the undesired effects of resonance due to the transverse modes of propagation of the pressure waves, and thus enable a further improvement in noise deadening.
  • a low-noise integrated air-filtering device designated as a whole by 1, comprises a casing 2, which has a longitudinal axis A of symmetry, an inlet pipe 3 and an outlet pipe 4, which are coaxial to the longitudinal axis A.
  • a filter cartridge 5 Housed inside the casing 2 are a filter cartridge 5, of a type in itself known, and a silencer device 7, which includes at least one resonator element 8 and one first damping element 10.
  • the resonator element 8, the first damping element 10 and the filter cartridge 5 are set in series together and form an axial sequence, in which the resonator element 8 and the first damping element 10 are set upstream of the filter cartridge 5.
  • the longitudinal axis A of symmetry is also a centroidal axis of the device 1.
  • the resonator element 8, the first damping element 10 and the filtering cartridge 5 define a linear pipe 11 coaxial to the longitudinal axis A of symmetry.
  • the linear pipe 11 is traversed by a flow of air sucked in towards the engine (not shown).
  • the said flow of air conveys pressure waves which are generated by the engine itself during its normal operation and which are the source of the noise that is to be attenuated.
  • the resonator 8 is an in-line Helmholtz resonator and has a neck 12, which has an adjustable length L, and a volume V.
  • the resonator element 8 is particularly suited for attenuating noise in a medium-to-low frequency band, up to approximately 300 Hz.
  • the frequency of maximum damping can be adjusted, as will be explained hereinafter.
  • the neck 12 of the resonator element 8 has an annular shape and is defined comprised between an outlet stretch 3a of the inlet pipe 3 and a first stretch 11a of the linear pipe 11.
  • outlet stretch 3a of the inlet pipe 3 is inserted, in an axially slidable way, inside the first stretch 11a of the linear pipe 11.
  • the axial position of the inlet pipe 3 with respect to the linear pipe 11 can be adjusted by means of an actuation device, comprising, for example, a rack 13, carried integrally by the inlet pipe 3 and set longitudinally, and a gear 14, driven by a motor, of a known type and not illustrated.
  • an actuation device comprising, for example, a rack 13, carried integrally by the inlet pipe 3 and set longitudinally, and a gear 14, driven by a motor, of a known type and not illustrated.
  • a diaphragm 15 can be inserted inside the casing 2 in order to reduce by a pre-set amount the volume V of the resonator element 8.
  • the first damping element 10 is a perforated-plug element with low density of perforation, for attenuation of the noise in a medium-to-high frequency band, up to approximately 900 Hz.
  • the density of perforation is between approximately 4% and 5%.
  • the integrated device 1 comprises a second damping element 18, set inside the casing 2, downstream of the filter cartridge 5.
  • the second damping element 18 is coaxial to the longitudinal axis A of symmetry and is connected to the outlet pipe 4.
  • the second damping element 8 is a perforated-plug element with high perforation density for noise damping in a high-frequency band, substantially with frequencies higher than 600 Hz.
  • Figure 2 shows damping curves of the resonator element 8, of the first damping element 10 and of the expansion chamber 17 in a frequency band of between 0 and 1000 Hz.
  • the damping curve for the resonator element 8 is illustrated with a solid line
  • the damping curve for the first damping element 10 is illustrated with a dashed line
  • the damping curve for the expansion chamber 17 (i.e., due exclusively to a sharp variation in the section of the pipe in which the air flows) is illustrated with a dashed-and-dotted line.
  • the inlet pipe 3, the linear pipe 11 and the outlet pipe 4 of the integrated device 1 itself are traversed by a flow of air in which substantially periodic pressure waves, which are a source of noise, propagate.
  • the noise is mainly attenuated by the resonator element 8 and by the first damping element 10.
  • the integrated device 1, as a whole, is particularly effective in damping transverse modes of propagation of the pressure waves.
  • the said result can be obtained when the flow of air develops substantially about a centroidal axis of the damping device (in the case of the integrated device 1, the flow of air develops substantially about the longitudinal axis A of symmetry, which is a centroidal axis).
  • the said secondary resonance frequencies are not therefore excited, and undesired resonance effects are thus prevented.
  • the maximum attenuating frequency of the resonator element 8 can be adjusted.
  • the characteristic frequency of resonance F R can be modified also by varying the volume V of the resonator element 8.
  • the diaphragm 15 which reduces the volume V by a pre-set amount. In this way, the integrated device 1 can be readily adapted to the noise characteristics of various engines.
  • the sequence of the elements inside the casing 2 may be different from the one illustrated.
  • the resonator element 8 and the first damping element 10 may be set downstream of the filter cartridge 5; on the other hand, the second damping element 18 may be set upstream of said filter cartridge 5.

Abstract

Low-noise integrated air-filtering device, including a casing (2), which has an inlet pipe (3) and an outlet pipe (4), and a filter element (5), which is set inside said casing (2). The integrated device is further provided with a silencer device (7) including at least one resonator element (8) and one first damping element (10), which are set in series together and are contained inside said casing (2). Said resonator element (8) has a neck (12) having a length (L) that can be adjusted.

Description

  • The present invention relates to a low-noise integrated air-filtering device.
  • As is known, noise reduction in reciprocating-type engines, especially internal-combustion engines for vehicles for non-military use, is a requirement that is assuming an ever-increasing importance. The said noise is mainly caused by pressure waves that are generated on account of the reciprocating motion of the pistons in the cylinders and that propagate along the air-intake and exhaust-gas pipes.
  • Consequently, in order to achieve the aim, silencer devices, such as perforated-plug elements, are currently employed, which enable conversion of part of the energy associated to the pressure waves into heat. Normally, the silencer devices are set along the exhaust pipe and contribute to reducing considerably the overall noise level of the engine.
  • Frequently, however, this is not sufficient, and it necessary to adopt additional solutions. In particular, it is possible to add further silencer elements also along the air-intake pipe, for example upstream of the air-intake filter.
  • The known solutions, however, present a number of drawbacks, which are linked mainly to the encumbrance, in so far as the silencer elements currently available must be inserted externally to the air-intake filter, and which are linked to the characteristics of noise-deadening of the silencer device, which can be made by assembling distinct elements together.
  • As is known to a person skilled in the branch, in fact, the performance of a silencer device is markedly affected by the geometry both of the device itself and of the flow of air that conveys the noise that is to be attenuated. On the other hand, the use of distinct silencer elements that are assembled along the air-intake pipe does not enable an optimal geometry, and hence noise is reduced only partially.
  • Furthermore, it is not possible to modify either the dimensions or the noise-attenuation characteristics of the individual elements that form the silencer device, which consequently is not suitable for being used on engines that are different, for example, in terms of displacement or in terms of other constructional features. It is thus necessary to provide different elements according to the type of engine on which the said elements are to be used, and this entails high production costs.
  • The purpose of the present invention is to provide a low-noise integrated air-filtering device which enables the above-mentioned drawbacks to be overcome and which, moreover, is of simple and inexpensive implementation.
  • Provided in accordance with the present invention is a low-noise integrated air-filtering device, comprising a casing, which has an inlet pipe and an outlet pipe, and a filter element, which set inside said casing, characterized in that it comprises a silencer device including at least one resonator element and one first damping element, which are set in series together and are contained inside said casing .
  • In this way, the device is not only compact and of reduced overall dimensions, but can also be built with an optimal geometry which enables noise abatement in an extremely efficient way. In particular, the use of a resonator element and a damping element, which substantially operate in contiguous frequency bands, makes it possible to achieve a high damping effect over a wide spectrum of frequencies.
  • In addition, the device forms a single body which can be conveniently mounted on different engines as a replacement for the traditional air-intake filter.
  • According to a further aspect of the present invention, said resonator element, said first damping element, and said filter element form an axial sequence.
  • In addition, the device has a centroidal axis of symmetry, and said resonator element, said first damping element and said filter element define a linear pipe which is coaxial with said centroidal axis of symmetry.
  • The linear geometry and the symmetry of the pipe with respect to a centroidal axis of symmetry enable effective reduction of the undesired effects of resonance due to the transverse modes of propagation of the pressure waves, and thus enable a further improvement in noise deadening.
  • For a better understanding of the present invention, an embodiment thereof will be described hereinafter, purely by way of non-limiting example and with reference to the attached drawings, in which:
    • Figure 1 is a simplified diagram of an integrated device according to the present invention, in a longitudinal cross-sectional view; and
    • Figure 2 presents plots of quantities regarding the device of Figure 1.
  • With reference to Figure 1, a low-noise integrated air-filtering device, designated as a whole by 1, comprises a casing 2, which has a longitudinal axis A of symmetry, an inlet pipe 3 and an outlet pipe 4, which are coaxial to the longitudinal axis A. Housed inside the casing 2 are a filter cartridge 5, of a type in itself known, and a silencer device 7, which includes at least one resonator element 8 and one first damping element 10. In detail, the resonator element 8, the first damping element 10 and the filter cartridge 5 are set in series together and form an axial sequence, in which the resonator element 8 and the first damping element 10 are set upstream of the filter cartridge 5.
  • According to the present invention, the longitudinal axis A of symmetry is also a centroidal axis of the device 1. In addition, the resonator element 8, the first damping element 10 and the filtering cartridge 5 define a linear pipe 11 coaxial to the longitudinal axis A of symmetry. In particular, the linear pipe 11 is traversed by a flow of air sucked in towards the engine (not shown). The said flow of air conveys pressure waves which are generated by the engine itself during its normal operation and which are the source of the noise that is to be attenuated.
  • Preferably, the resonator 8 is an in-line Helmholtz resonator and has a neck 12, which has an adjustable length L, and a volume V. In this way, the resonator element 8 is particularly suited for attenuating noise in a medium-to-low frequency band, up to approximately 300 Hz. In addition, the frequency of maximum damping can be adjusted, as will be explained hereinafter.
  • In detail, the neck 12 of the resonator element 8 has an annular shape and is defined comprised between an outlet stretch 3a of the inlet pipe 3 and a first stretch 11a of the linear pipe 11.
  • In particular, the outlet stretch 3a of the inlet pipe 3 is inserted, in an axially slidable way, inside the first stretch 11a of the linear pipe 11.
  • The axial position of the inlet pipe 3 with respect to the linear pipe 11 (and hence the length L of the neck 12) can be adjusted by means of an actuation device, comprising, for example, a rack 13, carried integrally by the inlet pipe 3 and set longitudinally, and a gear 14, driven by a motor, of a known type and not illustrated.
  • Optionally, a diaphragm 15 can be inserted inside the casing 2 in order to reduce by a pre-set amount the volume V of the resonator element 8.
  • The first damping element 10 is a perforated-plug element with low density of perforation, for attenuation of the noise in a medium-to-high frequency band, up to approximately 900 Hz. For example, the density of perforation is between approximately 4% and 5%.
  • An annular region, which is defined between the casing 2 and the first damping element 10 and which moreover is axially delimited by a first wall 17a and a second wall 17b, forms an expansion chamber 17, which contributes to attenuating the noise generated by the engine, as will be explained later on with reference to Figure 2.
  • According to a preferred embodiment of the present invention, the integrated device 1 comprises a second damping element 18, set inside the casing 2, downstream of the filter cartridge 5. In addition, the second damping element 18 is coaxial to the longitudinal axis A of symmetry and is connected to the outlet pipe 4. In particular, the second damping element 8 is a perforated-plug element with high perforation density for noise damping in a high-frequency band, substantially with frequencies higher than 600 Hz.
  • Figure 2 shows damping curves of the resonator element 8, of the first damping element 10 and of the expansion chamber 17 in a frequency band of between 0 and 1000 Hz. In detail, the damping curve for the resonator element 8 is illustrated with a solid line; the damping curve for the first damping element 10 is illustrated with a dashed line; and the damping curve for the expansion chamber 17 (i.e., due exclusively to a sharp variation in the section of the pipe in which the air flows) is illustrated with a dashed-and-dotted line.
  • As mentioned previously, when the engine on which the integrated device 1 is operating, the inlet pipe 3, the linear pipe 11 and the outlet pipe 4 of the integrated device 1 itself are traversed by a flow of air in which substantially periodic pressure waves, which are a source of noise, propagate.
  • The noise is mainly attenuated by the resonator element 8 and by the first damping element 10. The integrated device 1, as a whole, is particularly effective in damping transverse modes of propagation of the pressure waves. As is known to a person skilled in the branch, the said result can be obtained when the flow of air develops substantially about a centroidal axis of the damping device (in the case of the integrated device 1, the flow of air develops substantially about the longitudinal axis A of symmetry, which is a centroidal axis). In this way, in fact, it is possible to shift secondary resonance frequencies present in the damping and air-filtering devices towards high frequency values, namely ones that are outside the spectrum of frequencies of the pressure waves that generate noise. The said secondary resonance frequencies are not therefore excited, and undesired resonance effects are thus prevented.
  • In addition, the maximum attenuating frequency of the resonator element 8 can be adjusted. In an in-line Helmholtz resonator, such as the resonator element 8, the said maximum frequency of attenuation corresponds, in fact, to the characteristic resonance frequency FR given by the following equation: FR = 1 C2SLEFFV where C is the speed of sound, S is the area of a radial section of the neck 12 of the resonator element 8, and LEFF is the effective length of the neck 12. The said effective length LEFF is in turn defined, to a first approximation, by the following expression: LEFF = L + 0.8 S
  • Clearly, the possibility of varying the axial position of the inlet pipe 3 with respect to the linear pipe 11 enables adjustment of the length L of the neck 12 of the resonator element 8 and, consequently, also its characteristic frequency of resonance FR.
  • It is moreover evident from equation (1) that the characteristic frequency of resonance FR can be modified also by varying the volume V of the resonator element 8. For this purpose, as mentioned previously, it is possible to insert, inside the casing 12, the diaphragm 15, which reduces the volume V by a pre-set amount. In this way, the integrated device 1 can be readily adapted to the noise characteristics of various engines.
  • Finally, it is clear that modifications and variations may be made to the integrated device described herein, without thereby departing from the scope of the present invention.
  • In particular, the sequence of the elements inside the casing 2 may be different from the one illustrated. For example, the resonator element 8 and the first damping element 10 may be set downstream of the filter cartridge 5; on the other hand, the second damping element 18 may be set upstream of said filter cartridge 5.

Claims (9)

  1. A low-noise integrated air-filtering device, comprising a casing (2), which has an inlet pipe (3) and an outlet pipe (4), and a filter element (5), which is set inside said casing (2), characterized in that it comprises a silencer device (7) including at least one resonator element (8) and one first damping element (10), which are set in series together and are contained inside said casing (2).
  2. The device according to Claim 1, characterized in that said resonator element (8), said first damping element (10) and said filter element (5) form an axial sequence.
  3. The device according to Claim 2, characterized in that it has a centroidal axis of symmetry (A), and in that said resonator element (8), said first damping element (10) and said filter element (5) define a linear pipe (11) coaxial to said centroidal axis of symmetry (A).
  4. The device according to Claim 2 or Claim 3, characterized in that said resonator element (8) is an in-line Helmholtz resonator, and said first damping element (10) is a perforated-plug element with low perforation density.
  5. The device according to Claim 4, characterized in that said resonator element (8) has a neck (12) having a length (L) that can be adjusted.
  6. The device according to Claim 5, characterized in that said neck (12) of said resonator element (8) has an annular shape and is defined between an outlet stretch (3a) of said inlet pipe (3), which is inserted inside a first stretch (11a) of said linear pipe (11), and said first stretch (11a) of said linear pipe (11), said inlet pipe (3) being moreover axially slidable with respect to said linear pipe (11).
  7. The device according to Claim 6, characterized in that it comprises an expansion chamber (17) defined by an annular region which is comprised between said casing (2) and said first damping element (10) and which is moreover axially delimited by a first wall (17a) and a second wall (17b).
  8. The device according to any one of Claim 3 to 7, characterized in that it comprises a second damping element (18), set inside said casing (2), downstream of said filter element (5), said damping element (18) being coaxial to said centroidal axis of symmetry (A).
  9. The device according to Claim 7, characterized in that said second damping element (18) is a perforated-plug element with high perforation density.
EP02008733A 2001-04-26 2002-04-18 Low-noise integrated air-filtering device Expired - Lifetime EP1253312B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ITMI20010873 2001-04-26
IT2001MI000873A ITMI20010873A1 (en) 2001-04-26 2001-04-26 LOW NOISE AIR FILTERING DEVICE

Publications (2)

Publication Number Publication Date
EP1253312A1 true EP1253312A1 (en) 2002-10-30
EP1253312B1 EP1253312B1 (en) 2005-03-02

Family

ID=11447553

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02008733A Expired - Lifetime EP1253312B1 (en) 2001-04-26 2002-04-18 Low-noise integrated air-filtering device

Country Status (4)

Country Link
EP (1) EP1253312B1 (en)
AT (1) ATE290163T1 (en)
DE (1) DE60203059T2 (en)
IT (1) ITMI20010873A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE1018044A3 (en) * 2008-03-12 2010-04-06 Atlas Copco Airpower Nv Inlet silencer for compressor plant, has housing including integrated gas filter, where partition is provided in internal damping space of housing such that damping space splits into two subspaces
CN103362702A (en) * 2012-04-05 2013-10-23 通用汽车环球科技运作有限责任公司 Multi-mode air induction tuning duct
EP2021614B1 (en) 2006-05-29 2017-05-31 Mann + Hummel GmbH Air filter housing for a compact air filter element
CN113107724A (en) * 2021-04-30 2021-07-13 东风汽车集团股份有限公司 Air filter structure of air inlet system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2553326A (en) * 1946-08-16 1951-05-15 Burgess Manning Co Apparatus for silencing and filtering noise producing gases
GB1507247A (en) * 1975-11-25 1978-04-12 Dba Sa Air filter
JPH0219644A (en) * 1988-07-06 1990-01-23 Toyoda Spinning & Weaving Co Ltd Resonator type air cleaner
DE19641715A1 (en) * 1996-10-10 1998-04-16 Mann & Hummel Filter Intake system for an internal combustion engine
US6048386A (en) * 1996-04-26 2000-04-11 Donaldson Company, Inc. Integrated resonator and filter apparatus
EP1156205A2 (en) * 2000-05-19 2001-11-21 Siemens Canada Limited Air cleanner resonator mounting system and cover

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2553326A (en) * 1946-08-16 1951-05-15 Burgess Manning Co Apparatus for silencing and filtering noise producing gases
GB1507247A (en) * 1975-11-25 1978-04-12 Dba Sa Air filter
JPH0219644A (en) * 1988-07-06 1990-01-23 Toyoda Spinning & Weaving Co Ltd Resonator type air cleaner
US6048386A (en) * 1996-04-26 2000-04-11 Donaldson Company, Inc. Integrated resonator and filter apparatus
DE19641715A1 (en) * 1996-10-10 1998-04-16 Mann & Hummel Filter Intake system for an internal combustion engine
EP1156205A2 (en) * 2000-05-19 2001-11-21 Siemens Canada Limited Air cleanner resonator mounting system and cover

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 014, no. 157 (M - 0955) 27 March 1990 (1990-03-27) *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2021614B1 (en) 2006-05-29 2017-05-31 Mann + Hummel GmbH Air filter housing for a compact air filter element
BE1018044A3 (en) * 2008-03-12 2010-04-06 Atlas Copco Airpower Nv Inlet silencer for compressor plant, has housing including integrated gas filter, where partition is provided in internal damping space of housing such that damping space splits into two subspaces
CN103362702A (en) * 2012-04-05 2013-10-23 通用汽车环球科技运作有限责任公司 Multi-mode air induction tuning duct
CN103362702B (en) * 2012-04-05 2016-09-14 通用汽车环球科技运作有限责任公司 Multi-mode air-breathing tuning conduit
CN113107724A (en) * 2021-04-30 2021-07-13 东风汽车集团股份有限公司 Air filter structure of air inlet system

Also Published As

Publication number Publication date
ATE290163T1 (en) 2005-03-15
DE60203059T2 (en) 2006-01-26
ITMI20010873A0 (en) 2001-04-26
EP1253312B1 (en) 2005-03-02
DE60203059D1 (en) 2005-04-07
ITMI20010873A1 (en) 2002-10-26

Similar Documents

Publication Publication Date Title
US6752240B1 (en) Sound attenuator for a supercharged marine propulsion device
US6158546A (en) Straight through muffler with conically-ended output passage
US7967107B2 (en) Muffler apparatus for vehicle
JPH06207563A (en) Exhaust turbo-supercharger
US20080060622A1 (en) Supercharger with housing internal noise attenuation
JP2005084693A (en) Sound absorption device
JP2005069228A (en) Muffler
CN107587959B (en) Turbocharger
US20110108358A1 (en) Noise attenuator and resonator
JP2020026748A (en) Silencer
EP1908930A2 (en) Exhaust silencer for automotive vehicles
JP2006207378A (en) Noise reduction device for exhaust system and exhaust system having the same
EP1253312B1 (en) Low-noise integrated air-filtering device
US20040261621A1 (en) Disposable filtering and muffling assembly
JP2001524635A (en) Silencer with branch resonator
US2656005A (en) Retroverted passage type muffler with resonator chambers
JPH11351085A (en) Reciprocating internal combustion engine
US10161275B2 (en) Compact muffler having multiple reactive cavities providing multi-spectrum attenuation for enhanced noise suppression
JP2011017291A (en) Air suction device
RU2319856C2 (en) Internal combustion engine
CN113007068A (en) Novel suction muffler for refrigerator compressor
RU2460889C1 (en) Automotive ice exhaust gas silencer
RU2150018C1 (en) Air cleaner of vehicle internal-combustion engine
SU1178912A1 (en) Silencer of internal combustion engine
SU877093A2 (en) Noise silenser

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Free format text: AL;LT;LV;MK;RO;SI

17P Request for examination filed

Effective date: 20030428

17Q First examination report despatched

Effective date: 20030602

AKX Designation fees paid

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050302

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050302

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050302

Ref country code: CH

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050302

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050302

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050302

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050302

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REF Corresponds to:

Ref document number: 60203059

Country of ref document: DE

Date of ref document: 20050407

Kind code of ref document: P

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050418

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050418

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050418

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050430

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050602

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050602

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050613

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050817

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

ET Fr: translation filed
26N No opposition filed

Effective date: 20051205

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20060406

Year of fee payment: 5

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20060410

Year of fee payment: 5

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060418

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20060530

Year of fee payment: 5

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20060418

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20071101

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20070419

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20070430

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100418

PGRI Patent reinstated in contracting state [announced from national office to epo]

Ref country code: IT

Effective date: 20110616

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20160331

Year of fee payment: 15

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170418