[0001] The present invention relates to a low-noise integrated air-filtering device.
[0002] 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.
[0003] 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.
[0004] 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.
[0005] 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.
[0006] 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.
[0007] 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.
[0008] 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.
[0009] 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 .
[0010] 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.
[0011] 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.
[0012] According to a further aspect of the present invention, said resonator element, said
first damping element, and said filter element form an axial sequence.
[0013] 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.
[0014] 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.
[0015] 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.
[0016] 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.
[0017] 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.
[0018] 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.
[0019] 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.
[0020] 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.
[0021] 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.
[0022] 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.
[0023] 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%.
[0024] 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.
[0025] 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.
[0026] 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.
[0027] 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.
[0028] 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.
[0029] 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 F
R given by the following equation:

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 L
EFF is the effective length of the neck 12. The said effective length L
EFF is in turn defined, to a first approximation, by the following expression:

[0030] 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 F
R.
[0031] It is moreover evident from equation (1) that the characteristic frequency of resonance
F
R 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.
[0032] 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.
[0033] 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.
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.