U.S. patent number 3,665,965 [Application Number 05/040,607] was granted by the patent office on 1972-05-30 for apparatus for reducing flowing fluid pressure with low noise generation.
This patent grant is currently assigned to Masoneilan International, Inc.. Invention is credited to Hans D. Baumann.
United States Patent |
3,665,965 |
Baumann |
May 30, 1972 |
APPARATUS FOR REDUCING FLOWING FLUID PRESSURE WITH LOW NOISE
GENERATION
Abstract
Fluid pressure reducing apparatus presenting low noise
throttling plates. The low noise fluid pressure throttling
apparatus provides an assembly of a plurality of such plates, and
which may comprise a segment of or be interposed in a fluid flow
containing conduit. The low noise throttling plates are passaged by
multiple small section orifices producing a high frequency pressure
wave whose noise is more readily attenuated by the conduit. The
spacing of the plates in the pressure reducing assembly defines
with the intervening flow containing means a volume which is
dimensioned to produce resonant damping of the noise pressure wave
generated in the primary orifices. The pressure drop through the
reducing apparatus is divided into nearly equal ratio drops across
each plate, further minimizing noise generation.
Inventors: |
Baumann; Hans D. (Foxboro,
MA) |
Assignee: |
Masoneilan International, Inc.
(Norwood, MA)
|
Family
ID: |
21911918 |
Appl.
No.: |
05/040,607 |
Filed: |
May 26, 1970 |
Current U.S.
Class: |
138/42;
251/127 |
Current CPC
Class: |
F16L
55/04 (20130101); F16L 55/02718 (20130101) |
Current International
Class: |
F16L
55/04 (20060101); F16L 55/027 (20060101); F16L
55/02 (20060101); F15d 001/00 () |
Field of
Search: |
;138/42
;181/46,69,33.9,36.2,56 ;251/127 ;285/49 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Rothberg; Samuel B.
Claims
I claim:
1. Low noise generating apparatus for reducing the pressure of
fluid flow in a conduit, comprising:
a. upstream transverse wall means;
b. multiple, small, flow throttling passages of calculated total
area in and establishing small fluid pressure drop across and high
frequency of noise generation by said upstream wall means;
c. one or more downstream transverse wall means;
d. multiple, small, flow throttling passages of calculated total
area in and establishing small fluid pressure drop across and high
frequency of noise generation by said one or more downstream wall
means,
the number and/or size of said multiple, small, flow throttling
passages relatively increasing, and said calculated total areas of
said passages progressively increasing in constant ratio, from each
to the next in the succession of said upstream and downstream
transverse wall means,
said multiple, small, flow throttling passages in said upstream and
downstream transverse wall means provided in such determined large
number and small cross section as radiates noise energy at a
frequency at which it is highly attenuated within said conduit, and
whereby it accords the apparatus low accoustical efficiency;
and
e. means circumferentially containing the fluid flow intermediate
said upstream and downstream throttling passages and forming with
said transverse wall means a frame supporting and spacing said
throttling passages,
said circumferentially containing means comprising, with the one or
more pairs of any two adjacent of said upstream and downstream
transverse wall means, one or more resonant damping chambers,
each said resonant damping chamber defining, by the spacing of said
transverse wall means, a volume calculated to produce the resonant
frequency of the sound waves generated by the fluid flow through
said transverse wall means.
2. The apparatus of claim 1, wherein the number and/or size of the
throttling passages of one is varied from the number and/or size of
the throttling passages of other adjacent of said upstream and
downstream transverse wall means such as to divide the pressure
drop across said apparatus into substantially equal ratio pressure
drops across the individual of said upstream and downstream
transverse wall means.
3. The apparatus of claim 1, wherein the throttling passages of one
are offset in the flow direction from the passages of another of
said upstream and downstream transverse wall means.
4. The apparatus of claim 1, wherein said transverse wall means are
plates, and wherein said throttling passages are holes defining jet
orifices in said plates.
5. The apparatus of claim 1, wherein said transverse wall means
comprise annular plates, and wherein said circumferential
containing means comprises a spacer ring.
6. The apparatus of claim 1 and means uniting said transverse wall
means centrally of said circumferential containing means, said
centrally uniting means comprising a fastener engaging and adapted
to draw together said transverse wall means.
7. The apparatus of claim 6, and spacer means limiting said drawing
together by said fastener, said spacer means comprising one or more
collars, and said fastener engaged behind one of said transverse
wall means, passed through said one or more collars, and adjustably
secured to another said transverse wall means.
8. The apparatus of claim 1, and means positioning said transverse
wall means for determined upstream-downstream spacing of said flow
throttling passages.
9. The apparatus of claim 1, and means for adjusting the flow
capacity of said frame.
10. The apparatus of claim 9, wherein said flow capacity adjusting
means comprises means for closing a determined portion of the
passages of one or another of said wall means.
11. The apparatus of claim 10 wherein said passage closing means
comprise plate means removably supported against the upstream side
of said one or another wall means.
12. The apparatus of claim 11, wherein said plate means are carried
on fastener means removably securing together said wall means
centrally of said circumferential containing means.
Description
BACKGROUND OF THE INVENTION
The invention pertains to apparatus for reducing the pressure of
gaseous or liquid media flowing through a pipe or duct, and more
particularly for accomplishing the fluid pressure reduction with
minimum or greatly reduced generation of noise, or unwanted sound.
The problems attendant upon the annular of noise are well known to
include not only the human reaction criteria of annoyance, damage
to hearing, and reduction in work efficiency, but also the effects
on physical structures and equipment, such as structural fatigue,
and equipment malfunction.
In industrial plants, gas pressure reducing stations, and the like
where are found the throttling valve or aerodynamically generated
sound effects with which the invention is particularly concerned,
the noise problems attendant thereon are rapidly intensifying in
absolute terms, and have attained more recently a magnitude
heightened also be increased human sensibility to noise pollution.
But noise control efforts have heretofore been limited generally in
this country to the use of mufflers, attenuation chambers and the
like, or devices for absorption or insulation of the generated
noise. This invention, in contrast, cuts throttling noise at the
source, and thereby achieves superior results both in reducing
throttling noise and in reducing mechanical vibration from levels
experienced with conventional pressure reducing valves.
BRIEF SUMMARY OF THE INVENTION
In view of its novel aspects, the theoretical considerations on
which the invention is rested are here set forth in aid of its full
and clear understanding by those skilled in the art.
Fluid dynamic theory predicates a high dependence of the herein
concerned throttling noise energy on the pressure drop ratio and
fluid flow velocity. High pressure differentials across a jet or
constriction in the fluid flow generate noise energy which
increases at a rate greater than the rate of increase in the
pressure drop in ratio. The noise or vibration energy generated
also varies with the eighth power of the fluid velocity in the jet.
Both a high velocity, and a pressure drop ratio, then, lead to high
accoustical efficiency, or high energy conversion to noise.
By far the most efficient way to reduce throttling noise is, of
course, to decrease the velocity of the flow. In accomplishing this
by increasing the effective flow area only some of the resultant
noise reduction is offset by the noise being a function also of
flow area.
Any solid or fluid medium vibrating in response to noise energy
waves will convert a portion of the energy it receives to heat.
With fluids it is the fluid viscosity which occasions the
conversion, or damping. A similar noise energy damping reaction
occurs as well in solids.
Further, the amount of energy passed on through such media varies
with the negative power of the distance that the energy travels
within the medium. And in solids like the metals found in pipes,
the attenuation in the medium increases with the frequency of the
noise energy.
It is thus an object of the present invention to provide apparatus
for pressure reduction or throttling of fluid flow with a low
accoustical efficiency.
It is a further object of the invention to provide an accoustical
filter for absorbing downstream the noise of conventional valves
and thereby preventing the radiation of that noise through the
fluid conduit walls to its external surroundings.
It is a further object of the invention to provide a device for
throttling fluid flow with greatly reduced noise generation by
minimum fluid velocity constricting jet means.
It is a further object of this invention to provide a pressure
reducing or throttling device having constricting jet means
characterized by lowered pressure drop thereacross.
It is a further object of the present invention to provide a
pressure reducing apparatus which increases the viscous damping of
the noise energy in the flowing fluid.
It is a further object of the present invention to provide a fluid
pressure throttling device which generates noise at a frequency
which provides for greater attenuation of the noise energy by the
fluid conduit.
It is a further object of the invention to absorb part of the
aerydynamically created noise by a process of resonant damping
within said throttling device.
BRIEF DESCRIPTION OF DRAWINGS
In the drawings:
FIG. 1 is a plan view of the invention apparatus; and
FIG. 2 is a section along any bisecting line of FIG. 1; and
FIG. 3 is a perspective view of a modified form of the
apparatus.
DETAILED DESCRIPTION OF THE INVENTION
In the form of FIGS. 1 and 2 of the drawings a herein circular,
radially symmetrical conduit C is shown as having an inner wall
defining two axially in-line parts 3a, 3b which extend to either
side of a ring or annular spacer 4. The spacer 4 has a larger
diameter, cylindrical inner face 5 coaxial with conduit axis A--A',
and an intermediate, annular, infacing flange or lip 6 of full
circumferential extent.
A pair of transverse wall forming means or plates 7, 9 having a
tight fit within spacer 4 are held by suitable means, herein the
collars 8 and 11, against the opposite faces of lip 6. The collars
8 and 11 are in turn closed against the plates 7, 9 by the ends of
smaller diameter shoulders of conduit parts 3a, 3b when the same
are assembled with the spacer 4 as by external clamping means which
may be conventional and are, therefore, not shown.
Under the invention, the plates 7, 9 may be parallel mounted with
the ring 4 in a rigid assembly or frame in any desired manner, and
wherein the circumferentially containing means 4 is inserted in or
is a portion of the conduit C.
Upstream plate 7 is passaged by a multiplicity of jet orifices or
holes 12. The number of holes 12 is great, and their
cross-sectional area is small. The holes 12 will be understood to
be utilized in a number: cross-sectional area combination which for
a given fluid at a given or maximum expected flow rate produces the
desired low pressure drop across the plate 7, in the fluid flow
traversing the same in the left-right direction A--A'.
Under the invention the holes 12 are made numerous and individually
of small cross-sectional area also to increase the vibratory
frequency of the noise energy accompanying the pressure drop in
said flowing fluid.
Most of the noise energy generated in the upstream set of holes 12
is radiated by pressure waves from a region of noise energy
turbulence downstream of plate 7, and tends to proceed out through
the walls of the conduit C. In responding to these pressure waves,
the conduit C absorbs a portion of the energy from the waves by
damping effect of the conduit material.
This attenuation by the conduit may be expressed as:
A = 17 log (mf)
where
m = mass density of the wall and
f = frequency of the vibration.
The frequency is, of course, a direct function of the passages or
hole diameter. Under the invention, then, by reducing the diameter
of the upstream holes 12, and thereby increasing the frequency of
the noise energy generated therein, a larger portion of the noise
energy is attenuated in the conduit walls, and a corresponding
reduction is achieved in the noise radiated to or polluting the
environment.
The downstream plate 9 has a set of orifices or holes 14 which are
seen as offset from the holes 12. The number and cross-sectional
area of these holes is again adjusted to the desired pressure drop,
for a given fluid and flow rate, and is selected also and novelly
to provide, as before, increased frequency of vibration of, and
thereby enhanced conduit wall attenuation of, the generated
noise.
By varying the size and number of the holes 14 in the downstream
plate 9, compensation is made for the change in fluid density by
the reduction in pressure through the upstream plate 7. Further,
the total cross-sectional area of the holes 14 is made larger than
the total cross-sectional area of the holes 12, by the provision
either of more or larger holes 14 through the second plate 9.
In accordance with the invention, then, the pressure drop across
the perforated plates 7 and 9 is split up into equal or
substantially equal ratios. This results in a substantial decrease
of the overall noise level, since as above noted, the level of
noise energy generated in a jet increases more rapidly than the
rate of increase in the pressure drop ratio across the jet. In
other words, by thus keeping the pressure drop ratio across each
perforated plate smaller, there is achieved a reduction of noise
energy generated, over that for a single plate with a higher
accoustical efficiency in noise generation due to its higher
pressure drop.
For example, with a total pressure drop ratio of 4 the accoustical
efficiency for a single plate is 36 times greater than the
efficiency it would have with a pressure drop ratio of 2 across its
set of holes. With two plates each producing a pressure drop ratio
of 2 the total noise energy from the two plates in one-eighteenth
what it would have been with a single plate.
Centrally, a fastening or bolt 16 having a head 17 is passed
through an oversized opening in one of the plates 7, 9 and through
an intervening collar 18 and threaded into the other of the plates
7, 9, in part to intermediately clamp the plates 7, 9 together with
the spacer 6 in a unitary assembly, or frame.
The bolt 16 may also mount various flow restricting means such as
the flow regulating plate 19, which may be positioned between the
plates 7 and 9, or upstream of plate 7, the same to effectively
block a portion of the first and/or second of the channel sets 12,
14 thereby reducing the flow capacity of the plates so as to
maintain the same total pressure drop under different, reduced flow
conditions.
The aforementioned offsetting of the downstream holes 14, as
clearly shown in FIG. 2, will be understood to improve the pressure
reducing capability of the plates 7, 9 and at the same time to
enhance the resonant effect in the cavity or volume 21 defined by
or within the frame formed by the plates 7, 9 and the spacer 4. The
longitudinal or axial length of the collar 18 and the spacer lip 6
then, is calculated to comprehend or contain the desired amount of
fluid within the frame volume 21. For a particular conduit, and
given that the resonant frequency of the volume 21 varies with its
size, the same can be controlled, then, by adjusting the length as
aforesaid of the collar 6 and spacer 18.
The equation relating the plates 7, 9 may be stated as:
f = Ac/2 Vk
where
A = total area of the holes contained in the first plate 7;
c = the speed of sound in the fluid used;
V = the volume of the cavity 21; and
k = a constant.
By making a resonant frequency of the volume 21 nearly equal to the
frequency of noise energy generated in the holes 12 of the upstream
plate 7, large resonant pressure differentials will be built up in
the volume 21 at that frequency. Through the process of resonant
damping, and due to the viscosity of the fluid, the high resonant
pressure differentials result in an increased conversion of noise
energy to fluid heat.
It will be understood that the pressure reducing apparatus of the
invention may comprise the plates 7, 9 and also any other
transverse wall forming means susceptible of channeling by jet
passages such as the hole sets 12, 14.
Further, the desired resonant cavity may under the invention be
provided by a volume 21 having shape and proportion other than that
defined by the frame spacer 6 and plates 7, 9 herein particularly
disclosed and described.
Still further, the resonant cavity may be defined by and within a
frame comprising a plurality other or more than the described two
spaced transverse plates, or other wall forming means.
Thus, in FIG. 3 is shown a modified embodiment comprising a
plurality of three transverse plates, incorporating upstream plate
7 and a pair of downstream plates 9, 22. In this arrangement, the
downstream plate 22 will be understood to have openings 23 having
the similar position and proportion relationship to the openings 14
of downstream plate 9 as the latter have to the openings 12 of
upstream plate 7. Also, the plates 7, 9, 22 will be understood to
define resonant cavities, and to divide the frame volume, in
accordance with the invention teachings as hereinbefore
explained.
To accommodate the additional plate 22, the modified ring 4a may
have a lip 6a against which upstream plate 7 is held by collar 8,
and downstream plate 9 is engaged by insert ring 24, against the
opposite face of which the downstream plate 22 is in turn held by
collar 11. And modified bolt 16a will be understood to be passed
through intermediate plate 9 for threading into downstream plate
22, with the plates being spaced thereat by a pair of the collars
18.
Also shown in FIG. 3 is one expedient for closing the ends of
conduit portions 3a, 3b against the sides of the rings 4a,
comprising integral flanges 25, 26 on said conduit portions 3a, 3b,
and a series of radially disposed nut and bolt or similar
fastenings 27 therethrough as shown.
It will also be understood that the frame hereof may comprise the
described plate pluralities and the intervening conduit wall
portion as defined by the herein disclosed spacer, or by the
securing of the wall forming means or plates to the conduit inner
wall and in spaced assembly in any other desired or convenient
manner.
Further, in accordance with the invention, the plate assembly or
frame hereof may be utilized in downstream conjunction with a
conventional, single orifice throttling valve. It will be
appreciated that in such application the low noise plates hereof
operate to filter the major noise emanating from the throttling
valve, preventing the noise from travelling into the downstream
pipe and hence from radiating through that to the outside
environment.
* * * * *