US2100404A - Fluid transmission - Google Patents
Fluid transmission Download PDFInfo
- Publication number
- US2100404A US2100404A US628980A US62898032A US2100404A US 2100404 A US2100404 A US 2100404A US 628980 A US628980 A US 628980A US 62898032 A US62898032 A US 62898032A US 2100404 A US2100404 A US 2100404A
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- pressure
- water
- air
- frequency
- branch
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/04—Devices damping pulsations or vibrations in fluids
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/04—Devices damping pulsations or vibrations in fluids
- F16L55/045—Devices damping pulsations or vibrations in fluids specially adapted to prevent or minimise the effects of water hammer
- F16L55/05—Buffers therefor
- F16L55/052—Pneumatic reservoirs
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pipe Accessories (AREA)
Description
Nov. 30, 1937. w. P. MASON ET AL 2,100,404
FLUID TRANSMIS S ION Filed Aug. 16, 1932 Z'IS FREQUENCY J. E. TW EDD/1L5 By W AT T ORNE V which reference is made in explaining the inven- Patented Nov. 30, 19 37 PATENT 2,100,404 FLUID TRANSMISSION Warren P. Mason East Orange, N. 1., George T.
Stanton, Mamaroneck, N. Y., and {John E.. Tweeddale, Newark, N. J said Mason 'assignor to Bell Telephone Laboratories; Incorporated,
New York, N. Y., a corporation of New York, and said Stanton and Tweeddale assignors to Electrical Research Products, Inc., New York,
N. Y., a corporation of Delaware Application August 16, 1932, Serial No. 628,980
3 Claims.
This invention relates to fluid transmission and more particularly to arrangements for suppressing fluid pulsations in the pipes of a distribution or supply system.
An object of the invention is to prevent vibrations of the pipes of a fluid distribution system due to periodic ,pressure pulsations of a supply pump connected thereto.
Another object is to obtain a smooth steady flow of a fluid in a supply system.
In the water supply'systems of high buildings distribution throughout the building is generally from a gravity tank on the roof to which the water is pumped through vertical risers connected to the supply mains. Where centrifugal pumps are usedthe impeller blades induce in the water periodic pressure variations of a relatively high frequency which may be in the audible range. These pressure variations tend to set the riser pipes into vibration which may be imparted to the floors and walls of the buildings and produce an audible disturbance of loudness.
In accordance with this invention, a vibration filter is associated with the supply pipe of a fluid distribution system, preferably at a point close to the supply pump or other source .of pressure waves, the filter being so designedthat pressure waves of the objectionable frequencyare strongly attenuated while the steady flow of the fluid is not impeded.
A feature of the vfilter of resonant vibration absorbing means tuned to the disturbing frequency. Other features'will appear from the following detailed description and from the attached drawing, of which: 7
Fig. lshowsan embodiment of the invention in a water supply system;
Fig. 2 represents attenuation characteristics to tion; and
Fig. 3 illustrates amodified form of the invention. v
In the system of Fig. 1, a riser pipe I0 is connected through the device ll, .which constitutes a vibrationfllter, and a pump l2, to a water'supply main IS. .The filter comprises essentially a horizontal pipe section M in the mainsupply objectionable invention is'jth in the at the pulsation frequency. For example, if the pump'is of the'centrifugal type having four blades and rotating at 1800 revolutions per minute, the pulse frequency to which the branches should be resonant would be 120 cycles per second. I
The resonant branches act as absorbers of the pressure pulses and in combination with the inertia of the water in the pipe section I4 produce an attenuation of the pulses which is large at all frequencies above a certainlower limit and is particularly great in the neighborhood of the resonance frequency.
The amount-of air in each of: the branch pipes corresponds to the whole internal volume of the branch at atmospheric pressure. As the system becomes filled, a. certain amount of water is forced into the branches under the head in the riser l0 and the air is thus compressed to a smaller volume determined, ultimately, by the height of the riser." The head of water in the riser thus determines the elasticity, or resistance to compression, of the entrapped air and also'the mass ofwater in a branch. If the branch is of uniform sectional area itf ollows that its length for a desired resonance frequency will be determined by the water head or pressure. In the filter shown in Fig. 1, the side branches are closed at their outer ends by threaded plugs I1 and I8 by means of which somev adjustment of the length, and therefore of the resonance frequency can be effected.
The theory of the action of the filter under regular periodic pulses is greatly simplified by making use of the concept of impedance. It is well known that'when any body or system is subjected to a periodicforceof sinusoidal variation, the resulting motion of the body or system after it has settled down to a steady state has also a sinusoidal variation of the same frequency as the applied force. At the instants of application and removal of the force transient vibratory motions of other frequencies may occur but these are gen-. erally damped out in a very short time. The steady state velocity of motion is proportional to the magnitude of the applied'force and the ratio of the force to the velocity is termed the impedance of the body or system. For sinusoidal variations the root mean square values of the force and velocity are generally used in'determining this ratio. a
'In' systems of the type shown in Fig. 1,.it is convenient to take as the force the pressure intensity in the water and as the velocity therate of volumetric flow across the sections of the pipes. The force tending to produce the vibratory disturbthe sum of Zr and Zw, or
ances in the system is, of course, the pressure variation which is superimposed upon the normal water pressure by the pump impeller blades. The impedance thus defined is termed acoustic impedance since oscillations of the system are of the same type as when sound waves are propagated through the water. For a further discussion of acoustic impedance, reference is made to an article by W. P. Mason, The approximate networks of acoustic filters, Bell System Technical Journal, Vol. 11!, No. 2, April, 1930.
The velocity at any point in a'system may or may not be in phase with the pressure variations. If the system is incapable of storing energy by virtue of its elasticity or its inertia but dissipates it as heat, the velocity will be in phase with the pressure. In the system of Fig. 1 energy dissipation in the filter is practically negligible and the velocitiesin general are out of phase with the pressures.
Consider-now the acoustic impedances of the different portions of the system of Fig. 1. If 21 denotes the length of the connecting pipe it between the centres of the branches and S1 its cross-sectional area, the impedance Z1 of this section may be shown to be l z1=1wf 1 where p denotes the density of the water, 0 is equal to 21r times frequency, and a is the vector operator The operator 1: in Equation (1) indicates that the impedance is such that the velocity will be out of phase with the applied force and will lag behind the force.
The side branches have a length 1: part of which, Zw is filled with water and part, la, is filled with air under pressure. If the cross-sectional area be denoted by $2 the impedances Z. and Z; of the water and air portions, respectively, may be shown to be where P is the steady pressure of the enclosed air and 'y is the adiabatic constant for air, its value being approximately 1.4. The negative sign in Equation 3 indicates that the velocity in the impedance Z8 will lead the force in phase by an angle of 90.
The total impedance Z: of each side branch is a was, Equation 4 indicates that the impedance Z2 will be zero, that is, the branch will be resonant, when.
where Po' denotes normal atmospheric pressure. Further, since The pressure P is equal to the atmospheric pressure plus the pressure due to the head of water in the riser l0.
The effect of the filter in reducing the intensity of the pressure pulses may be arrived at approximately by considering first the pressure attenuation in a filter made up of an infinite number of sections such as shown in Fig. 1 connected end for end. In such a filter, the side branches would have twice the cross-sectional area of those in Fig. 1 and half the impedance. Since the sections are all alike the percentage diminution of pressure would be the same in each. Consequently, the relationship between the pressure m at the input of any section and the pressure in at its output may be written in the form i =e or log, %;==T (8) where e is the base of the Napierian logarithms. The quantity T thus defined is termed the-propagation constant per section of the filter; it may be evaluated in terms of Z1 and Z: by the equation z 2 which in combination with Equation 8 gives Since Equation 10 represents the pressure attenuation per section in an infinitely extended filter, it will not apply exactly to a short filter system such as shown in Fig. 1 due to the difference in the termination conditions. However, for frequencies above a critical frequency which lies below the side branch resonance, the error is found to be of little consequence. This critical frequency is determined by the condition T=2 sin 11- log, i=2 sin 11'} which evidently corresponds to the resonance of the connecting branch and the two side branches connected in series and isolated from the remainder of the system. It is desirable that the critical frequency defined by Equation 11 should be well below the resonance frequency of the side branches since this insures a large degree of attenuation at all frequencies above the critical frequency. This can be achieved by making the inertia effect of the connecting branch large and theside branch impedances small relatively thereto. The advantages of these proportions are illustrated by the curves of Fig. 2 which show the relative attenuations at different, frequencies obtained in two diflerent cases. Curve l9 shows the attenuation according to Equation 10 when 7 At frequencies below the critical frequency the curves indicate that the attenuation is zero. Actually the filter is capable of transmitting vibrations in this range with little or no attenuation. The system is analogous to an electrical broad-band filter of the type described in U. S. Patent 1,227,113 issued May 22, 1917 to G.- A. Campbell, the theory of which is discussed at length in the Bell System Technical Journal, vol. 1, Number 2, November 1922, pp. 1-32.
In the practicaldesign of the filter of Fig. 1, it is convenient to make the connecting branch l4 of about the same diameter as the main supply line to avoid increasing the frictional load on the pump. The condition that the impedance Z1 of this branch should be large in comparison with that of the side branches requires that the length 11 should be great and that the cross-sectional areas of the side branches should also be as large as possible. These requirements follow at once from Equations 1 and 4. Practically there are limits to the extent to which these dimensions can be increased. Due to the elasticity of the water, the pressure pulses have a definite wave length in the pipes equal to the velocity of sound in water divided by the frequency. If the length 21 is much greater than one quarter of the wave length of the disturbing frequency, Equation 1 will cease to be accurate and the performance of the filter will be vitiated. For example, if the pulse frequency is 120 cycles per second the length 11 should preferably not exceed'280 centimeters. The side branch areas are limited by the size of the opening that can be made in the side of the main pipe which, for circular section pipes, limits the side branch area to that of the main pipe.
In the foregoing discussion, it has been assumed that the amount of air in each side branch of the filter is determined by the quantity which will just fill the whole length 12 at normal atmospheric pressure. In practical designs this may lead to a ratio of la to lw which is very large or very small, depending upon the head of water in the riser pipe and the frequency of resonance wo. If there is a great disparity between the lengths Ia and lw then a small change in one of the volumes represented, such, for example, as might be caused by the absorption of part of the air by the water, will produce a disproportionate change in the resonance frequency No. It may be shown mathematically that in order to keep the side branch resonance most stable with variations in la and Zw the condition to be fulfilled is that the volume of air shall be equal to the volume of water, or
Substituting this value for la and l'w in Equation gives from which the length of the side branch is determined in terms of the pressure of the air, the adiabatic constant for air, the density of the water and the frequency of resonance.
If the length 12 is fixed in accordance with Equation (13) then it will be necessary to provide means for letting out part of the entrapped air or for introducing additional air, whichever may be required, inorder to adjust the volume of air to equal the volume of water in the side branch. Fig. 3 shows a modified form of the invention in which provision is made for varying the volume of air represented by la. A stopcock 2| is provided at the-top of the. side branch l6 for valving off air when the volume is too large. A tank 22 contains air under pressure which may be introduced into the side branch through a feed line 23, under the control of avalve 24. The pressure of the air in the tank must, of course, exceed the pressure P of the air in the side branch. A gauge 25 is provided for'the purpose of finding the level of the water. The desired level may be marked on the gauge glass, as shown at 26.
If the water level is below this mark, air is letout through stopcock 2|, and if above, additional air is admitted through valve 24. When the proper level is reached stopcocks 21, 24, 21 and 28 are closed. Thereafter, the water level should be checked periodically and air added as required to compensate for that absorbed by the water. What is claimed is: 1. In a water supply system comprising a main conduit and a pump for maintaining water pressure therein, means for suppressing pulsations of the water pressure due to the pump comprising a pair of side branches in said conduit adapted to retain entrapped air when the conduit is filled with water, the dimensions of said side branches being proportioned with respect to the normal water pressure to produce resonance in each of said branches at the pulsation frequency of said pump, and the separation of said branches being approximately equal to one quarter the wave length of the pressure waves corresponding to the pulsation frequency.
2. In a hydraulic system comprising a pipe line subject to periodic pressure impulses, an elongated chamber of uniform cross-sectional area communicating with said pipe line, means for supplying a gaseous medium under pressure to said chamber, means for valving off excess quantitles of said gaseous medium; and means for indicating when the volume of liquid in said chamber is equal to the volume of gas in said chamber, the length of said chamber being proportioned with respect to the normal fluid pressure to be resonant at the frequency of said periodic pressure impulses when the volume of liquid in said chamber equals the volume of gas in said chamber.
3. In a water supply system comprising a main conduit and a pump for maintaining water pressure therein, means for suppressing pulsations of the'water pressure due to the pump comprising a side branch having unrestricted communication'with said conduit, said branch having a closed end and containing a column of water having thereabove a cushion of air, and said cushion being adapted by variations in volume to accommodate differences of pressure in said column of water incident to the operation of the pump, wherein said volumes of air and water may be so proportioned as to produce resonance in said branch at the pulsation frequency of said pump.
WARREN P. MASON. GEORGE T. STANTON. JOHN E. TWEEDDALE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US628980A US2100404A (en) | 1932-08-16 | 1932-08-16 | Fluid transmission |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US628980A US2100404A (en) | 1932-08-16 | 1932-08-16 | Fluid transmission |
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US2100404A true US2100404A (en) | 1937-11-30 |
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US628980A Expired - Lifetime US2100404A (en) | 1932-08-16 | 1932-08-16 | Fluid transmission |
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Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2460045A (en) * | 1944-02-01 | 1949-01-25 | Holophane Co Inc | Airplane engine test cell and lighting therefor |
US2674343A (en) * | 1949-02-10 | 1954-04-06 | Malerme Paul Eugene | Air damper for lubricant distributors |
US2681013A (en) * | 1950-07-14 | 1954-06-15 | Ernest B Ogdon | Apparatus for maintaining air cushions in pumps |
US2727470A (en) * | 1952-04-01 | 1955-12-20 | California Research Corp | Pulsation dampener |
US3149572A (en) * | 1961-11-13 | 1964-09-22 | William E Davis | Adjustable diaphragm pump |
US3818931A (en) * | 1972-06-08 | 1974-06-25 | J Carpenter | Water hammer arrester |
US3905357A (en) * | 1974-05-13 | 1975-09-16 | Theodore J Ismert | Cushion maintaining device for water service lines |
US4590796A (en) * | 1985-01-23 | 1986-05-27 | Floscan Instrument Co., Inc. | Apparatus and method for pulsation damping and flow measurement in liquid fuel system |
WO1991005201A1 (en) * | 1989-09-29 | 1991-04-18 | Jaromir Tobias | Active accumulator vibration absorbing system |
US5018698A (en) * | 1989-09-29 | 1991-05-28 | Jaromir Tobias | Motor vehicle vibration isolation support mounting system |
US5101929A (en) * | 1989-07-18 | 1992-04-07 | Jaromir Tobias | Vibration isolation support mounting system |
US5141202A (en) * | 1989-09-29 | 1992-08-25 | Jaromir Tobias | Active accumulator vibration absorbing support system |
US5168703A (en) * | 1989-07-18 | 1992-12-08 | Jaromir Tobias | Continuously active pressure accumulator power transfer system |
US5310017A (en) * | 1989-07-18 | 1994-05-10 | Jaromir Tobias | Vibration isolation support mounting system |
US5487652A (en) * | 1993-03-05 | 1996-01-30 | Sgs-Thomson Microelectronics, Inc. | Fuel flow stabilizer |
WO1996021519A2 (en) * | 1995-01-09 | 1996-07-18 | Campbell Hausfeld/Scott Fetzer Co. | Airless paint sprayer intake dampener and inlet valve spring |
US5639219A (en) * | 1995-01-09 | 1997-06-17 | Campbell Hausfeld/Scott Fetzer Co. | Airless paint sprayer intake dampener and inlet valve spring |
US6116872A (en) * | 1997-02-04 | 2000-09-12 | Hitachi Construction Machinery Co., Ltd | Ripple reducing device |
US6412509B1 (en) * | 1999-10-08 | 2002-07-02 | UNIVERSITá DEGLI STUDI DI UDINE | Passive surge control method for compression systems and relative device |
US20040140149A1 (en) * | 2000-09-15 | 2004-07-22 | Terpay Gregory Weston | Passive device for noise reduction |
US20070144598A1 (en) * | 2005-12-22 | 2007-06-28 | John Dooley | Power steering system frequency suppressor |
US20080271946A1 (en) * | 2005-02-21 | 2008-11-06 | Dayco Fluid Technologies S.P.A. | Pipe/Silencer Device Assembly |
US20120061165A1 (en) * | 2010-09-11 | 2012-03-15 | Ford Global Technologies, Llc | Reservoir-less power steering system |
US20140076577A1 (en) * | 2011-03-29 | 2014-03-20 | Schlumberger Technology Corporation | System and method for reducing pressure fluctuations in an oilfield pumping system |
US20140245733A1 (en) * | 2013-03-01 | 2014-09-04 | Deere & Company | In-line parallel standpipe manifold |
WO2016112445A1 (en) * | 2015-01-13 | 2016-07-21 | Embraer S.A. | Fluid attenuators and methods, especially useful for aircraft hydraulic systems |
-
1932
- 1932-08-16 US US628980A patent/US2100404A/en not_active Expired - Lifetime
Cited By (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2460045A (en) * | 1944-02-01 | 1949-01-25 | Holophane Co Inc | Airplane engine test cell and lighting therefor |
US2674343A (en) * | 1949-02-10 | 1954-04-06 | Malerme Paul Eugene | Air damper for lubricant distributors |
US2681013A (en) * | 1950-07-14 | 1954-06-15 | Ernest B Ogdon | Apparatus for maintaining air cushions in pumps |
US2727470A (en) * | 1952-04-01 | 1955-12-20 | California Research Corp | Pulsation dampener |
US3149572A (en) * | 1961-11-13 | 1964-09-22 | William E Davis | Adjustable diaphragm pump |
US3818931A (en) * | 1972-06-08 | 1974-06-25 | J Carpenter | Water hammer arrester |
US3905357A (en) * | 1974-05-13 | 1975-09-16 | Theodore J Ismert | Cushion maintaining device for water service lines |
EP0189314A2 (en) * | 1985-01-23 | 1986-07-30 | FloScan Instrument Company, Inc | Apparatus and method for pulsation damping and flow measurement in liquid fuel system |
US4590796A (en) * | 1985-01-23 | 1986-05-27 | Floscan Instrument Co., Inc. | Apparatus and method for pulsation damping and flow measurement in liquid fuel system |
EP0189314A3 (en) * | 1985-01-23 | 1989-03-15 | FloScan Instrument Company, Inc | Apparatus and method for pulsation damping and flow measurement in liquid fuel system |
US5101929A (en) * | 1989-07-18 | 1992-04-07 | Jaromir Tobias | Vibration isolation support mounting system |
US5168703A (en) * | 1989-07-18 | 1992-12-08 | Jaromir Tobias | Continuously active pressure accumulator power transfer system |
US5310017A (en) * | 1989-07-18 | 1994-05-10 | Jaromir Tobias | Vibration isolation support mounting system |
WO1991005201A1 (en) * | 1989-09-29 | 1991-04-18 | Jaromir Tobias | Active accumulator vibration absorbing system |
US5018698A (en) * | 1989-09-29 | 1991-05-28 | Jaromir Tobias | Motor vehicle vibration isolation support mounting system |
US5050835A (en) * | 1989-09-29 | 1991-09-24 | Jaromir Tobias | Active accumulator vibration absorbing support system |
US5141202A (en) * | 1989-09-29 | 1992-08-25 | Jaromir Tobias | Active accumulator vibration absorbing support system |
US5487652A (en) * | 1993-03-05 | 1996-01-30 | Sgs-Thomson Microelectronics, Inc. | Fuel flow stabilizer |
WO1996021519A2 (en) * | 1995-01-09 | 1996-07-18 | Campbell Hausfeld/Scott Fetzer Co. | Airless paint sprayer intake dampener and inlet valve spring |
WO1996021519A3 (en) * | 1995-01-09 | 1996-10-31 | Campbell Hausfeld Scott Fetzer | Airless paint sprayer intake dampener and inlet valve spring |
US5639219A (en) * | 1995-01-09 | 1997-06-17 | Campbell Hausfeld/Scott Fetzer Co. | Airless paint sprayer intake dampener and inlet valve spring |
US6116872A (en) * | 1997-02-04 | 2000-09-12 | Hitachi Construction Machinery Co., Ltd | Ripple reducing device |
US6412509B1 (en) * | 1999-10-08 | 2002-07-02 | UNIVERSITá DEGLI STUDI DI UDINE | Passive surge control method for compression systems and relative device |
US20040140149A1 (en) * | 2000-09-15 | 2004-07-22 | Terpay Gregory Weston | Passive device for noise reduction |
US20080271946A1 (en) * | 2005-02-21 | 2008-11-06 | Dayco Fluid Technologies S.P.A. | Pipe/Silencer Device Assembly |
US7896403B2 (en) * | 2005-02-21 | 2011-03-01 | Dayco Fluid Technologies S.P.A. | Pipe/silencer device assembly |
US20070193641A1 (en) * | 2005-12-22 | 2007-08-23 | John Dooley | Power steering system frequency suppressor |
US7296651B2 (en) | 2005-12-22 | 2007-11-20 | Eaton Corporation | Power steering system frequency suppressor |
US20070144598A1 (en) * | 2005-12-22 | 2007-06-28 | John Dooley | Power steering system frequency suppressor |
US7721765B2 (en) * | 2005-12-22 | 2010-05-25 | Eaton Corporation | Power steering system frequency suppressor |
US20100200097A1 (en) * | 2005-12-22 | 2010-08-12 | John Dooley | Power steering system frequency suppressor |
US7886771B2 (en) * | 2005-12-22 | 2011-02-15 | Eaton Corporation | Power steering system frequency suppressor |
US20120061165A1 (en) * | 2010-09-11 | 2012-03-15 | Ford Global Technologies, Llc | Reservoir-less power steering system |
US8701402B2 (en) * | 2010-09-11 | 2014-04-22 | Ford Global Technologies, Llc | Reservoir-less power steering system |
US20140076577A1 (en) * | 2011-03-29 | 2014-03-20 | Schlumberger Technology Corporation | System and method for reducing pressure fluctuations in an oilfield pumping system |
US20140245733A1 (en) * | 2013-03-01 | 2014-09-04 | Deere & Company | In-line parallel standpipe manifold |
WO2016112445A1 (en) * | 2015-01-13 | 2016-07-21 | Embraer S.A. | Fluid attenuators and methods, especially useful for aircraft hydraulic systems |
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