WO1998049487A1 - Energy attenuation apparatus and method for a system conveying pressurized liquid - Google Patents
Energy attenuation apparatus and method for a system conveying pressurized liquid Download PDFInfo
- Publication number
- WO1998049487A1 WO1998049487A1 PCT/US1998/008847 US9808847W WO9849487A1 WO 1998049487 A1 WO1998049487 A1 WO 1998049487A1 US 9808847 W US9808847 W US 9808847W WO 9849487 A1 WO9849487 A1 WO 9849487A1
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- WIPO (PCT)
- Prior art keywords
- conduit
- energy attenuation
- inlet
- attenuation apparatus
- outlet
- Prior art date
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Classifications
-
- 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
- F16L55/041—Devices damping pulsations or vibrations in fluids specially adapted for preventing vibrations
Definitions
- This invention relates to a new energy attenuation apparatus for a system conveying liquid under pressure and to a method of attenuating energy in such a system.
- the invention is particularly suitable for placement in a system conveying liquid under pressure for the attenuation of pressure pulsations in the liquid, especially in the hydraulic system of the power steering unit of a vehicle.
- the invention would also be suitable for other hydraulic fluids.
- This object is realized pursuant to one energy attenuation apparatus of the present invention by providing a tubular means having an inlet opening for receiving liquid from the system, and an outlet opening for returning the liquid to the system, wherein an inlet conduit extends concentrically into the tubular means through the inlet opening thereof, wherein an annular space is formed between the inlet conduit and the tubular means, and wherein in a portion of the inlet conduit disposed in the tubular means the inlet conduit is provided with at least one aperture for introducing liquid therefrom into the annular space.
- the aforementioned object is also realized pursuant to another energy attenuation apparatus of the present invention by providing housing means containing at least one chamber, an inlet conduit extending into said at least one chamber, wherein in a portion thereof disposed in said housing means said inlet conduit has at least one aperture for introducing liquid therefrom into said at least one chamber of said housing means, and an outlet conduit extending out of said at least one chamber wherein in a portion thereof disposed in said housing means said outlet conduit has at least one aperture for receiving liquid from said at least one chamber of said housing means.
- Another object of this invention is to provide a new method of attenuating energy in a system conveying liquid under pressure, the method of this invention having one or more of the novel features of this invention as set forth above or hereinafter shown or described.
- FIG. 1 illustrates a simplified automotive power steering system that incorporates one exemplary embodiment of the energy attenuation apparatus of this invention
- FIG. 2 shows a power steering system utilizing the inventive energy attenuation apparatus
- FIG. 3 illustrates one exemplary embodiment of the inventive energy attenuation apparatus in a specific pressure line or return line of an automotive power steering system
- FIG. 4 is a cross-sectional view of one exemplary embodiment of the energy attenuation apparatus of this invention.
- FIG. 5 is a view simitar to that of FIG. 4 of a second exemplary embodiment of the energy attenuation apparatus of this invention.
- FIG. 6 is a view similar to that of FIG. 4 of a third exemplary embodiment of an energy attenuation apparatus of this invention.
- FIG. 7 is a view similar to that of FIG. 4 of a further exemplary embodiment of an energy attenuation apparatus of this invention.
- FIG. 8 is a view similar to that of FIG. 4 of yet another exemplary embodiment of an energy attenuation apparatus of this invention
- FIG. 9 is a view similar to that of FIG. 4 of a further exemplary embodiment of an energy attenuation apparatus of this invention
- FIG. 10 is a view similar to that of FIG. 4 of another exemplary embodiment of an energy attenuation apparatus of this invention.
- FIG. 11 is a cross-sectional view of another exemplary embodiment of an energy attenuation apparatus of this invention
- FIG. 12 is a view similar to that of FIG. 11 of yet another exemplary embodiment of an energy attenuation apparatus of this invention
- FIG. 13 is a view similar to that of FIG. 11 showing a further exemplary embodiment of an energy attenuation apparatus of this invention
- FIG. 14 is a view similar to that of FIG. 11 showing another exemplary embodiment of an energy attenuation apparatus of this invention with a restrictor;
- FIG. 15 is a cross-sectional view of another exemplary embodiment of the energy attenuation apparatus of this invention.
- FIG. 16 is a view similar to that of FIG. 11 of yet another exemplary embodiment of an energy attenuation apparatus of this invention.
- FIG. 17 is a view similar to that of FIG. 11 showing a further exemplary embodiment of an energy attenuation apparatus of this invention
- FIG. 18 is a view similar to that of FIG. 11 showing a further exemplary embodiment of an energy attenuation apparatus of this invention
- FIG. 19 is a view similar to that of FIG. 11 showing another exemplary embodiment of an energy attenuation apparatus of this invention with a restrictor;
- FIGS. 20-22 show portions of inlet and/or outlet conduits that are provided with alternative configurations of apertures
- FIG. 23 illustrates a simplified automotive power steering system in which are disposed two energy attenuation apparatus of this invention
- FIGS. 24 and 25 show various embodiments of tuning cable arrangements for use in conjunction with the energy attenuation apparatus of this invention
- FIG. 26 illustrates one exemplary embodiment of the inventive energy attenuation apparatus of the present invention in conjunction with a further attenuation apparatus in a specific pressure line or return line of an automotive power steering system
- FIG. 27 is a partial block diagram showing one arrangement for use in conjunction with the present invention.
- FIG. 28 is a graph showing the improvement in pressure attenuation achieved with the energy attenuation apparatus of this invention.
- FIG. 1 illustrates a simplified automotive power steering system.
- the power steering pump 11 generates pressure ripples that are transmitted through tubing, such as steel tubing, to the pressure line 12, the power steering gear 13, the return line 14, and the reservoir 15, and finally flow back to the pump 11 itself by means of the supply line 16.
- tubing such as steel tubing
- the reservoir 15 and the pump 11 could actually be a single unit.
- the energy attenuation apparatus of this invention which is generally indicated by the reference numeral 20, is illustrated as being disposed in the pressure line 12 between the pump 11 and the gear 13.
- FIGS. 2-27 Various exemplary embodiments of the energy attenuation apparatus 20 and components and arrangements thereof are illustrated in FIGS. 2-27, and will be described in detail subsequently.
- the energy attenuation apparatus 20 that is shown disposed in the pressure line 12 in FIG. 1 is shown in greater detail in FIG. 4.
- the energy attenuation apparatus 20 comprises a canister or housing 21 that in the illustrated embodiment is a two-part housing made up of the parts 22 and 23 that are interconnected by the ring 24.
- a single chamber 25 is formed in the housing 21.
- the size and shape of the housing 21 can vary with the space available to accommodate same as well as with the existing requirements.
- a three-part housing could be used, including a central portion with identical caps or end portions on each side thereof.
- liquid enters the housing 21 for example from the pressure side of the pump 11 , by means of an inlet conduit 27, such as a tube or pipe.
- this inlet conduit 27 extends well into the chamber 25 of the housing 21.
- the inlet conduit 27 is provided with a plurality of apertures or holes 28 that allow the liquid to enter the chamber 25 from the conduit 27.
- the liquid From the chamber 25, which is also known as a mixing area or a flow control chamber, the liquid enters an outlet conduit 29 by means of a plurality of apertures or holes 30 formed therein.
- the inlet and outlet conduits 27 and 29 are sealingly disposed in the housing 21 in any convenient manner, as indicated schematically at the locations 31 and 32 respectively.
- the outlet conduit 29 is connected to the pressure line 12 so that the liquid, in this case power steering fluid, can be conveyed to the gear 13.
- FIG.4 provides for a single, hollow chamber into which a straight inlet conduit extends and from which a straight outlet conduit emerges
- FIGS. 5-19 wherein other housing and conduit configurations of this invention are shown and are generally indicated by the reference numerals 20A-20O, wherein parts thereof similar to the energy attenuation apparatus 20 of FIG. 4 are indicated by like reference numerals that where appropriate are followed by the reference letter A, B, C, D, E, F, G, H, I, J , K, L, M, N, or O.
- FIGS. 5 and 6 differ from that shown in FIG. 4 only in that the chamber 25 is partially filled with a flow control or filler means.
- the energy attenuation apparatus 20A of FIG. 5 shows a housing 21 having a chamber 25 that is partially filled with spherical filler means 34A.
- filler means 34A can be solid or hollow beads or balls made of steel, rubber, plastic, or any other suitable material, and help to increase the dissipation of energy.
- the filler means 34A, as well as the filler means to be discussed subsequently, should be made of a non-corrosive material and should be able to withstand temperatures up to 149° C (300° F).
- FIG. 6 illustrates an embodiment of an energy attenuation apparatus 20B wherein the housing 21 has a chamber 25 that is partially filled with irregularly shaped flow control or filler means 34B.
- the filler means 34B can be made of any suitable material, again solid or hollow, and could even comprise gravel. A sponge or foamlike filler means could also be used as long as it is compatible with operating parameters.
- FIG. 7 shows a housing 21 having chamber means that is not only partially filled with filler means 34C, such as steel balls, but is also subdivided into a plurality of chambers by baffle plates, as will be discussed in greater detail subsequently.
- FIGS. 8-10 illustrate how either one or both of the inlet and outlet conduits can be bent, rather than having the straight configuration of the previous embodiments.
- the outlet conduit 29D of the energy attenuation apparatus 20D is bent at right angles prior to exiting the housing 21.
- the inlet conduit 27E of the energy attenuation apparatus 20E of FIG. 9 is bent at right angles after having entered the chamber 25 of the housing 21.
- the chambers 25 of the energy attenuation apparatus 20D and 20E could also be provided with a flow control or filler means.
- both the inlet conduit 27F and the outlet conduit 29F are bent at right angles within the housing 21 although they could also extend linearly as in some of the previously described embodiments.
- the attenuation apparatus 20F also differs from the previously illustrated embodiments of FIGS. 4-6, 8 and 9 in that the housing 21 does not contain a single chamber, but rather is divided into two chambers 35 and 36. This division of the housing 21 into two chambers is effected by a further flow control means in the form of a baffle 37, which in the illustrated embodiment is disposed in the center of the housing 21.
- the baffle plate 37 is provided with a plurality of holes 38 in order to allow liquid to flow from the chamber 35 to the chamber 36.
- FIG. 7 illustrates a housing 21 that is provided with three such baffles 45, each of which is provided with a plurality of holes 46 in order to allow liquid to flow from the inlet conduit 27 to the outlet conduit 29 through the various chambers 47-50 into which the housing 21 is subdivided by the baffle plates 45.
- the inlet and outlet conduits 27, 29 are illustrated as extending far into the housing 21 , thus extending through two or even all three of the baffle plates 45. It will be understood that the inlet and outlet conduits 27, 29 need not extend so far into the housing 21 , and could, if desired, respectively extend through only a single one of the baffles 45.
- the inlet conduit 27 is illustrated as being provided with six holes, while the outlet conduit 29 is shown as being provided with eight holes 30, the number of holes as well as the dimensions and shapes thereof could vary, although it is presently provided that the inlet conduit 27 have a lesser number of holes or apertures than does the outlet conduit 29.
- the reverse arrangement would be theoretically possible, whereby the important feature is that the number of holes of the inlet and outlet conduits differ from one another.
- the number of holes, and the other parameters thereof, will vary as a function, for example, of the size of the pump as well as of the operating conditions.
- the holes can be provided on only one side of a given conduit, or on both sides thereof.
- the holes are showing as being aligned with one another in a longitudinal direction of the conduit, such holes could also be provided in a staggered or otherwise random configuration. It is expedient to have the holes of the inlet conduit angularly offset from those of the outlet conduit so that there is no direct flow between the conduits. If each conduit has only one row of holes, these rows could be offset by 180° relative to one another. If each conduit has two rows of holes, preferably disposed 90° apart, the rows of one of the conduits would be disposed so as to be 90° from the closest row of the other conduit.
- baffle 37 of the embodiment of the energy attenuation apparatus 20F shown in FIG. 10 is illustrated as extending in a transverse direction, a similar baffle plate could also be provided in the embodiments of FIGS. 4-6, 8 and 9, wherein such baffle plate would then be disposed in a longitudinal direction of the housing 21 between the inlet and the outlet conduits.
- inlet and outlet conduits need not necessarily have the same length within the housing 21.
- the diameters thereof need not be the same.
- the diameter or even the shape of the holes of the inlet and outlet conduits can differ from one another.
- the inlet and outlet conduits could be a single conduit.
- FIG. 11 wherein a single, continuous tube or conduit 52 of polymeric material, such as Teflon, is illustrated. Although a straight conduit 52 has been shown, other configurations are also possible.
- the embodiment of the energy attenuation apparatus 20G shown in FIG. 11 is also provided with apertures in the peripheral surface of the conduit.
- the apertures 53 are in the form of holes, with two holes that are 180° apart being shown.
- apertures 53 can have any other desired shape, such as an oval shape.
- One specific configuration of slanted oval apertures 53 is illustrated in the energy attenuation apparatus 20H of FIG. 12. A combination of the configurations illustrated in the apparatus of FIGS. 4-10 on the one hand and FIGS.
- 11 and 12 on the other hand is illustrated by way of example in the energy attenuation apparatus 20I of FIG. 13.
- two separate inlet and outlet conduits 27I, 29I are provided.
- these inlet and outlet conduits are aligned with one another and are separated from one another by a slight gap 54, for example a gap of approximately 0.79 to 3.18 mm (1/32 to 1/8 of an inch).
- the inlet conduit 27I is provided with apertures 28, while the outlet conduit 29I is provided with apertures 30.
- 11-14 can also be provided with any of the other features of the previously discussed embodiments, such as the flow control means or filler means 34, as well as one or more flow control means in the form of baffle plates.
- a restrictor means could be provided in one or more of the conduit means 27, 29 or 52.
- the energy attenuation apparatus 20J of FIG. 14 shows such a restrictor 55 disposed in the right hand portion of the conduit 52.
- Such a restrictor 55 could be provided at either end of the conduit 52, or at both ends, and could also be provided in one or both of the inlet and outlet conduits 27, 29 of some of the previously described embodiments.
- the passage 56 through the restrictor 55 has an inner diameter that is smaller than the inner diameter of the tube or conduit in which it is disposed.
- the passage 56 of the restrictor 55 could have a diameter of from 2.39 to 5.08 mm (0.094 to 0.20 inches).
- the embodiment of the energy attenuation apparatus 20K shown in FIG. 15 is also provided with apertures in the peripheral surface of the conduit.
- the apertures 53 are in the form of holes, with two holes that are 180° apart being shown approximately in the middle of the tube 52, although the holes 53 could also be disposed closer to one end, for example a third of the way from the inlet end.
- various numbers and arrangements of such apertures 53 are possible, and it would even be possible to provide only a single aperture since only a single conduit is present.
- the apertures 53 can have any other desired shape, such as an oval shape.
- the single conduit 52 is surrounded by a rubber hose 57, with a narrow annular space 51 of from 0.79 to 9.53 mm (1/32 to 3/8 of an inch) or longer being formed between the outer periphery of the conduit 52 and the inner periphery of the hose 57.
- the annular space 51 serves for receiving hydraulic fluid from the conduit 52 via the apertures 53 thereof; the liquid is again returned to the conduit 52 via the apertures 53.
- the hose 57 can also be made of polymeric material, or, as shown in the embodiment of the energy attenuation apparatus 20M of FIG. 17, can be made of metal.
- the tubular means 57 whether a hose or a casing, has a right-cylindrical cross-sectional configuration.
- conduit 52L In the embodiment of the energy attenuation apparatus 20L illustrated in FIG. 16, a single conduit 52L is again shown. However, in this embodiment the conduit 52L does not extend all the way from the inlet end to the outlet end of the hose 57M, but stops short of the outlet end; the conduit 52L can end 0.635 to 22.86 cm (0.25 to 9 inches) or more from the outlet end of the hose 57M, and in one exemplary embodiment of the present invention, for a conduit length of 27.94 cm (11 inches), ends 3.81 cm (1.5 inches) from the outlet end of the hose 57M.
- FIG. 15 A combination of the concepts illustrated in the apparatus of FIGS. 4-10 on the one hand and FIG. 15 on the other hand is illustrated by way of example in the energy attenuation apparatus 20N of FIG. 18.
- two separate inlet and outlet conduits 27N, 29N are provided.
- these inlet and outlet conduits are aligned with one another and are separated from one another by a slight gap 54, for example a gap of approximately 0.79 mm (1/32) (presently preferred) to 3.18 mm (1/8 of an inch), or even up to 2.54 cm (one inch) or more.
- the inlet conduit 27N is provided with apertures 28, while the outlet conduit 29N is provided with apertures 30.
- the embodiments of the energy attenuation apparatus of FIGS. 15-18 can also be provided with any of the other features of the previously discussed embodiments, such as the flow control means or filler means 34, as well as one or more flow control means in the form of baffle plates.
- a restrictor means could be provided in one or more of the conduit means 27, 29 or 52.
- the energy attenuation apparatus 20O of FIG. 19 shows such a restrictor 55 disposed in the central portion of the conduit 52.
- Such a restrictor 55 could be provided at either end of the conduit 52, or at both ends, and could also be provided in one or both of the inlet and outlet conduits 27, 29 of some of the previously described embodiments. It is to be understood that the passage 56 through the restrictor 55 has an inner diameter that is smaller than the inner diameter of the tube or conduit in which it is disposed. For example, the passage 56 of the restrictor 55 could have a diameter of from 0.91 to 0.25 cm (0.36 to 0.10 of an inch).
- FIGS. 20-22 show some other shapes for the holes in the inlet and outlet conduits.
- the inlet and/or outlet conduit 40 illustrated in FIG. 20 is provided with oval apertures 41.
- the inlet and/or outlet conduit 42 of FIG. 21 is provided with triangular apertures 43.
- the inlet and/or outlet conduit 44 of FIG. 22 is provided with rectangular apertures 45.
- inlet and outlet conduits are shown as having closed ends within the chamber or chambers of the housing 21 or hose 57, the ends of the inlet and/or outlet conduits can also be opened, or could also be provided with holes.
- FIG. 1 as being disposed between the pump 11 and the gear 13, it is believed that such an attenuation apparatus could alternatively be disposed between the gear 13 and the reservoir 15 in the return line 14 in order to reduce vibration caused by the power steering gear 13.
- two attenuation apparatus could be provided.
- FIG. 23 shows a system having two energy attenuation apparatus 20, one in the pressure line 12 to a control valve 17 (similar to the gear 13 of FIG. 1 ), and another in the return line 14.
- FIG. 3 illustrates an exemplary embodiment of an actual pressure or return line (bent to accommodate space requirements) in which is disposed an inventive energy attenuation apparatus 20, which in this embodiment is provided with an optional venting means 43.
- the inventive energy attenuation apparatus can also be used in conjunction with a variety of other sound and vibration attenuation apparatus, which are then also disposed in the pressure line 12 and/or the return line 14.
- a 1/4 wave cable tuning assembly can be provided, for example by disposing a steel cable in a separate hose section. Examples of such tuning cable arrangements in hose sections are shown in FIGS. 24 and 25, wherein FIG. 24 shows a single tuning cable 59 disposed in the hose section or conduit means 60, whereas FIG. 25 shows two separate tuning cables 59 disposed in a hose section or conduit means 60.
- the tuning cable or cables are made of polymeric material, such as Teflon, they can also be provided with apertures in the peripheral surface thereof.
- FIG. 27 shows an arrangement where the tubing T is split into branches 62, each of which leads to an energy attenuation apparatus that is schematically indicated by one of the boxes 63 or 64.
- This parallel arrangement can either be disposed in series with one of the inventive attenuation apparatus 20-200, or one of the boxes 63, 64 can contain an inventive energy attenuation apparatus while the other box contains a known attenuation device. Furthermore, both boxes 63 and 64 can contain the same or different ones of the inventive energy attenuation apparatus. It should also be noted that two or more of the inventive energy attenuation apparatus could be disposed in series and/or in parallel with one another. For example, in the exemplary embodiment illustrated in FIG. 3, the portion shown as a hose section can be one or more of the embodiments illustrated in FIGS. 15-19. In addition although FIG. 3 shows a canister- type energy attenuation apparatus 20, this could be replaced by another one of the embodiments of FIGS.
- the housing 21 and the inlet and outlet conduits 27, 29 were made of stainless steel.
- the housing 21 had an approximately cylindrical shape, and in a small embodiment thereof had a length of approximately 85 mm, a diameter of approximately 50.1 mm, and a thickness of approximately 1 mm.
- the stainless steel inlet and outlet conduits 27, 29 had an inner diameter of approximately 9.5 mm (3/8 of an inch) and a thickness of approximately 1 mm.
- the diameter of the holes in the inlet and outlet conduits 27, 29 was approximately 3.89 mm.
- the ratio of the diameter of the housing means to the diameter of the conduit should be at least 2:1 , and could be as much as 10.7:1 or even greater.
- a large volume can also be achieved for the narrow hose or casing embodiments by providing for a very long hose or casing, for example one having a length of several feet, such as even 2.2 meters (seven feet) or longer if sufficient space is available.
- the hose 57 had a length of approximately 12.7 to 101.6 cm (5 to 40 inches) or greater and a diameter of 0.95 to 1.59 cm (3/8 to 5/8 of an inch) or greater.
- the diameter of the conduit 52 was 0.95 cm (3/8 of an inch) or less.
- the housing means 21 had a length of 15.24 cm (6 inches), a diameter of approximately 5.08 cm (2 inches), and a thickness of approximately 1 mm.
- the conduit 52 had a diameter of approximately 0.95 cm (3/8 inch), so that the ratio of the diameter of the housing means 21 to the diameter of the conduit 52 was approximately 5.33:1.
- the conduit 52 had a diameter of 1.27 cm ( 1 of an inch), whereby the ratio of the diameter of the housing 21 to the diameter of the conduit means 52 was 4:1.
- the housing 21 had a length of approximately 6.35 cm (2.5 inches) (note that the housing 21 can have a length of 25.4 cm (10 inches) or greater) and a diameter of 5.08 cm (2 inches).
- the diameter of the conduit 52 was 0.95 cm (3/8 of an inch), while the passage 56 of the restrictor 55 had a diameter of 2.87 mm (0.113 of an inch).
- FIG. 28 This phenomenon, along with the significant improvement provided by the inventive energy attenuation apparatus, is shown in FIG. 28, wherein pressure is plotted against the harmonics order of a given pump, with this pump generating ten pulses per revolution thereof. These 10 pulses are considered as the 10th order with the following harmonics being 20th, 30th, etc.
- This graph which was plotted for the system of FIG. 1 , namely the embodiment of the energy attenuation apparatus 20 of FIG. 4, was effected at a system pressure of 900 psi and a pump speed of 1200 RPM.
- this invention not only provides a new energy attenuation apparatus, but also this invention provides a new method for attenuating sound or energy in a liquid conveying system.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
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- Jet Pumps And Other Pumps (AREA)
- Rotary Pumps (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
Description
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Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP54743498A JP2001522442A (en) | 1997-04-30 | 1998-04-27 | Energy attenuation device and method for pressurized liquid transport system |
KR1019997009969A KR100559684B1 (en) | 1997-04-30 | 1998-04-27 | Energy attenuation apparatus and method for a system conveying pressurized liquid |
CA002287865A CA2287865C (en) | 1997-04-30 | 1998-04-27 | Energy attenuation apparatus and method for a system conveying pressurized liquid |
BR9809424-6A BR9809424A (en) | 1997-04-30 | 1998-04-27 | Apparatus and method of energy attenuation for a pressurized liquid transport system. |
AU71734/98A AU745077B2 (en) | 1997-04-30 | 1998-04-27 | Energy attenuation apparatus and method for a system conveying pressurized liquid |
EP98918903A EP0979371A4 (en) | 1997-04-30 | 1998-04-27 | Energy attenuation apparatus and method for a system conveying pressurized liquid |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/846,912 US6085792A (en) | 1997-04-30 | 1997-04-30 | Energy attenuation apparatus for a system conveying liquid under pressure and method of attenuating energy in such a system |
US08/846,912 | 1997-04-30 |
Publications (1)
Publication Number | Publication Date |
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WO1998049487A1 true WO1998049487A1 (en) | 1998-11-05 |
Family
ID=25299291
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1998/008847 WO1998049487A1 (en) | 1997-04-30 | 1998-04-27 | Energy attenuation apparatus and method for a system conveying pressurized liquid |
Country Status (9)
Country | Link |
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US (4) | US6085792A (en) |
EP (1) | EP0979371A4 (en) |
JP (1) | JP2001522442A (en) |
KR (1) | KR100559684B1 (en) |
AR (1) | AR015618A1 (en) |
AU (1) | AU745077B2 (en) |
BR (1) | BR9809424A (en) |
CA (1) | CA2287865C (en) |
WO (1) | WO1998049487A1 (en) |
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EP1309814A1 (en) * | 2000-08-15 | 2003-05-14 | Dayco Products, Llc. | Energy attenuation apparatus for a system conveying liquid under pressure and method of attenuating energy |
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US6269841B1 (en) * | 1997-04-30 | 2001-08-07 | Dayco Products Llc | Energy attenuation apparatus for a system conveying liquid under pressure and method of attenuating energy in such a system |
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DE19848379A1 (en) * | 1998-10-21 | 2000-05-04 | Vickers Aeroquip Int Gmbh | Arrangement for damping a pulsation of a fluid conveyed by a conveying device |
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US6591870B1 (en) * | 2002-03-22 | 2003-07-15 | Dayco Products, Llc | Energy attenuation restrictor device and method of forming such restrictor device |
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US7325570B1 (en) | 2004-12-06 | 2008-02-05 | Coupled Products, Llc | Method and apparatus for noise suppression in a fluid line |
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EP1309814A4 (en) * | 2000-08-15 | 2006-08-16 | Dayco Products Llc | Energy attenuation apparatus for a system conveying liquid under pressure and method of attenuating energy |
Also Published As
Publication number | Publication date |
---|---|
CA2287865A1 (en) | 1998-11-05 |
EP0979371A1 (en) | 2000-02-16 |
KR20010020350A (en) | 2001-03-15 |
AR015618A1 (en) | 2001-05-16 |
US6089273A (en) | 2000-07-18 |
KR100559684B1 (en) | 2006-03-10 |
US6085792A (en) | 2000-07-11 |
US6123108A (en) | 2000-09-26 |
US5983946A (en) | 1999-11-16 |
JP2001522442A (en) | 2001-11-13 |
BR9809424A (en) | 2000-06-13 |
AU7173498A (en) | 1998-11-24 |
EP0979371A4 (en) | 2007-10-17 |
AU745077B2 (en) | 2002-03-14 |
CA2287865C (en) | 2006-01-10 |
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