WO2011069241A1 - Système de compression de fluide - Google Patents

Système de compression de fluide Download PDF

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Publication number
WO2011069241A1
WO2011069241A1 PCT/CA2010/001910 CA2010001910W WO2011069241A1 WO 2011069241 A1 WO2011069241 A1 WO 2011069241A1 CA 2010001910 W CA2010001910 W CA 2010001910W WO 2011069241 A1 WO2011069241 A1 WO 2011069241A1
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WO
WIPO (PCT)
Prior art keywords
piston
chamber
fluid
compression
piston portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/CA2010/001910
Other languages
English (en)
Inventor
Régis FORTIN
André EMOND
Michel Bisson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
STC Footwear Inc
Original Assignee
STC Footwear Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by STC Footwear Inc filed Critical STC Footwear Inc
Priority to US13/060,878 priority Critical patent/US9175676B2/en
Priority to CA2732482A priority patent/CA2732482C/fr
Publication of WO2011069241A1 publication Critical patent/WO2011069241A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B25/00—Multi-stage pumps
    • F04B25/02—Multi-stage pumps of stepped piston type
    • A—HUMAN NECESSITIES
    • A43—FOOTWEAR
    • A43B—CHARACTERISTIC FEATURES OF FOOTWEAR; PARTS OF FOOTWEAR
    • A43B13/00—Soles; Sole-and-heel integral units
    • A43B13/14—Soles; Sole-and-heel integral units characterised by the constructive form
    • A43B13/18—Resilient soles
    • A43B13/20—Pneumatic soles filled with a compressible fluid, e.g. air, gas
    • A43B13/203—Pneumatic soles filled with a compressible fluid, e.g. air, gas provided with a pump or valve
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B9/00—Piston machines or pumps characterised by the driving or driven means to or from their working members
    • F04B9/14—Pumps characterised by muscle-power operation

Definitions

  • the technical field relates generally to converting mechanical energy to fluid energy, and more particularly to fluid compression systems and fluid pumps.
  • Different energy conversion systems exist for converting mechanical energy to fluid energy, i.e. fluid pressure.
  • a fluid compression system such as a pump, whereby a force is applied on an enclosed fluid, thereby raising the pressure of the fluid.
  • An example of this type of pump is a common bicycle pump, such as used to inflate tires.
  • Another example is a piston and cylinder system, whereby mechanical work is done by the piston on the fluid inside the cylinder, thereby compressing or raising the pressure of this fluid. This system is commonly used in internal combustion engines.
  • Bicycle pumps may also require a large stroke length, as in piston and cylinder systems.
  • a fluid compression system for pressurizing a fluid
  • the fluid compression system comprising a compression surface having a variably-sized surface area, a housing, the housing and the compressor surface enclosing a fluid volume therebetween, the compression surface being movable over a length of the housing, the fluid volume being compressed as the compression surface is moved towards an end of the housing, the surface area of the compression surface being at least two different sizes as the compression surface is moved in the housing, the compression surface having a smaller surface area and pumping a smaller volume of fluid towards the end of the compression stroke.
  • a fluid pump comprising a chamber containing a fluid, the chamber having a fluid inlet and a fluid outlet, a compression member having a compression surface with an effective surface area movable against fluid pressure in the chamber, the compression member having a compression stroke and a return stroke, the effective surface area of the compression member decreasing in size together with a corresponding cross- sectional area of the chamber from a maximal area at a beginning of the compression stroke to a minimal area at the end of the compression stroke.
  • a method for imparting pressure to a fluid by direct displacement of a compression member in a chamber containing a fluid the chamber having a fluid inlet and a fluid outlet, the compression member having a compression surface on which the fluid in the chamber exerts a pressure, the compression surface of the compression member having a variable effective surface area
  • the method comprising: reducing the effective surface area of the compression member and a corresponding cross- sectional area of the chamber along a compression stroke of the compression member in the chamber, the effective surface area of the compression member and the cross- sectional area of the chamber being smaller towards the end of the compression stroke than at a beginning of the compression stroke.
  • a fluid compression system comprising a piston mounted for reciprocable movement in a pressure chamber adapted to contain a fluid, the piston having a compression stroke and a return stroke, wherein an effective area of the piston on which the fluid exert a pressure on the compression stroke decreases from a maximal effective area at a beginning of the compression stroke to a minimal effective area at the end of the compression stroke.
  • a fluid compression system comprising a pressure chamber and a piston mounted for reciprocable movement in the pressure chamber, the pressure chamber and the piston having a variable effective area for pressuring the fluid, the variable effective area becoming smaller as the piston proceed towards the end of its compression stoke.
  • a non-linear gas pump comprising at least three concentric pistons disposed radially one inside the other, a hollow intermediately-sized piston circumscribing in abutment an inner radial piston and a hollow outer radial piston circumscribing in abutment the intermediately-sized piston, securing means on the pistons such that the three concentric pistons remain integral, a force-conveying member being in contact with the inner radial piston, a housing having at least three cylinders consecutively longitudinally spaced one from the other, with a first cylinder of a volume substantially similar to that of the outer radial piston, a second cylinder spaced longitudinally from the first cylinder and of a volume substantially similar to that of the intermediately-sized piston and a third cylinder spaced longitudinally from the second cylinder and of a volume substantially similar to that of the inner radial piston, the third cylinder being connected to a conduit for allowing fluid passage therethrough, the volume of the
  • a device for recovering and converting mechanical energy into fluid energy comprising a force transmitting member adapted to be connected to a source of mechanical energy, a piston connected to the force transmitting member and movable thereby, the piston being mounted for movement in a pressure chamber containing a fluid, the piston and the pressure chamber having an effective area on which the fluid exert a pressure, the effective area of the piston and the chamber varying along a movement axis of the piston in the chamber, the effective area becoming smaller as the piston travels towards an end of a compression stroke thereof, thereby proving for the pumping of a smaller volume of fluid at the end of the compression stroke than at a beginning thereof, and a tank connected in fluid flow communication with the pressure chamber for receiving the fluid compressed by the piston.
  • Figure 1 is a perspective view of a cross-section of one particular
  • Figures 2a, 2b, 2c and 2d are cross-sectional sequential schematic views illustrating four positions in the compression stroke of one embodiment of the fluid compression system.
  • Figure 3 is an enlarged view of the fluid compression system shown in Fig. 1 illustrating the details of the attachment means used to detachably interconnect the piston sections of the fluid compression system.
  • Figure 4 shows an alternative embodiment of a locking system that can be used to detachably interconnect the piston sections of the fluid compression system.
  • Figures 5a to 5d are schematic views illustrating a further alternative to the attachment means or locking system illustrated in Figs. 3 and 4.
  • Figures 6a, 6b and 6c are schematic views illustrating three positions in the compression stroke of an alternative embodiment of the fluid compression system illustrated in Figure 1.
  • Figures 7a, 7b and 7c are schematic views illustrating three positions in the compression stroke of an embodiment of a bladder-type fluid compression system.
  • Figures 8a, 8b and 8c are schematic views illustrating three positions in the compression stroke of an alternative embodiment of the bladder-type fluid compression system shown in Figures 7a, 7b and 7c.
  • Figure 9 illustrates one possible application in which the fluid compression system can be used for retrieving mechanical energy and converting it into fluid energy.
  • Figures 10a and 1 Ob are schematic views illustrating two positions in the compression stroke of a further alternative embodiment of the bladder-type fluid compression system.
  • the compression surface compresses a fluid volume using a variably-sized surface area in order to obtain a rapid gain of fluid pressure even for applications in which the piston is actuated at relatively low frequencies and under the action of relatively small forces.
  • the compression surface using a first surface area Al , will compress a fluid volume.
  • the compression surface using a surface area A2
  • the surfaces areas Al and A2 may not be equal, i.e. may be different.
  • the compression surface has a variable surface area, wherein the surface area of the compression surface may change as the fluid is being compressed.
  • the fluid compression system 10 may generally comprise a compression member, such as a piston 12, mounted for movement in a housing 20 defining a pressure chamber 22, and a force-conveying member 32 for transmitting a driving force to the piston 12.
  • the housing 20 includes a cover 20a which may be bolted or otherwise secured to a base 20b.
  • a gasket 21 is provided at the joint between the base 20b and the cover 20a.
  • the force-conveying member 32 extends axially through the cover 20a from a piston-rod surface 13a of the piston 12 (the top surface of the piston in Fig. 1) opposite to an effective fluid compression surface 13b thereof (the bottom surface of the piston in Fig. 1).
  • the fluid compression surface 13b of the piston 12 and the housing chamber 22 defines a variable fluid volume.
  • the effective area of the piston compression surface 13b on which the fluid exerts a pressure varies during the compression stroke of the piston 12.
  • the housing chamber 22 comprises a plurality (three in the illustrated embodiment) of axially serially interconnected chamber portions, which may include a large chamber portion 24, an intermediate chamber portion 26 and a small chamber portion 28.
  • the large chamber portion 24 is firstly positioned inside the housing chamber 22, followed by the intermediate chamber portion 26 which begins and extends past where the large chamber portion 24 ends, which itself is followed by the small chamber portion 28 which begins and extends past where the intermediate chamber portion 26 ends.
  • the piston 12 is located inside the large chamber portion 24.
  • a first annular shoulder 29 is defined at the interface between the large chamber portion 24 and the intermediate chamber portion 26.
  • a second annular shoulder 31 is defined at the interface between the intermediate chamber portion 26 and the small chamber portion 28.
  • the piston 12 comprises a corresponding number (three in the illustrated example) of releasably interconnected concentric piston portions, including an outer annular hollow piston portion 14 which circumscribes an intermediate annular hollow piston portion 16 which itself circumscribes an inner piston portion 18.
  • These piston portions 14, 16 and 18 are releasably integral (i.e. detachably interconnected) through the use of attachment means 30 located therebetween.
  • the compression surface 13b is defined by the surface areas of the bottom surfaces of the three piston portions 14, 16, 18.
  • the outer piston portion 14 is substantially sized so as to fit in the large chamber portion 24 and for sealing engagement with an O-ring 33 mounted in a circumferential groove defined in the inner surface of the large chamber portion 24.
  • the intermediate piston portion 16 is substantially sized so as to tightly fit in the intermediate chamber portion 26 and the inner piston portion 18 is substantially sized so as to tightly fit in the small chamber portion 28.
  • the force-conveying member 32 is connected, such as by threads, to the inner piston portion 18, and is used to transmit a force directly to the inner piston portion 18. As will be seen hereinafter, the force is then transmitted from inner piston portion 18 to the intermediate piston portion 16 and the outer piston portion 14 via the attachment means 30 until the piston portions separate from one another.
  • the piston 12 comprises three piston portions, in another embodiment, the piston may comprise any number of a plurality of piston portions, for example, 2, 3, 4 or more piston portions.
  • the force-conveying member 32 may be attached to an underside portion of inner piston portion 18, so as to pull on inner piston portion 18, as opposed to applying a downwards force on it.
  • a fluid intake 36 and a compressed fluid exhaust 34 Near the bottom of the small chamber portion 28 is a fluid intake 36 and a compressed fluid exhaust 34.
  • the fluid compression system 10 Once the fluid compression system 10 has compressed the fluid volume defined by the housing chamber 22, the fluid will exhaust from the housing chamber 22 through the exhaust 34. Once the compressed fluid has been exhausted from the housing chamber 22, fresh fluid will be admitted to the housing chamber 22 through the fluid intake 36.
  • one-way valves 39 and 41 are respectively provided at the fluid exhaust 34 and at the fluid intake 36 to prevent reverse fluid flow therethrough.
  • the valves 39 and 40 are set to open at the predetermined pressures.
  • the fluid compression system 10 additionally comprises o- rings 37a and 37b, which are mounted on shoulders 29 and 31 to minimize any fluid escaping from the intermediate chamber portion 26 to the large chamber portion 24 and from the small chamber portion 28 to the intermediate chamber portion 26, respectively.
  • Additional o-rings 37c and 37d are respectively mounted on the radially inner surface of the intermediate piston portion 16 and the radially inner surface of the outer piston portion 14 to respectively prevent fluid leakage between the intermediate piston portion 16 and the inner piston portion 18 and between the outer piston portion 14 and the intermediate piston portion 16.
  • the piston portions 14, 16, 18 and the housing chamber portions 24, 26, 28 may be of a different shape, i.e. be elliptical, rectangular, triangular, etc.
  • the three piston portions of the piston 12 have entered the housing chamber 22 and are located at the bottom end of the large chamber portion 24 with the outer piston portion 14 resting axially against annular shoulder 29.
  • the piston 12 has compressed the fluid volume by an amount equal to the size of the large chamber portion 24, using a compression surface 13b equal to the bottom surface areas of the three piston portions 14, 16, 18.
  • the piston 12 has further compressed the fluid volume by an amount equal to the size of the intermediate chamber portion 26, but in this step, the piston 12 has done so with a smaller compression surface 13b equal to the bottom surfaces of the intermediate and inner piston portions 16, 18.
  • the engagement of the intermediate piston portion 16 with the shoulder 31 prevents the intermediate piston portion 16 from moving further into the housing chamber 22 beyond the intermediate chamber portion 26.
  • the continued pushing action of the force-conveying member 32 on the inner piston portion 18 automatically causes the attachment means 30 to release the intermediate piston portion 16 from the inner piston portion 18, thereby allowing the inner piston portion 18 to continue its stroke to the fourth position illustrated in Fig. 2d.
  • the inner piston portion 18 has entered and is located at or substantially near the bottom end of the small chamber portion 28.
  • the piston 12 has further compressed the fluid volume by an amount substantially equal to the size of the small chamber portion 28, but in this step, the compression is done with a compression surface 13b equal to the bottom surface of the inner piston portion 18.
  • the compressed fluid volume is then exhausted through the exhaust 34 where it can be stocked in a tank before being used in a given application.
  • the one-way valve prevents the compressed fluid from flowing back into chamber 22 during the return stoke of the piston 12.
  • the compressed fluid volume may begin to be exhausted through the exhaust 34, prior to the inner piston portion reaching the end of the small chamber portion 28.
  • the intake 36 may begin to admit fresh fluid into the housing chamber 22 and the piston portions 14, 16, 18 may be returned to the initial position, as seen in figure 1 , where the piston portions 14, 16, 18 are integral one with another.
  • the fluid compression system 10 is therefore reciprocable.
  • the fluid compression system 10 comprises a return stroke, whereby the piston portions 14, 16, 18 may, from the position shown in Figure 4, return to the initial position, as seen in Figure 1.
  • This return stroke may be caused by a biasing member (not shown), such as a spring, which is attached to the force conveying member 32, and which causes the force conveying member to return to the initial position as seen in Figure 1 , when the fluid volume has been compressed and exhausted through the compressed fluid exhaust 34, as seen in Figure 4.
  • a biasing member such as a spring
  • piston portions 14, 16, 18 also return to their initial position, as seen in Figure 1, where they are once again maintained integral by the attachment means 30.
  • the piston portions 14 and 16 may reconnect with the inner piston portion 18 due to the inner piston portion 18 which abuts and so raises inner shoulders 47 and 49, which are respectively provided on the outer and intermediate piston portions 14 and 16.
  • the inner shoulders 47 and 49 respectively provide arresting surfaces for the inner and intermediate piston portions 18 and 16 during the return stroke of the piston 12.
  • the piston portions 14, 16, 18 may also be returned to the initial position by the action of the fluid which is admitted into the housing chamber 22 through the fluid intake 36. When the compressed fluid volume has been exhausted from the housing chamber 22, as seen in Figure 4, the fluid which enters through the fluid intake 36 may also serve to raise the piston portions 14, 16, 18.
  • the fluid compression system 10 presents many advantages.
  • the fluid compression system may attain high compression ratios, in a short span of time or in a short length of displacement of the piston, as compared to typical piston and cylinder systems, where the cylinder has only one diameter throughout its length and is relatively long.
  • the chamber initially has a diameter defined by the large chamber portion 24 and subsequently, has smaller diameters as exemplified by the diameters of the intermediate and small chamber portions 26, 28 respectively.
  • the fluid volume inside the housing chamber is at a relatively low pressure, and the pressure of the fluid volume may quickly rise as the fluid volume is compressed by a large compression surface area, i.e. the surface areas of all three piston portions 14, 16, 18.
  • the pressure of the fluid volume inside the housing chamber will be greater, and in order to maintain a sustained rate of compression, the fluid volume may be compressed with a smaller compression surface area, i.e. the surface areas of the intermediate and inner piston portions 16, 18 and then afterwards, with only the surface area of the inner piston portion 18. Because of the relationship between pressure and area and due to the compression surface having a variable surface area, the fluid compression system may be used to obtain higher compression ratios than in typical piston and cylinder systems.
  • the force-conveying member 32 is only connected to the inner piston portion 18, so a force is only directly transmitted to inner piston portion 18.
  • the compression surface 13 becomes smaller, no force is applied to the larger piston portions, as only the smaller piston portions are actually compressing the fluid volume.
  • the outer piston portion 14 has reached the bottom end of the large chamber portion 24, a force is no longer indirectly transmitted to the outer piston portion 14, the force is solely applied to the inner piston portion 18, and because the inner piston portion 18 is held integral with intermediate piston portion 16, the intermediate and inner piston portions 16, 18 translate through intermediate chamber portion 26.
  • the intermediate and inner piston portions 16, 18 thereby compress the fluid volume located inside the housing chamber 22 using the compression surface 13, defined by the bottom surface areas of said piston portions 16, 18. No force is thereby wasted by being transmitted to piston portions which are not currently compressing the fluid volume. This means that whatever force is applied on the inner piston portion 18 will always serve to pressure the compression surface 13 into compressing the fluid volume, regardless of the housing chamber portion in which the piston portions are currently compressing the fluid volume.
  • a constant force is applied on the inner piston portion 18, through the force-conveying member 32. It is to be noted that in another embodiment, a force may be applied independently to all three piston portions 14, 16, 18 or simultaneously to all three. In other embodiments, the force-conveying member 32 may be of a different shape than that shown in Figure 1 and should not be limited in scope to this particular form.
  • the fluid compression system 10 may also comprise a compressed fluid accumulation tank (not shown) which is located at the end of the compressed fluid exhaust 34.
  • the accumulation tank serves to retain or hold the compressed fluid volume which is exhausted from the housing chamber 22 and is directed to the accumulation tank through the compressed fluid exhaust 34.
  • the valve 39 permits and controls passage of the compressed fluid volume through the compressed fluid exhaust 34 and into the accumulation tank.
  • the valve is a oneway valve or check valve.
  • the valve may be another type of valve, such as a pressure regulated valve.
  • the valve only allows the compressed fluid volume to pass through the compressed fluid exhaust 34 and so into the accumulation tank, when the pressure of the compressed fluid volume located inside the housing chamber 22 is greater than the pressure of the fluid located inside the accumulation tank.
  • the piston portions 14, 16, 18 are held releasably integral through the use of a releasable connecting/locking mechanism or attachment means 30 located therebetween.
  • Different connector or attachment means 30 may be used to maintain the piston portions 14, 16, 18 releasably integral.
  • the type of attachment means 30 shown in the embodiment of Figure 1 is shown in greater detail in Figure 3.
  • the attachment means 30 may comprise at least two of locking pins 38 which are located inside the outer and intermediate piston portions 14, 16, respectively, and which extend radially, from an inner radial end to an outer radial end therein.
  • the outer and intermediate piston portions 14, 16 each have at least one locking pin 38 located therein.
  • the outer and intermediate piston portions 14, 16 each have three locking pins 38 located therein, which are spaced equally apart circumferentially.
  • Inner balls 40a are located at the inner radial ends of the locking pins 38 and outer balls 40b are located at the outer radial ends of the locking pins 38.
  • the intermediate and inner piston portions 16, 18 each have a circumferential groove 44 located on an outer radial portion thereof, in proximity to the compression surface 13. As seen in Figure 3, when the intermediate and inner piston portions 16, 18 are integral, the inner balls 40a at the inner radial end of the intermediate piston portion 16 are located in a portion of the circumferential groove 44 located on the outer radial portion of the inner piston portion 18.
  • the inner balls 40a at the inner radial end of the outer piston portion 14 are located in a portion of the circumferential groove 44 located on the outer radial portion of the intermediate piston portion 16. Therefore, when a force is applied to the inner piston portion 18, the inner piston portion 18 will move integrally with the outer and intermediate piston portions 14, 16, because the balls 40 located at the inner radial ends of the locking pins 38 between the piston portions 14, 16, 18, will maintain the piston portions integral. It is to be noted that in other embodiments, where more or less piston portions are used, the fluid compression system 10 may require a relatively greater or lesser amount of locking pins.
  • annular grooves 42 are provided in an inner surface of the housing chamber 22 near the ends of the large and intermediate chamber portions 24, 26.
  • the outer balls 40b which are the most outer radially positioned are located substantially inside the respective piston portions 14, 16 and roll or slide on the inner surface of the housing chamber 22.
  • the balls 40b located inside the outer piston portion 14 reach the annular groove 42 in the wall of the large chamber portion 24, the balls 40b protrude from the outer piston portion 14 into the circumferential groove 42, thereby allowing the locking pins 38 to move radially outwardly.
  • intermediate piston portion 16 and the inner balls 40a will cause the inner balls 40a to move radially outside of the groove 44, thereby disconnecting the outer piston portion 14 from the intermediate piston portion 16 and, thus, the inner piston portion 18.
  • the intermediate and inner piston portions 16, 18 then continue displacing into the intermediate chamber portion 26 and the inner balls 40a of the outer piston portion 14 will ride on the radially outer surface of the intermediate piston portion 16 outside of the groove 44 defined therein.
  • a similar procedure occurs when the intermediate and inner piston portions 16, 18 are moving integrally in the
  • annular groove 42 and the circumferential groove 44 are each described as being annular and circumferential, respectively, in another embodiment, the grooves 42, 44 may simply be depressions, holes or grooves of another shape, and need not be completely circumferential.
  • intermediate piston portion 16 may reconnect with the outer piston portion 14, through this same attachment means 30.
  • the inner piston portion 18 moves upwards in the small chamber portion 28, no balls are located inside the circumferential groove 44 therein. Once the inner piston portion 18 exits the small chamber portion 28, the inner piston portion 18 will abut the inner shoulder 49 of the intermediate piston portion 16, and so the intermediate and inner piston portions 16, 18 may move inside the intermediate chamber portion 26.
  • the outer balls 40b protruding into the annular groove 42 of the wall of the intermediate chamber portion 26 will be pushed into the intermediate piston portion 16 by the wall of the chamber housing 22.
  • the outer balls 40b will then press against the locking pin 38, and the locking pin 38 will press against the inner balls 40a, such that the inner balls 40a located inside the intermediate piston portion 16 will protrude into the circumferential groove 44 of the inner piston portion 18.
  • the intermediate and inner piston portions 16, 18 will then integrally move upwards inside the intermediate chamber portion 26 during the return stroke. A similar procedure occurs with the outer piston portion 14, when the intermediate and inner piston portions 16, 18 integrally exit the intermediate chamber portion 26 and enter the large chamber portion 24.
  • the attachment means 30 may comprise a circumferential groove 50 defined in an inner radial surface of the outer and intermediate piston portions 14, 16, and seats or cavities 52 defined in an outer radial surface of the intermediate and inner (not shown) piston portions 16, 18.
  • At least one spring 46 is located in each of the cavities 52, the springs 46 are for normally biasing a ball 48 in engagement inside an associated one of the grooves 50.
  • the balls 48 are biased by the spring 46 into abutment with the
  • piston portion will therefore stop moving integrally with the other piston portions, and the ball 48 will roll or slide along the inner surface of the housing chamber 22, as the piston portion in which it is located continues its movement.
  • other attachment means may be used to maintain the piston portions releasably integral, such as a releasable lock or various fasteners, such as a bolt or a clip, for example.
  • FIG. 5a, 5b, 5c and 5d Another alternative embodiment of the attachment means 30 is shown in Figures 5a, 5b, 5c and 5d.
  • a force-conveying member 232 has a helical form and rotates 180 degrees over every displacement L.
  • An upper plate 270 is located above the outer piston portion 14 and is attached thereon, and a lower plate 272 is located above the intermediate piston portion 16 and is attached thereon.
  • the force-conveying member 232 has a locking member 274 which extends outer radially from the force-conveying member 232 and which is located near a bottom thereof.
  • the upper plate 270 as seen in the top view of the upper plate of Figure 5a, has a rectangular opening 276 therein and the lower plate 272, as seen in the top view of the lower plate 272 in Figure 5c, has a rectangular opening 278 therein.
  • the locking member 274 In the initial position, as seen in Figure 5a, the locking member 274 is aligned 180 degrees opposite to the rectangular opening 276. As the force-conveying member 232 begins moving inner piston 18 into the housing chamber 22, the locking member 274 pushes on the upper plate 270, which pushes on the lower plate 272, and so the three piston portions 14, 16, 18 displace integrally into the housing chamber 22.
  • the locking member 274 is aligned with the rectangular opening 276, as seen in Figure 5b, and it may pass through this opening 276, and so be free of upper plate 270.
  • the locking member 274 may then abut the lower plate 272, and is now positioned 180 degrees opposite the rectangular opening 278 in the lower plate 272.
  • the locking member 274 may be aligned with the rectangular opening 278, as seen in Figure 5c, and the locking member 274 may then pass through opening 278, and so be free of lower plate 272.
  • seals 45a may be applied between inner piston portion 18 and intermediate piston portion 16 on a bottom portion of inner piston portion 18, seals 45b may be applied between intermediate piston portion 16 and outer piston portion 14 on a bottom portion of intermediate piston 16, and seals 45c may be applied between outer piston portion 14 and an inner surface of housing chamber 22 on a bottom portion of outer piston portion 14. Seals 45a, 45b and 45c may be used to prevent fluid leakage between each of the pistons portions 14, 16, 18 and the inner surface of the housing chamber 22.
  • An alternative embodiment of the fluid compression system is shown in
  • the fluid compression system 110 comprises a housing chamber 122 defining a fluid volume, and a piston 112.
  • the fluid volume is enclosed by the piston 1 12 and the housing chamber 122.
  • the piston 112 has an outer annular piston portion 114 which circumscribes an inner piston portion 118, and which has a longitudinal length greater than that of the inner piston portion 1 18.
  • the piston portions 1 14, 1 18 are held releasably integral through the use of attachment means (not shown).
  • the bottom surface of the piston 112 defines a compression surface 113 having a variably-sized surface area. As shown in Figure 6a, the piston portions 1 14, 1 18 are initially maintained integral by the attachment means and the compression surface 1 13 is defined by the bottom surfaces of the piston portions 1 14, 1 18.
  • a force is applied on the piston portion 118 and the piston 1 12 translates in a longitudinal direction until it reaches the position shown in Figure 6b.
  • the piston portions 114, 118 remain integral until the outer piston portion 114 abuts the end of the housing chamber 122.
  • the attachment means release the inner piston portion 118 from the outer piston portion 114 and the inner piston portion 1 18 is free to further translate in housing chamber 122.
  • the compression surface 1 13 is now defined by the bottom of the inner piston portion 118 and the radial walls 123 of the outer piston portion 1 14 now form part of the enclosure for the fluid volume.
  • the inner piston portion 1 18 further translates into the housing chamber 122, thereby further compressing the fluid volume therein, until the inner piston portion 118 reaches an end of the housing chamber 122.
  • the compressed fluid volume is then exhausted through the compressed fluid exhaust 134. It is to be noted that the compressed fluid volume may begin to be exhausted prior to the inner piston portion 118 reaching an end of the housing chamber 122. In another embodiment, it is not necessary for the inner piston portion 1 18 to fully reach an end of the housing chamber 122.
  • the fluid compression system 110 similarly to the fluid compression system 10, still makes use of a compression surface having a variably-sized surface area, in order to achieve a higher compression ratio in a relatively shorter span of time and a relatively shorter length of the housing chamber 122, when compared to a typical piston and cylinder system.
  • the fluid compression system 10 may comprise a piston having an effective compression surface which varies continuously along the compression stroke of the piston.
  • the piston could take the form of a deformable membrane or bladder.
  • the compression cycle of one embodiment of this bladder- type fluid compression system is shown in Figures 7a, 7b, and 7c.
  • the fluid compression system 10' may comprise a flexible membrane 54, which acts as a piston, and which defines a compression surface 13' having a variably-sized surface area.
  • the flexible membrane 54 may form an enclosure such as to have a fluid volume located therein.
  • a force is applied on the flexible membrane, and the flexible membrane is deformed so as to compress the fluid volume located therein.
  • the flexible membrane 54 may undergo continuous deformation, and as such, the surface area of the compression surface 13' may progressively decrease as the fluid volume in a flexible membrane 54 is compressed.
  • the compressed fluid volume may be isolated in a particular section 55 of the flexible membrane 54, as seen in Figure 7b.
  • the compressed fluid is exhausted through the compressed fluid exhaust 34'.
  • new fluid may then be introduced to the flexible membrane 54 through the fluid intake 36' and the flexible membrane may recover its initial configuration, such that the compression cycle may begin anew.
  • This particular embodiment of the fluid compression system may involve continuous compression of the fluid volume, and as such, the fluid compression system encompasses more than a compression cycle having clear distinct stages.
  • the compression cycle of another embodiment of this bladder-type fluid compression system is shown in Figures 8a, 8b and 8b.
  • the compression surface 13" and the shape of the flexible membrane 54' may deform in a pre-determined manner, and as such, as opposed to the embodiment shown in Figures 7a, 7b and 7c, no particular section is required to isolate the fluid volume.
  • a fluid bladder 356 can be interposed between the force transmitting member 332 and the flexible membrane 354 which is used to impart a pressure to the fluid contained in the housing 320.
  • the fluid bladder 356 allows applying a variable pressure on the flexible membrane 354 when a compression force or load is transmitted to the force transmitting member 332.
  • the cross-sectional area of the chamber defined by the housing 320 gradually decreases together with the effective surface area of the membrane 354 as the same is pressed down against the inner wall of the housing chamber during the compression stroke of the device.
  • the fluid compression system may be used in a large number of applications.
  • the compressed fluid volume in the accumulation tank may be used as an energy source, such as to power a turbine in an electricity generator and in so doing, generate electricity.
  • the compressed fluid volume may be air and the compressed air in the accumulation tank may be used as a source of compressed air in any pressurized air-based system, such as a pressurized air gun for example.
  • the compressed fluid volume may be water and the pressurized water in the accumulation tank may be used as a source of pressurized water in any pressurized water-based system, such as high pressure water cleaner.
  • the fluid compression system may be used to compress many types of fluids, such as gases, i.e. air, or liquids, compressible or incompressible, such as water.
  • the fluid compression system 10 is used in the sole of a shoe or boot which can be worn by a person. Every time a person presses down on the shoe, a force is applied on the force-conveying member 32 and the fluid compression system 10 compresses the fluid volume located therein. This allows for a large amount of compression to occur in a short span of time, i.e. whenever a person who is walking takes a step.
  • This fluid volume may then be used to power a turbine and generate electricity.
  • This electricity may then be used to power an electronics device, such as a cellphone, a radio, a global positioning system device, a portable music player or various other consumer electronics product.
  • the fluid volume being compressed is air, the temperature of the air may rise as the air is compressed.
  • the compressed hot air may then be used in order to heat the shoe or boot, for example by expelling the hot air throughout the sole of the shoe.
  • the compressed air may also be used to cool the sole or boot by releasing the compressed air at a relatively high velocity, such as in a fan.
  • the compressed air may also be used in a heat exchanger system, in order to provide additional cooling or heating of the shoe or boot.
  • FIG. 9 A specific embodiment of the fluid compression system 10, as used in a shoe or boot of a person is shown in Figure 9.
  • the force-conveying member 32 is surmounted by a piston or top plate 56, which is located inside a cylinder 58 and which has a diameter substantially equal to the diameter of the cylinder 58.
  • This top plate 56 divides the cylinder 58 into an upper portion 60 and a lower portion 62 thereof.
  • the upper portion 60 of the cylinder 58 is connected to air pockets 64 or air cushions, located in the sole of the shoe or boot.
  • This lower portion 62 of the cylinder is connected to an air intake 66 located in the sole of the shoe, and to an air exhaust 68 located in the sole of the shoe.
  • the air pockets 64 When a person presses down on the shoe or boot, the air pockets 64 will be compressed and air located therein will be evacuated towards the upper portion 60 of the cylinder 58. This air will create a downwards pressure on the top plate 56, which will translate the force-conveying member 32 downwards and will exert a force on the inner piston portion 18.
  • the air located in the lower portion 62 of the cylinder 58 will be evacuated from the cylinder 58 through the air exhaust 68.
  • the piston 12 will then compress the air located inside the housing chamber 22, and the compressed air will subsequently be exhausted through the compressed fluid exhaust 34.
  • the return cycle begins.
  • Fresh air is introduced to the housing chamber 22 through the fluid intake 36, air will be introduced into the lower portion 62 of the cylinder 58 from the air intake 66, air will leave the upper portion 60 of the cylinder 58 and thereby inflate the air pockets 64, the top plate 56 will translate upwards and the piston 12 will return to its initial position, as seen in Figure 9.
  • air will be introduced into the lower portion 62 of the cylinder 58 from the air intake 66, air will leave the upper portion 60 of the cylinder 58 and thereby inflate the air pockets 64, the top plate 56 will translate upwards and the piston 12 will return to its initial position, as seen in Figure 9.
  • the initial position of the piston 12 may differ.
  • the fluid compression system 10 may be used in a different configuration with a shoe or a boot.
  • the fluid compression system 10 may be used in any vibratory environment having sufficient motion to compress the fluid volume therein.
  • Many structures experience a visible amount of vibration due to mechanical stresses or motions, for example bridges may vibrate due to cars or buildings may vibrate due to wind motion.
  • By installing the fluid compression system in a bridge or building it may be possible to harness the motion of this bridge or building using the fluid compression system, and thereby provide an accumulation of compressed fluid.
  • This compressed fluid may then be used with a turbine, in order to provide electricity.
  • This electricity may then be used to power road lights, street signs or a number of other electric devices.
  • the fluid compression system may therefore be used as a device which converts mechanical energy to electrical energy.
  • the fluid compression system may also be used as a bicycle tire pump or as a pump for inflatable objects, such as an inflatable mattress, an inflatable toy or additionally as a pump for sporting goods, such as a football, soccer ball, basketball etc.
  • Pumping these elements with the present fluid compression system may be done quicker than with a traditional manual pump, as it is now possible to attain high compression ratios while using a shorter cylinder length. Because the force exerted on the fluid compression system may always be applied on the inner piston portion and therefore to the compression surface, any force applied on the fluid compression system will serve to compress the fluid volume located inside the housing chamber.
  • the fluid compression system may therefore also be used as a device which converts mechanical energy to fluid energy, or which provides pressurized fluid using mechanical energy.
  • the fluid compression system may be used to recover such energy losses.
  • these recovered energy losses may be stored in the form of an accumulation of compressed fluid, or in another embodiment, they may be used to power an electricity-generating turbine.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Details Of Reciprocating Pumps (AREA)

Abstract

L'invention porte sur une pompe à fluide (10) qui possède un élément de compression (12) possédant une surface de compression de dimension variable (13b), qui peut se déplacer à l'encontre d'une pression de fluide dans une chambre (22). L'aire de surface effective de l'élément de compression (12) décroît en dimension avec une aire de section correspondante de la chambre (22) pour passer d'une aire maximale au début de la course de compression à une aire minimale à la fin de la course de compression. L'utilisation d'une aire de surface de dimension variable pour comprimer un volume de fluide permet d'obtenir un gain rapide de la pression de fluide, même dans des applications dans lesquelles l'élément de compression (12) est actionné à des fréquences relativement basses et sous l'action de forces relativement petites.
PCT/CA2010/001910 2009-12-08 2010-11-29 Système de compression de fluide Ceased WO2011069241A1 (fr)

Priority Applications (2)

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US13/060,878 US9175676B2 (en) 2009-12-08 2010-11-29 Fluid compression system
CA2732482A CA2732482C (fr) 2009-12-08 2010-11-29 Systeme de comression de fluide

Applications Claiming Priority (2)

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US26762109P 2009-12-08 2009-12-08
US61/267,621 2009-12-08

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WO2011069241A1 true WO2011069241A1 (fr) 2011-06-16

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CA (1) CA2732482C (fr)
WO (1) WO2011069241A1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9103465B2 (en) * 2011-07-18 2015-08-11 Safoco, Inc. Dual piston actuator and method of use
US20150330377A1 (en) * 2014-05-19 2015-11-19 Beto Engineering & Marketing Co., Ltd. Hand pump having electric generator
USD902959S1 (en) * 2014-06-23 2020-11-24 Ying-Chieh Liao Pumping device
DE102014221097A1 (de) * 2014-10-17 2016-04-21 Robert Bosch Gmbh Kolbenpumpe
JP6305480B2 (ja) * 2016-09-01 2018-04-04 日機装株式会社 無脈動ポンプ
US10973276B2 (en) * 2017-01-23 2021-04-13 Massachusetts Institute Of Technology Energy harvesting footwear comprising three compressible volumes
CN110159506A (zh) * 2019-06-28 2019-08-23 深圳市恒瑞兴自动化设备有限公司 防结晶注液泵
CN110657080B (zh) * 2019-09-10 2022-02-15 河南科技大学 用于短行程液压缸液压装置的双速手动加压泵
CN111335946B (zh) * 2020-03-30 2024-06-25 中国十九冶集团有限公司 隧道排水系统及排水方法
WO2022099327A1 (fr) * 2020-11-05 2022-05-12 Cloete Lorinda Compresseur
EP4474643B1 (fr) * 2023-06-09 2026-02-04 Tonand Inc. Piston dans un dispositif hydraulique à déplacement variable
US11994121B1 (en) * 2023-06-09 2024-05-28 Tonand Inc. Piston in piston variable displacement hydraulic device
CN119122797B (zh) * 2024-11-13 2025-02-11 佛山鸿沣医疗科技有限公司 一种基于压力反馈自调节的气泵及压力反馈自调节方法

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1263401A (en) * 1917-05-04 1918-04-23 William M Fraser Pump.
GB2341898A (en) * 1998-06-26 2000-03-29 David John Kay Shaw Pump with tapered bore
US6239501B1 (en) * 1998-05-26 2001-05-29 Robert Komarechka Footwear with hydroelectric generator assembly
US20080127510A1 (en) * 2006-12-01 2008-06-05 Honeywell International Inc. Footwear energy harvesting system
US20080181800A1 (en) * 2007-01-31 2008-07-31 Gardner Denver Thomas Gmbh Positive displacement pump for transporting a fluid with automatic adaptation to the compressibility of the fluid

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3775027A (en) * 1971-10-01 1973-11-27 Gray Manuf Co Inc Two-speed pump
US4823482A (en) * 1987-09-04 1989-04-25 Nikola Lakic Inner shoe with heat engine for boot or shoe
US5542827A (en) 1995-02-08 1996-08-06 Navistar International Transportation Corp. Multiple nested pistons hand priming pump with spring biasing
UA73089C2 (en) * 1999-04-22 2005-06-15 Device with combined chamber and piston (versions)

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1263401A (en) * 1917-05-04 1918-04-23 William M Fraser Pump.
US6239501B1 (en) * 1998-05-26 2001-05-29 Robert Komarechka Footwear with hydroelectric generator assembly
GB2341898A (en) * 1998-06-26 2000-03-29 David John Kay Shaw Pump with tapered bore
US20080127510A1 (en) * 2006-12-01 2008-06-05 Honeywell International Inc. Footwear energy harvesting system
US20080181800A1 (en) * 2007-01-31 2008-07-31 Gardner Denver Thomas Gmbh Positive displacement pump for transporting a fluid with automatic adaptation to the compressibility of the fluid

Also Published As

Publication number Publication date
CA2732482C (fr) 2014-02-11
US20120233989A1 (en) 2012-09-20
US9175676B2 (en) 2015-11-03
CA2732482A1 (fr) 2011-06-08

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