WO2009112866A1 - Pump - Google Patents

Pump Download PDF

Info

Publication number
WO2009112866A1
WO2009112866A1 PCT/GB2009/050245 GB2009050245W WO2009112866A1 WO 2009112866 A1 WO2009112866 A1 WO 2009112866A1 GB 2009050245 W GB2009050245 W GB 2009050245W WO 2009112866 A1 WO2009112866 A1 WO 2009112866A1
Authority
WO
WIPO (PCT)
Prior art keywords
pump according
actuator
cavity
end wall
main cavity
Prior art date
Application number
PCT/GB2009/050245
Other languages
French (fr)
Inventor
James Edward Mccrone
Justin Rorke Buckland
David Mark Blakey
Original Assignee
The Technology Partnership Plc
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 The Technology Partnership Plc filed Critical The Technology Partnership Plc
Priority to CA2718390A priority Critical patent/CA2718390A1/en
Priority to EP09720214.7A priority patent/EP2268923B1/en
Priority to JP2010550268A priority patent/JP5335003B2/en
Priority to CN2009801090360A priority patent/CN101986787A/en
Priority to AU2009223958A priority patent/AU2009223958B2/en
Priority to US12/922,589 priority patent/US8734131B2/en
Publication of WO2009112866A1 publication Critical patent/WO2009112866A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B45/00Pumps or pumping installations having flexible working members and specially adapted for elastic fluids
    • F04B45/04Pumps or pumping installations having flexible working members and specially adapted for elastic fluids having plate-like flexible members, e.g. diaphragms
    • F04B45/047Pumps having electric drive
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F7/00Pumps displacing fluids by using inertia thereof, e.g. by generating vibrations therein
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B45/00Pumps or pumping installations having flexible working members and specially adapted for elastic fluids
    • F04B45/08Pumps or pumping installations having flexible working members and specially adapted for elastic fluids having peristaltic action
    • F04B45/10Pumps or pumping installations having flexible working members and specially adapted for elastic fluids having peristaltic action having plate-like flexible members

Definitions

  • This invention relates to a pump for fluid and, in particular to a pump in which the pumping cavity is closely a disc-shaped cylindrical cavity, having closely-circular end walls.
  • the design of such a pump is disclosed in WO2006/1 11775.
  • end walls are driven into oscillating displacement in a direction substantially perpendicular to the plane of the end wall by an actuator.
  • that end-wall surface may, but need not, be itself formed as an element of a composite vibration actuator such as a piezoelectric unimorph or bimorph.
  • the end wall may be formed as a passive material layer driven into oscillation by a separate actuator in force-transmitting relation (e.g. mechanical contact, magnetic or electrostatic) with it.
  • Mode-matching ensures that the work done by the actuator on the fluid in the cavity adds constructively across the driven end-wall surface, enhancing the amplitude of the pressure oscillation in the cavity and delivering high pump efficiency.
  • a pump which is not mode-matched there may be areas of the end-wall surface in which the work being done by the end-wall on the fluid reduces rather than enhances the amplitude of the pressure oscillation in the fluid within the cavity: the useful work done by the actuator on the fluid is reduced and the pump becomes less efficient.
  • Figure 3A of WO2006/11 1775 shows a pump in which one end- wall 12 is formed by the lower surface of disc 17 and is excited into vibrational motion by a piezoelectric actuator formed by disc 17 and piezoelectric disc 20. Together, disc 17 and piezoelectric disc 20 form a composite bending-mode actuator whose vibration excites radially-symmetric pressure waves in the fluid within the cavity 1 1.
  • the amplitude of motion of end-wall 12 is a maximum at the centre of the cavity and a minimum at its edge.
  • a pump incorporating such a composite actuator is relatively simple to construct, as the actuator may be rigidly clamped to the cavity around its perimeter where the amplitude of motion of the actuator is close to zero.
  • Figure 3B of WO2006/11 1775 shows a preferable arrangement in which the amplitude of motion of the actuator and therefore of the end-wall 12 approximates a Bessel function and has an antinode at the cavity perimeter.
  • the driven end wall and the pressure oscillation in the fluid within the cavity are mode-matched, and the efficiency of the pump is improved.
  • the actuator must have an antinode of vibration at the side-wall, to which it might normally be mounted.
  • WO2006/1 11775 which shows a pump driven by a simple unimorph actuator.
  • the actuator consists of a piezoelectric disc attached to a second disc. If such an actuator is clamped at the cavity perimeter its lowest order mode will be as shown schematically in Figure 3A.
  • the thickness and diameter of the piezoelectric disc are determined by the need to achieve the required frequency of vibration and mode-shape in the actuator, effectively fixing the volume of piezoelectric material that may be used.
  • this limitation on piezoelectric disc volume puts a limit on the useful power output of the actuator.
  • the piezoelectric disc is subject to high strain at its centre, where the amplitude of motion of the actuator and its radius of curvature are highest. It is known that high strains can lead to the degradation of piezoelectric material through its depolarisation, thereby reducing the amplitude of motion of the actuator and thus limiting actuator lifetime. Such high strain at the centre of the actuator may also lead to fatigue of the glue layer between the piezoelectric disc and the second disc if the two are joined by gluing, again leading to reduced actuator lifetime.
  • a fluid pump comprising: a chamber which, in use, contains a fluid to be pumped, the chamber including a main cavity having a substantially cylindrical shape bounded by first and second end walls and a side wall and a secondary cavity extending radially outwards of the main cavity; one or more actuators which, in use, cause oscillatory motion of the first end wall in a direction substantially perpendicular to the plane of the first end wall; and whereby, in use, the axial oscillations of the end walls drive radial oscillations of the fluid pressure in the main cavity; and wherein the secondary cavity spaces the side wall from the first end wall such that the first end wall can move relative to the side wall when the actuator is activated.
  • the secondary cavity may space the side wall from the first end wall such that the first end wall can move independently of the side wall when the actuator is activated.
  • the present invention overcomes the challenge of positioning an antinode of actuator vibration at the main cavity edge by physically separating the mechanical actuator mount from the side wall.
  • the actuator is mounted rigidly at a diameter greater than that of the side-wall, with the main cavity being defined by a side-wall which approaches but does not touch the surface of the actuator.
  • the radial acoustic wave in the main cavity is substantially reflected by the side-wall, creating the desired radial standing wave in the main cavity with pressure anti-node at the curved side-walls, but the actuator does not contact the side-wall, enabling it to vibrate with or closely with, an anti-node of displacement at that radius, as desired.
  • the side-wall is similarly defined, but with a compliant material filling the gap between the top of the side-wall and the surface of the actuator.
  • the use of an actuator whose active element is a ring of piezoelectric material to drive the oscillation of the actuator further overcomes the problems of limited piezoelectric material volume and high strain within the piezoelectric material. Because such a piezoelectric ring may be of significantly larger outer diameter than its piezoelectric disc counterpart it may have a significantly larger area. This enables a higher volume of piezoelectric material to be employed, and removes the piezoelectric material from the high -strain region at the centre of the actuator.
  • a gap is provided between the top of the side wall and the first end wall.
  • a layer of compliant material may be provided between the top of the side wall and the first end wall.
  • the secondary cavity may include a thinner portion between a rigid mount positioned radially outward of the side wall and the first end wall and a deeper portion radially outward of the side wall.
  • the side wall may taper towards the first end wall.
  • the first end wall is preferably mounted on the radially outermost portion of the secondary cavity.
  • At least two apertures through the chamber walls are preferably provided, at least one of which is a valved aperture.
  • a second actuator may be provided such that, in use, the second actuator causes oscillatory motion of the second end wall in a direction substantially perpendicular to the second end wall.
  • One or both actuators may include an active element which is either piezoelectric or magnetostrictive and maybe a disc or a ring.
  • the active element is preferably excited in a radial mode to induce axial deflection of one or both of the end walls.
  • the distance between the inner and outer circumferences of the active element is approximately one half of a wavelength of the actuator mode- shape.
  • the active element is preferably designed such that its inner and outer circumferences are located substantially at nodes of the actuator vibrational mode-shape, i.e. the actuator material substantially spans the area between such two nodes of vibration.
  • the distance between the inner and outer circumferences of the active element may be approximately one quarter of a wavelength of the actuator mode- shape.
  • the active element is preferably designed such that its outer diameter is substantially adjacent the radially outermost portion of the secondary chamber.
  • the actuator may include a solenoid.
  • the thickness of the first end wall is preferably shaped to optimise the actuator displacement profile for mode-shape matching.
  • the actuator is preferably constructed such that the piezoelectric or magnetostrictive material is pre-com pressed in the actuator rest position.
  • the main cavity radius, a, and height h preferably satisfy the following inequalities: a/h is greater than 1.2; and h 2 /a is greater than 4x10 "10 m.
  • the main cavity radius, a also preferably satisfies the following inequality: /c 0 . c_min k 0 . c_max
  • the motion of the driven end wall(s) and the pressure oscillations in the main cavity are preferably mode-shape matched and the frequency of the oscillatory motion may be within 20% of the lowest resonant frequency of radial pressure oscillations in the main cavity.
  • the ratio — may be greater than 20.
  • the volume of the main cavity may be h less than 10ml.
  • the frequency of the oscillatory motion is preferably equal to the lowest resonant frequency of radial pressure oscillations in the main cavity.
  • the lowest resonant frequency of radial fluid pressure oscillations in the main cavity is preferably greater than 500Hz.
  • One or both of the end walls may have a frusto-conical shape such that the end walls are separated by a minimum distance at the centre and by a maximum distance at the edge.
  • the end wall motion is preferably mode-shape matched to the pressure oscillation in the main cavity.
  • the amplitude of end wall motion preferably approximates the form of a Bessel function.
  • any unvalved apertures in the chamber walls are located at a distance of 0.63a plus or minus 0.2a from the centre of the main cavity, where a is the main cavity radius.
  • any valved apertures in the chamber walls are located near the centre of the end walls.
  • the ratio — is preferably greater than 10 "7 metres and the working fluid is a preferably a gas.
  • Figures 1 A to C is a schematic representation of the pump according to the prior art in which the actuator displacement and pressure oscillation in the cavity are not mode-matched;
  • Figure 2 is a schematic representation of a preferable embodiment according to the prior art in which the actuator displacement and pressure oscillation in the cavity are mode-matched;
  • Figure 3 illustrates one embodiment of the present invention, enabling the preferential mode-matched condition to be achieved;
  • Figures 4A to C illustrates further embodiments of the present invention;
  • FIGS 5 and 6 illustrate possible actuator constructions which may be employed in the present invention
  • Figure 7 shows one further possible actuator design that may be employed in the present invention
  • Figure 8 illustrates a tapered main cavity.
  • FIG. 1 A is a schematic representation of the pump according to the prior art.
  • a cavity 11 is defined by end walls 12 and 13, and a side wall 14.
  • the cavity is substantially circular in shape, although elliptical and other shapes could be used.
  • the cavity 11 is provided with a nodal air inlet 15, which in this example is unvalved.
  • the first end-wall 12 is defined by the lower surface of a disc 17 attached to a main body 18. The inlet and outlet pass through the main body 18.
  • the actuator comprises a piezoelectric disc 20 attached to a disc 17.
  • the actuator is caused to vibrate in a direction substantially perpendicular to the plane of the cavity, thereby generating radial pressure oscillations within the fluid in the cavity.
  • Figure 1 B shows one possible displacement profile of the driven wall 12 of the cavity.
  • the amplitude of motion is maximum at the centre of the cavity, and minimum at its edge.
  • the solid curved line and arrows indicate the wall displacement at one point in time, and the dashed curved line its position one half cycle later.
  • the displacements as drawn are exaggerated, and the piezoelectric disc is omitted from the drawing for clarity.
  • Figure 1 C shows one possible pressure oscillation profile for the cavity shown in Figures 1A and 1 B.
  • the solid curved line and arrows indicate the pressure at one point in time, and the dashed curved line the pressure one half-cycle later.
  • the radial dependence of the pressure in the cavity is approximately a Bessel function having the following characteristics: 3.83 Equation 1 where r is the radial distance from the centre of the cavity, a is the cavity radius, and
  • P 0 is the pressure at the centre of the cavity.
  • Figures 1 B and 1 C show the modes of actuator displacement and pressure oscillation that are typically employed in the operation of the pump of Figure 1A. It can be seen from inspection that the two modes are only moderately well matched in this case: where the actuator acts to enhance the pressure oscillation at the centre of the cavity it must necessarily act to decrease it near the cavity wall where the pressure oscillation is of the opposite sign.
  • the degree of mode-matching may be expressed by the product of the actuator velocity and pressure integrated over the area of the cavity.
  • the actuator velocity and pressure may be represented by:
  • V ⁇ r,t V ⁇ r).sin ⁇ t)
  • P(r,t) P(r).sin( ⁇ t + ⁇ )
  • V(r) expresses the radial dependence of the actuator velocity
  • P(r) expresses the radial dependence of the pressure oscillation in the cavity
  • angular velocity
  • t time
  • the phase difference between the pressure and velocity.
  • the degree of mode-matching may be defined by the integral of pressure and velocity over the surface of the actuator:
  • M Equation 3
  • V(O) and P(O) are respectively the actuator velocity and pressure at the centre of the cavity
  • dA is an element of area
  • the integral is taken across the area of the actuator in direct communication with the cavity.
  • the amplitude of motion of the actuator is small close to the edge of the cavity and the central area of the actuator dominates this integral.
  • Figure 2 shows one possible preferable arrangement in which the actuator has a mode-shape which is well matched to the mode-shape of the pressure oscillation in the cavity. The actuator now acts to increase the amplitude of the pressure oscillation in the cavity at all points, and the degree of mode-matching as expressed by Equation 2 is increased.
  • FIG. 3A shows one possible embodiment of the present invention where the pump chamber is now divided into a main cavity 110 and a secondary cavity 23.
  • the actuator disc 17 is mounted to 18 around its perimeter. Mounting the actuator in this way enables a relatively rigid mount to be used, facilitating manufacture of the pump.
  • the actuator is preferably driven in the vibrational mode shown in Figure 3B.
  • the side-wall 14 is formed by a step change in cavity depth at radius a, with the secondary cavity 23 extending beyond this radius at reduced depth to the radius at which the actuator is attached to the pump body 21.
  • the step- change in cavity depth at the side-wall 14 acts to reflect the acoustic wave within the main cavity 110, generating the necessary standing wave, while the actuator motion remains unconstrained at this diameter, enabling the desired result of creating an anti-node of actuator vibration at the effective edge of the main cavity 110 .
  • the degree of reflection at the side-wall 14 of Figure 3A depends primarily on two factors: the acoustic impedance of the side-wall material, and the height of the side- wall 14 relative to the depth of the main cavity 110 . To a first approximation, the reflection coefficient, R, of a full-height main cavity wall is given by:
  • Equation 5 Equation 5 where hwaii is the height of the side-wall, and h Ca v ⁇ t y the height of the main cavity. It is therefore important that the height of the side- wall be maximised for the design shown in Figure 3A.
  • FIGs 4A to 4C show variations of the present invention.
  • Figure 4A shows a pump in which the secondary cavity has an increased depth outside the side-wall 14.
  • This design feature is intended to minimise the extent of the narrow gap between the top of the side-wall 14 and the actuator disc 17 as high pressures may be generated in this gap leading to a loss of pump efficiency.
  • the side-wall 14 of Figure 4A should be as narrow as reasonably possible while maintaining its acoustic impedance and thus its reflection coefficient.
  • a tapered side-wall 14 may be preferable, an example of which is shown in Figure 4C. In order to achieve optimal acoustic reflection at the inside edge of such a side-wall, it is preferable that the inside edge of the side-wall remains vertical as shown.
  • Figure 4B shows a pump in which a suitably compliant member fills the gap between the top of the side-wall 14 and the actuator disc 17.
  • a suitably compliant member fills the gap between the top of the side-wall 14 and the actuator disc 17.
  • Such complaint member acts to further improve the reflection of acoustic energy at the side-wall.
  • the stiffness of the compliant member must be carefully chosen to avoid significant damping of the actuator motion.
  • Figure 5 shows one possible actuator design that may be employed in the present invention and which embodies a piezoelectric disc 20.
  • the radius of this disc should be approximately equal to the radius of the first vibrational node of the actuator and therefore, for a mode-matched pump design, the radius of the piezoelectric disc should be approximately equal to the radius of the first node of the pressure oscillation in the main cavity.
  • the sign of the actuator curvature changes: the in- plane expansion of the piezoelectric disc that generates the curvature of the central actuator antinode region acts against generating the required curvature (now of the opposite sign) beyond the first vibrational node.
  • a simple unimorph actuator of this type should be configured such that the piezoelectric element spans only areas in which the actuator curvature is of a single sign.
  • Figure 6 shows a second possible actuator design that may be employed in the present invention.
  • Figure 6A shows the approximate radial positioning of a piezoelectric ring 20 on the disc 17.
  • Figure 6B shows the resulting displacement profile of the actuator with the piezoelectric ring omitted from the drawing for clarity.
  • the PZT spans approximately one half-wavelength of the actuator's vibrational mode-shape, in which region the curvature of the actuator is again of one sign.
  • the in-plane expansion and contraction of the piezoelectric ring (indicated by the double-headed arrow) efficiently drives the vibration of the actuator.
  • the embodiment of Figure 6 is preferable to that of Figure 5 as the volume of piezoelectric material and therefore the maximum power output of the actuator are both higher.
  • the piezo disc of Figure 5A may therefore extend to a radius of approximately 0.63a, this being the radius of the first zero of the Bessel function that has its first maximum at the main cavity radius, a.
  • the maximum useful area of such a piezoelectric disc is therefore approximately 1.2a 2 .
  • the piezoelectric ring of Figure 6 may extend from a radius of 0.63a to a radius of 1.44a (the next Bessel function zero), in which region the curvature of the Bessel function is again of a single sign.
  • the maximum useful area of such a piezoelectric ring is therefore approximately 5.3a 2 .
  • the actuator motion may only approximate a Bessel function, however this simple calculation illustrates the significant advantage of moving to a ring actuator in terms of the area of piezoelectric material and therefore the maximum power output of the actuator.
  • Figure 7 shows one further possible actuator design that may be employed in the present invention.
  • Figure 7A shows the approximate radial positioning of the piezoelectric ring 20 on the disc 17.
  • Figure 7B shows the resulting displacement profile of the actuator with the piezoelectric ring omitted from the drawing for clarity.
  • the PZT spans approximately one quarter-wavelength of the actuator's vibrational mode-shape, in which region the curvature of the actuator is again of one sign.
  • the in-plane expansion and contraction of the piezoelectric ring (indicated by the double-headed arrow) efficiently drives the vibration of the actuator.
  • Figure 8 illustrates a tapered main cavity in which one end wall, in this case the second end wall, is frusto-conical in shape. It will be seen how the main cavity 1 10 has a greater height at the side-wall 14, whereas at the centre, the distance between the end walls 12, 13 is at a minimum. Such a shape provides an increased pressure at the centre of the cavity. Typically, the diameter of the cavity is 20mm and the height at the centre is 0.25mm and the height at the radial extreme is 0.5mm.

Landscapes

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

Abstract

A fluid pump comprising a chamber which, in use, contains a fluid to be pumped, the chamber including a main cavity having a substantially cylindrical shape bounded by first and second end walls and a side wall and a secon dary cavity extending radially outwards of the main cavity, one or more actuators which, in use, cause oscillatory motion of the first end wall in a direction substantially perpendicular to the plane of the first end wall, and whereby, in use, the axial os cillations of the end walls drive radial oscillations of the fluid pressure in the main cavity, and wherein the secondary cavity spaces the side wall from the first end wall such that the first end wall can move relative to the side wall when the actuator is activated.

Description

PUMP
This invention relates to a pump for fluid and, in particular to a pump in which the pumping cavity is closely a disc-shaped cylindrical cavity, having closely-circular end walls. The design of such a pump is disclosed in WO2006/1 11775.
In such a pump one or both end walls are driven into oscillating displacement in a direction substantially perpendicular to the plane of the end wall by an actuator. Where an end wall is so driven, that end-wall surface may, but need not, be itself formed as an element of a composite vibration actuator such as a piezoelectric unimorph or bimorph. Alternatively, the end wall may be formed as a passive material layer driven into oscillation by a separate actuator in force-transmitting relation (e.g. mechanical contact, magnetic or electrostatic) with it.
It is preferable to match the spatial profile of the motion of the driven end wall(s) to the spatial profile of the pressure oscillation in the cavity, a condition described herein as mode-matching. Mode-matching ensures that the work done by the actuator on the fluid in the cavity adds constructively across the driven end-wall surface, enhancing the amplitude of the pressure oscillation in the cavity and delivering high pump efficiency. In a pump which is not mode-matched there may be areas of the end-wall surface in which the work being done by the end-wall on the fluid reduces rather than enhances the amplitude of the pressure oscillation in the fluid within the cavity: the useful work done by the actuator on the fluid is reduced and the pump becomes less efficient.
This problem is demonstrated in the prior art by Figure 3 of WO2006/1 11775. Figure 3A of WO2006/11 1775 shows a pump in which one end- wall 12 is formed by the lower surface of disc 17 and is excited into vibrational motion by a piezoelectric actuator formed by disc 17 and piezoelectric disc 20. Together, disc 17 and piezoelectric disc 20 form a composite bending-mode actuator whose vibration excites radially-symmetric pressure waves in the fluid within the cavity 1 1. The amplitude of motion of end-wall 12 is a maximum at the centre of the cavity and a minimum at its edge. A pump incorporating such a composite actuator is relatively simple to construct, as the actuator may be rigidly clamped to the cavity around its perimeter where the amplitude of motion of the actuator is close to zero. However in many practical designs using conventional solid materials for construction of the curved side-walls of the cavity the acoustic impedance of those side-walls is greater t han that of the working fluid and consequently the pressure oscillation in the fluid within the cavity will have an antinode at the end-wall. Since, at this location, the side-wall as shown in Figure 3 of WO2006/1 11775 has a node, such an arrangement cannot deliver mode-matching that is effective across the full surface area of the end-walls. Indeed, the failure of mode-matching occurs principally at the outer radii of the end-walls, so a substantial area fraction of the end walls and working fluid volume are not vibrationally mode- matched.
Figure 3B of WO2006/11 1775 shows a preferable arrangement in which the amplitude of motion of the actuator and therefore of the end-wall 12 approximates a Bessel function and has an antinode at the cavity perimeter. In this case, the driven end wall and the pressure oscillation in the fluid within the cavity are mode-matched, and the efficiency of the pump is improved. However, it is not obvious how such a pump may be constructed, as the actuator must have an antinode of vibration at the side-wall, to which it might normally be mounted. Two further problems of the prior art are illustrated by Figure 1 of
WO2006/1 11775, which shows a pump driven by a simple unimorph actuator. The actuator consists of a piezoelectric disc attached to a second disc. If such an actuator is clamped at the cavity perimeter its lowest order mode will be as shown schematically in Figure 3A. There are two limitations to this design. Firstly, the thickness and diameter of the piezoelectric disc are determined by the need to achieve the required frequency of vibration and mode-shape in the actuator, effectively fixing the volume of piezoelectric material that may be used. As there is a limit to the power that may be delivered efficiently per unit volume of piezoelectric material, this limitation on piezoelectric disc volume puts a limit on the useful power output of the actuator. Secondly the piezoelectric disc is subject to high strain at its centre, where the amplitude of motion of the actuator and its radius of curvature are highest. It is known that high strains can lead to the degradation of piezoelectric material through its depolarisation, thereby reducing the amplitude of motion of the actuator and thus limiting actuator lifetime. Such high strain at the centre of the actuator may also lead to fatigue of the glue layer between the piezoelectric disc and the second disc if the two are joined by gluing, again leading to reduced actuator lifetime.
The present invention aims to overcome one or more of the above indentified problems. According to the invention, there is provided a fluid pump comprising: a chamber which, in use, contains a fluid to be pumped, the chamber including a main cavity having a substantially cylindrical shape bounded by first and second end walls and a side wall and a secondary cavity extending radially outwards of the main cavity; one or more actuators which, in use, cause oscillatory motion of the first end wall in a direction substantially perpendicular to the plane of the first end wall; and whereby, in use, the axial oscillations of the end walls drive radial oscillations of the fluid pressure in the main cavity; and wherein the secondary cavity spaces the side wall from the first end wall such that the first end wall can move relative to the side wall when the actuator is activated.
The secondary cavity may space the side wall from the first end wall such that the first end wall can move independently of the side wall when the actuator is activated.
The present invention overcomes the challenge of positioning an antinode of actuator vibration at the main cavity edge by physically separating the mechanical actuator mount from the side wall.
In one embodiment the actuator is mounted rigidly at a diameter greater than that of the side-wall, with the main cavity being defined by a side-wall which approaches but does not touch the surface of the actuator. In such a configuration the radial acoustic wave in the main cavity is substantially reflected by the side-wall, creating the desired radial standing wave in the main cavity with pressure anti-node at the curved side-walls, but the actuator does not contact the side-wall, enabling it to vibrate with or closely with, an anti-node of displacement at that radius, as desired. In further embodiments the side-wall is similarly defined, but with a compliant material filling the gap between the top of the side-wall and the surface of the actuator.
In a preferred embodiment, the use of an actuator whose active element is a ring of piezoelectric material to drive the oscillation of the actuator further overcomes the problems of limited piezoelectric material volume and high strain within the piezoelectric material. Because such a piezoelectric ring may be of significantly larger outer diameter than its piezoelectric disc counterpart it may have a significantly larger area. This enables a higher volume of piezoelectric material to be employed, and removes the piezoelectric material from the high -strain region at the centre of the actuator.
Preferably, a gap is provided between the top of the side wall and the first end wall. A layer of compliant material may be provided between the top of the side wall and the first end wall.
The secondary cavity may include a thinner portion between a rigid mount positioned radially outward of the side wall and the first end wall and a deeper portion radially outward of the side wall. The side wall may taper towards the first end wall. The first end wall is preferably mounted on the radially outermost portion of the secondary cavity.
At least two apertures through the chamber walls are preferably provided, at least one of which is a valved aperture.
A second actuator may be provided such that, in use, the second actuator causes oscillatory motion of the second end wall in a direction substantially perpendicular to the second end wall.
One or both actuators may include an active element which is either piezoelectric or magnetostrictive and maybe a disc or a ring.
The active element is preferably excited in a radial mode to induce axial deflection of one or both of the end walls.
Preferably the distance between the inner and outer circumferences of the active element is approximately one half of a wavelength of the actuator mode- shape. In such a case the active element is preferably designed such that its inner and outer circumferences are located substantially at nodes of the actuator vibrational mode-shape, i.e. the actuator material substantially spans the area between such two nodes of vibration.
The distance between the inner and outer circumferences of the active element may be approximately one quarter of a wavelength of the actuator mode- shape. In such a case the active element is preferably designed such that its outer diameter is substantially adjacent the radially outermost portion of the secondary chamber.
In an alternative configuration, the actuator may include a solenoid.
The thickness of the first end wall is preferably shaped to optimise the actuator displacement profile for mode-shape matching. The actuator is preferably constructed such that the piezoelectric or magnetostrictive material is pre-com pressed in the actuator rest position.
The main cavity radius, a, and height h, preferably satisfy the following inequalities: a/h is greater than 1.2; and h2/a is greater than 4x10"10 m.
The main cavity radius, a, also preferably satisfies the following inequality: /c0. c_min k0. c_max
2πf 2πf where c_min is 115 m/s, c_max is 1970 m/s, f is the operating frequency and /co is a constant (Zc0 = 3.83).
The motion of the driven end wall(s) and the pressure oscillations in the main cavity are preferably mode-shape matched and the frequency of the oscillatory motion may be within 20% of the lowest resonant frequency of radial pressure oscillations in the main cavity.
The ratio — may be greater than 20. The volume of the main cavity may be h less than 10ml.
The frequency of the oscillatory motion is preferably equal to the lowest resonant frequency of radial pressure oscillations in the main cavity. The lowest resonant frequency of radial fluid pressure oscillations in the main cavity is preferably greater than 500Hz.
One or both of the end walls may have a frusto-conical shape such that the end walls are separated by a minimum distance at the centre and by a maximum distance at the edge. The end wall motion is preferably mode-shape matched to the pressure oscillation in the main cavity.
The amplitude of end wall motion preferably approximates the form of a Bessel function.
It is preferable that any unvalved apertures in the chamber walls are located at a distance of 0.63a plus or minus 0.2a from the centre of the main cavity, where a is the main cavity radius.
It is preferable that any valved apertures in the chamber walls are located near the centre of the end walls. h2 The ratio — is preferably greater than 10"7 metres and the working fluid is a preferably a gas.
Examples of the present invention will now be described with reference to the accompanying drawings, in which:
Figures 1 A to C is a schematic representation of the pump according to the prior art in which the actuator displacement and pressure oscillation in the cavity are not mode-matched; Figure 2 is a schematic representation of a preferable embodiment according to the prior art in which the actuator displacement and pressure oscillation in the cavity are mode-matched;
Figure 3 illustrates one embodiment of the present invention, enabling the preferential mode-matched condition to be achieved; Figures 4A to C illustrates further embodiments of the present invention;
Figures 5 and 6 illustrate possible actuator constructions which may be employed in the present invention;
Figure 7 shows one further possible actuator design that may be employed in the present invention; and Figure 8 illustrates a tapered main cavity.
Figure 1 A is a schematic representation of the pump according to the prior art. A cavity 11 is defined by end walls 12 and 13, and a side wall 14. The cavity is substantially circular in shape, although elliptical and other shapes could be used. The cavity 11 is provided with a nodal air inlet 15, which in this example is unvalved. There is also a valved air outlet 16 located substantially at the centre of end wall 13. The first end-wall 12 is defined by the lower surface of a disc 17 attached to a main body 18. The inlet and outlet pass through the main body 18.
The actuator comprises a piezoelectric disc 20 attached to a disc 17. When an appropriate electrical drive is applied, the actuator is caused to vibrate in a direction substantially perpendicular to the plane of the cavity, thereby generating radial pressure oscillations within the fluid in the cavity.
Figure 1 B shows one possible displacement profile of the driven wall 12 of the cavity. In this case the amplitude of motion is maximum at the centre of the cavity, and minimum at its edge. The solid curved line and arrows indicate the wall displacement at one point in time, and the dashed curved line its position one half cycle later. The displacements as drawn are exaggerated, and the piezoelectric disc is omitted from the drawing for clarity.
Figure 1 C shows one possible pressure oscillation profile for the cavity shown in Figures 1A and 1 B. The solid curved line and arrows indicate the pressure at one point in time, and the dashed curved line the pressure one half-cycle later. For this mode and higher-order modes there is an anti-node of pressure at the cavity wall. The radial dependence of the pressure in the cavity is approximately a Bessel function having the following characteristics: 3.83 Equation 1
Figure imgf000008_0001
where r is the radial distance from the centre of the cavity, a is the cavity radius, and
P0 is the pressure at the centre of the cavity.
Figures 1 B and 1 C show the modes of actuator displacement and pressure oscillation that are typically employed in the operation of the pump of Figure 1A. It can be seen from inspection that the two modes are only moderately well matched in this case: where the actuator acts to enhance the pressure oscillation at the centre of the cavity it must necessarily act to decrease it near the cavity wall where the pressure oscillation is of the opposite sign.
The degree of mode-matching may be expressed by the product of the actuator velocity and pressure integrated over the area of the cavity. For example, where the actuator velocity and pressure may be represented by:
V{r,t) = V{r).sin{ωt)
Equation 2
P(r,t) = P(r).sin(ωt +§) where the function V(r) expresses the radial dependence of the actuator velocity, P(r) expresses the radial dependence of the pressure oscillation in the cavity, ω is angular velocity, t is time, and φ is the phase difference between the pressure and velocity. The degree of mode-matching may be defined by the integral of pressure and velocity over the surface of the actuator:
M = Equation 3
Figure imgf000008_0002
where M represents the degree of mode-matching, V(O) and P(O) are respectively the actuator velocity and pressure at the centre of the cavity, dA is an element of area, and the integral is taken across the area of the actuator in direct communication with the cavity. In the design of Figure 1 the amplitude of motion of the actuator is small close to the edge of the cavity and the central area of the actuator dominates this integral. Figure 2 shows one possible preferable arrangement in which the actuator has a mode-shape which is well matched to the mode-shape of the pressure oscillation in the cavity. The actuator now acts to increase the amplitude of the pressure oscillation in the cavity at all points, and the degree of mode-matching as expressed by Equation 2 is increased. It should be noted that while the product of V(r) and P(r) is lower towards the cavity perimeter than it is at the cavity centre, the larger interaction area close to the cavity perimeter means that the cavity perimeter contributes significantly to the overall degree of mode-matching. The present invention concerns practical ways of achieving this preferential arrangement, i.e. achieving an antinode of actuator displacement at the cavity wall. Figure 3A shows one possible embodiment of the present invention where the pump chamber is now divided into a main cavity 110 and a secondary cavity 23. In this design the actuator disc 17 is mounted to 18 around its perimeter. Mounting the actuator in this way enables a relatively rigid mount to be used, facilitating manufacture of the pump. The actuator is preferably driven in the vibrational mode shown in Figure 3B. The side-wall 14 is formed by a step change in cavity depth at radius a, with the secondary cavity 23 extending beyond this radius at reduced depth to the radius at which the actuator is attached to the pump body 21. The step- change in cavity depth at the side-wall 14 acts to reflect the acoustic wave within the main cavity 110, generating the necessary standing wave, while the actuator motion remains unconstrained at this diameter, enabling the desired result of creating an anti-node of actuator vibration at the effective edge of the main cavity 110 . The degree of reflection at the side-wall 14 of Figure 3A depends primarily on two factors: the acoustic impedance of the side-wall material, and the height of the side- wall 14 relative to the depth of the main cavity 110 . To a first approximation, the reflection coefficient, R, of a full-height main cavity wall is given by:
R = (zWalι - ZFlmd λ Equation 4 yZWall + £Fluιd J where ZWaιι is the acoustic impedance of the side-wall material and ZFluld is the acoustic impedance of the fluid in the main cavity 110. In order to achieve a strong main cavity resonance it is therefore important that the acoustic impedance of the wall material is either significantly larger or significantly smaller than that of the fluid in the main cavity. The former condition may be readily satisfied where the wall is made of metal or some plastics and the fluid in the main cavity is a gas, however other combinations are possible. Where the side-wall does not extend to the full height of the main cavity, the degree of reflection will be reduced. To a first approximation, the reflection coefficient in this case will be given by:
Figure imgf000010_0001
Equation 5 where hwaii is the height of the side-wall, and hCavιty the height of the main cavity. It is therefore important that the height of the side- wall be maximised for the design shown in Figure 3A.
Figs 4A to 4C show variations of the present invention. Figure 4A shows a pump in which the secondary cavity has an increased depth outside the side-wall 14. This design feature is intended to minimise the extent of the narrow gap between the top of the side-wall 14 and the actuator disc 17 as high pressures may be generated in this gap leading to a loss of pump efficiency. For this reason it is preferable that the side-wall 14 of Figure 4A should be as narrow as reasonably possible while maintaining its acoustic impedance and thus its reflection coefficient. A tapered side-wall 14 may be preferable, an example of which is shown in Figure 4C. In order to achieve optimal acoustic reflection at the inside edge of such a side-wall, it is preferable that the inside edge of the side-wall remains vertical as shown. Figure 4B shows a pump in which a suitably compliant member fills the gap between the top of the side-wall 14 and the actuator disc 17. Such complaint member acts to further improve the reflection of acoustic energy at the side-wall. The stiffness of the compliant member must be carefully chosen to avoid significant damping of the actuator motion.
Figure 5 shows one possible actuator design that may be employed in the present invention and which embodies a piezoelectric disc 20. For optimal operation the radius of this disc should be approximately equal to the radius of the first vibrational node of the actuator and therefore, for a mode-matched pump design, the radius of the piezoelectric disc should be approximately equal to the radius of the first node of the pressure oscillation in the main cavity. Beyond this first vibration node of the actuator the sign of the actuator curvature changes: the in- plane expansion of the piezoelectric disc that generates the curvature of the central actuator antinode region acts against generating the required curvature (now of the opposite sign) beyond the first vibrational node. As a general rule, a simple unimorph actuator of this type should be configured such that the piezoelectric element spans only areas in which the actuator curvature is of a single sign.
Figure 6 shows a second possible actuator design that may be employed in the present invention. Figure 6A shows the approximate radial positioning of a piezoelectric ring 20 on the disc 17. Figure 6B shows the resulting displacement profile of the actuator with the piezoelectric ring omitted from the drawing for clarity. In this arrangement the PZT spans approximately one half-wavelength of the actuator's vibrational mode-shape, in which region the curvature of the actuator is again of one sign. As a result the in-plane expansion and contraction of the piezoelectric ring (indicated by the double-headed arrow) efficiently drives the vibration of the actuator. The embodiment of Figure 6 is preferable to that of Figure 5 as the volume of piezoelectric material and therefore the maximum power output of the actuator are both higher. For example if the pump is mode-matched then the radial dependence of the actuator motion will match the radial dependence of the pressure oscillation in the main cavity and will therefore approximate the Bessel function of Equation 1 . The piezo disc of Figure 5A may therefore extend to a radius of approximately 0.63a, this being the radius of the first zero of the Bessel function that has its first maximum at the main cavity radius, a. The maximum useful area of such a piezoelectric disc is therefore approximately 1.2a2.
Again assuming a Bessel function dependence, the piezoelectric ring of Figure 6 may extend from a radius of 0.63a to a radius of 1.44a (the next Bessel function zero), in which region the curvature of the Bessel function is again of a single sign. The maximum useful area of such a piezoelectric ring is therefore approximately 5.3a2. The actuator motion may only approximate a Bessel function, however this simple calculation illustrates the significant advantage of moving to a ring actuator in terms of the area of piezoelectric material and therefore the maximum power output of the actuator.
Figure 7 shows one further possible actuator design that may be employed in the present invention. Figure 7A shows the approximate radial positioning of the piezoelectric ring 20 on the disc 17. Figure 7B shows the resulting displacement profile of the actuator with the piezoelectric ring omitted from the drawing for clarity. In this arrangement the PZT spans approximately one quarter-wavelength of the actuator's vibrational mode-shape, in which region the curvature of the actuator is again of one sign. As a result the in-plane expansion and contraction of the piezoelectric ring (indicated by the double-headed arrow) efficiently drives the vibration of the actuator.
Figure 8 illustrates a tapered main cavity in which one end wall, in this case the second end wall, is frusto-conical in shape. It will be seen how the main cavity 1 10 has a greater height at the side-wall 14, whereas at the centre, the distance between the end walls 12, 13 is at a minimum. Such a shape provides an increased pressure at the centre of the cavity. Typically, the diameter of the cavity is 20mm and the height at the centre is 0.25mm and the height at the radial extreme is 0.5mm.

Claims

1. A fluid pump comprising: a chamber which, in use, contains a fluid to be pumped, the chamber including a main cavity having a substantially cylindrical shape bounded by first and second end walls and a side wall and a secondary cavity extending radially outwards of the main cavity; one or more actuators which, in use, cause oscillatory motion of the first end wall in a direction substantially perpendicular to the plane of the first end wall; and whereby, in use, the axial oscillations of the end walls drive radial oscillations of the fluid pressure in the main cavity; and wherein the secondary cavity spaces the side wall from the first end wall such that the first end wall can move relative to the side wall when the actuator is activated.
2. A fluid pump according to claim 1 , wherein a gap is provided between the top of the side wall and the first end wall.
3. A pump according to claim 2, wherein a layer of compliant material is provided between the top of the side wall and the first end wall.
4. A pump according to any one of the preceding claims, wherein the secondary cavity includes a thinner portion between the side wall and the first end wall and a deeper portion radially outward of the side wall.
5. A pump according to claim 4, wherein the side wall tapers towards the first end wall.
6. A pump according to any one of the preceding claims, wherein the first end wall is mounted on the radially outermost portion of the secondary cavity.
7. A pump according to any one of the preceding claims, further comprising at least two apertures through the chamber walls, at least one of which is a valved aperture.
8. A pump according to any one of the preceding claims, further comprising a second actuator, wherein, in use, the second actuator causes oscillatory motion of the second end wall in a direction substantially perpendicular to the second end wall.
9. A pump according to any one of the preceding claims, wherein the actuator includes an active element which is either a piezoelectric or magnetostrictive disc.
10. A pump according to any one of the preceding claims, wherein the actuator includes an active element which is either a piezoelectric or magnetostrictive ring.
1 1. A pump according to claim 9 or 10, wherein the active element is excited in a radial mode to induce axial deflection of one or both of the end walls.
12. A pump according to claim 1 1 , wherein the radial distance between the inner and outer circumferences of active element ring is approximately one half of a wavelength of the actuator mode-shape.
13. A pump according to claim 12, wherein the inner and outer circumferences of the active element ring are located substantially at nodes of the actuator vibrational mode-shape.
14. A pump according to claim 1 1 , wherein the distance between the inner and outer circumferences of the ring is approximately one quarter of a wavelength of the actuator mode-shape.
15. A pump according to claim 14, wherein the outer circumference of the ring is substantially adjacent the radially outermost portion of the secondary cavity.
16. A pump according to any one of claims 1 to 8, wherein the actuator includes a solenoid.
17. A pump according to any one of the preceding claims, wherein the thickness of the first end wall is shaped to optimise the actuator displacement profile for mode- shape matching.
18. A pump according to any one of claims 9 to 15, wherein the actuator is constructed such that the piezoelectric or magnetostrictive material is pre- compressed in the actuator rest position.
19. A pump according to any one of the preceding claims, wherein the main cavity radius, a, and height h, satisfy the following inequalities: a/h is greater than 1.2; and h2/a is greater than 4x10"10 m.
20. A pump according to claim 19, wherein the main cavity radius, a, also satisfies the following inequality:
/c0. c_min k0. c_max
2πf 2πf where c_min is 115 m/s, c_max is 1970 m/s, f is the operating frequency and /co is a constant (Zc0 = 3.83).
21. A pump according to any one of the preceding claims, wherein, in use, the motion of the driven end wall(s) and the pressure oscillations in the main cavity are mode-shape matched and the frequency of the oscillatory motion is within 20% of the lowest resonant frequency of radial pressure oscillations in the main cavity.
22. A pump according to any one of claims 19 to 21 , wherein the ratio — is h greater than 20.
23. A pump according to any one of the preceding claims, wherein the volume of the main cavity is less than 10ml.
24. A pump according to any one of the preceding claims, wherein, in use, the frequency of the oscillatory motion is equal to the lowest resonant frequency of radial pressure oscillations in the main cavity.
25. A pump according to any one of the preceding claims, wherein, in use, the lowest resonant frequency of radial fluid pressure oscillations in the main cavity is greater than 500Hz.
26. A pump according to any one of the preceding claims, wherein one or both of the end walls have a frusto-conical shape such that the end walls are separated by a minimum distance at the centre and by a maximum distance at the edge.
27. A pump according to any one of the preceding claims, wherein the end wall motion is mode-shape matched to the pressure oscillation in the cavity.
28. A pump according to any one of the preceding claims, wherein the amplitude of end wall motion approximates the form of a Bessel function.
29. A pump according to any one of the preceding claims, wherein any unvalved apertures in the chamber walls are located at a distance of 0.63a plus or minus 0.2a from the centre of the main cavity, where a is the main cavity radius.
30. A pump according to any one of the preceding claims, wherein any valved apertures in the chamber walls are located near the centre of the main cavity.
31. A pump according to any one of claims 19 to 30, wherein the ratio — is a greater than 10 metres and the working fluid is a gas.
PCT/GB2009/050245 2008-03-14 2009-03-13 Pump WO2009112866A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CA2718390A CA2718390A1 (en) 2008-03-14 2009-03-13 Pump
EP09720214.7A EP2268923B1 (en) 2008-03-14 2009-03-13 Pump
JP2010550268A JP5335003B2 (en) 2008-03-14 2009-03-13 pump
CN2009801090360A CN101986787A (en) 2008-03-14 2009-03-13 Pump
AU2009223958A AU2009223958B2 (en) 2008-03-14 2009-03-13 Pump
US12/922,589 US8734131B2 (en) 2008-03-14 2009-03-13 Pump

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0804739.1A GB0804739D0 (en) 2008-03-14 2008-03-14 Pump
GB0804739.1 2008-03-14

Publications (1)

Publication Number Publication Date
WO2009112866A1 true WO2009112866A1 (en) 2009-09-17

Family

ID=39328110

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2009/050245 WO2009112866A1 (en) 2008-03-14 2009-03-13 Pump

Country Status (9)

Country Link
US (1) US8734131B2 (en)
EP (1) EP2268923B1 (en)
JP (1) JP5335003B2 (en)
CN (1) CN101986787A (en)
AU (1) AU2009223958B2 (en)
CA (1) CA2718390A1 (en)
GB (1) GB0804739D0 (en)
RU (1) RU2459114C2 (en)
WO (1) WO2009112866A1 (en)

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2960922A1 (en) * 2010-06-08 2011-12-09 Centre Nat Rech Scient ULTRASONIC PROGRESSIVE WAVE MICRO PUMP FOR LIQUID
WO2012104648A1 (en) 2011-02-03 2012-08-09 The Technology Partnership Plc Pump
US8371829B2 (en) 2010-02-03 2013-02-12 Kci Licensing, Inc. Fluid disc pump with square-wave driver
CN102939492A (en) * 2010-02-03 2013-02-20 凯希特许有限公司 Singulation of valves
WO2013083978A1 (en) 2011-12-06 2013-06-13 The Technology Partnership Plc Acoustic sensor
JP2016052599A (en) * 2010-10-26 2016-04-14 ソメトリクス,インコーポレイテッド Device and method for opening air duct
EP3290211A1 (en) * 2016-09-05 2018-03-07 Microjet Technology Co., Ltd Fluid control device
US10087923B2 (en) 2012-02-10 2018-10-02 The Technology Partnership Plc. Disc pump with advanced actuator
GB2569417A (en) * 2018-07-31 2019-06-19 Ttp Ventus Ltd Microfluidic drive system
US10697449B2 (en) 2016-09-05 2020-06-30 Microjet Technology Co., Ltd. Fluid control device
US10788028B2 (en) 2016-09-05 2020-09-29 Microjet Technology Co., Ltd. Fluid control device with alignment features on the flexible plate and communication plate
US11067073B2 (en) 2016-09-05 2021-07-20 Microjet Technology Co., Ltd. Fluid control device
US11098951B2 (en) 2018-09-09 2021-08-24 Ultrahaptics Ip Ltd Ultrasonic-assisted liquid manipulation
US11169610B2 (en) 2019-11-08 2021-11-09 Ultraleap Limited Tracking techniques in haptic systems
US11189140B2 (en) 2016-01-05 2021-11-30 Ultrahaptics Ip Ltd Calibration and detection techniques in haptic systems
US11204644B2 (en) 2014-09-09 2021-12-21 Ultrahaptics Ip Ltd Method and apparatus for modulating haptic feedback
US11276281B2 (en) 2015-02-20 2022-03-15 Ultrahaptics Ip Ltd Algorithm improvements in a haptic system
US11307664B2 (en) 2016-08-03 2022-04-19 Ultrahaptics Ip Ltd Three-dimensional perceptions in haptic systems
EP4006367A1 (en) 2020-11-27 2022-06-01 European Space Agency Gas bearing system
US11360546B2 (en) 2017-12-22 2022-06-14 Ultrahaptics Ip Ltd Tracking in haptic systems
US11374586B2 (en) 2019-10-13 2022-06-28 Ultraleap Limited Reducing harmonic distortion by dithering
US11378997B2 (en) 2018-10-12 2022-07-05 Ultrahaptics Ip Ltd Variable phase and frequency pulse-width modulation technique
US11529650B2 (en) 2018-05-02 2022-12-20 Ultrahaptics Ip Ltd Blocking plate structure for improved acoustic transmission efficiency
US11531395B2 (en) 2017-11-26 2022-12-20 Ultrahaptics Ip Ltd Haptic effects from focused acoustic fields
US11543507B2 (en) 2013-05-08 2023-01-03 Ultrahaptics Ip Ltd Method and apparatus for producing an acoustic field
US11550395B2 (en) 2019-01-04 2023-01-10 Ultrahaptics Ip Ltd Mid-air haptic textures
US11553295B2 (en) 2019-10-13 2023-01-10 Ultraleap Limited Dynamic capping with virtual microphones
US11550432B2 (en) 2015-02-20 2023-01-10 Ultrahaptics Ip Ltd Perceptions in a haptic system
US11704983B2 (en) 2017-12-22 2023-07-18 Ultrahaptics Ip Ltd Minimizing unwanted responses in haptic systems
US11715453B2 (en) 2019-12-25 2023-08-01 Ultraleap Limited Acoustic transducer structures
US11727790B2 (en) 2015-07-16 2023-08-15 Ultrahaptics Ip Ltd Calibration techniques in haptic systems
US11816267B2 (en) 2020-06-23 2023-11-14 Ultraleap Limited Features of airborne ultrasonic fields
US11842517B2 (en) 2019-04-12 2023-12-12 Ultrahaptics Ip Ltd Using iterative 3D-model fitting for domain adaptation of a hand-pose-estimation neural network
US11886639B2 (en) 2020-09-17 2024-01-30 Ultraleap Limited Ultrahapticons
WO2024052578A1 (en) 2022-09-11 2024-03-14 Bioliberty Ltd Soft robotic assistive device
US11955109B2 (en) 2016-12-13 2024-04-09 Ultrahaptics Ip Ltd Driving techniques for phased-array systems
WO2024165863A1 (en) 2023-02-08 2024-08-15 Foster & Freeman Limited A volatile substance sampling device

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0224986D0 (en) 2002-10-28 2002-12-04 Smith & Nephew Apparatus
GB0325129D0 (en) 2003-10-28 2003-12-03 Smith & Nephew Apparatus in situ
ES2340085T5 (en) 2006-09-28 2014-04-16 Smith & Nephew, Inc. Portable wound therapy system
CA2705898C (en) 2007-11-21 2020-08-25 Smith & Nephew Plc Wound dressing
GB0723855D0 (en) 2007-12-06 2008-01-16 Smith & Nephew Apparatus and method for wound volume measurement
GB201015656D0 (en) 2010-09-20 2010-10-27 Smith & Nephew Pressure control apparatus
US9067003B2 (en) 2011-05-26 2015-06-30 Kalypto Medical, Inc. Method for providing negative pressure to a negative pressure wound therapy bandage
US9084845B2 (en) 2011-11-02 2015-07-21 Smith & Nephew Plc Reduced pressure therapy apparatuses and methods of using same
CN104066990B (en) * 2012-03-07 2017-02-22 凯希特许有限公司 Disc pump with advanced actuator
RU2014138377A (en) 2012-03-20 2016-05-20 СМИТ ЭНД НЕФЬЮ ПиЭлСи REDUCED PRESSURE THERAPY SYSTEM OPERATION MANAGEMENT BASED ON DETERMINING THE THRESHOLD THRESHOLD
US9334858B2 (en) 2012-04-19 2016-05-10 Kci Licensing, Inc. Disc pump with perimeter valve configuration
US9427505B2 (en) 2012-05-15 2016-08-30 Smith & Nephew Plc Negative pressure wound therapy apparatus
CN104364526B (en) * 2012-06-11 2016-08-24 株式会社村田制作所 Aerator
TWI552838B (en) * 2013-06-24 2016-10-11 研能科技股份有限公司 Micro-gas pressure driving apparatus
DE112015000889B4 (en) * 2014-02-21 2023-04-20 Murata Manufacturing Co., Ltd. fan
WO2015178104A1 (en) * 2014-05-20 2015-11-26 株式会社村田製作所 Blower
JP6332461B2 (en) * 2014-08-20 2018-05-30 株式会社村田製作所 Blower
JP6725528B2 (en) 2014-12-22 2020-07-22 スミス アンド ネフュー ピーエルシーSmith & Nephew Public Limited Company Device and method for negative pressure wound therapy
DE102016200256A1 (en) * 2016-01-13 2017-07-13 Robert Bosch Gmbh Pumping device and particle detector with a pumping device
RU175857U1 (en) * 2016-12-28 2017-12-21 федеральное государственное бюджетное научное учреждение "Научно-исследовательский институт перспективных материалов и технологий" Piezoelectric micropump
CN109505764B (en) * 2017-09-15 2021-04-06 研能科技股份有限公司 Gas delivery device
TWI646261B (en) 2017-09-15 2019-01-01 研能科技股份有限公司 Gas delivery device
CN110821804B (en) * 2018-08-10 2021-03-23 研能科技股份有限公司 Driving frequency sweep compensation method of micropump
RU2702624C1 (en) * 2018-10-19 2019-10-09 Федеральное государственное бюджетное учреждение науки Институт проблем управления им. В.А. Трапезникова Российской академии наук Piezoelectric electric-jet converter
GB2606743B (en) 2021-05-19 2023-12-27 Lee Ventus Ltd Microfluidic pump control

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1994019609A1 (en) * 1993-02-23 1994-09-01 Erik Stemme Displacement pump of diaphragm type
DE4422743A1 (en) * 1994-06-29 1996-01-04 Torsten Gerlach Micropump
US20050219288A1 (en) * 2004-04-02 2005-10-06 Jim Vogeley Piezoelectric devices and methods and circuits for driving same
WO2006111775A1 (en) * 2005-04-22 2006-10-26 The Technology Partnership Plc Pump
US20070035213A1 (en) * 2005-08-10 2007-02-15 Alps Electric Co., Ltd. Piezoelectric pump

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5171132A (en) * 1989-12-27 1992-12-15 Seiko Epson Corporation Two-valve thin plate micropump
JP2002227770A (en) * 2001-02-02 2002-08-14 Matsushita Electric Ind Co Ltd Small pump
JP2003139064A (en) * 2001-10-31 2003-05-14 Matsushita Electric Ind Co Ltd Small pump
WO2005012729A1 (en) * 2003-08-04 2005-02-10 Nec Corporation Diaphragm pump and cooling system with the diaphragm pump
JP3951998B2 (en) * 2003-09-29 2007-08-01 ブラザー工業株式会社 Liquid transfer device
JP4383207B2 (en) * 2004-03-01 2009-12-16 アルプス電気株式会社 Fluid pump
CN2818844Y (en) * 2005-08-12 2006-09-20 北京工业大学 Piezo-electric pump without valve
US8211054B2 (en) * 2006-05-01 2012-07-03 Carefusion 303, Inc. System and method for controlling administration of medical fluid
CN200955485Y (en) * 2006-07-14 2007-10-03 北京工业大学 Single-chip-type flow-pipe valve-free piezoelectric pump
CN200989293Y (en) * 2006-10-19 2007-12-12 吉林大学 Micro water spraying propulsion pump
JP4600403B2 (en) * 2007-02-23 2010-12-15 ブラザー工業株式会社 Liquid transfer device

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1994019609A1 (en) * 1993-02-23 1994-09-01 Erik Stemme Displacement pump of diaphragm type
DE4422743A1 (en) * 1994-06-29 1996-01-04 Torsten Gerlach Micropump
US20050219288A1 (en) * 2004-04-02 2005-10-06 Jim Vogeley Piezoelectric devices and methods and circuits for driving same
WO2006111775A1 (en) * 2005-04-22 2006-10-26 The Technology Partnership Plc Pump
US20070035213A1 (en) * 2005-08-10 2007-02-15 Alps Electric Co., Ltd. Piezoelectric pump

Cited By (59)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102939492B (en) * 2010-02-03 2014-08-13 凯希特许有限公司 Singulation of valves
US8371829B2 (en) 2010-02-03 2013-02-12 Kci Licensing, Inc. Fluid disc pump with square-wave driver
CN102939492A (en) * 2010-02-03 2013-02-20 凯希特许有限公司 Singulation of valves
US8646479B2 (en) 2010-02-03 2014-02-11 Kci Licensing, Inc. Singulation of valves
WO2011154634A1 (en) * 2010-06-08 2011-12-15 Centre National De La Recherche Scientifique Ultrasonic traveling wave micropump for liquid
FR2960922A1 (en) * 2010-06-08 2011-12-09 Centre Nat Rech Scient ULTRASONIC PROGRESSIVE WAVE MICRO PUMP FOR LIQUID
JP2016052599A (en) * 2010-10-26 2016-04-14 ソメトリクス,インコーポレイテッド Device and method for opening air duct
US11324626B2 (en) 2010-10-26 2022-05-10 Sommetrics, Inc. Device and method for opening an airway
US10975855B2 (en) 2011-02-03 2021-04-13 The Technology Partnership Plc. Fluid pump including a pressure oscillation with at least one nodal diameter
WO2012104648A1 (en) 2011-02-03 2012-08-09 The Technology Partnership Plc Pump
US20140050604A1 (en) * 2011-02-03 2014-02-20 The Technology Partnership Plc. Pump
US9869659B2 (en) 2011-12-06 2018-01-16 The Technology Partnership Plc. Acoustic sensor
WO2013083978A1 (en) 2011-12-06 2013-06-13 The Technology Partnership Plc Acoustic sensor
US10087923B2 (en) 2012-02-10 2018-10-02 The Technology Partnership Plc. Disc pump with advanced actuator
US11624815B1 (en) 2013-05-08 2023-04-11 Ultrahaptics Ip Ltd Method and apparatus for producing an acoustic field
US11543507B2 (en) 2013-05-08 2023-01-03 Ultrahaptics Ip Ltd Method and apparatus for producing an acoustic field
US11656686B2 (en) 2014-09-09 2023-05-23 Ultrahaptics Ip Ltd Method and apparatus for modulating haptic feedback
US11768540B2 (en) 2014-09-09 2023-09-26 Ultrahaptics Ip Ltd Method and apparatus for modulating haptic feedback
US11204644B2 (en) 2014-09-09 2021-12-21 Ultrahaptics Ip Ltd Method and apparatus for modulating haptic feedback
US11830351B2 (en) 2015-02-20 2023-11-28 Ultrahaptics Ip Ltd Algorithm improvements in a haptic system
US11550432B2 (en) 2015-02-20 2023-01-10 Ultrahaptics Ip Ltd Perceptions in a haptic system
US11276281B2 (en) 2015-02-20 2022-03-15 Ultrahaptics Ip Ltd Algorithm improvements in a haptic system
US12100288B2 (en) 2015-07-16 2024-09-24 Ultrahaptics Ip Ltd Calibration techniques in haptic systems
US11727790B2 (en) 2015-07-16 2023-08-15 Ultrahaptics Ip Ltd Calibration techniques in haptic systems
US11189140B2 (en) 2016-01-05 2021-11-30 Ultrahaptics Ip Ltd Calibration and detection techniques in haptic systems
US11307664B2 (en) 2016-08-03 2022-04-19 Ultrahaptics Ip Ltd Three-dimensional perceptions in haptic systems
US12001610B2 (en) 2016-08-03 2024-06-04 Ultrahaptics Ip Ltd Three-dimensional perceptions in haptic systems
US11714492B2 (en) 2016-08-03 2023-08-01 Ultrahaptics Ip Ltd Three-dimensional perceptions in haptic systems
EP3290211A1 (en) * 2016-09-05 2018-03-07 Microjet Technology Co., Ltd Fluid control device
US10364910B2 (en) 2016-09-05 2019-07-30 Microjet Technology Co., Ltd. Fluid control device
US11067073B2 (en) 2016-09-05 2021-07-20 Microjet Technology Co., Ltd. Fluid control device
US10788028B2 (en) 2016-09-05 2020-09-29 Microjet Technology Co., Ltd. Fluid control device with alignment features on the flexible plate and communication plate
US10697449B2 (en) 2016-09-05 2020-06-30 Microjet Technology Co., Ltd. Fluid control device
US11955109B2 (en) 2016-12-13 2024-04-09 Ultrahaptics Ip Ltd Driving techniques for phased-array systems
US11531395B2 (en) 2017-11-26 2022-12-20 Ultrahaptics Ip Ltd Haptic effects from focused acoustic fields
US11921928B2 (en) 2017-11-26 2024-03-05 Ultrahaptics Ip Ltd Haptic effects from focused acoustic fields
US11360546B2 (en) 2017-12-22 2022-06-14 Ultrahaptics Ip Ltd Tracking in haptic systems
US11704983B2 (en) 2017-12-22 2023-07-18 Ultrahaptics Ip Ltd Minimizing unwanted responses in haptic systems
US11529650B2 (en) 2018-05-02 2022-12-20 Ultrahaptics Ip Ltd Blocking plate structure for improved acoustic transmission efficiency
US11883847B2 (en) 2018-05-02 2024-01-30 Ultraleap Limited Blocking plate structure for improved acoustic transmission efficiency
GB2569417A (en) * 2018-07-31 2019-06-19 Ttp Ventus Ltd Microfluidic drive system
GB2569417B (en) * 2018-07-31 2020-06-17 Ttp Ventus Ltd Microfluidic drive system
US11740018B2 (en) 2018-09-09 2023-08-29 Ultrahaptics Ip Ltd Ultrasonic-assisted liquid manipulation
US11098951B2 (en) 2018-09-09 2021-08-24 Ultrahaptics Ip Ltd Ultrasonic-assisted liquid manipulation
US11378997B2 (en) 2018-10-12 2022-07-05 Ultrahaptics Ip Ltd Variable phase and frequency pulse-width modulation technique
US11550395B2 (en) 2019-01-04 2023-01-10 Ultrahaptics Ip Ltd Mid-air haptic textures
US11842517B2 (en) 2019-04-12 2023-12-12 Ultrahaptics Ip Ltd Using iterative 3D-model fitting for domain adaptation of a hand-pose-estimation neural network
US11374586B2 (en) 2019-10-13 2022-06-28 Ultraleap Limited Reducing harmonic distortion by dithering
US11742870B2 (en) 2019-10-13 2023-08-29 Ultraleap Limited Reducing harmonic distortion by dithering
US11553295B2 (en) 2019-10-13 2023-01-10 Ultraleap Limited Dynamic capping with virtual microphones
US11169610B2 (en) 2019-11-08 2021-11-09 Ultraleap Limited Tracking techniques in haptic systems
US11715453B2 (en) 2019-12-25 2023-08-01 Ultraleap Limited Acoustic transducer structures
US12002448B2 (en) 2019-12-25 2024-06-04 Ultraleap Limited Acoustic transducer structures
US11816267B2 (en) 2020-06-23 2023-11-14 Ultraleap Limited Features of airborne ultrasonic fields
US11886639B2 (en) 2020-09-17 2024-01-30 Ultraleap Limited Ultrahapticons
EP4006367A1 (en) 2020-11-27 2022-06-01 European Space Agency Gas bearing system
US12077322B2 (en) 2020-11-27 2024-09-03 European Space Agency Gas bearing system
WO2024052578A1 (en) 2022-09-11 2024-03-14 Bioliberty Ltd Soft robotic assistive device
WO2024165863A1 (en) 2023-02-08 2024-08-15 Foster & Freeman Limited A volatile substance sampling device

Also Published As

Publication number Publication date
JP2011513649A (en) 2011-04-28
JP5335003B2 (en) 2013-11-06
RU2459114C2 (en) 2012-08-20
EP2268923B1 (en) 2019-01-09
CN101986787A (en) 2011-03-16
AU2009223958B2 (en) 2012-01-19
US20110081267A1 (en) 2011-04-07
RU2010141978A (en) 2012-04-20
GB0804739D0 (en) 2008-04-16
EP2268923A1 (en) 2011-01-05
US8734131B2 (en) 2014-05-27
CA2718390A1 (en) 2009-09-17
AU2009223958A1 (en) 2009-09-17

Similar Documents

Publication Publication Date Title
US8734131B2 (en) Pump
US20210164464A1 (en) Blower
JP4795428B2 (en) pump
EP3080460B1 (en) Acoustic-resonance fluid pump
EP2438301B1 (en) Fluid disc pump
US8821134B2 (en) Fluid disc pump
JP2009529119A5 (en)
JP2009529119A (en) Fluid energy transfer device
US20150023821A1 (en) Disc pump with advanced actuator
CN104066990A (en) Disc pump with advanced actuator
JP4466236B2 (en) Transducer
US10260495B2 (en) Blower with a vibrating body having a restraining plate located on a periphery of the body
WO2011097090A2 (en) Energy transfer fluid diaphragm and device
JP2023538907A (en) Drive assemblies, motors, and terminals
WO2019130853A1 (en) Pump and fluid control device
WO2019073739A1 (en) Pump and fluid control device
SU1721311A1 (en) Vibration pump
SU1721310A1 (en) Vibration pump
JPH0449874A (en) Ultrasonic wave motor

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 200980109036.0

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 09720214

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 2010550268

Country of ref document: JP

Ref document number: 2009223958

Country of ref document: AU

Ref document number: 1925/MUMNP/2010

Country of ref document: IN

WWE Wipo information: entry into national phase

Ref document number: 2718390

Country of ref document: CA

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2009223958

Country of ref document: AU

Date of ref document: 20090313

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 2009720214

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2010141978

Country of ref document: RU

WWE Wipo information: entry into national phase

Ref document number: 12922589

Country of ref document: US