Patent Grant
11401974
The present disclosure relates to a flow therapy apparatus for delivering gas to patients.
Breathing assistance apparatuses are used in various environments such as hospital, medical facility, residential care, or home environments to deliver a flow of gas to users or patients.
The applicant has identified explosion safety risk if some gases, such as high concentration oxygen for example, come into contact with electrical and/or electronics components in breathing assistance apparatuses.
Accordingly, it would be desirable to provide an apparatus for delivering a flow of gas that isolates gas flow from electrical and/or electronic components, and/or at least provides the public with a useful choice.
Thus, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, a bearing mount for supporting a bearing is disclosed, the bearing mount comprising:
an annular body,
a collar extending concentrically with the annular body and outwardly from the annular body, the collar having a narrower outer diameter than an outer diameter of the annular body forming a recess between the annular body and the collar,
a central bore extending through the annular body and the collar, the central bore having a wall and a ledge extending radially inwardly from the wall of the central bore,
the ledge being disposed near one end of the central bore and the collar being disposed near another end of the central bore,
wherein the bearing mount is arranged to receive the bearing in the central bore such that the bearing is radially supported by the inner surface of the bearing mount, and axially supported by the ledge, and
wherein at least part of the bearing mount is arranged to flex or resiliently deform when a force is applied to the bearing mount to reduce the amount of the force that is translated to the bearing.
In some configurations, at least part of the bearing mount is arranged to flex or resiliently deform such that the collar moves in a direction generally parallel to the bearing rotational axis when the force is applied to the bearing mount.
In some configurations, at least part of the bearing mount is arranged to flex or resiliently deform when a force is applied to the bearing mount such that the force translated to the bearing retained in the central bore remains generally constant as the force applied to the bearing mount increases beyond a threshold.
In some configurations, the recess provides an area into which the annular body may flex or resiliently deform when a force is applied to the bearing mount.
In some configurations, the annular body extends outwardly at a non-perpendicular angle relative to the bearing rotational axis.
In some configurations, the annular body comprises a rim at or near the outer periphery of the annular body.
In some configurations, the ledge is substantially perpendicular to the bearing rotational axis.
In some configurations, at least the annular body comprises a silicone material.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, a blower for an apparatus for delivering a flow of gas is disclosed, the blower comprising:
a casing,
an impeller,
a motor for driving the impeller, the motor including:
a rotatable shaft,
a rotor connected to the rotatable shaft, and
a stator,
a bearing arranged to allow rotation of the rotatable shaft relative to the casing, and
a bearing mount as disclosed above, wherein the bearing mount is arranged to support the bearing.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, a blower for an apparatus for delivering a flow of gas is disclosed, the blower comprising:
a casing including a casing ledge and a flexible or resilient member,
a stator including a first stator ledge and a second stator ledge,
wherein the casing ledge supports the first stator ledge, and the flexible or resilient member supports the second stator ledge.
In some configurations, the blower further comprises:
a casing cap operatively connected to the casing, and
a vibration isolating member located between the stator and the casing cap arranged to bias the stator in a direction towards the first stator ledge.
In some configurations, the vibration isolating member is compressible.
In some configurations, the vibration isolating member is or comprises an elastomeric material.
In some configurations, the elastomeric material is silicone.
In some configurations, the flexible member is configured to flex beyond a periphery of the stator to allow removal of the stator from the casing.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, a blower for an apparatus for delivering a flow of gas is disclosed, the blower comprising:
a casing including:
a casing cap, wherein the casing cap includes a collar defining a bearing mount recess arranged to receive a bearing mount,
wherein the bearing mount is arranged to support a bearing,
a motor chamber, wherein a first side of the motor chamber is defined by the casing cap, and a second side of the motor chamber is defined by a partition,
wherein the partition is arranged to be connected to the casing cap, and
wherein connection of the casing cap and the partition causes a preload force to be exerted on the bearing via the bearing mount.
In some configurations, the at least part of the bearing mount is arranged to flex or resiliently deform such that another part of the bearing mount moves in a direction generally parallel to the bearing rotational axis when the force is applied to the bearing mount.
In some configurations, at least part of the bearing mount is arranged to flex or resiliently deform when a force is applied to the bearing mount such that the force translated to the bearing retained in the central bore remains generally constant as the force applied to the bearing mount increases beyond a threshold.
In some configurations, at least part of the bearing mount is arranged to flex or resiliently deform such that another part of the bearing mount moves in a direction generally parallel to the bearing rotational axis when the force is applied to the bearing mount.
In some configurations, at least part of the bearing mount is arranged to flex or resiliently deform when a force is applied to the bearing mount such that the force translated to the bearing retained in the central bore remains generally constant as the force applied to the bearing mount increases beyond a threshold.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising:
a controller,
a housing defining a gasflow passage,
a motor with an impeller to deliver gas through the gasflow passage,
a flexible printed circuit board electrically connected to the motor for electrically connecting the motor to the controller, and a sensor system, wherein the flexible printed circuit board also electrically connects the sensor system to the controller.
In some configurations, the flexible printed circuit board has signal tracks electrically connecting the sensor system to the controller and motor tracks electrically connecting the motor to the controller, wherein the signal tracks are positioned over the top of the motor tracks with a substrate between the signal tracks and motor tracks.
In some configurations, the flexible printed circuit board has signal tracks electrically connecting the sensor system to the controller and motor tracks electrically connecting the motor to the controller, wherein the signal tracks are positioned towards one side of the flexible printed circuit board and the motor tracks are positioned towards another side of the flexible printed circuit board with a substrate between the signal tracks and motor tracks.
In some configurations, the apparatus further comprises a space or gap formed in the substrate between the signal traces and the motor traces.
In some configurations, the apparatus further comprises a seal that provides a seal around the flexible printed circuit board where it exits the housing.
In some configurations, an end of the flexible printed circuit board is receivable by an edge connector of the controller.
In some configurations, the flexible printed circuit board has one or more stiffened regions to assist with attaching the flexible printed circuit board to other components.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising:
a controller,
a sensor system,
a housing defining a gasflow passage,
a motor with an impeller to deliver gas through the gasflow passage,
a flexible printed circuit board having a body and two branches extending from the body, one of the branches electrically connected to the motor for electrically connecting the motor to the controller, and the other of the branches electrically connected to the sensor system for electrically connecting the sensor system to the controller.
In some configurations, the flexible printed circuit board has signal tracks electrically connecting the sensor system to the controller and motor tracks electrically connecting the motor to the controller, wherein, at the body, the signal tracks are positioned towards one side of the flexible printed circuit board and the motor tracks are positioned towards another side of the flexible printed circuit board with a substrate between the signal tracks and motor tracks.
In some configurations, the apparatus further comprises a space or gap formed in the substrate between the signal traces and the motor traces.
In some configurations, the apparatus further comprises a seal that provides a seal around the flexible printed circuit board where it exits the housing.
In some configurations, an end of the flexible printed circuit board is receivable by an edge connector of the controller.
In some configurations, the flexible printed circuit board has one or more stiffened regions to assist with attaching the flexible printed circuit board to other components.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising: a housing defining a gasflow passage,
a motor in the housing, the motor including a stator including a laminated stator core and windings, and
a shield to pneumatically isolate the stator from the gasflow passage.
In some configurations, gas, which is or comprises oxygen, flows through the gasflow path.
In some configurations, gas is isolated from the stator.
In some configurations, the shield is a substantially annular component.
In some configurations, the shield is selectively removable.
In some configurations, the shield is a separately manufactured component that is later assembled with stator.
In some configurations, the stator is overmoulded with the shield, the shield comprising an overmould material.
In some configurations, the stator further includes one or more guards that insulate the windings from the stator core.
In some configurations, the guards are configured such that overmoulded material lies at least partially between the stator core and the windings.
In some configurations, the stator core comprises an annular portion and a plurality of stator teeth extending from the annular portion, the windings being wound around each of the stator teeth, each stator tooth having an inwardly facing tooth face.
In some configurations, the overmould material further covers the tooth faces of the stator teeth.
In some configurations, the one or more guards have retaining features for retaining the stator within a housing, and wherein the overmould material does not cover the retaining features.
In some configurations, the retaining features include a face of the guard that is configured to cooperate with one or more ledges and/or clips on the housing.
In some configurations, the retaining features are configured to prevent lateral and/or axial motion of the stator.
In some configurations, the overmould material covers all surfaces of the stator except for a portion of the guard or guards.
In some configurations, the motor further comprises an electrical connection on the stator, the electrical connection being at least partially covered by the overmould material.
In some configurations, the electrical connection is a PCB that is electrically connected to the windings.
In some configurations, the PCB is a flexible printed circuit, and wherein the flexible printed circuit includes a first portion connected to the windings and a second portion that extends from the motor, and wherein the first portion is covered by the overmould material.
In some configurations, the first portion is a stiffer section that the adjoining portion of the flexible printed circuit.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising:
a housing defining a gasflow passage, the gas flowing through the gasflow passage being a high concentration oxygen gas,
a motor including a stator including a laminated stator core and windings, and
an elastomeric shield to pneumatically isolate the windings from the gasflow passage.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising:
a controller,
a housing defining a gasflow passage,
a motor with an impeller to deliver gas through the gasflow passage,
a flexible printed circuit electrically connected to the motor for electrically connecting the motor to the controller.
In some configurations, the apparatus further comprises a sensor system, wherein the flexible printed circuit also electrically connects the sensor system to the controller.
Optionally in some configurations, the flexible printed circuit has signal traces electrically connects the sensor system to the controller and motor traces electrically connecting the motor to the controller, wherein the signal traces are positioned over the top of the motor traces with a substrate between the sensor traces and motor traces.
In some configurations, the flexible printed circuit has signal traces electrically connecting the sensor system to the controller and motor traces electrically connecting the motor to the controller, wherein the signal traces are positioned towards one side of the flexible printed circuit and the motor traces are positioned towards another side of the flexible printed circuit with a substrate between the signal traces and motor traces. Optionally a portion of substrate may be provided or may be present between the motor traces and the signal traces. A portion of substrate may be located between the adjacent motor traces. Adjacent motor traces may be disposed on separate layers of the flexible printed circuit. Alternatively an air gap may be located between motor traces and/or the signal traces that are disposed on the same layer of the printed circuit board.
In some configurations, the apparatus further comprises a seal that provides a seal around the flexible printed circuit where it exits the housing.
In some configurations, an end of the flexible printed circuit is receivable by an edge connector of the controller.
In some configurations, the flexible printed circuit has one or more stiffened regions to assist with attaching the flexible printed circuit to other components.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising:
a controller,
a sensor system,
a housing defining a gasflow passage,
a motor with an impeller to deliver gas through the gasflow passage,
a flexible printed circuit having a body and two branches extending from the body, one of the branches electrically connected to the motor for electrically connecting the motor to the controller, and the other of the branches electrically connected to the sensor system for electrically connecting the sensor system to the controller.
Optionally in some configurations, the flexible printed circuit has signal traces electrically connecting the sensor system to the controller and motor traces electrically connecting the motor to the controller, wherein, at the body, the signal traces are positioned over the top of the motor traces with a substrate between the signal traces and motor traces.
In some configurations, the flexible printed circuit has signal traces electrically connecting the sensor system to the controller and motor traces electrically connecting the motor to the controller, wherein, at the body, the signal traces are positioned towards one side of the flexible printed circuit and the motor traces are positioned towards another side of the flexible printed circuit. Optionally a substrate or a portion of substrate is positioned between the signal traces and motor traces.
In some configurations, the apparatus further comprises a seal that provides a seal around the flexible printed circuit where it exits the housing.
In some configurations, an end of the flexible printed circuit is receivable by an edge connector of the controller.
In some configurations, the flexible printed circuit has one or more stiffened regions to assist with attaching the flexible printed circuit to other components.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising:
a housing defining a gasflow passage,
an electrical component in the housing, and
an elastomeric shield to pneumatically isolate the electrical component from the gasflow passage.
In some configurations, the electrical component comprises a motor with windings and an impeller to deliver gas through the gasflow passage, wherein the windings of the motor are pneumatically isolated from the gasflow passage.
In some configurations, the shield is a substantially annular component.
In some configurations, the shield is selectively removable.
In some configurations, the shield is overmoulded with the electrical component.
In some configurations, the shield is a separately manufactured component that is later assembled with the electrical component.
In some configurations, gas that is or comprises oxygen flows through the gasflow path.
In some configurations, the gas is isolated from the electrical component.
Additionally, in accordance with certain features, aspects and advantages of at least one of the embodiments disclosed herein, an apparatus for delivering a flow of gas is disclosed, the apparatus comprising:
a housing defining a gasflow passage, the gas flowing through the gasflow passage being a high concentration oxygen gas,
a motor with windings and an impeller to deliver gas through the gasflow passage, and
an elastomeric shield to pneumatically isolate the windings from the gasflow passage. Features from one or more embodiments may be combined with features of one or more other embodiments. Additionally, more than one embodiment may be used together during a process of respiratory support of a patient.
In some configurations the elastomeric shield may be made from at least one of a thermoplastic, thermoset or silicone material.
In one configuration the elastomeric shield is formed from a PBT (polybutylene terephthalate) material.
In some configurations the PCB as described herein is a flexible printed circuit (FPC).
In some configurations the FPC as described herein is a multi-layer structure. In one exemplary configuration the FPC may include at least three layers each support a conductive track and three insulation layers, and one optional ground layer.
In some configurations the FPC may include flexible or weakened regions to allow for bending about at least one axis. In some configurations the flexible or weakened regions may allow for bending about 2 axes.
In some configurations the apparatus for delivering gas may include a grommet positioned on or adjacent or in contact with the FPC.
In some configurations the grommet provides a seal between components when assembled. The grommet is preferably coupled to a portion of the FPC. The grommet provides a seal where the FPC leaves the housing where the motor is located.
The term “comprising” as used in this specification means “consisting at least in part of”. When interpreting each statement in this specification that includes the term “comprising”, features other than that or those prefaced by the term may also be present. Related terms such as “comprise” and “comprises” are to be interpreted in the same manner.
It should be understood that alternative embodiments may comprise any or all combinations of two or more of the parts, elements or features illustrated, described or referred to in this specification.
This invention may also be said broadly to consist in the parts, elements and features referred to or indicated in the specification of the application, individually or collectively, and any or all combinations of any two or more said parts, elements or features.
To those skilled in the art to which the invention relates, many changes in construction and widely differing embodiments and applications of the invention will suggest themselves without departing from the scope of the invention as defined in the appended claims. The disclosures and the descriptions herein are purely illustrative and are not intended to be in any sense limiting. Where specific integers are mentioned herein which have known equivalents in the art to which this invention relates, such known equivalents are deemed to be incorporated herein as if individually set forth.
Specific embodiments and modifications thereof will become apparent to those skilled in the art from the detailed description herein having reference to the figures that follow, of which:
A flow therapy apparatus 10 is shown in
A patient breathing conduit 16 is coupled to a gasflow output 344 in the housing 100 of the flow therapy apparatus 10, and is coupled to a patient interface 17 such as a nasal cannula with a manifold 19 and nasal prongs 18. Additionally, or alternatively, the patient breathing conduit 16 could be coupled to a face mask. Additionally or alternatively, the patient breathing conduit could be coupled to a nasal pillows mask, and/or a nasal mask, and/or a tracheostomy interface, or any other suitable type of patient interface. The gasflow, which may be humidified, that is generated by the flow therapy apparatus 10 is delivered to the patient via the patient breathing conduit 16 through the cannula 17. The patient breathing conduit 16 can have a heater wire 16a to heat gasflow passing through to the patient. The heater wire 16a is under the control of the controller 13. The patient breathing conduit 16 and/or patient interface 17 can be considered part of the flow therapy apparatus 10, or alternatively peripheral to it. The flow therapy apparatus 10, breathing conduit 16, and patient interface 17 together form a flow therapy system.
General operation of a flow therapy breathing apparatus 10 will be known to those skilled in the art, and need not be described in detail here. However, in general terms the controller 13 controls the flow generator 11 to generate a gasflow of the desired flow rate, controls one or more valves to control the mix of air and oxygen or other alternative gas, and controls the humidifier 12 if present to humidify the gasflow and/or heat the gasflow to an appropriate level. The gasflow is directed out through the patient breathing conduit 16 and cannula 17 to the patient. The controller 13 can also control a heating element in the humidifier 12 and/or the heating element 16a in the patient breathing conduit 16 to heat the gas to a desired temperature that achieves a desired level of therapy and/or comfort for the patient. The controller 13 can be programmed with or can determine a suitable target temperature of the gasflow.
Operation sensors 3a, 3b, 3c, 20, 25 such as flow, temperature, humidity, and/or pressure sensors can be placed in various locations in the flow therapy apparatus 10 and/or the patient breathing conduit 16 and/or cannula 17. Output from the sensors can be received by the controller 13, to assist it to operate the flow therapy apparatus 10 in a manner that provides optimal therapy. In some configurations, providing optimal therapy includes meeting a patient's inspiratory demand. The apparatus 10 may have a transmitter and/or receiver 15 to enable the controller 13 to receive 8 signals from the sensors and/or to control the various components of the flow therapy apparatus 10, including but not limited to the flow generator 11, humidifier 12, and heater wire 16a, or accessories or peripherals associated with the flow therapy apparatus 10. Additionally, or alternatively, the transmitter and/or receiver 15 may deliver data to a remote server or enable remote control of the apparatus 10.
The flow therapy apparatus 10 may comprise a high flow therapy apparatus. As used herein, “high flow” therapy refers to administration of gas to the airways of a patient at a relatively high flow rate that meets or exceeds the peak inspiratory demand of the patient. The flow rates used to achieve “high flow” may be any of the flow rates listed below. For example, in some configurations, for an adult patient ‘high flow therapy’ may refer to the delivery of gases to a patient at a flow rate of greater than or equal to about 10 litres per minute (10 LPM), such as between about 10 LPM and about 100 LPM, or between about 15 LPM and about 95 LPM, or between about 20 LPM and about 90 LPM, or between about 25 LPM and about 85 LPM, or between about 30 LPM and about 80 LPM, or between about 35 LPM and about 75 LPM, or between about 40 LPM and about 70 LPM, or between about 45 LPM and about 65 LPM, or between about 50 LPM and about 60 LPM. In some configurations, for a neonatal, infant, or child patient ‘high flow therapy’ may refer to the delivery of gases to a patient at a flow rate of greater than 1 LPM, such as between about 1 LPM and about 25 LPM, or between about 2 LPM and about 25 LPM, or between about 2 LPM and about 5 LPM, or between about 5 LPM and about 25 LPM, or between about 5 LPM and about 10 LPM, or between about 10 LPM and about 25 LPM, or between about 10 LPM and about 20 LPM, or between about 10 LPM and 15 LPM, or between about 20 LPM and 25 LPM. A high flow therapy apparatus with an adult patient, a neonatal, infant, or child patient, may deliver gases to the patient at a flow rate of between about 1 LPM and about 100 LPM, or at a flow rate in any of the sub-ranges outlined above. Gases delivered may comprise a percentage of oxygen. In some configurations, the percentage of oxygen in the gases delivered may be between about 20% and about 100%, or between about 30% and about 100%, or between about 40% and about 100%, or between about 50% and about 100%, or between about 60% and about 100%, or between about 70% and about 100%, or between about 80% and about 100%, or between about 90% and about 100%, or about 100%, or 100%.
As used herein, a ‘high concentration oxygen gas’ is a gas in which air may be supplemented with oxygen.
High flow therapy has been found effective in meeting or exceeding the patient's inspiratory demand, increasing oxygenation of the patient and/or reducing the work of breathing. Additionally, high flow therapy may generate a flushing effect in the nasopharynx such that the anatomical dead space of the upper airways is flushed by the high incoming gas flows. This creates a reservoir of fresh gas available of each and every breath, while minimising re-breathing of carbon dioxide, nitrogen, etc.
The patient interface may be a non-sealing interface to prevent barotrauma (e.g. tissue damage to the lungs or other organs of the respiratory system due to difference in pressure relative to the atmosphere). The patient interface may be a nasal cannula with a manifold and nasal prongs, and/or a face mask, and/or a nasal pillows mask, and/or a nasal mask, and/or a tracheostomy interface, or any other suitable type of patient interface.
As shown in
As shown in
The main housing upper chassis 102 has a peripheral wall arrangement 106. The peripheral wall arrangement defines a humidifier or liquid chamber bay 108 for receipt of a removable liquid chamber 300. The removable liquid chamber 300 contains a suitable liquid such as water for humidifying gases that will be delivered to a patient. A floor portion 136 of the liquid chamber bay 108 has a recess 138 to receive a heater arrangement such as a heater plate 140 or other suitable heating element(s) for heating liquid in the liquid chamber 300 for use during a humidification process.
As shown in
The tube 264 forming the gasflow passage extends upwardly through a downward outer extension tube or conduit 133 that is integrally formed with the upper housing chassis 102. A soft seal such as an O-ring seal (not shown) is located between the exterior of the gasflow passage tube 264 and the interior of downward outer extension tube or conduit 133, to provide a seal between the components when assembled. In other configurations, the gasflow passage tube 264 and the downward extension tube 133 could be configured to be fitted together via other arrangements while still providing for a seal between the components when assembled.
The configuration is such that if there is any leaking of gas from the motor or gasflow path following the motor via any seals, the gas will vent to atmosphere rather than ingressing into the interior of the main housing that contains the control boards and other electrical components as described below. The electrical components and electronics boards in the housing are pneumatically isolated from the gasflow path. The only way for gas to leak into the portion of the main housing 100 that contains the electronics boards and other electrical components will be if there is a physical crack in the housing 100 or another physical component
In the motor and/or sensor module 400, the pressure is lower before/upstream of the motor impeller, and the pressure is higher after/downstream of the motor impeller. An electrical connection will be provided for the motor upstream of the motor impeller, in the lower pressure region. If there is a failure in the housing in the portion near the electrical connection, air will be sucked into the low pressure side.
In an alternative configuration, the motor recess comprising items 252, 254, 256, 258, 260, 264 may be separately formed from the lower chassis 202. The motor assembly including the recess may be insertable into the recess opening 251 and attachable to the lower chassis 202. Upon insertion of the motor and/or sensor module 400 and recess into the lower chassis 202, the gasflow passage tube 264 will extend through the downward extension tube 133 and be sealed by the soft seal.
In the form shown, the recess 250 comprises a recess opening in a bottom wall of the housing. Alternatively, the recess opening could be in a different part of the housing, such as a side, front, or top of the housing.
The described configuration provides a chamber shaped to receive a motor and/or sensor module 400 as described below with reference to
With reference to
The apparatus 10 comprises a connection arrangement 320 for fluid coupling of the liquid chamber 300 to the apparatus 10. The connection arrangement 320 comprises a gases outlet port 322 that is in fluid communication, via a fixed L shaped elbow 324, with the gasflow passage from the flow generator 11.
The connection arrangement 320 further comprises a gases inlet port 340 (humidified gases return) that is embodied in a removable elbow 342. The removable elbow 342 has a patient outlet port 344 for coupling to the patient breathing conduit 16 to deliver gases to the patient interface 17. The gases outlet port 322, gases inlet port 340, and patient outlet port 344 each comprise soft seals such as O-ring seals (not shown) to provide a sealed gases passageway between the apparatus 10, the liquid chamber 300, and the patient breathing conduit 16.
The apparatus 10 has air and oxygen (or alternative auxiliary gas) inlets in fluid communication with the flow generator 11 to enable the flow generator 11 to deliver air, oxygen (or alternative auxiliary gas), or a suitable mixture thereof to the liquid chamber 300 and thereby to the patient. In some configurations, the gas comprises a blend of oxygen and ambient air. The apparatus 10 may have the arrangement shown in
As shown in
One or both of the electronics boards 272 are in electrical communication with the electrical components of the apparatus 10, including the display unit and user interface 14, flow generator 11, oxygen valve 362, and the heater plate 140 to operate the flow generator 11 to provide the desired flow rate of gas, operate the humidifier 12 to humidify and heat the gasflow to an appropriate level, and supply appropriate quantities of oxygen (or in alternative configurations quantities of an alternative auxiliary gas) to the gasflow.
The electronics boards 272 are in electrical communication with a connector arrangement 274 projecting from the rear wall 122 of the upper housing chassis 102. The connector arrangement 274 may be coupled to a nurse alarm, pulse oximetry port, and/or other suitable accessories. The electronics boards 272 are also in electrical communication with an electrical connector 276 that is also provided in the rear wall 122 of the upper housing chassis 102 to provide mains or battery power to the components of the apparatus 10. The electronics boards 272 are also in electrical communication with an electrical connector 278 for the removable elbow 342.
As mentioned above, operation sensors, such as flow, temperature, humidity, and/or pressure sensors can be placed in various locations in the flow therapy apparatus 10 and/or the patient breathing conduit 16 and/or cannula 17. The electronics boards 272 will be in electrical communication with those sensors. Output from the sensors can be received by the controller 13, to assist the controller 13 to operate the flow therapy apparatus 10 in a manner that provides optimal therapy, including meeting inspiratory demand.
As outlined above, the electronics boards 272 and other electrical and electronic components are pneumatically isolated from the gasflow path, thereby reducing or avoiding any explosion risk that could otherwise occur if there was not that isolation.
Various aspects of the device will now be described in more detail.
In the form shown in
The sensing layer comprises a gasflow path with one or more sensors, the gasflow path arranged to deliver gas to the outlet port of the housing.
The flow generator (blower) 11 will now be described in more detail. The flow generator 11 has a body 408 that defines an impeller chamber that contains a motor 402 that drives an impeller 20031. The motor 402 could be any suitable gas blower motor, and may for example be a motor and impeller assembly of the type described in published PCT specification WO2013/009193 and shown in
The motor 402 is a brushless DC motor operated using sensorless vector control (also termed ‘field oriented control’) controlled by the electronics board 272, for example, via a flexible printed circuit (FPC) 10001, which is described in more detail below. The control can be tuned to suit a low inertia impeller. The central hub 20032 of the impeller 20031 is engaged with a shaft 20060 that extends from the motor 402. Mounted to the shaft is a plurality of, preferably small, magnetic segments to form a rotor 20062. In one embodiment the magnet is 20 mm in diameter, but more generally the diameter could be less than 20 mm and preferably between 10 mm to 15 mm. The magnet volume is less than 1600 mm3 and can be between 500 mm3 and 1600 mm3. Surrounding the rotor 20062 is a laminated stator having a plurality of poles 20063 and windings 20068. The windings 20068 are selectively energised by the controller 13 via the FPC 10001 to facilitate rotation of the rotor, and therefore the shaft 20060 and impeller 20031, about the central axis defined by the centreline of the shaft 20060. In an alternate configuration, rather than an FPC, one or more rigid-flexible circuit/s or one or more flexible flat cable/s could be used.
A gases outlet 406 is in fluid communication with a gases inlet of the outlet gasflow path and sensing layer 420, which is stacked on top of the motor 402. This layer 420 comprises a body 422 which comprises a plurality of mounting legs 425 that can be inserted into a plurality of mounting slots (not shown) of the base 403 to secure the body 422 to the base 403. In other configurations, other structures or arrangements may be used to secure the body 422 to the base 403, including but not limited to fasteners, clips, or quick release arrangements. In one configuration, the body 422 defines a gasflow path that couples the gases outlet 406 with the gases inlet of the gasflow path and sensing layer 420. An alternative configuration such as but not limited to a coupling tube could be used to couple the gases outlet 406 with that gases inlet.
The body 422 defines a lower portion 426 of a sensing and gasflow path. The cover layer 440 has a body 442 that defines the upper portion 446 of the sensing and gasflow path, with the shape of the upper and lower portions 426, 446 corresponding substantially to each other.
As shown in
A gasflow outlet port 452 extends vertically through the body 442 of the cover layer 440, and is located at or adjacent an opposite exit end of the linear elongate portion 428, 448 of the gasflow path. The gas outlet port 452 is in fluid communication with an upper portion of the motor recess 250, which in turn is in fluid communication with the gasflow passage. Again, due to the wall 252 and ceiling 262 configuration of the recess 250, if there is gas leakage from the motor/sensor module 400, that will be vented to atmosphere rather than entering the portion of the main housing 100 that contains the bulk of the electronics and control equipment. The recess 250 may comprise spacer(s), such as lugs that protrude downwardly from ceiling 262 as shown in
It can be seen from
As shown in
One or both of the electronics boards 272 will be in electrical communication or coupled with the sensors to process information received from the sensors and operate the apparatus 10 based on the information received from the sensors.
The FPC 10001 has a body 10015 and two branches extending from the body. The branches are described with reference to the drawings in more detail below. In summary, one of the branches is electrically connected to the motor 402 for electrically connecting the motor to the electronics boards 272 or other parts of the controller 13 and the other of the branches electrically connected to the sensor system for electrically connecting the sensor system to the electronics boards 272 or other parts of the controller 13.
The FPC 10001 has an arcuate, circular, or semi-circular first end 10003 that electrically connects to the motor 402. The arcuate, circular, or semi-circular first end 10003 may have one or more fingers 10005. In the embodiment shown, the FPC 10001 has three traces that electrically connect to the motor 402. An adjacent portion 10007 of the FPC 10001 extends radially from the arcuate, circular, or semi-circular first end 10003, which then smoothly transitions into a connecting section 10011. In the embodiment shown the connecting section is an arcuate section that closely follows the shape of the flow generator. In an alternative embodiment, the arcuate section may be another shape, such as a straight section. One branch of FPC 10001 is formed by the connecting section 10011, adjacent portion 10007, and first end 10003. The connecting section 10011 may be a stiffer section that the adjoining portion of the FPC.
The FPC 10001 also electrically connects the sensing PCB 456 to the apparatus. In particular, the FPC 10001 electrically connects the sensing PCB 456 to the electronics boards 272. The FPC 10001 has a branch 10013 with a plurality of traces that electrically connect to the sensing PCB 456. The FPC 10001 includes at least two traces. More preferably the FPC includes at least four traces. In one embodiment, the plurality of traces is nine traces. The end of the branch 10013 is formed as a narrow extension 10025 for being received by the sensing PCB 456.
The branch 10013 and connecting section 10011 join together to lead all twelve traces to the electronics board 272. It will be appreciated that the number of traces in the FPC 10001 will depend on the signals and data that is required to be transmitted by the sensing printed circuit board (PCB) 456 or 2200.
In one embodiment, the FPC 10001 is configured with the eight signal traces being positioned towards one side of the ribbon and the three motor traces on the other side of the ribbon. An advantage of this embodiment is that the motor traces and signal traces are spaced apart from each other and cross-talk between the traces is eliminated, or at least reduced. In another embodiment, the FPC 10001 is configured with the signal traces being positioned over the top of the three motor traces. In such an embodiment, the FPC 10001 has a layer of polyimide or other substrate between the traces.
The end of the FPC 10001 includes an opposing end 10017 that connects to electronic boards 272. The opposing end 10017 is formed as two parallel tags 10019 for being received by an edge connector of the electronic boards 272 or other parts of the controller 13. The end of the FPC 10001 also has an extension 10021. Extension 10021 is a pull tab so a user can remove the FPC from the electronic boards easily (e.g. for maintenance).
The FPC 10001 may have one or more stiffened regions to assist with attaching the FPC 10001 to other components. The stiffened regions may be formed as tags or ears or may simply be a stiffer part of the ribbon. The stiffened regions are thickened regions of the FPC. For example particular areas e.g. areas requiring strengthening may be thicker areas. The thickened areas or regions of the FPC are stiffer than other areas. Alternatively stiffened areas of the FPC 10001 may be thicker regions of the FPC that can be achieved by depositing additional material within those specific regions. The additional material may be FR4 material or additional polyamide material or polyimide material. The stiffened regions can have any suitable shape.
The FPC 10001 also includes meshed ground plane. An advantage of the meshed ground plane is that it has some flexibility compared to a solid ground plane. However, the ground plane may be a solid plane in some embodiments.
The apparatus may have one FPC 10001 that electrically connects the sensors and motor to the control board as described and shown in
In another example embodiment the FPC 10001 comprises a plurality of signal traces and a plurality of motor traces. In this example the FPC 10001 comprises a total of eight sensor signal traces and three motor traces. The three motor traces correspond to each phase of the motor 402 (i.e. a three phase motor has three phases and hence each motor signal line corresponds to each phase of the motor). Preferably the FPC also includes a ground plane or a ground track. Alternatively any other suitable configuration for ground may be utilised. There in this example the FPC 10001 comprises eleven traces.
The shape of the FPC 10001 shown in
With reference to
The shield 10027 is a substantially annular component. When viewed from below, the shield completely covers the motor and part of the FPC 10001. In an alternative embodiment, the shield may not completely cover the motor from below, provided the shield isolates the windings and other electrical components. The shield 10027 fits snuggly around the motor and in particular, the windings 20068. The shield 10027 substantially encapsulates the motor to prevent or at least substantially inhibit oxygen ingress into the motor near the windings. This helps to reduce fire risk due to oxygen ingress into an area that can cause sparks due to short circuit or arcing. In some configurations the shield 10027 may completely encapsulate the motor windings. In some configurations the windings may be substantially sealed or isolated from air/oxygen.
The shield 10027 may be overmoulded onto the motor 402 as part of the manufacturing process. In an alternative embodiment, the shield 10027 may be formed, for example by moulding, as a separate component and then assembled with the motor 402. In this alternative embodiment, the shield may be formed as two or more parts that are assembled and sealed such that the electrical components of the motor 402 are pneumatically isolated from the gases from the gasflow path. The two or more components may be plastic components.
The shield 10027 has a tab 10029 for receiving the FPC 10001. The shield may be overmoulded onto the FPC as part of the manufacturing process. The overmould material flows into the gaps to encapsulate the FPC 10001. In an alternative embodiment, the shield may be formed, for example by moulding, as a separate component and then assembled with the FPC. The FPC 10001 also includes an extension 10023 that extends substantially upwardly and includes a bent section to direct upwardly to connect at least the motor traces to the control board e.g. control board 272. Alternatively the extension 10023 may connect to the sensing traces or a sensing PCB.
The shield 10027 may also act as a vibration isolator. The shield 10027 is configured to absorb vibrations caused by movement of the impeller or of other components of the motor during operation. The absorption of vibrations can mitigate rattling of the motor inside of the sub-assembly housing, which in turn can reduce noise emitted by the motor 402. The absorption of vibrations can also mitigate material fatigue on various components of the motor and/or sensor module 400. The shield 10027 may be constructed from a silicone material. In other configurations, other resilient materials including but not limited to acrylic resins and polyurethane resins might be used. In some configurations the shield may comprise an overmoulded material such as a thermoplastic or thermoset or silicone material. Preferably the material is an inert material that does not react to high oxygen concentrations. In one example the shield may be formed from PBT material (polybutylene terephthalate). Alternatively the shield material may be HDPE material or a nylon material.
In an alternative configuration, the vibration isolation properties of the shield 10027 may be increased by providing one or more springs or resilient structures that further vibrationally isolate and/or absorb vibrations caused by movement of the impeller or of other components of the motor during operation.
The FPC 23001 may further include a supporting structure, for example a supporting ring, on the circular portion that connects to the stator. The supporting structure may be any substantially rigid material, such as FR4 material, or additional polyamide material or polyimide material. The circular portion 23003 may be bonded (e.g. glued) to the supporting structure, and the combined structure may then clipped to the stator. This occurs before the windings are electrically connected to the FPC and the entire stator structure is overmoulded. The supporting structure holds the FPC in place during overmoulding to prevent, or at least substantially inhibit, the FPC from floating to the top of the overmould material during moulding before the overmoulded material sets. The supporting structure also prevents, or at least substantially inhibits, the FPC from distorting during overmoulding. In an alternative embodiment, the supporting structure may be a thickened region of the FPC substrate.
The FPC 23001 includes three motor traces. Each motor track corresponds to each pair of windings. The extension 23013 interconnects with the sensing PCB and supports the sensing traces from the sensors. Preferably at least one or more guards 23008 may be located that sandwich the stator core. The windings are wound around the guards as shown in
The FPC includes a grommet 23031, which provides a seal between the components when assembled. In particular, the grommet 23031 provides a seal where the FPC 23001 leaves the housing of the motor and/or sensor module 400. An elongate section 23006 extends from the FPC portion adjacent the windings to a circuit end 23017. The circuit end 23017 of the FPC may further comprise a pair of legs 23019 for being received by an edge connector of the electronic boards 272 or other parts of the controller 13. The FPC also includes a shield (not shown in
The FPC 23001 described is advantageous because it functions as a support to manage the wires from the stator. The use of the FPC provides for increased use configurations and prevents wires from getting tangled. The flexibility allows the FPC to be routed through various paths. The FPC may be a single layer FPC but alternatively may be a multi-layer FPC. The FPC 23001, as shown in
Some sections of the FPC 23001 may also include weakened sections or bending zones 23100. These weakened sections or bending zones 23100 are labelled FOLD on
The configuration described with reference to
Further components of the motor and/or sensor module will now be described in more detail. In particular, components of the flow generator 11 will now be described, with particular reference to
With reference to
The stator is overmoulded with the shield 77001, the shield comprising an overmould material.
The stator preferably comprises a stator core having an annular portion 82003 and a plurality of stator teeth 82005 extending from the annular portion, each stator tooth having an inwardly facing tooth face. The stator core may be a laminated stator core in a preferred embodiment. The windings are wound around each of the stator teeth 82005.
The stator further includes one or more guards 82001 that sandwich the stator core, and are located between the stator core and the windings, insulating the windings from the stator core.
The guards 82001 are preferably configured such that overmould material reaches at least partially between the stator core and the windings. For example, the guards 82001 may include apertures or recesses for ingress of overmould material during the overmould process. In the preferred embodiment, two guards 82001 are used, one being located on an upper face of the stator core and one being located on the lower face of the stator core. The two guards 82001 connect at a joining region 82007 in a plane of the stator faces, as shown in
The one or more guards 82001 may have retaining features for retaining the stator within a housing. In the preferred embodiment the overmould material does not cover the retaining features. The retaining features include a face of the guard that is configured to cooperate with one or more ledges and/or clips on the housing. The retaining features are configured to prevent lateral and/or axial motion of the stator 35003. The overmould material covers all surfaces of the stator except for a portion of the guard or guards 82001. The motor further comprises an electrical connection on the stator 35003. The electrical connection is at least partially covered by the overmould material. As described above in relation to earlier embodiments, the electrical connection is preferably an FPC that is electrically connected to the windings. The connecting section 10011 of the FPC has a first portion connected to the windings and a second portion that extends from the motor 402. The first portion is covered by the overmould material. As mentioned above, the connecting section is a stiffer section than the adjoining portion of the FPC.
The FPC may further include a supporting structure on the portion that connects to the stator. The supporting structure may be any substantially rigid material, such as FR4 material, or additional polyamide material or polyimide material. The supporting structure may be bonded (e.g. glued) to the supporting structure, and the combined structure may then clipped to the stator. This occurs before the windings are electrically connected to the FPC and the entire stator structure is overmoulded. The supporting structure holds the FPC in place during overmoulding to prevent, or at least substantially inhibit, the FPC from floating to the top of the overmould material during moulding before the overmoulded material sets. The supporting structure also prevents, or at least substantially inhibits, the FPC from distorting during overmoulding. In an alternative embodiment, the supporting structure may be a thickened region of the FPC substrate.
To manufacture the stator, two guards 82001 are placed on the core, one above the stator core and one below the stator core. Wire is then wound around each of the stator teeth using conventional techniques to provide the windings. The FPC is then placed on the guard and electrically connected to the windings. The stator core, surrounded by the guards 82001, and the windings are then placed in a mould and the shield is formed by moulding a suitable material around those components to form the shield. In a preferred embodiment, the shield material covers the joining region, such that oxygen ingress is minimised or prevented through any gaps between the guards 82001. The overmould material preferably further covers the tooth faces of the stator teeth.
In alternative embodiments, the order of the steps described above may be different. For example, the stator core, windings, and guard may be placed in a mould, the FPC is placed in the mould, then the shield is formed by moulding a suitable material around those components to form the shield.
In an alternative embodiment, the shield may be selectively removable. In particular, the shield may be a separately manufactured component that is later assembled with the stator 35003.
The drawings and related description of the flow generator show the flow generator upside down compared to the typical in-use position. That is the component referred to as a top casing will be a bottom part of the flow generator in use and the components referred to as a bottom casing and bottom casing cap will be top parts of the flow generator in use.
It can be seen that the flow generator 11 appears generally circular in plan view, as shown in
In the preferred form, the outlet passage 25008 is a short passage formed as an integral part of the casing 25001 and aligned substantially tangentially to the circumference to the remainder of the generally circular casing 25001. A flow generator casing outlet or exit 25009 (see e.g.
The flow generator casing 25001 encloses the impeller 72001 in use, except for the inlet 25007 and the exit 25009 of the outlet passage 25008. As described elsewhere in this specification, rotation of the impeller 72001 is driven by the motor 402, the fan or impeller 72001 being adapted for connection to the motor.
In the preferred form, the flow generator outlet passage or exit passage 25008 has a generally rectangular cross-section, and the exit passage 25008 is aligned substantially tangentially to the casing 25001. However, the cross-section of the flow generator outlet passage 25008 could be any suitable shape, such as oval, rectangular or circular. The flow generator outlet passage 25008 could also be arranged at any suitable angle to the impeller unit, for example facing radially outwards, or at any suitable angle between tangential and radial. The flow generator outlet passage 25008 causes the gases forced outwards by the impeller unit to coalesce as a fluidic gases stream, and dictates the direction in which the gases stream flows. The overall path or overall direction of the gases flow will be along the passage from the fan towards the flow generator casing exit 25009.
With reference to
The flow generator also includes a partition 33001 between the top casing 25002 and the bottom casing 25003. The partition 33001 and the inner surface of the top casing 25002 are profiled to substantially enclose the impeller blades when the top casing 25002, bottom casing 25003, partition 3301 and bottom casing cap 25005 are assembled. This forms a first interior region 62001 (“upper region”), which is shown in
The top casing 25002 has the inlet 25007 that defines the gases entry into the flow generator 11. The flow generator casing 25001 defines a volute where gases are collected and directed through before emission from the blower. In one configuration, the volute can be considered to be defined by the bottom casing 25003 and comprises a scroll disposed on an opposing side of the partition 33001 as the impeller 72001. In another configuration, the volute can be considered to be defined by the top casing 25002 and the bottom casing 25003, comprising the aforementioned scroll, in addition to the first interior region. The scroll transitions into the outlet passage 25008.
The scroll can increase from a lower cross sectional surface area to a higher cross sectional surface area along a length of the scroll. In other words, the cross sectional area of the scroll can increase as the scroll tends towards the outlet passage 25008.
Preferably the volute of either configuration also has a sealing inner wall 35001. The sealing inner wall 35001 defines a space internal to the lower casing that may be used to house the motor 402. The bottom casing 25003 and the partition 33001 form a second interior region 62003 (“lower region”), which is shown in
The outlet passage 25008 of the flow generator unit 11 is connected to the volute via an opening. The opening and the volute wall define a tongue whereby gases circulating in the volute are diverged into the outlet passage 25008.
The partition 33001 is generally circular and substantially divides the top casing 25002 from the bottom casing 25003 thereby defining the upper and lower gases flow (interior) regions of the blower. To allow gases to flow from the upper region to the lower region an opening is located at, or close to the outer edge of the partition. The opening is most preferably formed by a cut-away in the partition 33001, or some other configuration/shape of the casing such that the combination/arrangement of the partition 33001 and the casing creates an opening or gap between the two. In the embodiment shown, the opening partition 33001 is circular and is located concentrically within the casing. As a result, the opening is an annular opening that is the same width around the perimeter of the partition 33001.
In an alternative embodiment, the curvature/centre of radius of the circumferential aperture may be offset from the centre of radius of the partition 33001 or otherwise has a curvature that differs from that of the circumference of the partition 33001 resulting in an eccentric or otherwise offset circumferential aperture around the circumference of the partition 33001. This produces an aperture with a crescent (“smile”) shaped opening that spans a leading edge to a trailing edge, the aperture may be of any shape with a gradual opening and closing relative to the plane of impeller rotation.
The width and length of the aperture controls the velocity in the lower (volute) section of the housing. A wider and longer aperture increases velocity in the volute, for example.
By dividing the flow generator internal space into two separate regions a number of advantages can be realised. In a conventional blower, high velocity gases leaving the impeller are incident to the edge, or tongue, that defines a physical boundary where gases are split from the volute to enter the outlet passage. High velocity gas flow incident the tongue is turbulent and results in inefficiency, reducing flow generator performance. The turbulence caused by the tongue also introduces a source of noise. In contrast, dividing the casing of the preferred blower into the upper and lower regions reduces the impact caused by the tongue. The upper region allows the gases to circulate at a high speed. The gradual radial opening and closing of the preferred 33001 provides a fluid path to the lower region that is free from (or has reduced) aerodynamically turbulent edges. When circulating gases have entered the lower region, the enlarged volume of the volute encourages the gases to slow and increase pressure. The reduced gases velocity reduces the impact of turbulence normally caused by the tongue to a low or negligible level. The flow generator is therefore able to operate across a wide pressure and flow range with substantially reduced noise output when compared to other blowers. A wider and longer opening increases the flow rate of the lower region relative to the upper region. Therefore, the size of the opening is selected according to the desired flow rate and pressure range of the flow generator 11.
The shaft 33003 is held within the motor by a bearing structure. Preferably the bearing structure has one or more bearings 48001 and one or more bearing mounts 42001/50001. In one embodiment, the bearing mounts 42001/50001 engage with an outer race 48003 of each respective bearing on an inner surface and with the stator 35003 on an outer surface. The preferred engagement of the bearing mounts 42001/50001 to the bearings and the stator is frictional. To promote a frictional engagement, the bearing mounts 42001/50001 are made of a soft, yet resilient and/or flexible material such as silicone rubber or other elastomeric material. The material can be low creep, temperature stable, low compression set with a high tan delta (highly viscous), highly damped. Examples comprise:
Other cold cast rubbery compounds such as RTV (Room Temperature curing Vulcanites) by Dow Corning, Whacker and others.
Such materials allow the bearing mounts 42001/50001 to compress when installed, then expand or deform into their chosen location to be held in place.
The bearing mounts 42001/50001 provide compliance to the rotatable shaft 33003. As rotatable objects, such as the rotor, shaft 33003 and impeller 72001 usually suffer from some degree of rotational imbalance, the bearing mounts 42001/50001 are able to isolate inherent rotation induced vibration from the motor rotor. It has been found that combination of the lightweight, shroudless impeller having a low rotational inertia, as described above, together with the given compliance of the bearing mounts 42001/50001 enables the rotor, shaft 33003 and impeller 72001 to be manufactured and any post manufacture balancing process for the rotating components entirely omitted. These advantages benefit manufacturing costs and time. The lightweight nature of the impeller allows any imbalances to be compensated by the bearing mounts 42001/50001. A lightweight impeller also allows faster speed response of the impeller to changing conditions. Any unwanted fluctuations in pressure due the lack of shroud can be compensated for by quickly changing the impeller speed to return pressure to the desired level.
With reference to
The bearing mount 42001 has an annular body 42003, a collar 42005 extending from the annular body, and a central bore 42007 extending through the annular body and the collar. The central bore 42007 has a wall 42009 and a ledge 42011 extending radially inwardly from the wall 42009 of the central bore. The central bore defines a bearing rotational axis. The annular body and the collar are substantially concentric with the bearing rotational axis. The ledge is disposed near one end of the central bore and the collar is disposed near another end of the central bore.
The bearing mount 42001 also includes a tapered surface 42017, as shown in
The bearing mount 42001 is arranged to receive the bearing 48001 in the central bore 42007 such that the bearing 48001 is radially supported by the inner surface of the bearing mount 42001. The bearing 48001 is axially supported by the ledge 42011. The bearing mount 42001 acts to isolate the shaft 33003 and bearing 48001 from external vibrations, whilst preventing any vibrations sourced from the rotor 33006 or shaft 33003 from being transferred outside the shaft assembly.
At least part of the bearing mount 42001 is arranged to flex or resiliently deform when a force is applied to the bearing mount 42001 to reduce the amount of the force that is translated to the bearing 48001 and therefore the shaft 33003
The at least part of the bearing mount 42001 is arranged to flex or resiliently deform such that the collar 42005 moves in a direction generally parallel to the bearing rotational axis when the force is applied to the bearing mount 42001.
The at least part of the bearing mount 42001 is arranged to flex or resiliently deform when a force is applied to the bearing mount 42001 such that the force translated to the bearing retained in the bearing mount 42001 remains generally constant as the force applied to the bearing mount increases beyond a threshold.
The recess 42015 reduces the likelihood that, when the bearing mount 42001 flexes under axial load, the bearing mount 42001 will contact the rotor. This recess 42015 is applied to both the bottom bearing mount flexing upwards and contacting the underside of the rotor, and the top bearing mount flexing downwards and contacting the top side of the rotor.
The collar is disposed on an opposite side of the annular body to the ledge 42011.
The ledge 42011 is substantially perpendicular to the bearing rotational axis.
At least the annular body comprises a silicone material. In the preferred embodiment, the entire bearing mount 42001 comprises a silicone material. The bearing mount 42001 is a unitary component. The silicone material is liquid silicone rubber (LSR). The silicone material may be a vibration resistant grade of silicone. The desired material properties include, but are not limited to:
A circular bearing mount 42001 evenly distributes the load on the bearing mount 42001 along the structure that supports it (the bottom casing cap 25005 and/or the partition 33001).
In this configuration, δ>γ and β>α, while β<γ. More specifically:
δ:α=2.6:1,δ:β=2:1 and δ:γ=1.3:1
Providing a bearing mount 42001 having an annular body external diameter greater than the collar outer diameter (δ>γ), results in a bearing mount having a lateral distance between the top of the bearing mount 42001 collar and the outer edge of the bearing mount 42001. This distance provides the recess 42015 around the edge of the bearing mount 42001. The recess allows the bearing mount 42001 to flex and behave as described around
Providing a bearing mount 42001 having a bearing mount 42001 aperture greater than the bearing mount ledge aperture (β>α), provides the bearing mount ledge 42011. As described earlier, this ledge 42011 supports the bearing 48001 in the axial direction.
In this configuration, the collar height is greater than the ridge height (ζ>η) and the tapered surface height is greater than the ridge height (κ>η).
It is preferred that the bearing mount ledge thickness p is relatively small to reduce the profile of the bearing mount 42001, while also having sufficient thickness to retain and secure the bearing.
The τ:μ ratio of 4:1.2 results in a relatively thin ledge thickness μ minimising the profile of the bearing mount 42001, whilst being thick enough to provide enough support for the bearing.
It will be appreciated that one or more of the dimensions discussed above may be altered depending on different factors, such as the amount of vibration dampening required, or the size and shape of other components. However, the bearing mount will meet the conditions set out above, including:
δ>γ
β>α
β<γ
For example the annular body external diameter could be about 12.5 mm, about 13 mm, about 13.5 mm, about 14 mm, about 14.5 mm, about 15 mm, about 15.5 mm, about 16 mm, about 16.5 mm, about 17 mm, about 17.5 mm, about 18 mm, or about 15.5 mm.
The collar diameter could be about 9 mm, about 9.5 mm, about 10 mm, about 10.5 mm, about 11 mm, about 11.5 mm, about 12 mm, about 12.5 mm, about 13 mm, about 13.5 mm, about 14 mm, about 14.5 mm, or about 15 mm.
The central bore diameter could be about 5 mm, about 5.5 mm, about 6 mm, about 6.5 mm, about 7 mm, about 7.5 mm, about 8 mm, about 8.5 mm, about 9 mm, about 9.5 mm, about 10 mm, about 10.5 mm, or about 11 mm.
The ledge diameter could be 3 mm, about 3.5 mm, about 4 mm, about 4.5 mm, about 5 mm, about 5.5 mm, about 6 mm, about 6.5 mm, about 7 mm, about 7.5 mm, about 8 mm, about 8.5 mm, or about 9 mm.
The collar height could be 1.7 mm, about 1.8 mm, about 1.9 mm, about 2 mm, about 2.1 mm, about 2.2 mm, about 2.3 mm, 2.4 mm, about 2.5 mm, about 2.6 mm, or about 2.7 mm.
The ridge height could be 0.7 mm, about 0.8 mm, about 0.9 mm, about 1 mm, about 1.1 mm, about 1.2 mm, about 1.3 mm, 1.4 mm, about 1.5 mm, about 1.6 mm, or about 1.7 mm.
The tapered surface height could be about 1.5 mm, about 1.6 mm, about 1.7 mm, about 1.8 mm, about 1.9 mm, about 2 mm, about 2.1 mm, about 2.2 mm, about 2.3 mm, 2.4 mm, or about 2.5 mm.
The ledge thickness could be 0.7 mm, about 0.8 mm, about 0.9 mm, about 1 mm, about 1.1 mm, about 1.2 mm, about 1.3 mm, 1.4 mm, about 1.5 mm, about 1.6 mm, or about 1.7 mm.
The central bore thickness (or depth) to the top of the ledge could be about 2.3 mm, about 2.5 mm, about 3 mm, about 3.5 mm, about 4 mm, about 4.5 mm, about 5 mm, about 5.5 mm, about 6 mm, about 6.3 mm, or about 6.5 mm.
The total height of the bearing could be about 4 mm, about 4.5 mm, 5 mm, about 5.5 mm, about 6 mm, about 6.5 mm, about 7 mm.
The ratio of λ:μ could be about 3:1, about 3.5:1, about 4:1, about 4.5:1, about 5:1, about 5.5:1, about 6:1, about 6.5:1, about 7:1, about 7.5:1, about 8:1, about 8.5:1, about 9:1, about 9.5:1, about 10:1, about 10.5:1, about 11:1, about 11.5:1, about 12:1, about 12.5:1, about 13:1, about 13.5:1, about 14:1, about 14.5:1, about 15:1, about 15.5:1, or about 16:1. Ratios greater than or equal to 3.5:1 can be advantageous when a stronger or more rigid material is used to manufacture the bearing mount 42001. In this case, less material can be used in ledge 42011 relative to ratios with an antecedent below 3.5:1 whilst still providing similar performance supporting the bearing 48001. Ratios lower than 3.5:1 can be advantageous when a softer, less rigid and/or more flexible material is used to manufacture the bearing mount 42001. In this case, a thicker ledge is beneficial to provide sufficient support to the bearing 48001. The ratio τ:ϵ could be about 1:0.95, about 1:1, about 1:1.05, about 1:1.1, about 1:1.15, about 1:1.2, about 1:1.25, about 1:1.3, about 1:1.35, about 1:1.4, about 1:1.45, about 1:1.5, about 1:1.55, about 1:1.6, about 1:1.65, about 1:1.7, or about 1:1.75. Ratios less than or equal to 1:1 can be advantageous in providing smaller profile bearing mount 42001. Ratios greater than 1:1 can be advantageous in providing increased support to the bearing 48001 within the bearing mount 42001.
The ratio τ:μ could be about 2.5:1, about 3:1, about 3.5:1, about 4:1, about 4.5:1, about 5:1, about 5.5:1, or about 6:1. Ratios greater than or equal to 3.3:1 can be beneficial in providing enhanced support to the bearing 48001. Ratios less than 3.3:1 can be beneficial in providing a reduced bearing mount 42001 profile, and requiring less material.
The ratio τ:λ could be about 2.4:1, about 2.5:1, about 3:1, about 3.5:1, about 4:1, about 4.5:1, about 5:1, about 5.5:1, or about 6:1. Ratios less than or equal to 1:1.05 can be beneficial in providing a reduced profile bearing mount 42001 requiring less material. Ratios greater than 1:1.5 can advantageously provide additional support to the bearing 48001 or a more resilient and/or stiffer bearing mount 42001 where desired.
This embodiment of the bearing mount 50001 has similar features and functions to the features and functions of the first bearing mount 42001 described above. The features and functions of the second embodiment bearing mount 50001 that are different to those of the first embodiment are described below.
The differences between this second embodiment of the bearing mount 50001 and the first embodiment of the bearing mount 42001 are:
The annular body 50003 has an external diameter δ2=18.9 mm, the central bore has a diameter (corresponding to the inner diameter of the bearing mount collar) δ2=7.5 mm, the collar has an outer diameter γ2=11.5 mm and the bearing mount ledge defines a bearing mount ledge aperture with a diameter α2=5.7 mm.
Again, in this configuration, δ2>γ2 and β2>α2, while β2<γ2. More specifically:
δ2:α2=3.3:1,δ2:β2=2.5:1 and β2:γ2=1.6:1
Again, preferably δ>γ and β>α for the reasons discussed in the previous embodiment.
As shown in
For example the annular body external diameter could be about 16 mm, about 16.5 mm, about 17 mm, about 17.5 mm, about 18 mm, about 18.5 mm, about 19 mm, about 19.5 mm, about 20 mm, about 20.5 mm, about 21 mm, about 21.5 mm, or about 22 mm.
The collar diameter could be about 8.5 mm, about 9 mm, about 9.5 mm, about 10 mm, about 10.5 mm, about 11 mm, about 11.5 mm, about 12 mm, about 12.5 mm, about 13 mm, about 13.5 mm, about 14 mm, or about 14.5 mm.
The central bore diameter could be about 4.5 mm, about 5 mm, about 5.5 mm, about 6 mm, about 6.5 mm, about 7 mm, about 7.5 mm, about 8 mm, about 8.5 mm, about 9 mm, about 9.5 mm, about 10 mm, or about 10.5 mm.
The ledge diameter could be 3 mm, about 3.5 mm, about 4 mm, about 4.5 mm, about 5 mm, about 5.5 mm, about 6 mm, about 6.5 mm, about 7 mm, about 7.5 mm, about 8 mm, about 8.5 mm, or about 9 mm.
The collar height could be 1.7 mm, about 1.8 mm, about 1.9 mm, about 2 mm, about 2.1 mm, about 2.2 mm, about 2.3 mm, 2.4 mm, about 2.5 mm, about 2.6 mm, or about 2.7 mm.
The ridge height could be 0.7 mm, about 0.8 mm, about 0.9 mm, about 1 mm, about 1.1 mm, about 1.2 mm, about 1.3 mm, 1.4 mm, about 1.5 mm, about 1.6 mm, or about 1.7 mm.
The tapered surface height could be about 1.5 mm, about 1.6 mm, about 1.7 mm, about 1.8 mm, about 1.9 mm, about 2 mm, about 2.1 mm, about 2.2 mm, about 2.3 mm, 2.4 mm, or about 2.5 mm.
The ledge thickness could be 0.7 mm, about 0.8 mm, about 0.9 mm, about 1 mm, about 1.1 mm, about 1.2 mm, about 1.3 mm, 1.4 mm, about 1.5 mm, about 1.6 mm, or about 1.7 mm.
The central bore thickness (or depth) to the top of the ledge could be about 2.3 mm, about 2.5 mm, about 3 mm, about 3.5 mm, about 4 mm, about 4.5 mm, about 5 mm, about 5.5 mm, about 6 mm, about 6.3 mm, or about 6.5 mm.
The total height of the bearing could be about 4 mm, about 4.5 mm, 5 mm, about 5.5 mm, about 6 mm, about 6.5 mm, about 7 mm.
The ratio of λ2:μ2 could be about 3:1, about 3.5:1, about 4:1, about 4.5:1, about 5:1, about 5.5:1, about 6:1, about 6.5:1, about 7:1, about 7.5:1, about 8:1, about 8.5:1, about 9:1, about 9.5:1, about 10:1, about 10.5:1, about 11:1, about 11.5:1, about 12:1, about 12.5:1, about 13:1, about 13.5:1, about 14:1, about 14.5:1, about 15:1, about 15.5:1, or about 16:1. The ratio τ:ϵ could be about 1:0.95, about 1:1, about 1:1.05, about 1:1.1, about 1:1.15, about 1:1.2, about 1:1.25, about 1:1.3, about 1:1.35, about 1:1.4, about 1:1.45, about 1:1.5, about 1:1.55, about 1:1.6, about 1:1.65, about 1:1.7, or about 1:1.75.
The ratio τ:μ2 could be about 2.5:1, about 3:1, about 3.5:1, about 4:1, about 4.5:1, about 5:1, about 5.5:1, or about 6:1.
The ratio τ:λ2 could be about 2.4:1, about 2.5:1, about 3:1, about 3.5:1, about 4:1, about 4.5:1, about 5:1, about 5.5:1, or about 6:1.
The partition 33001 is connected to the bottom casing cap 25005 via a number of screws. When the screws are tightened, there can be a variability in the amount of torque applied. Rigid bearing mounts would result in different forces being transferred to the bearings and shaft 33003 from the rest of the flow generator depending on the tightness of the partition 33001 and bottom casing cap 25005 connection. This can lead to a variety of disadvantageous features such as an imbalanced bearing, shaft, rotor and/or impeller which can lead to higher noises, lower efficiencies and a lower operating lifetime of the assembly.
By providing bearing mounts that can deform, the bearing mounts mitigate this effect of variability of tightness. Securing the partition to the bottom casing cap secures the bearing mounts within the motor assembly. As the partition and the bottom casing cap are tightened, forces resulting from the tightening are transferred to the bearing mounts and the bearings. The illustrated bearing mounts are configured to exhibit a preferential load transfer to the bearings as a result of the tightening. As the bottom casing cap and the partition are tightened, the force transferred through the bearing mounts to the bearings increases to a threshold value at a threshold tightness. After this force threshold is reached (corresponding to the threshold tightness between the partition and the bottom casing cap), the bearing mounts are configured to deform to minimise the transfer of any additional load to the bearings and therefore the shaft of the motor 402. This behaviour is a function of the shape of the bearing mounts as illustrated. The partition and the bottom casing cap may be tightened further, however the bearing mounts will flex to insulate the bearings and the shaft from the additional force exerted on the bearing mounts rather than transferring the forces through the bearing mounts to the bearings and/or shaft.
If the axial force on the bearings increases beyond the threshold, the bearing mounts will deform so that, the force will act on the bearing mount and excess will not be transferred to the bearing, or the excess transferred to the bearing is minimised.
When the partition 33001 is connected to the bottom casing cap 25005, the bearing mount 50001 is able to flex to reduce or dampen the effect of the tightening parts on the bearing and shaft 33003 of the blower. In addition to this, the recess 57003 again reduces the likelihood that the bearing mount will flex to the point that its periphery will contact the rotor. Similar or the same behaviour occurs at the bearing mount 50001 in the bearing mount recess of the partition.
As the bearing mount flexes, the outer rim can pivot within the cooperating cavity. When the outer rim pivots, the surface of the outer rim will slide relative to the surface of the recess. With reference to
The profile and physical properties of the bearing mount provide a preload, or biasing force, to the bearings 48001 when the flow generator is assembled. The preload increases the lifetime of the bearings 48001.
When the bottom casing cap 25005 is secured to the partition 33001, a preload is introduced into the bearing mount via the labelled bearing mount compression force, which in turn introduces a preload to the bearings. The preload introduced onto the bearings 48001 can be diagonal (relative to the rotational axis of the bearing) due to the deformation of the bearing mount. The preload eliminates the clearance that is designed into standard bearings. Almost all radial bearings are made with a clearance or space between their components to allow for free movement. This space, if not taken up by a preload can allow the rolling elements to slide rather than roll, or can allow for the inner and outer bearing races to misalign. The preload introduced via the bearing mounts provides bearing system rigidity, reduced vibration and improved bearing life.
With reference to
The combination of various features of the present invention provide advantages, which can be achieved using a single impeller. Using a lightweight/low inertia impeller (e.g. by removing some or all of the shroud and/or reducing blade material) reduces imbalance of the impeller due to manufacturing tolerances. Previously, after manufacture and during assembly of a blower, it has been necessary to remove/add material to the impeller to improve balancing. The lightweight nature of the impeller means that any small imbalance can be tolerated without requiring rectification. Coupled to this, where the imbalance is not small enough, the resilient/flexible bearing mounts can compensate for any imbalance in the impeller. As the impeller is lightweight enough, any imbalance is of a small enough magnitude to be compensated for by the bearing mounts, without the need for altering the weight of the impeller during assembly.
The lightweight construction also allows for a larger diameter impeller, which in turn provides higher tip speed for a particular RPM. This allows for lower RPM operation of the flow generator while still achieving the required pressure (which is dependent on tip speed). Having a lower RPM reduces vibration to an acceptable level, or to a level that can be compensated for by the bearing structure and/or stator mount. The lightweight construction of the impeller as mentioned previously enables the larger impeller as it provides lower inertia that achieves the required pressures/response. That is, lower torque is required to speed up and slow down the impeller to reach the required tip speeds/pressures. This improves dynamic performance (response). In addition to this, small magnets in the motor (combined with the bearing structure) remove the need for balancing during assembly, improve dynamic performance.
The resilient/flexible bearing structure allows for self-alignment, compliance, damping and preload of the impeller and shaft assembly. This makes assembly easier, and in combination with the lightweight/low inertia impeller reduce or negates the need for balancing modifications during assembly, as mentioned previously. The bearing structure provides for relaxed tolerances during manufacture as it compensates for larger tolerances. The bearing structure also isolates and/or damps vibrations, also allowing high RPM speeds of the impeller where necessary.
The partition 33001 that separates the flow generator into first and second regions separates out the high velocity region to reduce noise. This allows for and maintains a constant high velocity of flow while diffusing the velocity to pressure.
With reference to
The stator support system also includes a vibration isolating member located between the stator and the bottom casing cap 25005 arranged to bias the stator 35003 in a direction towards the first stator ledge. The vibration isolating member is described in more detail below.
The bottom casing ledges 64001 and resilient members 64003 cooperate with the stator 35003 to support the stator in the bottom casing 25003. Each bottom casing ledge 64001 has a curved inner surface 64002 that substantially corresponds to the curve of the stator 35003. In the embodiment shown, there are three bottom casing ledges 64001, however there may be more or fewer bottom casing ledges 64001. The bottom casing ledges 64001 are evenly spaced around the bottom casing 25003. The bottom casing ledges 64001 are all at the same height. In the embodiment shown, there are three resilient members 64003, however there may be more or fewer resilient members 64003. The resilient members 64003 are evenly spaced around the bottom casing 25003. The resilient members 64003 are all at the same height.
The bottom casing ledges 64001 and resilient members 64003 are integrally formed with the bottom casing 25003.
With reference to
The ledges 64001 support the stator and secure the stator from motion in a direction parallel to the axis of the shaft, by acting as a physical impediment to said motion, since the end of the ledge 77002 and the stator peripheral ledge overlap. The peripheral ledge of the stator also includes a lateral retaining feature 77003 preventing or limiting the stator 35003 from being able to rotate with respect to the bottom casing 25003.
The stator 35003 is retained in place when forced vertically through the bottom of the bottom casing (when the apparatus is in the position shown in
The flow generator preferably includes a biasing component or components to bias components together and remove any play or space between those components. When the flow generator is assembled, there is vertical clearance to allow the stator to be inserted and the casings to be assembled into a unified casing. The clearance creates play between the components and allows for the components to move or vibrate relative to each other. Additionally, the resilient members 64003, by nature of being resilient, may flex somewhat when the stator 35003 is in place and the motor is operating due to vibration. This flexing may result in the stator 35003 being able to vibrate between resilient members 64003 and ledges 64001 after insertion. To remove the play and minimise the possible vibration of the stator, the biasing component is provided. The biasing component biases or urges the components together to remove the play. In particular, the biasing component biases the components together in a direction that is parallel to the direction of the shaft.
The vibration isolator member
The stator preload cap 70001 can be an elastomeric material (e.g. silicone). The stator preload cap 70001 can span an entire perimeter of the adjacent surface of the stator, or can be broken into segments only spanning partial perimeters of the adjacent surface of the stator 35003. The illustrated stator preload cap 70001 is annular with a central opening. Alternately, the stator preload cap can be cylindrical or another shape. The stator preload cap 70001 can include additional stator preload cap openings configured to permit airflow through the stator preload cap. These additional openings can correspond with the openings in the bottom casing cap. This allows air to flow through the motor assembly more easily or effectively, assisting in dissipating heat from the motor assembly.
The preferred form of the impeller is shown in
The impeller is constructed to be lightweight. Preferably, this is by making the impeller shroudless, or at least partially shroudless, thereby removing weight. To achieve a lightweight impeller, as shown in
For example, a conventional shrouded impeller commonly used on a breathing assistance device, weighing approximately 17 grams and having inertia of 6 kg·mm2, can respond to pressure fluctuations of 10 cmH2O in approximately 2 seconds. By contrast, the preferred impeller, weighing approximately 1.7 grams and inertia of 0.5 kg·mm2, responds pressure fluctuations of 10 cmH2O in approximately 100 ms. As the impeller has a lower mass and rotational inertia compared to conventional impellers, the impeller exhibits much less pressure fluctuation. The reduced pressure fluctuation is less disruptive to a patient's breathing process, and therefore advantageously increases patient comfort.
As mentioned, the lightweight of the impeller can be achieved by omitting a shroud. However, it is not necessary to omit the entire shroud—rather just sufficient shroud to bring the weight of the impeller to a suitable level. Therefore, lightweight can be achieved by having as much open space (area or volume) between the blades as possible. The open space can be defined in terms of the blade volume to blade sweep volume ratio/percentage. That is, the blades sweep a volume X when rotating and the blades themselves have a combined volume Y (which is the volume of each blade combined). Alternatively, from a plan perspective, the open space can be defined in terms of the blade area to the blade sweep area. The ratios should be kept as low as possible. In one embodiment, for example the swept volume of the impeller is approximately 19,000 mm3, where the blades constitute a volume of approximately 1,200 mm3. The ratio of swept volume to blade volume is therefore approximately 16:1, thereby defining an impeller that is lightweight compared to the smaller, more densely designed and heavier impellers used earlier.
The lightweight impeller can have a weight for example of less than 2 grams and preferably between 0.8 and 1.8 grams, or more preferably, between 1.2 and 1.7 grams, or even more preferably 1.7 grams. These are just examples or a preferred embodiment and the impeller need not be this weight, but some other weight that renders it lightweight.
Alternatively, a lightweight impeller can be designed to remove as much of the shroud as necessary to bring the moment of inertia to radius ratio down to preferably less than 15 gram*mm, and more preferably between 8-12 gram*mm and in one possible embodiment approximately 11 gram*mm. For example, in one possible embodiment, such an impeller can have a radius of 35 mm, a circumference of 219 mm, and at 15,000 rpm a moment of inertia of 344.22, a tip speed of 54.98 m/s, a pressure of 1,800 Pa and a tip speed to inertia to radius ratio of 3.5 or more and for example 5.59. More generally, a lightweight impeller could have dimensions/parameters within the following ranges (note these ranges are indicative—not limiting):
A pressure ratio to inertia to radius ratio of greater than 50:1 Pascals per gram*mm and preferably 80:1 Pa per gram*mm or more at 1,000 Pa.
Lightweight impellers enable larger radius impellers to be used. Yet larger radius impellers can be used than those mentioned above. Larger radius impellers provide greater tip speed and pressure. The construction of the impeller allows for greater radius impellers because the lightweight nature of the impeller is such that even with larger impellers, the inertia is still low enough to provide the required response and pressures.
The lightweight nature of the impeller can be achieved through removing mass through any suitable means, such as removing the shroud and/or material from the impeller and/or using lighter materials. One possible manner in which to reduce impeller mass is to reduce the number of blades.
With reference to
The first curve 72008 extends outwardly from the hub 72003 along a curve with a radius of about 65 mm. The first curve 72008 extends, with its outward edge extending from the offset 72006, to a point 72011 where a chord 72012 formed by the curve is angled at 13.5° from the shown vertical axis 72013.
The second curve 72010 extends outwardly from the end of the first curve 72008 with a radius of about 20 mm. The second curve 72010 extends from the end of the first curve 72008 to a point 72014 where a chord 72015 formed by the curve 72010 is angled at 35° from the shown vertical axis 72013.
Although the present disclosure has been described in terms of certain embodiments, other embodiments apparent to those of ordinary skill in the art also are within the scope of this disclosure. Thus, various changes and modifications may be made without departing from the spirit and scope of the disclosure. For instance, various components may be repositioned as desired. Features from any of the described embodiments may be combined with each other and/or an apparatus may comprise one, more, or all of the features of the above described embodiments. Moreover, not all of the features, aspects and advantages are necessarily required to practice the present disclosure. Accordingly, the scope of the present disclosure is intended to be defined only by the claims that follow.
The various configurations described are exemplary configurations only. For example, while the motor and/or sensor sub-assembly recess is described as being in the underside of the main housing, it could alternatively be in a rear, side, front, or top of the housing. With such a variant, the air and/or oxygen inlets may also be positioned differently as required.
The features are described with reference to a flow therapy apparatus that is capable of delivering heated and humidified gases to a patient or user. The apparatus may be suitable for treating chronic obstructive pulmonary disease (COPD). The apparatus may be configured to deliver gases to a patient interface at a high flow rate (high flow therapy).
Alternatively, one, some, or all of the features may be provided in an apparatus for a different purpose. The apparatus may be a high flow therapy apparatus, or may be a low flow therapy apparatus. The features may also be provided in an apparatus for providing continuous positive airway pressure (CPAP), which may deliver gases (humidified or otherwise) at positive pressure.
One or some of the features may alternatively be provided in an apparatus that does not require a humidifier and therefore does not require the liquid chamber 300 or chamber bay 108 features. For example, it will be appreciated that the configuration that isolates the motor and gasflow path from the electrical and electronic components has broad applications in other types of gas delivery apparatuses.
The ‘flow therapy apparatus’ language is intended to cover all such variants.
Reference to any prior art in this specification is not, and should not be taken as, an acknowledgement or any form of suggestion that that prior art forms part of the common general knowledge in the field of endeavour in any country in the world.
Where reference is used herein to directional terms such as “up”, “down”, “forward”, “rearward”, “horizontal”, “vertical” etc, those terms refer to when the apparatus is in a typical in-use position, and are used to show and/or describe relative directions or orientations.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/NZ2018/050056 | 4/23/2018 | WO | 00 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2018/199774 | 11/1/2018 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 2189252 | Reggio | Feb 1940 | A |
| 2874722 | Hamblin | Feb 1959 | A |
| 2929944 | Shewmon | Mar 1960 | A |
| 3040670 | Schenck et al. | Jun 1962 | A |
| 3047345 | Burton | Jul 1962 | A |
| 3395649 | Marischen | Aug 1968 | A |
| 3424508 | Kizer et al. | Jan 1969 | A |
| 3495628 | Boender | Feb 1970 | A |
| 3926223 | Petzetakis | Dec 1975 | A |
| 4033808 | Petzetakis | Jul 1977 | A |
| 4161667 | Buckman | Jul 1979 | A |
| 4233972 | Hauff et al. | Nov 1980 | A |
| 4357552 | MacMillan | Nov 1982 | A |
| 4530639 | Mowill | Jul 1985 | A |
| 4531551 | Eichelberger et al. | Jul 1985 | A |
| 4590951 | O'Connor | May 1986 | A |
| 4623812 | van de Griend | Nov 1986 | A |
| 4713530 | Schittenhelm et al. | Dec 1987 | A |
| 4773448 | Francis | Sep 1988 | A |
| 4837921 | Tassinario | Jun 1989 | A |
| 4888465 | Hoffmann | Dec 1989 | A |
| 4889116 | Taube | Dec 1989 | A |
| 4903736 | Baston et al. | Feb 1990 | A |
| 5127442 | Blomqvist | Jul 1992 | A |
| 5211171 | Choromokos | May 1993 | A |
| 5432322 | Ingram et al. | Jul 1995 | A |
| 5484270 | Adahan | Jan 1996 | A |
| 5521357 | Lock et al. | May 1996 | A |
| 5521576 | Collins | May 1996 | A |
| 5567127 | Wentz | Oct 1996 | A |
| 5591292 | Blomqvist | Jan 1997 | A |
| 5601400 | Kondo et al. | Feb 1997 | A |
| 5605444 | Paton et al. | Feb 1997 | A |
| 5608591 | Klaassen | Mar 1997 | A |
| 5640951 | Huddart et al. | Jun 1997 | A |
| 5662611 | Beiser et al. | Sep 1997 | A |
| 5672927 | Viskochil | Sep 1997 | A |
| 5694268 | Dunfield et al. | Dec 1997 | A |
| 5701883 | Hete et al. | Dec 1997 | A |
| 5797727 | Peters et al. | Aug 1998 | A |
| 5875783 | Draegerwerk | Mar 1999 | A |
| 5878743 | Zdrojkowski et al. | Mar 1999 | A |
| 5967764 | Booth et al. | Oct 1999 | A |
| 6050262 | Jay | Apr 2000 | A |
| 6073630 | Adahan | Jun 2000 | A |
| 6105649 | Levingston et al. | Aug 2000 | A |
| 6194692 | Oberle | Feb 2001 | B1 |
| 6210116 | Kuczaj et al. | Apr 2001 | B1 |
| 6216691 | Kenyon et al. | Apr 2001 | B1 |
| 6222158 | Nakata et al. | Apr 2001 | B1 |
| 6302105 | Wickham et al. | Oct 2001 | B1 |
| 6376952 | Stenta | Apr 2002 | B1 |
| 6401713 | Hill et al. | Jun 2002 | B1 |
| 6435180 | Hewson et al. | Aug 2002 | B1 |
| 6439861 | Shieh | Aug 2002 | B1 |
| 6483087 | Gardner et al. | Nov 2002 | B2 |
| 6487047 | Balakrishnan | Nov 2002 | B1 |
| 6516801 | Boussignac | Feb 2003 | B2 |
| 6537405 | Henderson et al. | Mar 2003 | B1 |
| 6543449 | Woodring et al. | Apr 2003 | B1 |
| 6601621 | Wixey et al. | Aug 2003 | B2 |
| 6622724 | Truitt et al. | Sep 2003 | B1 |
| 6629528 | Wickham et al. | Oct 2003 | B1 |
| 6644310 | Delache et al. | Nov 2003 | B1 |
| 6700255 | Stenta | Mar 2004 | B1 |
| 6717299 | Bacile et al. | Apr 2004 | B2 |
| 6722359 | Chalvignac | Apr 2004 | B2 |
| 6802648 | Merot et al. | Oct 2004 | B2 |
| 6817088 | Lin | Nov 2004 | B1 |
| 6848444 | Smith et al. | Feb 2005 | B2 |
| 6899100 | Wickham et al. | May 2005 | B2 |
| 6910483 | Daly et al. | Jun 2005 | B2 |
| 7012346 | Hoffman et al. | Mar 2006 | B2 |
| 7028677 | Martin | Apr 2006 | B2 |
| 7096864 | Mayer et al. | Aug 2006 | B1 |
| 7121874 | Jeon | Oct 2006 | B1 |
| 7128069 | Farrugia et al. | Oct 2006 | B2 |
| 7240583 | Wingett et al. | Jul 2007 | B2 |
| 7241131 | Booth et al. | Jul 2007 | B1 |
| 7244099 | Yamasaki | Jul 2007 | B2 |
| 7262568 | Takada | Aug 2007 | B2 |
| 7314046 | Schroeder et al. | Jan 2008 | B2 |
| 7340966 | DiMatteo et al. | Mar 2008 | B2 |
| 7365458 | Yoshida | Apr 2008 | B2 |
| 7384237 | Baecke et al. | Jun 2008 | B2 |
| 7413173 | DiMatteo et al. | Aug 2008 | B2 |
| 7448383 | Delache et al. | Nov 2008 | B2 |
| 7508102 | Sugiyama et al. | Mar 2009 | B2 |
| 7516743 | Hoffman | Apr 2009 | B2 |
| 7571725 | Virr et al. | Aug 2009 | B2 |
| 7617823 | DiMatteo et al. | Nov 2009 | B2 |
| 7677246 | Kepler et al. | Mar 2010 | B2 |
| 7708013 | Niland et al. | May 2010 | B2 |
| 7827981 | Bamford | Nov 2010 | B2 |
| 7874290 | Chalvignac | Jan 2011 | B2 |
| 7913692 | Kwok | Mar 2011 | B2 |
| 7938112 | Mayer et al. | May 2011 | B2 |
| 7939975 | Saga et al. | May 2011 | B2 |
| 7942380 | Bertinetti et al. | May 2011 | B2 |
| 7975688 | Truitt | Jul 2011 | B1 |
| 8006691 | Kenyon et al. | Aug 2011 | B2 |
| 8011362 | Adams | Sep 2011 | B2 |
| 8020551 | Virr et al. | Sep 2011 | B2 |
| 8020556 | Shahar | Sep 2011 | B2 |
| 8020557 | Bordewick et al. | Sep 2011 | B2 |
| 8028693 | Trevor-Wilson et al. | Oct 2011 | B2 |
| 8042535 | Kenyon et al. | Oct 2011 | B2 |
| 8074645 | Bordewick et al. | Dec 2011 | B2 |
| 8074647 | Truitt et al. | Dec 2011 | B2 |
| 8080907 | Jeung | Dec 2011 | B2 |
| 8122884 | Daly et al. | Feb 2012 | B2 |
| 8186345 | Payton et al. | May 2012 | B2 |
| 8302598 | Haase et al. | Nov 2012 | B2 |
| 8353292 | Chalvignac | Jan 2013 | B2 |
| 8375944 | Kwok | Feb 2013 | B2 |
| 8375945 | Kepler et al. | Feb 2013 | B2 |
| 8393320 | Kenyon | Mar 2013 | B2 |
| 8450898 | Sears et al. | May 2013 | B2 |
| 8453640 | Martin et al. | Jun 2013 | B2 |
| 8469025 | Mayer et al. | Jun 2013 | B2 |
| 8481902 | Leboeuf et al. | Jul 2013 | B2 |
| 8496001 | Schermeier et al. | Jul 2013 | B2 |
| 8499760 | Schermeier et al. | Jul 2013 | B2 |
| D688788 | Spruell et al. | Aug 2013 | S |
| 8517012 | Daly et al. | Aug 2013 | B2 |
| 8544465 | Smith et al. | Oct 2013 | B2 |
| 8553364 | Schreiber et al. | Oct 2013 | B1 |
| 8602025 | Bordewick et al. | Dec 2013 | B2 |
| 8602747 | Takada | Dec 2013 | B2 |
| 8627819 | DeVries et al. | Jan 2014 | B2 |
| 8631789 | Virr et al. | Jan 2014 | B2 |
| 8631791 | Bordewick et al. | Jan 2014 | B2 |
| 8638014 | Sears et al. | Jan 2014 | B2 |
| 8701662 | Pujol et al. | Apr 2014 | B2 |
| 8733349 | Bath et al. | May 2014 | B2 |
| 8739780 | Tang et al. | Jun 2014 | B2 |
| 8816558 | Sears et al. | Aug 2014 | B2 |
| 8899232 | Farrugia et al. | Dec 2014 | B2 |
| 8915247 | Chalvignac | Dec 2014 | B2 |
| 8931481 | Jones et al. | Jan 2015 | B2 |
| 8973576 | Kenyon | Mar 2015 | B2 |
| 9004067 | Kenyon et al. | Apr 2015 | B2 |
| 9010324 | Martin et al. | Apr 2015 | B2 |
| 9038629 | Smith et al. | May 2015 | B2 |
| 9038631 | Bath et al. | May 2015 | B2 |
| 9038632 | Crumblin et al. | May 2015 | B2 |
| 9048715 | Kodani et al. | Jun 2015 | B2 |
| 9072860 | Lithgow et al. | Jul 2015 | B2 |
| 9089660 | Chalvignac | Jul 2015 | B2 |
| 9127691 | Hagen et al. | Sep 2015 | B2 |
| 9132250 | Allum | Sep 2015 | B2 |
| 9132252 | Barlow | Sep 2015 | B2 |
| 9227035 | Crumblin et al. | Jan 2016 | B2 |
| 9272116 | Mayer et al. | Mar 2016 | B2 |
| 9302066 | Bertinetti et al. | Apr 2016 | B2 |
| 9302067 | Mayer et al. | Apr 2016 | B2 |
| 9358359 | Lithgow et al. | Jun 2016 | B2 |
| 9375543 | Lubrett et al. | Jun 2016 | B2 |
| 9393377 | Smith et al. | Jul 2016 | B2 |
| 9402970 | Virr et al. | Aug 2016 | B2 |
| 9427538 | Daly et al. | Aug 2016 | B2 |
| 9479022 | Hoemann et al. | Oct 2016 | B2 |
| 9481424 | Hagen et al. | Nov 2016 | B2 |
| 9539409 | Crumblin et al. | Jan 2017 | B2 |
| 9545493 | Mayer et al. | Jan 2017 | B2 |
| 9545494 | Mayer et al. | Jan 2017 | B2 |
| 9555211 | Mayer et al. | Jan 2017 | B2 |
| 9610416 | Jones et al. | Apr 2017 | B2 |
| 9610420 | Lithgow et al. | Apr 2017 | B2 |
| 9656034 | Kepler et al. | May 2017 | B2 |
| 9737682 | Maurer et al. | Aug 2017 | B2 |
| 9750907 | Librett et al. | Sep 2017 | B2 |
| 9802022 | Smith et al. | Oct 2017 | B2 |
| 10052450 | Mayer et al. | Aug 2018 | B2 |
| 10137264 | Darby et al. | Nov 2018 | B2 |
| 10195389 | Virr et al. | Feb 2019 | B2 |
| 10238822 | Barlow et al. | Mar 2019 | B2 |
| 20030235012 | Nishizawa | Dec 2003 | A1 |
| 20050103339 | Daly et al. | May 2005 | A1 |
| 20050188989 | Delache et al. | Sep 2005 | A1 |
| 20050202697 | Caveney et al. | Sep 2005 | A1 |
| 20050210622 | Baecke et al. | Sep 2005 | A1 |
| 20060017815 | Stavely et al. | Jan 2006 | A1 |
| 20060096596 | Occhialini et al. | May 2006 | A1 |
| 20060158785 | Arya et al. | Jul 2006 | A1 |
| 20060237013 | Kwok | Oct 2006 | A1 |
| 20070017518 | Farrugia et al. | Jan 2007 | A1 |
| 20070132335 | Ionel et al. | Jun 2007 | A1 |
| 20070166659 | Hasse et al. | Jul 2007 | A1 |
| 20070251527 | Sleeper | Nov 2007 | A1 |
| 20070277827 | Bordewick et al. | Dec 2007 | A1 |
| 20070284952 | Ihle | Dec 2007 | A1 |
| 20080000474 | Jochle et al. | Jan 2008 | A1 |
| 20080142368 | Warren et al. | Jun 2008 | A1 |
| 20080149306 | Hwang et al. | Jun 2008 | A1 |
| 20080178879 | Roberts et al. | Jul 2008 | A1 |
| 20080216831 | McGinnis et al. | Sep 2008 | A1 |
| 20080216835 | McGinnis et al. | Sep 2008 | A1 |
| 20080304986 | Kenyon et al. | Dec 2008 | A1 |
| 20090020120 | Schatzl et al. | Jan 2009 | A1 |
| 20090071480 | Adams | Mar 2009 | A1 |
| 20090194101 | Kenyon | Aug 2009 | A1 |
| 20090223514 | Smith et al. | Sep 2009 | A1 |
| 20090256295 | Kodama | Oct 2009 | A1 |
| 20090301485 | Kenyon et al. | Dec 2009 | A1 |
| 20090315492 | Oomura | Dec 2009 | A1 |
| 20090320842 | Doherty | Dec 2009 | A1 |
| 20090324435 | Sears et al. | Dec 2009 | A1 |
| 20100000535 | Wickham et al. | Jan 2010 | A1 |
| 20100059055 | Brungart et al. | Mar 2010 | A1 |
| 20100059056 | Sears et al. | Mar 2010 | A1 |
| 20100116272 | Row et al. | May 2010 | A1 |
| 20100132711 | Kenyon | Jun 2010 | A1 |
| 20100170513 | Bowditch et al. | Jul 2010 | A1 |
| 20100192094 | Jeha et al. | Jul 2010 | A1 |
| 20110023874 | Bath et al. | Feb 2011 | A1 |
| 20110052205 | Yu et al. | Mar 2011 | A1 |
| 20110073110 | Kenyon | Mar 2011 | A1 |
| 20110114815 | Valovick | May 2011 | A1 |
| 20110132363 | Chalvignac | Jun 2011 | A1 |
| 20110197884 | Duff et al. | Aug 2011 | A1 |
| 20110203587 | Bertinetti et al. | Aug 2011 | A1 |
| 20120000463 | Bordewick et al. | Jan 2012 | A1 |
| 20120080032 | Bordewick et al. | Apr 2012 | A1 |
| 20120097156 | Bowman et al. | Apr 2012 | A1 |
| 20120107157 | Tsai | May 2012 | A1 |
| 20120138058 | Fu et al. | Jun 2012 | A1 |
| 20120152255 | Barlow et al. | Jun 2012 | A1 |
| 20120167879 | Bowman | Jul 2012 | A1 |
| 20120227738 | Virr et al. | Sep 2012 | A1 |
| 20120266873 | Lalonde | Oct 2012 | A1 |
| 20120269666 | Lin et al. | Oct 2012 | A1 |
| 20120285454 | Nibu et al. | Nov 2012 | A1 |
| 20120319543 | Adachi et al. | Dec 2012 | A1 |
| 20130098359 | Becker et al. | Apr 2013 | A1 |
| 20130152918 | Rummery | Jun 2013 | A1 |
| 20130164158 | Matsuba et al. | Jun 2013 | A1 |
| 20130280055 | Daly et al. | Oct 2013 | A1 |
| 20130298908 | Tang et al. | Nov 2013 | A1 |
| 20130306072 | Moir | Nov 2013 | A1 |
| 20130340757 | Smith et al. | Dec 2013 | A1 |
| 20140007871 | Bordewick et al. | Jan 2014 | A1 |
| 20140020684 | Klasek et al. | Jan 2014 | A1 |
| 20140034633 | Heintz et al. | Feb 2014 | A1 |
| 20140041663 | Daly et al. | Feb 2014 | A1 |
| 20140069432 | Mebasser et al. | Mar 2014 | A1 |
| 20140090645 | Sears et al. | Apr 2014 | A1 |
| 20140131904 | Tang et al. | May 2014 | A1 |
| 20140138804 | Takizawa et al. | May 2014 | A1 |
| 20140158131 | Kenyon et al. | Jun 2014 | A1 |
| 20140166007 | Bordewick et al. | Jun 2014 | A1 |
| 20140178079 | Yagisawa et al. | Jun 2014 | A1 |
| 20140202460 | Bath et al. | Jul 2014 | A1 |
| 20140205513 | Affaitati | Jul 2014 | A1 |
| 20140216460 | Bothma | Aug 2014 | A1 |
| 20140227091 | Kenyon et al. | Aug 2014 | A1 |
| 20140242816 | Rathburn | Aug 2014 | A1 |
| 20140261422 | Lang et al. | Sep 2014 | A1 |
| 20140264975 | Bath et al. | Sep 2014 | A1 |
| 20140299132 | Librett et al. | Oct 2014 | A1 |
| 20140332001 | Bath et al. | Nov 2014 | A1 |
| 20150000653 | Miller | Jan 2015 | A1 |
| 20150000655 | Desilva et al. | Jan 2015 | A1 |
| 20150000662 | Williams et al. | Jan 2015 | A1 |
| 20150000663 | Williams et al. | Jan 2015 | A1 |
| 20150000664 | Desilva et al. | Jan 2015 | A1 |
| 20150000669 | Miller | Jan 2015 | A1 |
| 20150003966 | Duquette | Jan 2015 | A1 |
| 20150007815 | Duquette et al. | Jan 2015 | A1 |
| 20150030317 | Bayer et al. | Jan 2015 | A1 |
| 20150047639 | Farrugia et al. | Feb 2015 | A1 |
| 20150122685 | Wakeham et al. | May 2015 | A1 |
| 20150136140 | Kenyon et al. | May 2015 | A1 |
| 20150136467 | Rathburn | May 2015 | A1 |
| 20150157818 | Darby et al. | Jun 2015 | A1 |
| 20150158478 | Stahr et al. | Jun 2015 | A1 |
| 20150190605 | Martin et al. | Jul 2015 | A1 |
| 20150230289 | Corona | Aug 2015 | A1 |
| 20150230750 | McDarby et al. | Aug 2015 | A1 |
| 20150231358 | Smith et al. | Aug 2015 | A1 |
| 20150250963 | Ramanan et al. | Sep 2015 | A1 |
| 20150290415 | Dunn | Oct 2015 | A1 |
| 20150301567 | Chen et al. | Oct 2015 | A1 |
| 20150320960 | Barlow et al. | Nov 2015 | A1 |
| 20150328418 | Bothma et al. | Nov 2015 | A1 |
| 20150335846 | Romagnoli et al. | Nov 2015 | A1 |
| 20160010649 | Aiello | Jan 2016 | A1 |
| 20160015919 | Librett et al. | Jan 2016 | A1 |
| 20160022954 | Bath et al. | Jan 2016 | A1 |
| 20160045693 | Librett et al. | Feb 2016 | A1 |
| 20160087505 | Turner et al. | Mar 2016 | A1 |
| 20160114121 | Holley et al. | Apr 2016 | A1 |
| 20160192507 | Rathburn | Jun 2016 | A1 |
| 20160199612 | Foote et al. | Jul 2016 | A1 |
| 20160303343 | Virr et al. | Oct 2016 | A1 |
| 20160310691 | Bath et al. | Oct 2016 | A1 |
| 20160317775 | Smith et al. | Nov 2016 | A1 |
| 20160333885 | Daly et al. | Nov 2016 | A1 |
| 20160339193 | Daly et al. | Nov 2016 | A1 |
| 20160346499 | Williams et al. | Dec 2016 | A1 |
| 20169512856 | Nibu et al. | Dec 2016 | |
| 20170082116 | Nibu et al. | Mar 2017 | A1 |
| 20170087327 | Crumblin et al. | Mar 2017 | A1 |
| 20170087328 | Mayer et al. | Mar 2017 | A1 |
| 20170114801 | Duquette | Apr 2017 | A1 |
| 20170151401 | Darby et al. | Jun 2017 | A9 |
| 20170157347 | Jones et al. | Jun 2017 | A1 |
| 20170182270 | Kenyon et al. | Jun 2017 | A1 |
| 20170204868 | Oshita et al. | Jul 2017 | A1 |
| 20170232221 | Kepler et al. | Aug 2017 | A1 |
| 20170248145 | Chu | Aug 2017 | A1 |
| 20170312473 | Desilva et al. | Nov 2017 | A1 |
| 20170326329 | Maurer et al. | Nov 2017 | A1 |
| 20170340847 | Taylor et al. | Nov 2017 | A1 |
| 20170350737 | Desilva et al. | Dec 2017 | A1 |
| 20180008795 | Smith et al. | Jan 2018 | A1 |
| 20180142690 | Row et al. | May 2018 | A1 |
| 20180156233 | Sawada et al. | Jun 2018 | A1 |
| 20190001091 | Bath et al. | Jan 2019 | A1 |
| Number | Date | Country |
|---|---|---|
| 741687 | Jul 2000 | AU |
| 2003204474 | Jan 2004 | AU |
| 2009288026 | Mar 2010 | AU |
| 2014250602 | Nov 2014 | AU |
| 1289037 | Sep 1991 | CA |
| 2636623 | Jul 2007 | CA |
| 2721674 | Oct 2009 | CA |
| 2778080 | Apr 2011 | CA |
| 2840594 | Jan 2013 | CA |
| 1266150 | Sep 2000 | CN |
| 101296722 | Oct 2008 | CN |
| 101321958 | Dec 2008 | CN |
| 101449064 | Jun 2009 | CN |
| 101466429 | Jun 2009 | CN |
| 101553667 | Oct 2009 | CN |
| 101836348 | Sep 2010 | CN |
| 201805562 | Apr 2011 | CN |
| 102832734 | Dec 2012 | CN |
| 106849411 | Jun 2017 | CN |
| 3310376 | Sep 1984 | DE |
| 4020522 | Jan 1992 | DE |
| 102005000819 | Jul 2006 | DE |
| 102007026565 | Dec 2007 | DE |
| 0634588 | Jan 1995 | EP |
| 1035330 | Sep 2000 | EP |
| 1064042 | Jan 2001 | EP |
| 1123674 | Aug 2001 | EP |
| 1 147 004 | Oct 2001 | EP |
| 1205203 | May 2002 | EP |
| 1210139 | Jun 2002 | EP |
| 1205203 | Jul 2002 | EP |
| 1205203 | Sep 2004 | EP |
| 1638503 | Mar 2006 | EP |
| 1638631 | Mar 2006 | EP |
| 1648544 | Apr 2006 | EP |
| 1662148 | May 2006 | EP |
| 1669098 | Jun 2006 | EP |
| 1760319 | Mar 2007 | EP |
| 1760319 | Jul 2007 | EP |
| 1824542 | Aug 2007 | EP |
| 1924311 | May 2008 | EP |
| 1933910 | Jun 2008 | EP |
| 2000675 | Dec 2008 | EP |
| 2010260 | Jan 2009 | EP |
| 2012858 | Jan 2009 | EP |
| 2098260 | Sep 2009 | EP |
| 2112938 | Nov 2009 | EP |
| 2308539 | Apr 2011 | EP |
| 2317150 | May 2011 | EP |
| 2337604 | Jun 2011 | EP |
| 2345443 | Jul 2011 | EP |
| 2345449 | Jul 2011 | EP |
| 2355880 | Aug 2011 | EP |
| 2392375 | Dec 2011 | EP |
| 2440277 | Apr 2012 | EP |
| 2464404 | Jun 2012 | EP |
| 2470246 | Jul 2012 | EP |
| 2471568 | Jul 2012 | EP |
| 2494213 | Sep 2012 | EP |
| 2496297 | Sep 2012 | EP |
| 2501439 | Sep 2012 | EP |
| 2572747 | Mar 2013 | EP |
| 2694146 | Feb 2014 | EP |
| 2731656 | May 2014 | EP |
| 2809383 | Dec 2014 | EP |
| 2910271 | Aug 2015 | EP |
| 2968804 | Jan 2016 | EP |
| 2968805 | Jan 2016 | EP |
| 2968829 | Jan 2016 | EP |
| 2992921 | Mar 2016 | EP |
| 3013397 | May 2016 | EP |
| 3013398 | May 2016 | EP |
| 3013399 | May 2016 | EP |
| 3013400 | May 2016 | EP |
| 3013402 | May 2016 | EP |
| 3014224 | May 2016 | EP |
| 3014225 | May 2016 | EP |
| 3082920 | Oct 2016 | EP |
| 3148418 | Apr 2017 | EP |
| 3148419 | Apr 2017 | EP |
| 3149696 | Apr 2017 | EP |
| 3160561 | May 2017 | EP |
| 3160562 | May 2017 | EP |
| 3160564 | May 2017 | EP |
| 3213788 | Sep 2017 | EP |
| 3219350 | Sep 2017 | EP |
| 3311869 | Apr 2018 | EP |
| 3311871 | Apr 2018 | EP |
| 2 617 250 | Dec 1988 | FR |
| 2617250 | Dec 1988 | FR |
| 2 826 412 | Dec 2002 | FR |
| 2826412 | Dec 2002 | FR |
| 2901998 | Dec 2007 | FR |
| 144627 | Jul 1920 | GB |
| 146832 | Dec 1920 | GB |
| 525 551 | Aug 1940 | GB |
| 948382 | Feb 1964 | GB |
| 948382 | Feb 1964 | GB |
| 1041313 | Sep 1966 | GB |
| 2217924 | Nov 1989 | GB |
| 58133153 | Aug 1983 | JP |
| H09172748 | Jun 1997 | JP |
| 3060967 | Sep 1999 | JP |
| 2002-511786 | Apr 2002 | JP |
| 4046539 | Oct 2003 | JP |
| 2004-353655 | Dec 2004 | JP |
| 2007-506482 | Mar 2007 | JP |
| 2007-518497 | Jul 2007 | JP |
| 2009-533153 | Sep 2009 | JP |
| 2013-501541 | Jan 2013 | JP |
| 544142 | Jan 2009 | NZ |
| 544765 | Jan 2009 | NZ |
| 573198 | Jun 2010 | NZ |
| 573227 | Jul 2010 | NZ |
| 575332 | Oct 2010 | NZ |
| 564886 | Feb 2011 | NZ |
| 579384 | May 2011 | NZ |
| 585403 | Oct 2011 | NZ |
| 585404 | Oct 2011 | NZ |
| 585683 | Dec 2011 | NZ |
| 587113 | Dec 2011 | NZ |
| 586325 | Jan 2012 | NZ |
| 589766 | May 2012 | NZ |
| WO 8701599 | Mar 1987 | WO |
| WO 1999013931 | Mar 1999 | WO |
| WO 199922794 | May 1999 | WO |
| WO 0076053 | Dec 2000 | WO |
| WO 0110002 | Feb 2001 | WO |
| WO 2002049188 | Jun 2002 | WO |
| WO 2004108198 | Dec 2004 | WO |
| WO 2004112873 | Dec 2004 | WO |
| WO 2007019628 | Feb 2007 | WO |
| WO 2007024955 | Mar 2007 | WO |
| WO 2007024956 | Mar 2007 | WO |
| WO 2007038152 | Apr 2007 | WO |
| WO 2007048206 | May 2007 | WO |
| WO 2007117716 | Oct 2007 | WO |
| WO 2007134405 | Nov 2007 | WO |
| WO 2007149446 | Dec 2007 | WO |
| WO 2008028247 | Mar 2008 | WO |
| WO 2008051534 | May 2008 | WO |
| WO 2008092235 | Aug 2008 | WO |
| WO 2008102216 | Aug 2008 | WO |
| WO 2010028121 | Mar 2010 | WO |
| WO 2010084183 | Jul 2010 | WO |
| WO 2010096467 | Aug 2010 | WO |
| WO 2011017763 | Feb 2011 | WO |
| WO 2011022557 | Feb 2011 | WO |
| WO 2011022779 | Mar 2011 | WO |
| WO 2011051462 | May 2011 | WO |
| WO 2011054038 | May 2011 | WO |
| WO 2011062633 | May 2011 | WO |
| WO 2011112807 | Sep 2011 | WO |
| WO 2011116428 | Sep 2011 | WO |
| WO 2012024740 | Mar 2012 | WO |
| WO 2012094230 | Jul 2012 | WO |
| WO 2012113027 | Aug 2012 | WO |
| WO 2012135912 | Oct 2012 | WO |
| WO 2012145358 | Oct 2012 | WO |
| WO 2012174602 | Dec 2012 | WO |
| WO 2013009193 | Jan 2013 | WO |
| WO 2013020167 | Feb 2013 | WO |
| WO 2013152403 | Oct 2013 | WO |
| WO 2013163685 | Nov 2013 | WO |
| WO 2013163687 | Nov 2013 | WO |
| WO 2013173219 | Nov 2013 | WO |
| WO 2014007655 | Jan 2014 | WO |
| WO 2014097030 | Jun 2014 | WO |
| WO 2014138804 | Sep 2014 | WO |
| WO2015120521 | Sep 2014 | WO |
| WO 2014184377 | Nov 2014 | WO |
| WO 2014201513 | Dec 2014 | WO |
| WO2014205513 | Dec 2014 | WO |
| WO2015000025 | Jan 2015 | WO |
| WO2015048857 | Apr 2015 | WO |
| WO2015058255 | Apr 2015 | WO |
| WO2015061848 | May 2015 | WO |
| WO2015089582 | Jun 2015 | WO |
| WO2015120522 | Aug 2015 | WO |
| WO2015131219 | Sep 2015 | WO |
| WO2015179915 | Dec 2015 | WO |
| WO2015179916 | Dec 2015 | WO |
| WO2015179917 | Dec 2015 | WO |
| WO2015188227 | Dec 2015 | WO |
| WO2015192186 | Dec 2015 | WO |
| WO2015196255 | Dec 2015 | WO |
| WO2016000040 | Jan 2016 | WO |
| WO 2016009771 | Jan 2016 | WO |
| WO2016019292 | Feb 2016 | WO |
| WO2016029265 | Mar 2016 | WO |
| WO 2016194697 | Dec 2016 | WO |
| WO 2017006189 | Jan 2017 | WO |
| WO 2017027906 | Feb 2017 | WO |
| WO 2017068530 | Apr 2017 | WO |
| Entry |
|---|
| US 8,334,630 B2, 12/2012, Saban et al. (withdrawn) |
| European Patent Office, Supplementary European Search Report, Application No. EP 18 79 0549, dated Nov. 26, 2020, in 7 pages. |
| Patent Cooperation Treaty, International Search Report, Application No. PCT/NZ2018/050056, dated Sep. 11, 2018, in 32 pages. |
| China National Intellectual Property Administration, First Office Action and Search Report, Application No. 201880038646.5, dated Jan. 29, 2021 in 11 pages. |
| Examination Report for Australian Application No. 2013285620, dated Nov. 9, 2016; 3 pages. |
| Examination Report for Australian Application No. 2017204037, dated Nov. 16, 2017; 3 pages. |
| Examination Report No. 2 for Australian Application No. 2017204037, dated Jan. 3, 2018; 2 pages. |
| Examination Report No. 1 for Australian Application No. 2018203077, dated Dec. 13, 2019; 7 pages. |
| Examination Report for Canadian Application No. 2,840,594, dated Mar. 22, 2019; 3 pages. |
| Examination Report for Canadian Application No. 2,912,244, dated Nov. 5, 2018; 5 pages. |
| Examination Report for Canadian Application No. 2,912,244, dated Sep. 10, 2019; 5 pages. |
| China First Office Action; 201280034511.4; dated Jul. 29, 2015; 28 pages. |
| China First Office Action; 201380018302.5; dated Nov. 4, 2015; 9 pages. |
| Office Action issued in Chinese Patent Application No. 201710227593.9, dated Jan. 24, 2019, in 7 pages. |
| Office Action; Chinese Application No. 201710227593.9, dated Sep. 18, 2019; 9 pages. |
| China First Office Action; Application No. 2018062302200570; dated Jul. 3, 2018; 5 pages. |
| European Patent Office, Extended European Search Report, Application No. 13812942.4, dated Apr. 12, 2018, in 18 pages. |
| Extended European Search Report for European Patent Application No. 17157168.0, dated Jun. 12, 2017, in 7 pages. |
| Extended European Search report for European Patent Application No. 18194574.2, dated Apr. 3, 2019 in 9 pages. |
| International Search Report; PCT/IB2013/060549; dated Mar. 19, 2014; 5 pages. |
| Written Opinion; PCT/IB2013/060549, dated Mar. 19, 2014; 6 pages. |
| Japanese Examination Report with English Translation, dated Dec. 19, 2016; 8 pages. |
| Office Action issued in Japanese Patent Application No. 2017-189343, dated Sep. 12, 2018, in 6 pages. |
| International Search Report; PCT/NZ2012/000124; dated Oct. 29, 2012; 6 pages. |
| Written Opinion; PCT/NZ2012/000124; dated Oct. 29, 2012; 9 pages. |
| Sep. 24, 2013 International Search Report and Written Opinion for Application No. PCT/NZ2013/000006 filed on Feb. 1, 2013. |
| European Communication; 13812942.4; dated Nov. 21, 2018; 6 pages. |
| Australian Office Action; 2018200350; dated Dec. 17, 2018; 4 pages. |
| Australian Office Action; 2017261486; dated Jan. 23, 2019; 3 pages. |
| Australian Office Action; 2018200350; date Nov. 13, 2019; 3 pages. |
| http://www.broadleyjames.com/bionet-parts-list/rushton-60mm-5-7l.html. |
| http://www.fao.org/docrep/010/ah810e/ah810e07.htm. |
| Number | Date | Country | |
|---|---|---|---|
| 20200124104 A1 | Apr 2020 | US |
| Number | Date | Country | |
|---|---|---|---|
| 62586482 | Nov 2017 | US | |
| 62488845 | Apr 2017 | US |
