This patent application claims priority to and the benefit of French Patent Application No. 1650433, which was filed on Jan. 20, 2016, the entire contents of which are incorporated herein by reference.
The present disclosure relates to a gas fixing tool.
So-called gas sealing or fixing tools comprise an internal combustion engine operated by igniting an air-fuel mixture in a combustion chamber. An injection device injects the fuel (which can be made of gasoline, alcohol, and the like in liquid and/or gaseous form) into the chamber from a fuel cartridge. These tools are configured to drive fixing elements (such as hooks, nails, points, staples, or pins) into support materials (such as wood, concrete, or steel) to attach parts there.
In general, such a tool is portable and comprises a housing in which the internal combustion engine is mounted, propelling a piston that drives a fixing element. Such a tool can also comprise an electric power supply battery and a handle for grasping, holding, and firing, and on which a trigger is mounted.
A firing cycle comprises several steps such as the distribution of a quantity of fuel by the cartridge, the admission of the fuel into the chamber, the mixing of the fuel with the air in the chamber, the ignition and the combustion of the air-fuel mixture for the driving of the piston, and the evacuation of the combustion gases from the chamber.
A combustion chamber comprises a gas admission valve. This valve comprises a body that is movable between a first closing position and a second opening position of a gas admission orifice.
The first steps of a firing cycle are brought about by bearing the tool against the support material in which a fixing element is going to be anchored. This bearing causes fuel to be injected into the combustion chamber via the admission valve. The user of the tool must then manually depress the trigger of the tool to close the admission chamber and produce a spark in the chamber, resulting in an igniting of the air-fuel mixture in the chamber.
Ideally, the igniting of this mixture should occur in a very definite period of time. If the ignition occurs too early because the user has depressed the trigger too soon (while bearing the tool against the support material, for example), the air-fuel mixture might not be optimal and a poor combustion of this mixture might occur in the chamber. If the ignition occurs too late because the user has depressed the trigger too late (several seconds after bearing the tool against the support material), the air-fuel mixture injected into the chamber might be partly evacuated into the atmosphere and thus not be sufficient in quantity for its ignition to occur.
The diffusion of the air-fuel mixture contained in the chamber into the atmosphere after a predetermined time from bearing the tool against the material (typically on the order of a few seconds) is necessary for reasons of safety. In particular, this avoids the risk of too large a quantity of fuel building up in the combustion chamber when the tool is placed against the support material on several occasions close together.
Thus, there is a need to guarantee that the ignition of the mixture in the chamber does not occur too soon during a firing cycle.
The present disclosure provides a simple, effective, and economical solution to this problem.
The present disclosure concerns a gas fixing tool comprising:
characterized in that the tool further comprises a safety member configured to cooperate on the one hand with the actuating member and on the other hand with the trigger, so that the trigger is locked in its first position when the actuating member is in its first position.
The present disclosure thus makes it possible to guarantee the locking of the trigger in its first position of rest as long as the actuating member has not reached its second position. It will thus be understood that the user cannot activate the trigger until the tool is placed against the support material, and will not be able to activate it when the actuating member is moving between its first and its second position. Only when the actuating member is in its second position can the trigger be activated, which makes sure that the air-fuel mixture injected into the chamber will be optimal for its ignition. This is made possible by the safety member that cooperates with the actuating member and the trigger.
The tool according to the present disclosure may comprise one or more of the following characteristics, taken in isolation from each other or in combination with each other:
The present disclosure likewise concerns a gas fixing tool comprising:
characterized in that the tool comprises a mechanism to control the movement of the movable body, the mechanism being configured to cooperate on the one hand with the trigger or a member connected to the trigger and on the other hand with the movable element, so that the movement of the trigger from its first position to its second position causes the movement of the movable body from its first to its second position.
The tool according to the present disclosure may comprise one or more of the following characteristics, taken in isolation from each other or in combination with each other:
The present disclosure will be better understood, and other details, characteristics, and advantages of the present disclosure will appear more clearly upon reading the following description (which is a nonlimiting example) and making reference to the accompanying drawings.
The tool 10 represented in
The housing 12 of the tool has an axis 20 along which move the driving piston and, in the guide tip 18, the fixing elements.
The tool 10 comprises a handle 22 for grasping and manipulating the tool. This extends substantially perpendicular to the axis 20, being slightly slanted with respect to it depending on the application of the tool and the ergonomics during its use. The handle 22 likewise serves for firing by a trigger 23 mounted thereon.
The handle 22 defines a rear portion 12b of the housing 12 and the feeding magazine 16 is lodged in a front portion 12a of the housing, which extends substantially in parallel with the handle 22, that is, substantially perpendicular to the axis 20 or slightly slanted relative to this axis.
In the example shown, the housing 12 moreover comprises an upper portion 12c extending along the axis 20 and connecting the upper ends of the front 12a and rear 12b portions of the housing, and a lower portion 12d extending in parallel with the axis 20 and connecting the lower ends of the front 12a and rear 12b portions of the housing.
The shell comprises several seats and arrangements for mounting of internal elements of the tool, which can be seen in their mounting position in
First of all, the feeding magazine 16 for feeding fixing elements, which is configured to be lodged in the front portion 12a of the housing 12, is shown. The boxes 24 and 26 defining the thermal engine, and more particularly a precombustion chamber 28, a combustion chamber 30, and a working chamber 32 in which the aforementioned piston is mounted in sliding manner, are also shown.
The box 24 defining the chamber 28 is configured to be lodged in the handle 22, that is, in the rear portion 12b of the housing. The box 26 defines the combustion chamber 30 and the working chamber 32 and it is configured to extend in the upper portion 12c of the housing. The magazine 16 and the box 24 are substantially parallel to each other and perpendicular to the box 26 that extends between the magazine 16 and the box 24.
The magazine 16 has an elongated shape and delivers the fixing elements by its upper longitudinal end, which is connected to the guide tip 18. The box 24 has an elongated shape, generally cylindrical, and it extends substantially the entire longitudinal dimension of the handle 22. Finally, the box 26 has an elongated shape and comprises a rear end defining the chamber 30 and connected to the upper end of the box 24 and a front end connected to the guide tip 18.
At the free end, here in front, of the guide tip 18 there is provided a bearing member 34 configured to bear against the support material. As will be explained in further detail in the following, this bearing action causes the distribution of a predetermined quantity of fuel to the precombustion chamber 28 and is thus necessary to produce a firing, that is, a projecting of a fixing element.
The feeding of fuel to the precombustion chamber 28 is done by way of an injection device 36 from a fuel gas cartridge 38.
The cartridge 38 and a part (front) of the injection device 36 are lodged in the front portion 12a of the housing 12, and the rest of the device 36 extends between the cartridge and the chamber 28 in the lower portion 12d of the housing.
The fuel is in the liquid state in the cartridge 38 and needs to be evaporated, the combustible gas being intended to be mixed with air before being burned in the chambers 28 and 30.
The injection device 36 of a gas fixing tool generally makes possible the evaporation of the fuel, its mixing with air, and the injection of this mixture into the chamber 28.
A valve 40 configured to calibrate a quantity of liquid fuel is interposed between the liquid fuel cartridge 38 and an evaporator unit 42. A filter can be arranged in a seat or bore provided in the unit 42. A predetermined quantity of liquid fuel is discharged from the cartridge 38 by way of the valve 40 in the unit 42, passing through the filter, and it arrives in an evaporation cavity. The unit 42 is made of thermally conductive material, such as a metal. The liquid fuel circulating through the filter is at least partly converted into gaseous fuel thanks to the input of heat from the surroundings, which transmit calories to the evaporator unit 42.
Downstream from the filter and the evaporation cavity, the fuel at least partly vaporized continues to circulate in the unit 42, and it absorbs additional heat from the surroundings. The downstream part of the unit 42 contains an evaporation line 48, acting as a distribution manifold, to the precombustion chamber 28 of the fixing tool.
The dimensional parameters of the device 36, and in particular of the evaporation cavity and the line 48, such as the length, the diameter, the thickness, etc., are configured so the fuel is entirely converted into gas upon exiting from a discharge orifice downstream from the line 48. To aid in the transfer of heat from the surroundings, the unit 42 and/or the line 48 can possibly have one or more fins disposed at least on one of their surfaces.
Emerging from the discharge orifice, the gaseous fuel can be directly injected into the precombustion chamber 28. As an option, the gaseous fuel leaving the discharge orifice can feed one or more nozzles for the exiting of the fuel and the feeding of the precombustion chamber 28. The fuel gas in one variant can feed a jet pump 46 of the venturi type, in which ambient air is entrained into the jet pump 46 and mixed with the gaseous fuel injected by the one or more nozzles, so as to form an air-fuel mixture for the feeding of the chamber 28.
The line 48 can be formed of a single piece with a part of the evaporator unit 42. The line 48 has a general S or L shape.
The evaporator unit 42 comprises a bore in which an actuating element 50 is mounted and able to slide along the longitudinal axis X of the cartridge 38. This actuating element 50 has an elongated rectilinear shape and comprises an internal bore, for example in the shape of a T or L. This bore comprises a first axial portion which extends along the element 50 and emerges at its lower end, and a radial portion which extends between the upper end of the axial portion and the periphery of the element. The mouth of this radial portion is situated opposite the aforementioned filter of the evaporator unit 42.
The element 50 is movable between two positions: a high or resting position represented in
The movement of the element 50 from its resting position to its working position causes the release of a calibrated quantity of fuel from the cartridge 38. This fuel, in liquid form, circulates in the bore of the element 50 and crosses the filter of the evaporator unit 42, which holds back any impurities, before entering the evaporation cavity of the unit in which the transformation of the liquid fuel into gaseous fuel is initiated. The fuel circulates in the line 48 to complete its evaporation and arrives in the gaseous state in the area of the aforementioned nozzle. It is then atomized in the jet pump and mixed with air entering the pump by the venturi effect, the air-fuel mixture being then injected into the chamber 28 of the thermal engine.
Advantageously, and as represented in
As mentioned above, the thermal engine of the tool comprises a precombustion chamber 28, a combustion chamber 30, and a working chamber 32 in which the driving piston of a fixing element is able to move under the effect of the explosion of the air-fuel mixture in the combustion chamber 30.
The precombustion chamber 28 makes it possible to initiate the combustion of the air-fuel mixture. This chamber 28 comprises a cavity in which an ignition device such as a spark plug is installed.
The chambers 28, 30 are separated from each other by a valve 52 visible in
The mixture arrives in the chamber 30 with a relatively elevated pressure. The flame issuing from the chamber 28 reaches the chamber 30, the combustion at elevated pressure in the chamber 30 making it possible to improve the performance of the tool. The combustion in the chamber 30 produces a pressure rise in the chamber 30, which forces the piston to move into the working chamber 32.
In the example represented, the member 60 has a general L shape and comprises two arms 60a and 60b that are joined together. A first arm 60a, of greater length, has one free end and an opposite end connected to the second arm 60b, of shorter length. The ends of the arms 60a, 60b are joined together by a substantially cylindrical pin 62 defining a pivot axis Y for the member 60. The pivot Y axis is substantially perpendicular to a plane passing through the arms 60a and 60b. As can be seen in
The pin 62 has an elongated shape along the pivot axis Y and comprises a cylindrical peg 64 at each of its longitudinal ends. Each peg 64 is centered and guided in rotation in a complementary cylindrical seat 66 of a shell of the housing (
The free end of the arm 60a is configured to cooperate directly or by way of a suitable mechanism (such as a mechanical linkage) with the bearing member 34. The end of the arm 60b opposite the pin 62 is configured to cooperate by bearing engagement with the actuating element 50 of the device 36. This end of the arm is outfitted here with a roller 68 or a shoe, optionally mounted to rotate about an axis parallel to the pivot axis Y, at this end of the arm, and configured to cooperate by bearing engagement with the actuating element 50.
As is seen in particular in
The member 60 is movable by pivoting between a first position of rest, represented in
The pivoting of the member 60 here is brought about by the bearing of the tool 10, and more particularly its bearing member 34, against the support material. When the tool is not applied by way of its bearing member 34 against the support material, the member 60 is in its first position. The bearing of the tool against the support material causes the movement of the bearing member 34 with respect to the guide tip 18, which in turn causes the pivoting of the member 60 from its first to its second position.
The configuration of the member 60 and in particular the difference in length of the arms 60a and 60b makes it possible to exploit a leverage effect in the actuation of the device 36. That is, a mere bearing of the tool against the support material, the weight of the tool alone being enough to ensure the movement of the bearing member 34 from its first to its second position, is enough to actuate the distribution of fuel by the device 36 on account of the transmission of forces achieved by the member 60. The forces are transmitted by the end of the arm 60b or the roller to the actuating element 50 which is moved from its high position (
In the example shown, the member 70 has an elongated shape extending substantially along the axis 20 of the tool. It is lodged here in the upper portion 12c of the housing, just below the box 26 and the working chamber 32.
The member 70 comprises a front foot 70a and a rear leg 70b. The front foot 70a is substantially planar. Its free front end is configured to cooperate by bearing engagement with the free end of the arm 60a of the member 60. This end is outfitted here with a roller 72 or a shoe, mounted optionally able to rotate about an axis parallel to the pivot axis Y, on this end of the arm, and configured to cooperate by bearing engagement with the member 60.
The foot 70a comprises a slot 73 substantially passing through its center (in a direction parallel to the axis X lying in the plane passing through the axes 20 and X) in which is lodged a return device such as a compression spring 74. The axis of the spring 74 is contained in the plane of the foot and is substantially parallel to the axis 20 and/or to the axis of extension of the member 70. The foot 70a comprises, inside the slot 73, a cylindrical peg 76 engaging with the spring 74 to maintain it and guide its compression. The compression spring 74 may be deformed in the slot 73 of the foot 70a. Finally, the foot 70a comprises, between the roller 72 and the spring 74, at the base of the peg 76, abutment components in the axial direction (along the axis of extension of the member 70) that are formed here by two transverse and coplanar ribs 78 situated respectively on the upper and lower faces of the foot 70a.
As can be seen in
The rear leg 70b of the member 70 has a substantially rectilinear shape and extends from the rear end of the foot 70a. The leg 70b comprises at its rear end a flange 82 oriented toward the bottom and configured to cooperate by bearing or abutment engagement with the trigger 23 for purposes of locking it in its position of rest.
The member 70 can move in translation between a first position of rest, represented in
The movement of the member 70 here is caused by the bearing engagement of the tool, and more precisely by the pivoting of the member 60. When the member 60 is in its first position, the free end of its arm 60a is at a distance from the member 70 which remains in its front position of rest (
It is therefore seen that the translation, here toward the rear, of the member 70 will cause a movement toward the rear of the flange 82 locking the trigger 23.
The trigger 23 of the tool is more visible in
The trigger 23 likewise comprises at its upper end an abutment component configured to cooperate with the flange 82 of the member 70. In the example shown, the trigger 23 comprises an upper lug 86 whose upper face 86a, here being planar, is configured to cooperate by bearing or abutment engagement, with the lower free end of the flange 82.
As can be seen in the drawings, when the members 60 and 70 are in their positions of rest (
The trigger 23 comprises gear teeth 88 for engaging, here by way of a pinion 90 represented in
The trigger 23 comprises two series of teeth 88 which are disposed in parallel planes substantially perpendicular to the axis Z. Each series of teeth 88 forms a gear sector, extending about the axis Z. The series of teeth are separated from each other by a recess 94 of the trigger 23. The teeth 88 are situated at the rear end of the trigger in the area of lateral walls of the trigger, and the recess 94 emerges toward the rear between these walls.
The pinion 90 is movable in rotation about an axis V parallel to the axes Y and Z. It comprises two coaxial cylindrical pegs 96 for centering and guiding the pinion in rotation, which are configured to being lodged respectively in seats 96a of complementary shape in the shells of the housing (
The pinion 90 comprises, between the pegs 96, two or three annular rows of teeth. It comprises a first annular row of teeth 100a configured to being lodged in the recess 94 of the trigger and able to move freely within this recess. Furthermore, it comprises at least one annular row of teeth 100b configured to being intermeshed with the teeth 88 of the trigger 23. These teeth 100b can be situated on either side of the teeth 100a, the pinion thus comprising two annular rows of teeth 100b separated from each other by the teeth 100a. As a variant, the teeth 100b can extend between the teeth 100a and have a width larger than that of the teeth 100a so that they protrude on either side from the teeth 100a and can intermesh with the teeth 88 of the trigger. As can be seen in
The rack 92 is formed by a longitudinal element such as a ruler, one portion of whose longitudinal end, here the upper one, comprises rack teeth 93. These rack teeth 93 are configured to cooperate with the teeth 100a of the pinion 90, as illustrated in
The rack 92 here has substantially a T shape in cross section and comprises two coplanar longitudinal lateral flanges 97 which cooperate by sliding with longitudinal flanges 98 having substantially an L cross section of the box 24. The flanges 98 can be formed by a single piece with the box 24. The flanges 98 form a slideway inside which the rack 92 can slide along the longitudinal axis of the box 24 and of the chamber 28.
The rack 92 is guided in translation with respect to the box 24 by the flanges 98. The rack 92 is movable between a first position of rest, the high position here, and a second or low position. It is biased in its first position by an elastic return device, such as compression springs 101 (
The rack 92 comprises at its lower longitudinal end a tongue 107 which is oriented substantially perpendicular to the axis of extension of the rack and on the side with the box 24. The tongue 107 here is formed as a single piece with the T-shaped part. This tongue 107 passes through a slot of the box 24 and can slide into this slot during the movements of the rack 92.
The movable body 112b has a piston shape and carries a gasket 116 at its periphery, configured to cooperate with a peripheral edge of the evacuation orifice. The movable body 108b has a hollow cylindrical shape and carries a gasket 118 at its periphery, configured to cooperate with a peripheral edge of the chamber 28. The fixed body 108a is configured to being engaged with the lower end of the movable body 108b and it has a complementary shape, here cylindrical, to the internal bore of the movable body 108b. This fixed body 108a carries a gasket 120 at its periphery, configured to cooperate with the internal cylindrical surface of the movable body 108b. The movable body 108b is connected to the lower end of the rod 114 by way of two arms 122 extending upward in the prolongation of the movable body. These arms 122 here are diametrically opposite in relation to the longitudinal axis of the chamber 28 and of the box 24.
The movable body 108b of the admission valve 108 comprises an external annular groove 124 in which is engaged the tongue 107 of the rack 92, as can be seen in
The description of the overall functioning of the tool of the embodiment as described above will now be resumed by referring to
The actuating of the element 50 causes the releasing of a predetermined quantity of fuel, which is mixed with air and injected in the precombustion chamber 28 through its admission orifice 110, the valve 108 being opened (the movable body 108b being in high position).
The translation of the member 70, and thus of its flange 82, makes it possible to unlock the trigger 23.
The different members and parts of the tool 110 of this variant are similar to those of the tool 10, except for the actuating member 160, the safety member 170, the trigger 123, and the longitudinal element 192, which are described in the following.
The actuating member 160 of the injection device (not shown) is distinguished from that 60 described in the foregoing in that it comprises a third arm 160c. This third arm 160c extends backward and upward from the middle of the arm 160a configured to cooperate (directly or indirectly) with the bearing member (not visible). The arms 160a, 160c thus substantially form a Y. The free end of the arm 160c is in the shape of a fork 161 with two lateral branches, whose upper free ends here are folded back toward the front and/or the free end of the arm 160a.
This member 160 is configured here to cooperate by bearing engagement with the actuating element of the injection device, as described above.
Unlike the previous embodiment, the free end of the arm 160a is configured to cooperate only (directly or by way of an appropriate mechanism) with the bearing member of the tool. This end is not configured to cooperate with the member 170. It is the free end or fork 161 of the arm 160c which is configured to cooperate by bearing or abutment engagement with the member 170.
The member 160 is movable by pivoting between a first position of rest, shown in
The pivoting of the member 160 is caused here by the bearing of the tool 110, and more particularly its bearing member, against the support material. When the tool has not been applied by way of its bearing member against the support material, the member 160 is in its first position. The bearing of the tool against the support material causes the movement of the bearing member with respect to the guide tip, which in turn causes the pivoting of the member 160 from its first to its second position.
The safety member 170, which enables the locking of the trigger 123 in its position of rest, is configured here to cooperate with the actuating member 160, the trigger 123, as well as the longitudinal element 192.
In the example shown, the member 170 has an elongated shape and is mounted pivotably about an axis S substantially parallel to the pivoting axis Y of the member 160. The member 170 comprises two coaxial lateral pegs 171 in the vicinity of its front end, which define the axis S. They are configured to be mounted in rotary manner in seats of complementary shape in the shells of the housing. The portion of the member 170 extending forward from the axis S has a shorter length than that which extends backward from this axis S in the example shown.
The front portion of the member 170 (in front of the pegs 171) extends between the branches of the fork 161 and carries at its front free end a transverse pin 173 (substantially parallel to the axis S), which is able to bear against and cooperate with the branches and their folded-back ends of the fork 161. As can be seen in the drawings, when the member 160 is in its first position, the member 170 is maintained and locked in a first predetermined angular position about the axis S, by the bearing of the pin 173 against the branches and the folded-back ends of the branches. The member 170 is biased in this angular position of rest by an elastic return device, which comprises here a spring 174 mounted about the axis S and bearing respectively against the member 170 and the housing of the tool.
The rear portion of the member 170 (behind the pegs 171) comprises at its rear free end a pin 175 for bearing against the longitudinal element 192. At a distance from the axis S and from this pin 175, the rear portion of the member 170 comprises a transverse slot 177 (in a direction parallel to the axis S), through which passes a physical axle 179 carried by the trigger 123.
The slot 177 has an elongated or oblong shape so that the physical axle 179 is lodged with play in this slot (
The member 170 is movable by pivoting between its first position of rest shown in
The movement of the member 170 here is brought about by the actuating of the trigger 123, which is made possible by the releasing of the member 170 by the member 160.
The trigger 123 of the tool 110 is mounted to be pivoting, here, by its upper end, about an axis Z substantially parallel to the axes Y and S. In typical fashion, it comprises a surface 184, here the front surface, for bearing against by at least one finger of the user, such as an index finger.
The trigger 123 likewise comprises at its upper and rear end coaxial lateral cylindrical pegs 125 which are mounted to be rotational in seats of complementary shape in the shells of the housing. The trigger 123 furthermore carries the aforethought axle 179, here at its upper and front end.
When the member 160 is in its position of rest (
The longitudinal element 192 has the shape of a ruler, one longitudinal end of which, here the upper end, comprises a surface 193a for the bearing of the pin 175 of the member 170. This longitudinal element 192 can be formed by a simple metal sheet which has been cut out and bent. The element 192 is mounted to slide on the box 124, along its longitudinal axis, this box being able to have a sliding component, for example, of the slideway type, similar to those described with reference to the preceding embodiment.
The element 192 is movable between a first position of rest, here the high position, and a second or low position. It is biased in its first position by an elastic return device, such as a compression spring 200.
The element 192 comprises at its lower longitudinal end at least one tongue 193b which is oriented substantially perpendicular to the axis of extension of the element 192 and on the side with the box 124. This tongue 193b passes through a slot 195 of the box 124 and can slide into this slot during the movements of the element 192. It is engaged in a groove or recess of the movable body 108b of the admission valve for purposes of the movement of this body inside the precombustion chamber and the opening and closing of the admission orifice of this chamber. In the example shown, the spring 200 biases the longitudinal element 192 in its position of rest by bearing against the movable body 108b.
The actuating and safety members of these figures are similar to those of
The actuating member 260 of
Various modifications to the above-described embodiments will be apparent to those skilled in the art. These modifications can be made without departing from the spirit and scope of this present subject matter and without diminishing its intended advantages. Not all of the depicted components described in this disclosure may be required, and some implementations may include additional, different, or fewer components as compared to those described herein. Variations in the arrangement and type of the components; the shapes, sizes, and materials of the components; and the manners of attachment and connections of the components may be made without departing from the spirit or scope of the claims set forth herein. Also, unless otherwise indicated, any directions referred to herein reflect the orientations of the components shown in the corresponding drawings and do not limit the scope of the present disclosure. This specification is intended to be taken as a whole and interpreted in accordance with the principles of the invention as taught herein and understood by one of ordinary skill in the art.
Number | Date | Country | Kind |
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16 50433 | Jan 2016 | FR | national |
Number | Name | Date | Kind |
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Number | Date | Country |
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0 123 717 | Nov 1984 | EP |
1 243 383 | Sep 2002 | EP |
2 087 220 | Oct 2011 | EP |
2 428 320 | Mar 2013 | EP |
2 875 160 | Mar 2006 | FR |
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Entry |
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New Zealand First Examination Report for New Zealand Application No. 727867, dated May 30, 2017 (4 pages). |
New Zealand Further Examination Report for New Zealand Application No. 727867, dated Dec. 7, 2017 (4 pages). |
Australian Examination Report No. 1 for Australian Application No. 2016277633, dated Jul. 7, 2017 (6 pages). |
Australian Examination Report No. 2 for Australian Application No. 2016277633, dated Apr. 11, 2018 (3 pages). |
Number | Date | Country | |
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20170203424 A1 | Jul 2017 | US |