Aerosol spray device
09856070 ยท 2018-01-02
Assignee
Inventors
- Ghasem Ghavami-Nasr (Driffield, GB)
- Andrew John Yule (Driffield, GB)
- Martin Laurence Burby (Driffield, GB)
Cpc classification
B65D83/48
PERFORMING OPERATIONS; TRANSPORTING
B05B7/0483
PERFORMING OPERATIONS; TRANSPORTING
B05B1/3442
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
An aerosol spray device comprising a pressurized or pressurizable container and a spray discharge assembly mounted on the container. The spray discharge assembly comprises a valve stem moveable from a first limit position to a second limit position to effect spray discharge from the device, a spray outlet region having an outlet orifice from which fluid from the container is discharged, and a flow conduit for supplying fluid from the container to the spray outlet region. The flow conduit has at least one first inlet for liquid from the container and at least one second inlet at the same distance along the conduit as the first inlet(s) or downstream of the first inlet(s) for propellant gas from a headspace of the container. A valving arrangement is adapted such that movement of the valve stem from its first to second limit position opens the first and the second inlets to cause a bubble laden flow to be created in the flow conduit and movement of the valve stem back to its first limit position closes the first and second inlets.
Claims
1. A valving arrangement for an aerosol spray device comprising a pressurised or pressurisable container holding a liquid to be discharged from the device by a propellant comprising: a valve stem moveable from a first limit position to a second limit position to effect spray discharge from the device; a flow conduit for supplying fluid from the container to a spray outlet region, said flow conduit being provided in said valve stem having at least one first inlet for liquid from the container and at least one second inlet at the same distance along the conduit as said first inlet(s) or downstream of said first inlet(s) for propellant gas from a headspace of the container, wherein each of said first liquid inlet(s) and said second gas inlet(s) is provided in said valve stem; and a single seal configured to isolate both the first and second inlets from the liquid to be discharged and the propellant gas when the valve stem is in its first limit position, wherein movement of the valve stem from its first to its second limit position opens said first and said second inlets to the liquid to be discharged and the propellant gas to respectively cause gas and liquid to be introduced separately into the flow conduit to thereby cause a bubble laden flow to be created therein and movement of the valve stem back to its first limit position isolates said first and said second inlets from the liquid to be discharged and the propellant gas.
2. The valving arrangement of claim 1, further comprising a housing, said housing at least partially defining a liquid flow path connecting the liquid in the container to the first inlet(s) and a separate gas flow path connecting the headspace with the second inlet(s).
3. The valving arrangement of claim 2, wherein a lower region of the valve stem locates within the housing and the single seal is mounted on the housing for relative sliding engagement with the valve stem.
4. The valving arrangement of claim 2, wherein each of the first liquid inlet(s) and the second gas inlet(s) are on the opposite side of the single seal to the liquid to be discharged and the propellant gas when the valve stem is in its first limit position.
5. The valving arrangement of claim 2, wherein each of the first liquid inlet(s) and the second gas inlet(s) are on the opposite side of the single seal to the liquid flow path and the gas flow path when the valve stem is in its first limit position.
6. The valving arrangement of claim 1, wherein a cylindrical interface is formed between the seal and the valve stem.
7. The valving arrangement of claim 1, being adapted to discharge a gaseous propellant from the container that is a gas at a temperature of 25 C. and a pressure of at least 50 bar.
8. A valving arrangement for an aerosol spray device comprising a pressurised or pressurisable container holding a liquid to be discharged from the device by a propellant comprising: a valve stem moveable from a first limit position to a second limit position to effect spray discharge from the device; a flow conduit for supplying fluid from the container to a spray outlet region, said flow conduit being provided in said valve stem having at least one first inlet for liquid from the container and at least one second inlet at the same distance along the conduit as said first inlet(s) or downstream of said first inlet(s) for propellant gas from a headspace of the container, wherein each of said first liquid inlet(s) and said second gas inlet(s) is provided in said valve stem; a single seal configured to isolate both the first and second inlets from the liquid to be discharged and the propellant gas when the valve stem is in its first limit position; a housing, said housing at least partially defining a liquid flow path connecting the liquid in the container to the first inlet(s) and a separate gas flow path connecting the headspace with the second inlet(s); and wherein movement of the valve stem from its first to its second limit position opens said first and said second inlets to the liquid to be discharged and the propellant gas to respectively cause gas and liquid to be introduced separately into the flow conduit to thereby cause a bubble laden flow to be created therein and movement of the valve stem back to its first limit position isolates said first and said second inlets from the liquid to be discharged and the propellant gas; wherein a lower region of the valve stem locates within the housing and the single seal is mounted on the housing for relative sliding engagement with the valve stem; a distributor plug mounted immediately below the single seal within the housing and further defining said separate liquid and gas flow paths.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention will be further described by way of example only with reference to the accompanying drawings, in which:
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DETAILED DESCRIPTION
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(20) The valve assembly 3 comprises a generally cylindrical, axially movable valve stem 7 having an axial bore 8 extending from the upper end of valve stem 7 part way towards the lower end thereof. At its lower end, valve stem 7 locates within a cylindrical housing 9 positioned internally of the container 2 and at its upper end is fitted with an actuator in the form of a cap 10 having a spray outlet region 11. This cap 10 (which may be of the type available under the name Kosmos from Precision Valve (UK) Ltd) is moulded so as to locate on the top of valve stem 7 and has an internal L-shaped conduit formed as a first section 12a collinear with the bore 8 of valve stem 7 and a second section 12b that extends at right angles to section 12a and leads to spray outlet region 11. Provided at the outlet end of region 11 is a conventional MBU (Mechanical Break-Up Unit) insert 13 which is described in more detail below.
(21) In broad outline, the aerosol spray device 1 is operated by pressing down on the cap 10 to cause downward movement of valve stem 7 with resultant discharge of a spray from spray outlet region 11, the spray being produced in the manner described more fully below.
(22) As shown in the drawings, valve stem 7 is biased upwardly of the container 2 by means of a coil spring 14 locating at its upper end around a lower bulbous nose 15 on the valve stem 7. Lower end of coil spring 14 locates around an aperture 16 in lower wall 17 of the housing 9. Depending from wall 17 is a tubular spigot 18 having a lower wall enlarged end 19 to which is fitted a dip tube 20 which extends to the base of the container 2. It will be appreciated from the drawing that the lower region of container 2 is in communication with the interior of the housing 9 via the dip tube 20, spigot 18 and aperture 16 (which provides a liquid inlet for housing 9).
(23) For reasons which will become clear from the subsequent description, valve stem 7 has an external diameter slightly less than the internal diameter of housing 9 so that an annular clearance 21 is defined between valve stem 7 and housing 9.
(24) Annular gaskets 22 and 23 formed of rubber or other elastomeric material are provided at upper and central regions respectively of the housing 9 and are dimensioned to seal against the outer surface of valve stem 7. To facilitate understanding of the device as further described below, the aforementioned annular clearance is shown as being sub-divided into two sections referenced as 21a and 21b. Section 21a of the annular clearance extends between the two gaskets 22 and 23, whereas section 21b of the annular clearance is below the lower gasket 23. Formed in the wall of the housing 9 between the two gaskets 22 and 23 are a plurality of ports 24 which provide for communication between the pressurised gas in the head space 6 and the annular clearance 21a.
(25) Internally, valve stem 7 is formed with the flow conduit 8 (extending coaxially along the valve stem 7) and a liquid feed chamber 26 which communicates with the flow conduit 8 via a passageway 27. Flow conduit 8 extends from the upper end of valve stem 7 for over 50% of the length thereof. Chamber 26 is below flow conduit 8 and is of greater diameter than flow conduit 8 but significantly smaller length.
(26) Two liquid feed passageways 28 extend transversely from the liquid feed chamber 26 and open at the outer surface of valve stem 7. As will be appreciated from the more detailed description given below, liquid 5 from within the container 2 passes (during spray discharge) radially inwardly of the liquid feed passageways 28 into chamber 26 and then via passageway 27 into the flow conduit 8. In this way, flow passageway 27 provides a liquid inlet for the flow conduit 8.
(27) Two gas bleed inlet passageways 29 extend transversely from the flow conduit 8 to open at the exterior surface of valve stem 7. The liquid feed passageways 28 and gas bleed inlet passageways 29 are axially spaced from each other by a distance such that, in the rest condition of the aerosol as shown in
(28) It will be appreciated that constructions in which there is only one such liquid feed passageway 28 and/or one gas bleed inlet passageway 29 are also practical. By way of example of the letter alternative arrangement, the embodiment illustrated in
(29) Reference is now made to the spray outlet region 11 of the actuator cap 10. This region 11 is formed internally with an integrally moulded boss 30 arranged such that, on the one hand, it defines an annular clearance or gallery 31 within the actuator cap 10 and, on the other hand, its free end is located a short distance from the exterior of cap 10 to leave a cylindrical gap in which the MBU insert 13 is located. This insert is described in more detail below but, at this point, it will be appreciated that conduit section 12b communicates with the annular gap 31 so that fluid being discharged from container 2 may pass circumferentially around this gap.
(30) MBU insert 13 is of conventional construction and is shown in more detail in the insets to
(31) To operate the device 1, actuator cap 10 is depressed so that valve stem 7 moves downwardly against the bias of spring 14. As a result, gas bleed inlet passageways 29 are displaced from the gasket 22 such that compressed gas can bleed from heed space 6 into the flow conduit 8 via the ports 24 (In the wall of housing 9), the annular clearance 21a and the gas bleed inlet passageways 29. Simultaneously with, or preferably slightly later then, the creation of the gas flow, one or more of the liquid inlet passageways 28 are opened by virtue of moving past lower gasket 23. Liquid 6 can now flow into liquid feed chamber 26 by passage upwardly along the dip tube 20, through the inlet 16 into the housing 9, into annular clearance 21b and through the liquid inlet passageways 28. Liquid 5 introduced into liquid feed chamber 26 passes via passageway 28 into flow conduit 8 where it is mixed with compressed gas bled through the passageways 29. A bubble laden flow of homogeneous bubbles with similar diameters and without significant coalescence or stratification is formed in flow conduit 8 and flows along the conduit 8 into conduit section 12a (within actuator cap 10) and then into conduit section 12b. From this latter conduit section, the bubble laden flow passes into, and around, the annular gallery 31 and then enters the outer ends of swirl channels 34 before passing into swirl chamber 35 and out through discharge orifice 32.
(32) In the construction of the aerosol spray device 1, it should be ensured that the total cross-sectional area of the gas bleed passageways 29 should not be so large that excessive gas is bled into the conduit 8 such that the container 2 is depleted of pressurised gaseous propellant before all of the liquid 5 in the container has been discharged. Typically, the total cross-sectional area of the gas bleed inlet passageways 29 should be equivalent to that of a singular, circular section inlet with a diameter of 0.15-0.7 mm.
(33) Preferred dimensions for the construction of spray device 1 to ensure production of a bubble laden flow of homogeneous bubbles with similar diameters and without coalescence or stratification are shown in the following table:
(34) TABLE-US-00001 Reference Item Numeral Diameter Length Gas bleed inlet 29 0.15 mm each (two 1.0 mm provided) Liquid inlet 27 0.4 mm (one 1.0 mm passageway provided) Conduit in Valve Stem 8 1 mm 10 mm Exit Orifice of MBU 32 0.33 mm Well 33 0.75 mm 0.3 mm (depth) Channels 34 0.2 mm (width) 0.3 mm (depth)
(35) With the dimensions as indicated above, the spray device 1 is particularly suitable for consumer aerosol products such as polishes and air fresheners.
(36) The (second) embodiment shown in
(37) Reference is now made to
(38) The (fourth) embodiment shown in
(39) As thus far described, the MBU inserts 13 shown in
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(41) The arrangement of
(42) It should be noted that, although the embodiments of
(43) In the arrangement of
(44) The embodiment of
(45) Further alternative embodiments are illustrated in
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(47) As with the embodiment of
(48) The gas bleed inlet 81 is similar to that (71) of the embodiment of
(49) The chamber 104 is dimensioned so as to be a close sliding fit around that region of the valve stem 7 where the gas bleed inlet 81 and the liquid feed inlet 82 open at the outer surface of valve stem 7. As a result of the close sliding fit, no liquid can leak past the valve stem/chamber interface and so the gas flow path will not be contaminated with any liquid from the chamber, which leakage could impede the performance of the spray aerosol.
(50) When the valve stem 7 is depressed, the gas bleed inlet 81 and the liquid feed inlet 82 are pushed pest the gasket 23 and into communication with the respective gas channel 83 and fluid inlet channel 84.
(51) In order to prevent rotation of the valve stem 7 within the housing 9, the housing may include a projection 91 for cooperative engagement with a corresponding recess 92 in the valve stem. To prevent the valve stem 7 from extending too far out of the housing 9, a lower portion of the stem may be enlarged, defining a step 94 that acts. In conjunction with the underside of the distributor plug 101, as a limit stop (see
(52) Another alternative embodiment is illustrated in
(53) Instead of a projection from the housing cooperating with a recess on the valve stem to prevent relative rotation of those parts, in this embodiment lugs 7a project from the valve stem 7 and are received in grooves 9a in the interior of the housing 9 and extending parallel to the axis thereof. The liquid inlet arrangement is also different, in that an axial channel 106 through the lower portion of the valve stem 7 extends to be in fluid communication with the aperture 16 in the lower wall of the housing 9. A transverse opening 108 is located at the upper end of the channel 106 and connects the channel 106 to the annular clearance 21 between the stem 7 and the housing 9.
(54) At the upper end of the housing, the distributor plug 101 of
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(57) It should be appreciated that various modifications may be made to the illustrated embodiments. Thus, for example, the spray devices shown in
(58) Furthermore although all embodiments are illustrated with an MBU insert with four swirl channels, it is possible more generally to use inserts with 1 to 8 such channels.
(59) It should be appreciated that the flow conduit/valving arrangements shown in, and described with reference to,
(60) The following non-limiting Example illustrates the invention.
EXAMPLE
(61) This Example was carried out using an aerosol spray device in accordance with the invention having a discharge assembly with a flow conduit, diameter 1.0 mm and length in the stem 15.0 mm, having a single liquid inlet having a diameter of 0.40 mm and downstream thereof a single gas inlet having a diameter of 0.20 mm. Both diameters are as measured at the point of entry of the inlet into the flow conduit. The liquid and gas inlets are separated by 2.4 mm The aerosol spray device was fitted with an AQUA MBU insert having a 0.23 mm exit orifice and the general arrangement was similar to that shown in
(62) The canister of the device had an Interior volume of 486 ml which was 50% filed with deionised water. The canister was pressurised to an internal pressure of 12.13 bar using an electrical transducer type of manometer having an accuracy better than 0.01 bar (1.0 kPa).
(63) The valve stem was depressed for successive, discrete periods of 20 seconds until the container was empty. For each discharge, the can pressure was measured and recorded. Additionally for each discharge the spray was collected and weighed (although as an alternative the can could be weighed before and after the discharge, the difference giving the mass of liquid spray, making the reasonable assumption that the mass of gas discharged is negligible).
(64) The mass measurements were used to calculate volume of liquid sprayed (dVL) during spray discharge.
(65) Values for the volume of atomising gas released (dVat ml) were determined by standard equations making use of the ideal gas law relating pressure, volume, mass and temperature of gas so that the mass of gas in the canister is calculated before and after the 20 s spraying interval. In this respect, the product GAS pressure (Abe) X Gas Volume (in can) is proportional to the Mass of Gas left in the can (according to the Gas Law, assuming a constant temperature which is the case for these experiments). This does not need to be used explicitly because the initial volume and pressure of the gas in the can and thus the gas density and thus the Initial gas mass in the can are known. The gas density after 20 s can be calculated using the new can pressure and multiplying by the volume of gas in the can (which has increased by a known volume that is equal to the measured volume of liquid sprayed in 20 s) to give the mass of gas left in the can. The difference between the mass of gas in the can before and after the 20 s is the mass of gas that has left the gas.
(66) The average liquid and gas flow rates during the time interval (QL m/min and Qg ml/min respectively) were simply calculated by dividing the time interval into the volumes of liquid and gas passing through the MBU in that time. Finally the ratio of Qg/QL were determined.
(67) The results are shown in the following Table.
(68) TABLE-US-00002 vol liquid atom gas initial final liquid total atom- initial final flow flow Dis- pressure pressure time vol discharge izing liquid liquid rate rate charge bar bar interval sprayed time gas in in QL Qg ratio No. g g dt sec dVL sec dVat ml can ml can ml ml/min ml/min Qg/QL 1 12.13 10.56 20 16.3 20 193.07 243 226.7 48.90 579.20 11.84 2 10.56 9.27 20 13.9 40 193.10 226.7 212.8 41.70 579.29 13.69 3 9.27 8.23 20 14.2 60 153.12 212.8 198.6 42.60 459.36 10.78 4 8.23 7.32 20 13.7 80 147.30 198.6 184.9 41.10 441.91 10.75 5 7.32 6.58 20 12.7 100 126.59 184.9 172.2 38.10 379.76 9.97 6 6.58 5.96 20 12.0 120 109.44 172.2 160.2 36.00 328.33 9.12 7 5.96 5.39 20 10.9 140 117.38 160.2 149.3 32.70 352.14 10.77 8 5.39 4.90 20 10.8 160 102.33 149.3 138.5 32.40 306.98 9.47 9 4.90 4.46 20 10.3 180 94.21 138.5 128.2 30.90 282.63 9.15 10 4.46 4.09 20 10.0 200 83.31 128.2 118.2 30.00 249.92 8.33 11 4.09 3.74 20 9.6 220 80.61 118.2 108.6 28.80 241.84 8.40 12 3.74 3.42 20 8.6 240 86.20 108.6 100 25.80 258.59 10.02 13 3.42 3.14 20 8.4 260 70.98 100 91.6 25.20 212.94 8.45 14 3.14 2.83 20 8.3 280 90.47 91.6 83.3 24.90 271.40 10.90 15 2.83 2.58 20 6.3 300 70.54 83.3 75 24.90 211.63 8.50 16 2.58 2.39 20 7.3 320 55.84 75 67.7 21.90 167.51 7.65 17 2.39 2.19 20 7.2 340 58.59 67.7 60.5 21.60 175.78 8.14 18 2.19 2.03 20 6.6 360 47.21 60.5 53.9 19.80 141.63 7.15 19 2.03 1.86 20 6.5 380 54.85 53.9 47.4 19.50 164.54 8.44 20 1.86 1.72 20 6.4 400 46.20 47.4 41 19.20 138.61 7.22
It can be seen from the Table that the Gas/Liquid volume ratio (final column) is between 8 and 11 for most of the lifetime of the aerosol canister, which represents a very satisfactory result.
(69) For a given exit orifice size the dependency of gas and liquid flow rates on gas and liquid inlet diameters is complex; for example it is proposed that reducing the liquid inlet diameter produces a lowering of pressure inside the conduit which increases the inflow of gas into the conduit. However this increased gas inflow increase the blockage of the bubbly flow at the swirl inlets and exit orifice of the MBU which produces a lowering of the liquid inflow rate from the value expected. In order to take into account these complex effects the inventors carried out testing of valves with different gas and liquid inlet diameters and exit orifice diameters. These are carried out as a function of pressure as a canister empties during spraying. In order to compare the performances using different orifices it is found to be necessary to compare flow rates at different representative pressures and the second table shows this comparison for a range of 16 valve geometries and for two MBU's (exit orifices 0.23 mm and 0.33 mm) for the pressure 9.5 bar. It is noted that when there is more than one liquid inlets it is the equivalent area inlet diameter that should be specified for comparison purposes, i.e. the diameter of a single orifice that would have the same cross sectional area as the sum of the cross sectional areas of all of the liquid inlets.
(70) TABLE-US-00003 Number Dilq Dexit 0.23 mm Dexit 0.33 mm of (equiv) Dgas Qliq Qg Qgas/ Qliq Qg Qgas/ Liq Intake mm mm ml/min ml/min Qliq ml/min ml/min Qliq 1 0.3 0.2 23 1200 52 39 2200 56 1 0.3 0.2 35.7 390 10.9 65 1200 18.4 1 0.35 0.2 29.5 700 23.7 65 1300 20 1 0.4 0.15 33.3 130 3.9 116 97 0.8 1 0.4 0.2 42 579 13.8 2 0.42 0.25 54 170 3.1 79 320 4 2 0.42 0.35 19 1500 78 50 2400 46 1 0.45 0.2 35 820 23 82 1110 13.5 1 0.5 0.2 37.5 510 13.6 103 700 6.8 2 0.57 0.35 27 1100 40 59 1800 30.5 2 0.71 0.35 35 660 18.8 82 1450 17.7 2 0.42 0.25 42 270 6.4 82 560 6.8 1 0.4 0.2 37 510 13.7 76 1050 13.8 1 0.42 0.2 68 1500 22
(71) The performance information of the type in the second table is best interpreted by using iso-contour 3-dimensional surface plot charts and four examples of these are shown in the four
(72) Furthermore the procedure should be carried out for more than one value of exit orifice diameter; for example the data for the 0.23 mm orifice case shows best flow rates that are too low for air-freshener consumer products and this requires optimising the gas and liquid inlets using a larger exit orifice diameter. The third fourth
(73) To minimise the droplet sizes it is necessary to maximise the gas/liquid volume ratio however smaller exit orifices and higher canister pressures also reduce drop size.