Propellant conditioning assemblies

In the field of medical dosing device filling, a propellant conditioning assembly (10) comprises an input conduit (12) to receive a propellant at a constant pressure from a propellant reservoir (102). The conditioning assembly (10) also includes a bifurcation (18) to divide the input conduit (12) into first and second conditioning conduits (20, 22). The first conditioning conduit (20) includes a cooler device (24) to selectively cool a diverted first propellant stream (26) that flows through the first conditioning conduit (20), and the second conditioning conduit (22) includes a heater device (32) to selectively heat a diverted second propellant stream (34) that flows through the second conditioning conduit (22). The conditioning assembly (10) still further includes an output conduit (44) to receive the first and second propellant streams (26, 34). The relative proportion of the first and second propellant streams (26, 34) merging in the output conduit (44) is controlled to regulate the temperature of a merged constant pressure propellant feed (46) exiting from the output conduit (44).

This application is a U.S. National Phase entry under 35 U.S.C. § 371 of International application No. PCT/GB2018/050740, filed Mar. 21, 2018, which claims the benefit of Great Britain patent application No. 1706785.1, filed Apr. 28, 2017, the contents of each of which are incorporated herein by reference in their entireties.

This invention relates to a propellant conditioning assembly, a process plant including such an assembly, and a method of conditioning a propellant.

Drugs for treating illnesses such as respiratory disorders are frequently administered in aerosol formulations. Such aerosol drug formulations are typically delivered using a medical dosing device, e.g. a Metered Dose Inhaler (MDI), which contains the drug formulation along with a propellant. A nozzle or similar atomising outlet included within the dosing device is operated, e.g. depressed, to deliver the medication in an atomised form.

Example propellants for medical dosing devices include hydrofluorocarbons (HFCs) such as HFC 134a (1,1,1,2-tetrafluoroethane), HFC 227ea (1,1,1,2,3,3,3-heptafluoropropane) and HFC 152a (1,1-difluoroethane).

Conditioning a propellant, i.e. stabilising its liquid density by providing it at a constant pressure and temperature, is often essential prior to filling a dosing device with the propellant, especially when performing a dual fill of a dosing device with a concentrated drug suspension being added to the device prior to the propellant.

According to a first aspect of the invention there is provided a propellant conditioning assembly, for providing a propellant feed to a medical dosing device filling apparatus, the assembly comprising:an input conduit to receive a propellant at a constant pressure from a propellant reservoir;a bifurcation to divide the input conduit into first and second conditioning conduits, the first conditioning conduit including a cooler device to selectively cool a diverted first propellant stream flowing through the first conditioning conduit, and the second conditioning conduit including a heater device to selectively heat a diverted second propellant stream flowing through the second conditioning conduit; andan output conduit to receive the first and second propellant streams, the relative proportion of the first and second propellant streams merging in the output conduit being controlled to regulate the temperature of a merged constant pressure propellant feed exiting from the output conduit.

The ability to regulate the temperature of a constant pressure propellant feed exiting from an output conduit, i.e. the ability to condition the propellant in the foregoing manner is advantageous because it permits the continuous, inline conditioning of a propellant in real time. As a result, conditioned propellant is readily and consistently available, e.g. for a downstream medical dosing device filling apparatus, and there is no requirement to store large quantities of conditioned propellant.

This latter benefit is especially important with respect to flammable hydrofluorocarbon (HFC) propellants, such as HFC 152a (1,1-difluoroethane), as it avoids the associated fire and safety hazards.

Preferably the input conduit includes an input temperature sensor arranged to measure an input temperature of the propellant in the input conduit, the measured input temperature being used to control the selective operation of the cooler and heater devices.

The inclusion of such an input temperature sensor introduces a degree of feedback control to the propellant conditioning assembly of the invention, and allows relatively coarse changes to be made to the temperature of the respective propellant streams, which in turn allows for finer, subsequent regulation of the temperature of the merged propellant feed in the output conduit.

Optionally the cooler device is operated to cool the first propellant stream flowing through the first conditioning conduit when the measured input temperature is greater than a first temperature threshold.

Such an arrangement desirably cools the first propellant stream when the temperature of the propellant in the input conduit is higher than desired, and therefore makes available a cooled propellant stream for downstream merging in the output conduit with the second propellant stream.

The heater device may be operated to heat the second propellant stream flowing through the second conditioning conduit when the measured input temperature is less than a second temperature threshold.

Such an arrangement desirably heats the second propellant stream when the temperature of the propellant in the input conduit is lower than desired, and therefore makes available a heated propellant stream for downstream merging in the output conduit with the first propellant stream.

In a preferred embodiment of the invention the first and second temperature thresholds differ from one another.

Having differing first and second temperature thresholds helps to reduce the need to operate the cooler and heater devices, i.e. by causing one or other of them to operate only when the input temperature is outside the temperature range defined by the said first and second thresholds.

Preferably each of the cooler device and the heater device is or includes a heat exchanger.

Heat exchangers are able efficiently to remove or add heat to a respective propellant stream in a controlled and safe manner.

Optionally the first conditioning conduit includes a first flow control valve to control the flow rate through the first conditioning conduit and the second conditioning conduit includes a second flow control valve to control the flow rate through the second conditioning conduit.

The inclusion of such flow control valves permits the ready and effective control of the flow rate through each conditioning conduit, and hence helps also to control the relative proportion of first and second propellant streams that merge in the output conduit.

In another preferred embodiment of the invention the output conduit includes an output temperature sensor arranged to measure an output temperature of the merged constant pressure propellant feed in the output conduit, the measured output temperature being used to control the operation of the first and second flow control valves.

The inclusion of such an output temperature sensor introduces a further degree of feedback control to the propellant conditioning assembly of the invention and assists, via control of the first and second control valves, with close regulation of the temperature of the merged propellant feed in the output conduit.

In a still further preferred embodiment of the invention the first flow control valve is operated to increase the flow rate through the first conditioning conduit and/or the second flow control valve is operated to reduce the flow rate through the second conditioning conduit when the measured output temperature is above a first output threshold, and the first flow control valve is operated to reduce the flow rate through the first conditioning conduit and/or the second flow control valve is operated to increase the flow rate through the second conditioning conduit when the measured output temperature is below a second output threshold.

Such an arrangement permits fine control over the relative proportions of different temperature first and second propellant streams that merge in the output conduit, and hence similarly fine regulation of the temperature of the merged constant pressure propellant feed in the output conduit.

The input conduit may include an input flow rate sensor to measure the flow rate of the propellant through the input conduit.

The inclusion of such a flow rate sensor assists with controlling the relative proportion of first and second propellant streams that merge in the output conduit.

According to a second aspect of the invention there is provided a process plant, for providing a propellant feed to a medical device filling apparatus, comprising a propellant reservoir for a quantity of propellant and a supply line extending from the reservoir to a propellant conditioning assembly as described hereinabove, the supply line including a constant pressure pump to supply propellant at a constant pressure to the propellant conditioning assembly.

The process plant shares the benefits associated with the propellant conditioning assembly mentioned hereinabove.

According to a third aspect of the invention there is provided a method of conditioning a propellant, for feeding to a medical dosing device filling apparatus, comprising the steps of:(a) receiving in an input conduit a propellant at a constant pressure from a propellant reservoir;(b) dividing the input conduit into first and second conditioning conduits, the first conditioning conduit including a cooler device to selectively cool a diverted first propellant stream flowing through the first conditioning conduit, and the second conditioning conduit including a heater device to selectively heat a diverted second propellant stream flowing through the second conditioning conduit;(c) receiving the first and second propellant streams in an output conduit; and(d) controlling the relative proportion of the first and second propellant streams merging in the output conduit to regulate the temperature of a merged constant pressure propellant feed exiting from the output conduit.

The method of the invention similarly shares the benefits of the corresponding features of the propellant conditioning assembly of the invention.

A propellant conditioning assembly according to a first embodiment of the invention is designated generally by reference numeral10, as shown inFIG. 1.

The propellant conditioning assembly10includes an input conduit12which, in use, receives a propellant at a constant pressure from a propellant reservoir (not shown inFIG. 1).

The input conduit12includes an input temperature sensor14that is arranged to measure an input temperature TINof the propellant in the input conduit12, and an input flow rate sensor16to measure the flow rate of the said propellant. The input flow rate sensor16preferably includes high and low flow rate alarms, e.g. to alert an operative to potential malfunction of the propellant conditioning assembly10.

The propellant conditioning assembly10also includes a bifurcation18that divides the input conduit12into first and second conditioning conduits20,22.

The first conditioning conduit20includes a cooler device24to selectively cool a diverted first propellant stream26which flows through the first conditioning conduit20.

More particularly, the cooler device24includes a first heat exchanger28that is arranged in communication with a cooler module30which supplies a cooled fluid to the first heat exchanger28to remove heat, i.e. cool, the first propellant stream26as it passes through the first conditioning conduit20. Preferably the first heat exchanger28is a plate heat exchanger, and more preferably still a stainless steel welded plate heat exchanger, although other types of heat exchanger may also be used.

In the embodiment shown the cooler module30receives cooled fluid in the form of chilled water from a dedicated water chiller (not shown) that operates at a reduced temperature set and monitored by a high-level controller, e.g. located elsewhere within a process plant of which the propellant conditioning assembly10forms a part. Other cooled fluids may be used however, as may other ways of cooling the first heat exchanger28.

Meanwhile, the second conditioning conduit22includes a heater device32to selectively heat a diverted second propellant stream34which flows through the second conditioning conduit22.

The heater device32includes a second heat exchanger36that is arranged in communication with a heater module38which supplies a heated fluid to the second heat exchanger36to transfer warmth to, and thereby heat, the second propellant stream34as it passes through the second conditioning conduit22. Preferably the second heat exchanger36is again a plate heat exchanger, and more preferably still a stainless steel welded plate heat exchanger, although other types of heat exchanger may again also be used.

In the embodiment shown the heater module38receives heated fluid in the form of hot water from a dedicated water heater (not shown) that operates at an elevated temperature, which may similarly be set and monitored by a high-level controller located elsewhere within a process plant of which the propellant conditioning assembly10forms a part. Preferably the heater module38includes a safety device (not shown) to prevent overheating of the hot water. Other heated fluids may be used however, as may other ways of heating the second heat exchanger36. A self-acting float valve (also not shown) ensures that the water heater is provided with fresh water, as needed.

In addition to the foregoing, the first conditioning conduit20includes a first flow control valve40to control the flow rate of the first propellant stream26through the first conditioning conduit20. Also, the second conditioning conduit22includes a second flow control valve42to control the flow rate of the second propellant stream34through the second conditioning conduit22. Each flow control valve40,42includes a mechanical stop to prevent the valve40,42from being completely closed, and thereby maintain a degree of flow at all times through each of the first and second conditioning conduits20,22. Preferably the valves40,42are also controlled to ensure adequate flow through the propellant conditioning assembly10.

The propellant conditioning assembly10still further includes an output conduit44that receives the first and second propellant streams26,34and merges them into a constant pressure propellant feed46.

The output conduit44also includes an output temperature sensor48that is arranged to measure an output temperature TOUTof the merged propellant feed46in the output conduit44.

In use, the relative proportion of the first and second propellant streams26,34merging in the output conduit44is controlled to regulate the temperature of the merged constant pressure propellant feed46exiting from the output conduit44.

More particularly, the input temperature TINmeasured by the input temperature sensor14is firstly used to control the selective operation of the cooler and heater devices24,32. More particularly still, the cooler device24is operated to cool the first propellant stream26when the measured input temperature TINis greater than a first temperature threshold, and the heater device32is operated to heat the second propellant stream34when the measured input temperature TINis less than a second temperature threshold.

In the embodiment shown the first and second temperature thresholds differ from one another, although this need not necessarily be the case. By way of example, however, in the embodiment shown the first temperature threshold is 17° C. and the second temperature threshold is 15° C. Other temperature thresholds may however be used.

It follows that, in the embodiment shown, if the input temperature TINof the propellant received from the propellant reservoir is greater than 17° C. then the cooler device24, i.e. the first heat exchanger28and the associated cooler module30, is operated to cool the first propellant stream26and similarly, if the input temperature TINof the propellant received from the propellant reservoir is less than 15° C. then the heater device32, i.e. the second heat exchanger36and the associated heater module38, is operated to heat the second propellant stream34. Meanwhile, if the input temperature TINof the propellant lies within a 15° C. to 17° C. window then neither the cooler nor heater device24,32is operated.

At the same time, the output temperature TOUTmeasured by the output temperature sensor48is used, in conjunction with the flow rate measured by the input flow rate sensor14, to control the operation of the first and second flow control valves40,42.

More particularly, and by way of example only, the first flow control valve40is operated to increase the flow rate through the first conditioning conduit20and the second control valve42is operated to reduce the flow rate through the second conditioning conduit22when the measured output temperature TOUTis above a first output threshold, which preferably is the same as the first temperature threshold, i.e. preferably is 17° C. Similarly, the first control valve40is operated to reduce the flow rate through the first conditioning conduit20and the second control valve42is operated to increase the flow rate through the second conditioning conduit22when the measured output temperature TOUTis below a second output threshold, which preferably is the same as the second temperature threshold, i.e. preferably is 15° C.

In other embodiments of the invention, only one or other of the first and second flow control valves40,42may be operated to change the flow rate through the corresponding conditioning conduit20,22in response to the measured output temperature TOUTdiverging from the first and second output thresholds, which may also differ from 17° C. and 15° C., respectively.

In the foregoing manner, adjustment of the first and/or second flow control valves40,42to control the relative flow rates of different temperature first and second propellant streams26,34, provides fine control over the relative proportions of the different temperature first and second propellant streams26,34that merge in the output conduit44. Hence such adjustment similarly provides fine regulation of the temperature of the merged constant pressure propellant feed46in the output conduit44.

A process plant according to a further embodiment of the invention is designated generally by reference numeral100, as shown inFIG. 2.

The process plant100includes a propellant reservoir102in the form of a store tank104, which can be resupplied with propellant from a supply tanker106, via an off-loading pump108. Other types of propellant reservoir, such as a buffer vessel (not shown) which may be resupplied from a supply cylinder via an off-loading pump, are also possible however.

The process plant100additionally includes a supply line110which extends from the propellant reservoir102, i.e. the store tank104, to the propellant conditioning assembly10shown inFIG. 1. The supply line110includes a constant pressure pump112to supply propellant at a constant pressure to the said propellant conditioning assembly10.