Method and system for detecting malfunction of a MEMS micropump

Abstract

Method for detecting failure including possible under or over delivery of a micropump having at least an inlet valve, a pumping chamber with an inner pressure sensor and an outlet valve, said method comprising the determination of the pump tightness via the measurement of the pressure by said inner pressure sensor in said pumping chamber at least at certain intervals when the pump is inactive and the comparison with a value of reference.

Description

1. FIELD OF INVENTION

The present invention relates to MEMS (Micro-Electro-Mechanical System) micropumps which may be advantageously used for administrating insulin. Such pumps comprise a pumping chamber having a pumping membrane and an integrated sensor comprised between two check valves.

More specifically, the present invention concerns the methods for monitoring the state of a MEMS micropump.

2. STATE OF THE ART

The detection of dysfunctions, especially in medical devices, is important because the life of the patient may depend on proper functioning of said devices. In case of infusion pumps, for example, the potentially dangerous results of a failure are typically over-infusion or under-infusion of the drug into the patient.

Examples of dysfunctions are leaks, occlusions or presence of air bubbles in the pumping line.

State-of-the-art devices and methods for detecting dysfunctions in medical devices are for instance disclosed in the following patent documents: US 2008/214979, EP 1 762 263 and U.S. Pat. No. 7,104,763.

An example of MEMS micropump is disclosed in patent application WO 2010/046728. This MEMS micropump 1 as illustrated in FIG. 1 is a highly miniaturized and reciprocating membrane pumping mechanism. It is made from silicon or silicon and glass. It contains an inlet control member, here an inlet valve 2, a pumping membrane 3, a functional inner detector 4 which allows detection of various failures in the system and an outlet valve 5. The principle of such micro-pumps is known in the prior art, for example from U.S. Pat. No. 5,759,014.

FIG. 1a illustrates a cross section of a micropump with the stack of a glass layer as base plate 8, a silicon layer as second plate 9, secured to the base plate 8, and a second glass layer 10 as a top plate, secured to the silicon plate 9, thereby defining a pumping chamber 11 having a volume.

An actuator (not represented here) linked to the mesa 6 allows the controlled displacement of the pumping membrane 3. A channel 7 is also present in order to connect the outlet control member, the outlet valve 5 to the outer detector not represented here and finally to the outlet port placed on the opposite side of the pump.

The FIG. 1b illustrates another cross-section of the MEMS micropump including a cover 12 onto the channel 7, the outer detector 13, the fluidic channel 17 between the outer detector 13 and the outlet port 18.

In the pump 1, the pressure inside the pumping chamber varies during a pumping cycle depending on numerous factors, such as the actuation rate, the pressure at the inlet and the outlet, the potential presence of a bubble volume, the valve characteristics and their leak rates.

Dysfunctions are detected by analysing the pressure profile during actuation cycles.

The inner pressure sensor 4 and outer pressure sensor 13 in the micro-pump 1 are made of a silicon membrane placed between the pumping chamber 11 and the pump outlet 5 and between the pump outlet valve 5 and pump outlet port 18 respectively. The sensors are located in a channel formed between the surface of the micro-pumps silicon layer 9 and its top layer 10. In addition, the sensors comprise a set of strain sensitive resistors in a Wheatstone bridge configuration on the membrane, making use of the huge piezo-resistive effect of the silicon. A change of pressure induces a distortion of the membrane and therefore the bridge is no longer in equilibrium. The sensors are designed to make the signal linear with the pressure within the typical pressure range of the pump. The fluid is in contact with the surface of the interconnection leads and the piezo-resistors. A good electrical insulation of the bridge is ensured by using an additional surface doping of polarity opposite to that of the leads and the piezo-resistors.

Because the analysis methods are performed during actuation (in-stroke detection), the occurrence of events like insulin reservoir pressurization or any other free flow conditions between two strokes are not detected. At low flow rate hazardous conditions may be therefore detected too late, leading to severe patient injuries.

There is therefore a need to improve the existing methods and systems for detection a malfunction of a MEMS micropump.

3. GENERAL DESCRIPTION OF THE INVENTION

The present invention offers several improvements with respect to state-of-the-art methods and systems.

The present invention, which may advantageously use the micropump described in WO 2010/046728 which is inside a device like described in the application EP11171155.2. The WO 2010/046728 describes out-of-stroke detection methods based on the analysis of at least one integrated pressure sensor. The EP11171155.2 describes medical device which comprises three distinct cavities where the pumping element is localised in the first cavity, the second cavity (which is the reservoir) is designed to contain a fluid for delivering to the patient. The first and second cavities are separated by a rigid wall while the second and third cavities are tightly separated by a movable membrane in such a manner said membrane may move between the second and third cavities when the volume of fluid changes. Said device comprises two distinct venting means, the first one for the first cavity and the second one for the third cavity. If one of venting means is clogged, the device may over or under delevry the fluid contained in the reservoir (the second cavity).

Using the method according to the present invention any condition that induces a free flow can be detected in few seconds. The amount of over or under delivery can be estimated. The method according to the invention also allows the detection of reservoir overfilling.

In a preferred embodiment the method according to the invention is based on the concept of equivalent fluidic resistance of both inlet and outlet valves.

Preferably, the residual fluidic resistances of the valves are determined during the last actuation cycle and the real time monitoring of the pressure inside the pumping chamber allows the determination of the maximum possible over or under delivery while out-of-stroke.

In-stroke and out-of-stroke detection methods are jointly used to alarm the patient as soon as possible of the occurrence of a risk of over or under delivery.

4. DETAILED DESCRIPTION OF THE INVENTION

The invention will be better understood with the following illustrated examples.

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

FIG. 1a illustrates a cross section of a micropump.

FIG. 1b illustrates another cross-section of the MEMS micropump.

FIG. 2 shows a typical pumping cycle having 3 phases.

FIG. 3 shows a schematic fluidic model for the pumping device.

FIG. 4 shows detector signals using the actuation profile given in FIG. 2.

FIG. 5 shows detector signals using the actuation profile given in FIG. 2.

FIG. 6 shows the maximum flow rate at 37° C.

FIG. 7 shows the max leak rate in U/h.

FIG. 8 shows the pumping device and its different ports,

4.1. PUMP LEAKAGE

The pumping device is made of a reservoir comprising a particle and air filter, a MEMS micropump 1 having inlet (2) and outlet (5) check-valves, a pumping membrane (3) and integrated detectors (4 and 13) and means to connect the outlet (18) of the micropump to the patient body including e.g. a catheter.

All parts of the pumping device which are in contact with insulin define the fluidic pathway.

We define a leakage as any tightness defect that can lead to an over or under delivery

We distinguish here two kinds of leakage

1. a leak from the fluidic pathway to outside, due to typically to:

• • reservoir failure
  • pumpchip crack
  • septum issues
  • needle issues

2. a leak within the fluidic pathway, due to typically to:

• • particles below the valve seats
  • cracks in the valve seats

Leaks towards outside will usually induce under delivery. These kinds of leakage can be addressed by a test of the fluidic pathway tightness during production.

Crackguard rings are also implanted into the pumping membrane, the inlet and outlet valves. Any crack in the silicon opens electrically the crack-guard ring. The mechanical integrity of the movable or sensitive part of the micropump are therefore tested electrically during the functional test but also during the functioning of the device.

Leakage within the fluidic pathway can induce both over and under delivery.

The tightness of the valves prevents the direct communication between the insulin reservoir and the patient because even during actuation there is at least one valve normally close in the fluidic pathway. The presence of particles below one valve seat induces a back-flow that affects the pump accuracy. The presence of particles below both valves associated with a gradient of pressure between the inlet and the outlet induces a free flow.

Because there is a flow that can potentially transport particles below the valve seats, the test of valve tightness should be performed continuously while the test of tightness in production is sufficient to detect cracks of the valve seats because this is due to process issues only.

The present invention describes both in-production and in-functioning leak detection methods.

4.2. VALVE TIGHTNESS AND EQUIVALENT FLUIDIC RESISTANCE

We consider here a fully working pump unit, i.e. having passed all production tests with success. The fluidic pathway is therefore tight as well as the valves.

It is now important to discuss the notion of tightness because we are talking about flow rate of only few nanoliters per hour through hard valve seat having a finite roughness and no compliance.

We characterize a valve normally closed by its finite residual fluidic resistance R_in and R_out, for the inlet and the outlet respectively.

Because the two fluidic resistances are placed in series, there is potentially a risk a free flow when the sum of their fluidic resistances R_in+R_out reaches a threshold value and this independently of the individual values of R_in and R_out.

After the dry functional test, we characterize the pressure decay from the pressurized pumping chamber through the normally close valves placed here in parallel. We can have therefore access to R_eq only which is defined by:

$R_{\mathrm{eq}}=\frac{R_{\mathrm{in}}{R}_{\mathrm{out}}}{R_{\mathrm{in}}+R_{\mathrm{out}}}$

This expression can be written in a more compact way:1/R_eq=1/R_in+1/R_out

R_eq is driven by the lowest value between R_in and R_out. We define R_eq min as the minimum allowed value during the functional test. This value is correlated to the max leak rate Q_max allowed by the design input and by the minimum difference of pressure between the inlet and the outlet ΔP_th that can be detected by the pressure sensor.

The maximum leak rate is defined by:

$Q_{\max }=\frac{\Delta P_{\mathrm{th}}}{R_{\mathrm{in}}+R_{\mathrm{out}}}$

For a given value of R_eq and ΔP_th, the minimum value of the sum R₁₀₁=R_in+R_out is obtained for R_in=R_out=2 R_eq as demonstrated below:

$R_{\mathrm{tot}}=R_{\mathrm{in}}+R_{\mathrm{out}}=\frac{R_{\mathrm{in}}{R}_{\mathrm{out}}}{R_{\mathrm{eq}}}$

Then

$R_{\mathrm{tot}}=\frac{R_{\mathrm{out}}^2}{R_{\mathrm{out}}-R_{\mathrm{eq}}}$

The function R_tot is minimal for a value of R_out that nullifies the derivative:

$\frac{\partial R_{\mathrm{tot}}}{\partial R_{\mathrm{out}}}=0$

We get2R_out(R_out−R_eq)−R_out²=0

And finally R_tot is minimized forR_out=R_in=2R_eq

In the worst case, the max leak rate Q_max between the inlet and the outlet of the pump unit, for the pressure gradient ΔP_th, is finally:

$Q_{\max }=\frac{\Delta P_{\mathrm{th}}}{4R_{\mathrm{eq}}}$

To summarize, we define a pump unit as tight a pump unit having passed with success the dry test using the min value of R_{eq min} for the equivalent fluidic resistances of the leak. This pump unit will exhibit in the worst case a max leak of Q_max under the pressure gradient ΔP_th which corresponds to the minimum difference of pressure that can be detected by the integrated sensor.

4.3. VALVE TIGHTNESS AND PATIENT SAFETY

We simply review here the basic concepts around the valve tightness as an introduction to the detection methods.

To generate a leak (defined here as a flow from the reservoir to the patient) two elements are necessary:

• • a leaky fluidic pathway
  • a gradient of pressure.Origin of the Finite Fluidic Resistance of the Valve

When the pump is not actuated, the system can be considered as a pressurized reservoir at the pressure P_in, which is connected to the patient at the pressure P_out through two check valves having a finite residual fluidic resistance, a dead volume and a small elasticity in between.

Because the valve seats are not compliant to rigid particles, the risk of permanent opening shall be considered. The use of filter therefore limits the occurrence of a particle contamination but we cannot exclude particle release from the filter of the device itself or simply the displacement of a particle, which would be already present in the pump, below the valve seat during actuation. Leaks due to defect of the valve seats or defect of the bonding are detected during the functional test and are not considered here.

Pressure Gradient

In normal conditions P_in is null or slightly negative by design: the reservoir is made of a thermoformed plastic soft pouch is soldered onto a hard shell; a small negative pressure is therefore needed to buckle the soft pouch towards the hard shell because of its dedicated shape. The range is typically 0/−10 mbar.

The pressure of the patient can be considered as null or slightly negative (−0.9+/−1.7 mbar according to E. Stranden and H. O. Myhre, Microvascular Research 24, 241-248 (1982), and −2.6 mbar according to Guyton and Hall, Textbook of Medical Physiology, Saunders Elsevier, twelfth edition (2011).

The additional pressure due to the water column height shall be considered. For patch device the maximum head height is few cm, inducing only few mbar between the reservoir and the patient.

In normal conditions the pump unit is safe because over infusion is prevented by the small and negative gradient of pressure between the reservoir and the patient.

We consider now deviations from the normal conditions: we can have overpressure in the reservoir due to an overfilling or due to a compression of the pumping unit external shell that should pressurize the reservoir. The pump unit should be able to detect any reservoir pressure conditions that make potential leakage hazardous for the patient even if no leakage is observed because this is an abnormal situation. The reservoir hard shell design is made to prevent the transmission of pressure to the reservoir soft pouch. The pump unit triggers an alarm when the pressure sensor in the pump “sees” a reservoir pressure larger than ΔP_th mbar. This pressure should be monitored in real time to alarm as soon as possible the patient of abnormal conditions.

Leak Detection, Back Flow and Free Flow

Valve leakage could induce:

• • I. A back flow
  • II. A free flow

A back flow is a leak induced under infusion during actuation in normal conditions. A leak at the inlet (outlet) induces a backflow during expulsion (suction) phase. These backflows corresponds in all cases to an under infusion. An alarm should be ideally triggered when the criterion on the pumping accuracy is not met. It is important to note that for the delivery accuracy it is no longer important to know if the inlet or the outlet or both are leaking. A criterion based on the equivalent fluidic resistance of the leak is enough to evaluate the infusion error due to leakage.

A free flow is a flow in delivery pathway which is not controlled by the pumping unit. A free flow is therefore an under or over infusion from the reservoir to the patient due to valve leakages out of specifications. Because the valves are placed in series both valves should exhibit a significant leak. As discussed previously abnormal pressure conditions should be also present to induce the flow.

To get a valve opening of 0.5 um for instance, it is necessary to have several spherical hard particles of 0.5 um onto the valve seat. The presence of only one particle induces a tilt of the valve that reduces significantly the fluidic resistance as illustrated below. Only one particle of 0.8 um onto the valve seat is equivalent to a valve aperture of 0.5 um.

The valves have also the capability to compress soft particles. In the present invention the worst case would be considered for analytical calculations: a particle of x um generates an opening of x um. Soft or non-spherical particles are not considered.

4.4. IN-STROKE LEAK DETECTION PRINCIPLE

The in-stroke leak detection principle is based on the analysis of the pressure decay within the pumping chamber after actuation. The sensitivity of the method is due to the very low elasticity of the pumping chamber coupled to its very low dead volume.

A typical pumping cycle has 3 phases according to FIG. 2:

• • 1) “A” is a ½ push of the pumping membrane starting for the rest position located between the two stop limiter towards the upper limiter (infusion)
  • 2) “B” is a full pull of the pumping membrane from the upper to the lower stop limiter (filling)
  • 3) “C” is a ½ push of the pumping membrane from the lower limiter to the rest position (“R”) (infusion)

After the first or the third ½ push phases, the pressure in the pumping chamber is positive and equal to the outlet valve pretension for tight valves (+P_{val out}.

After the second pumping phase (filling), the pressure in the pumping chamber is negative and equal to the inlet valve pretension for tight valves (−P_{val in}).

The residual valve leakages induce a pressure decay that can be analyzed to determine their equivalent fluidic resistances R_eq. For very large leakage the backflow is too large to generate any pressure in the pumping chamber and the pressure remains constant.

When the pumping membrane is against a stop limiter (after the cycles 1 and 2), the elasticity of the pumping chamber is only limited to the detector membrane elasticity and the secondary deformation of the pumping and outlet membrane due to the pressure.

When the pumping membrane is located at its rest position without any voltage on the piezo actuator, the pumping chamber shows a much larger elasticity due to the pumping membrane at its rest position even by considering the stiffening induced by the short-circuited actuator tightly linked to it.

In all cases the presence of bubbles should be considered for the estimation of the elasticity.

The pressure decay after the phases 1 and 2 are therefore expected to be very fast while after the phase 3 we expect a slow decay.

We will focus on the analysis of the pressure decay after the phase 1 or 2.

4.5. ANALYTICAL MODEL

We distinguish two different methods for the leak detection: the dry test method, based on the analysis of the air pressure decay during a functional test, and the wet method used during the functioning of the pump. In both cases we should estimate the elasticity of the system. For the dry test we should focus on the air compressibility and the method is described firstly. For the wet test, because of the very low compressibility of the water, the elasticity of the pump is relevant. We provide therefore an estimation of the pumping chamber elasticity including potential bubbles and describe finally the in-functioning leak detection model.

FIG. 3 shows a schematic fluidic model for the pumping device.

Leak Detection During Dry Test

The method is based on the pressure decay analysis in the pumping chamber after a compression and a blocking of the outlet valve which is obtained by applying a large pressure onto its vent.

We consider therefore an isothermal compression which reduces the pumping chamber volume from V_S+V_D to V_D, where V is the stroke volume and V_D is the dead volume.

We note n(t) the number of mole of gas and V the volume of the pump at the time t.

The total differential of the pressure is:

$\mathrm{dP}={\left(\frac{\partial P}{\partial n}\right)}_V\mathrm{dn}+{\left(\frac{\partial P}{\partial V}\right)}_n\mathrm{dV}$

We obtain, using the ideal gas law:

$\frac{\mathrm{dP}}{P}=\frac{\mathrm{dn}}{n}-\frac{\mathrm{dV}}{V}$

In this expression, dn is the variation of the number of gas moles due to the isothermal flow and dV is the variation of volume due to the elasticity of the pump.

The variation of volume of the pump with the pressure is mainly due to the deformation of the different membranes (detector, actuation, outlet valve). We assume that this variation is linear:V=V₀+α_g(P−P₀)

A variation of dP induces a variation of volume:dV=α_gdP

The quantity dn is related to the net flow Q during dt:

$\frac{\mathrm{dn}}{n}=\frac{Q}{V}\mathrm{dt}$

We obtain:

$\frac{\mathrm{dP}}{\mathrm{dt}}=\frac{\mathrm{PQ}}{V+{\alpha }_{g}P}=\frac{Q_{\mathrm{in}}+Q_{\mathrm{out}}}{{\alpha }_g+\frac{V}{P}}$

The flows Q_in and Q_out are respectively the inflow and outflow in the pump.

For the dry test, we assume that the elasticity of the pump can be neglected when the pump is in contact with a stop limiter. The volume V is therefore constant and equal to V_D.

The former equation writes:

$\mathrm{dt}=-R_{\mathrm{eq}}{V}_D\frac{\mathrm{dP}}{P\left(P-P_0\right)}=\frac{R_{\mathrm{eq}}{V}_D}{P_0}\left(\frac{1}{P}-\frac{1}{P-P_0}\right)\mathrm{dP}$

This equation can be easily solved and we obtain:

$P=\frac{P_0}{1-\left(1-\frac{P_0}{P_{\max }}\right)\mathrm{Exp}\left[-\frac{P_0\left(t-t_0\right)}{R_{\mathrm{eq}}{V}_D}\right]}$

Where P_max is the max pressure obtained at the end of the compression of the pumping chamber.

We note τ_1/2 the time necessary to reduce the relative pressure by a factor 2:

${\tau }_{1/2}=\frac{R_{\mathrm{eq}}{V}_D}{P_0}\ln \left[1+\frac{P_0}{P_{\max }}\right]$

Typical values:

R_{eq min}=4E16 Pa·s/m⁻³.

For nitrogen the value of R_{eq min} is divided by 57 according to its viscosity.

If the criterion is verified, the max flow rate for water at 37° C., in the worst case, would be 0.032 ul/h for a pressure gradient of 100 mbar.

Elasticity of the System

Considering wet leak test, the elasticity of the pump α shall be included into the model.

The volume V(P) of the pump takes the form:V(P)=V₀+α(P−P₀)=V_liquid+V_bubble(P)

Where V₀ is the volume of the pump at P=P₀.

Because of the very low compressibility of water we neglect the volume change of the liquid with the pressure.

The elasticity of the different parts of the pump is estimated here including the bubbles.

Pumping Membrane

If the membrane is in contact against a stop limiter, the membrane only undergoes a secondary distortion by applying pressure.

Typical Values

ΔV_membrane=0.135 nl/100 mbar

α_membrane=1.35E−17 m³/Pa

If the pumping membrane is at its rest position, the elasticity is now driven by the membrane and the piezo bender.

The elasticity of the pumping membrane in that configuration is typically:

ΔV_membrane=8.28 nl/100 mbar

α_membrane=8.28E−16 m³/Pa

Detector

Typical Values

ΔV_detector=0.25 nl/100 mbar

α_detector=2.5E−17 m³/Pa

Outlet

The outlet valve is a circular membrane which shows the following typical elasticity if closed:

ΔV_outlet=0.096 nl/100 mbar

α_outlet=9.6E−18 m³/Pa

Pump Elasticity

When the pumping membrane is in contact with the stop limiters, when the valves are closed and when there is no bubble, the overall pump elasticity is the sum of the elasticity of the pumping membrane, the detector and the outlet membrane as shown in FIG. 4:

ΔV_pump=0.48 nl/100 mbar

α=4.8E−17 m³/Pa

When the piezo is not powered, the elasticity of the pump is mainly governed by the elasticity of the pumping membrane:

ΔV_pump=8.625 nl/100 mbar

α=8.625E−16 m³/Pa

Bubbles

According to the ideal gas law, we have:

$V_{\mathrm{bubble}}\left(P\right)=V_b\left(P\right)=\frac{P_0}{P}{V}_{b0}$

Where P is the absolute pressure and V_bo the volume of the bubble at P=P₀.

We note P=P₀+P′ where P′ is the relative pressure.

If P′«P₀ we can do the following approximation that simplifies the model:

$\frac{P_0}{P}=\frac{1}{1+\frac{P^{\prime }}{P_0}}\approx 1-\frac{P^{\prime }}{P_0}\approx 1-\frac{P-P_0}{P_0}$

We obtain:

$V_b\left(P\right)\approx V_{b0}\left(1-\frac{P-P_0}{P_0}\right)=V_{b0}+{\alpha }^{\prime }\left(P-P_0\right)$ $W\mathrm{ith}{\alpha }^{\prime }=-\frac{V_{b0}}{P_0}$

4.6. IN-FUNCTIONING LEAK DETECTION/WET LEAK DETECTION

For the test of pressure decay, the system can be seen as a pumping chamber at a pressure P with two fluidic resistances in parallel connected respectively to a pressure reservoir at P_in and P_out according to FIG. 3.

Volume of Liquid V_liq in the Pumping Chamber

We consider all contributions to the system elasticity in the case of a pumping membrane being in contact with a stop limiter and the two valves being closed.

We have therefore:V_liquid=V₀+α(P−P₀)−V_b=V₀+α(P−P₀)−V_b0−α′(P−P₀)Expression of the Pressure Decay

In order to estimate the evolution of the pressure just after the end of a stroke, i.e. when the relative pressure in the pumping chamber is equal to the inlet pretension (after a fill) or the outlet pretension (after an infusion), we simply write the equation of the matter conservation:

$Q+\frac{{\mathrm{dV}}_{\mathrm{liquid}}}{\mathrm{dt}}=0$

We can write, since the flow is laminar:

$Q=-\frac{{\mathrm{dV}}_{\mathrm{liquid}}}{\mathrm{dt}}=\frac{P-P_0-P_{\mathrm{in}}^{\prime }}{R_{\mathrm{in}}}+\frac{P-P_0-P_{\mathrm{out}}^{\prime }}{R_{\mathrm{out}}}=-\left(\alpha -{\alpha }^{\prime }\right)\frac{\mathrm{dP}}{\mathrm{dt}}=\frac{P-P_0}{R_{\mathrm{eq}}}-\frac{P_{\mathrm{in}}^{\prime }}{R_{\mathrm{in}}}-\frac{P_{\mathrm{out}}^{\prime }}{R_{\mathrm{out}}}$

Where P_in′ and P_out′ are relative pressures

$\hspace{1em}\{\begin{array}{c}{P}_{\mathrm{in}}=P_0+P_{\mathrm{in}}^{\prime }\\ P_{\mathrm{out}}=P_0+P_{\mathrm{out}}^{\prime }\end{array}$

We note

$\varepsilon =\frac{R_{\mathrm{in}}}{R_{\mathrm{out}}}$ $\chi =\frac{P_{\mathrm{in}}^{\prime }}{R_{\mathrm{in}}}+\frac{P_{\mathrm{out}}^{\prime }}{R_{\mathrm{out}}}$ $\xi =\chi R_{\mathrm{eq}}=\frac{P_{\mathrm{in}}^{\prime }}{1+\varepsilon }+\frac{P_{\mathrm{out}}^{\prime }}{1+\frac{1}{\varepsilon }}$ $\lambda =\frac{1}{R_{\mathrm{eq}}\left(\alpha -{\alpha }^{\prime }\right)}$ $\mathrm{And}$ $\beta =P_{\mathrm{out}}^{\prime }+P_{\mathrm{val}\mathrm{out}}-\chi R_{\mathrm{eq}}=P_{\mathrm{out}}^{\prime }+P_{\mathrm{val}\mathrm{out}}-\xi$

Thus

$\chi R_{\mathrm{eq}}=\frac{P_{\mathrm{in}}^{\prime }}{1+\varepsilon }+\frac{P_{\mathrm{out}}^{\prime }}{1+\frac{1}{\varepsilon }}$

We obtain:

$\frac{\mathrm{dP}}{P-P_0-\chi R_{\mathrm{eq}}}=-\frac{\mathrm{dt}}{R_{\mathrm{eq}}\left(\alpha -{\alpha }^{\prime }\right)}=-\lambda \mathrm{dt}$

Thus

$\ln \left(P-P_0-\chi R_{\mathrm{eq}}\right)=-\frac{t-t_0}{R_{\mathrm{eq}}\left(\alpha -{\alpha }^{\prime }\right)}+v$

Where ν is an integration constant.

During the infusion, just after the push move of the membrane (i.e. when the outlet valve closes) the pressure in the pumping chamber is equal to:P(t₀)−P₀=P_out′+P_{vol out}=χR_eq+e^ν

Finally the expression of the relative pressure P−P₀ in the pumping chamber takes the form:

$P-P_0=\chi R_{\mathrm{eq}}+\left(P_{\mathrm{out}}^{\prime }+P_{\mathrm{val}\mathrm{out}}-\chi R_{\mathrm{eq}}\right)e^{-\frac{t-t_0}{R_{\mathrm{eq}}\left(\alpha -{\alpha }^{\prime }\right)}}=\xi +\beta e^{-\lambda \left(t-t_0\right)}$ $\mathrm{Or}$ $P-P_0=\frac{P_{\mathrm{in}}^{\prime }}{1+\varepsilon }+\frac{P_{\mathrm{out}}^{\prime }}{1+\frac{1}{\varepsilon }}+\left(P_{\mathrm{out}}^{\prime }+P_{\mathrm{val}\mathrm{out}}-\frac{P_{\mathrm{in}}^{\prime }}{1+\varepsilon }-\frac{P_{\mathrm{out}}^{\prime }}{1+\frac{1}{\varepsilon }}\right)e^{-\frac{\left(t-t_0\right)\left(1+\varepsilon \right)}{R_{\mathrm{in}}\left(\alpha -{\alpha }^{\prime }\right)}}$

During the time τ after t₀, the total volume of liquid ΔV_liq that flows outside the pumping chamber is:

$\Delta V_{\mathrm{liq}}={\int }_{t_0}^{t_0+\tau }\frac{P-P_0-P_{\mathrm{in}}^{\prime }}{R_{\mathrm{in}}}\mathrm{dt}+{\int }_{t_0}^{t_0+\tau }\frac{P-P_0-P_{\mathrm{out}}^{\prime }}{R_{\mathrm{out}}}\mathrm{dt}={\int }_{\tau }{\mathrm{dt}}^{\prime }\left[\frac{\xi -P_{\mathrm{in}}^{\prime }+\beta e^{-\lambda t}}{R_{\mathrm{in}}}+\frac{\xi -P_{\mathrm{out}}^{\prime }+\beta e^{-\lambda t}}{R_{\mathrm{out}}}\right]$

Finally we obtain

$V_{\mathrm{tot}}=\frac{\beta }{\lambda }\left(\frac{1-e^{-\lambda \tau }}{R_{\mathrm{eq}}}\right)$ Pressure Leak Threshold

We set the leak alarm threshold at the relative pressure P_leak and we can estimate, according to the environment conditions and the device characteristics, the duration τ_leak necessary to reduce the pumping chamber pressure from the relative pressure P_{val out} towards P leak is:

${\tau }_{\mathrm{leak}}=-\frac{1}{\lambda }\ln \left[\frac{P_{\mathrm{leak}}-\xi }{\beta }\right]$

It is therefore possible to simulate the duration τ_leak by varying all parameters of the previous formula according to their respective ranges.

In the following detailed form, it is possible to see all terms that affect τ_leak:

${\tau }_{\mathrm{leak}}=-R_{\mathrm{eq}}\left(\alpha -{\alpha }^{\prime }\right)\ln \left[\frac{P_{\mathrm{leak}}-R_{\mathrm{eq}}\left(\frac{P_{\mathrm{in}}^{\prime }}{R_{\mathrm{in}}}+\frac{P_{\mathrm{out}}^{\prime }}{R_{\mathrm{out}}}\right)}{P_{\mathrm{out}}^{\prime }+P_{\mathrm{val}\mathrm{out}}-R_{\mathrm{eq}}\left(\frac{P_{\mathrm{in}}^{\prime }}{R_{\mathrm{in}}}+\frac{P_{\mathrm{out}}^{\prime }}{R_{\mathrm{out}}}\right)}\right]$

Considering the in-functioning criterion for the leak rate, we compare the measured duration τ_{leak mes} to a specification τ_spec: the device is acceptable in term of leak rate ifτ_{leak mes}≥τ_spec Leak Criterion Based on the Worst Case Conditions of Free Flow: In-Stroke Detection

The in-functioning leak test gives an indication of the equivalent fluidic resistance of the valve leaks R_eq.

We measure τ_{leak mes} and we would like to know in the worst case what is the biggest leak rate associated to that measurement.

• • 1. We determine first the conditions necessary to obtain the lowest R_eq corresponding to τ_{leak mes} and we derive R_eq
  • 2. We determine the worst configuration for R_in and R_out according to R_eq
  • 3. We determine the max leak rate Q_max from the reservoir towards the patient in the worst case

For a given R_eq, the max leak from the reservoir to the patient is met for:

$R_{\mathrm{out}}=R_{\mathrm{in}}=2R_{\mathrm{eq}}$ $R_{\mathrm{eq}}=-\frac{{\tau }_{\mathrm{leak}\mathrm{mes}}}{\left(\alpha -{\alpha }^{\prime }\right)\ln \left[\frac{P_{\mathrm{leak}}-\frac{P_{\mathrm{in}}^{\prime }}{2}-\frac{P_{\mathrm{out}}^{\prime }}{2}}{P_{\mathrm{val}\mathrm{out}}+\frac{P_{\mathrm{out}}^{\prime }}{2}-\frac{P_{\mathrm{in}}^{\prime }}{2}}\right]}$

The measurement of R_eq depends on the pressure conditions at the inlet and the outlet as well as the quantity of air inside the pumping chamber. The detector launches an alarm when the pressure in the reservoir exceeds P_{in th} and when the bubble in the pump exceed V_{b th} (with the corresponding value of α′_th). We assume that the pressure at the outlet is null.

Thus

$R_{\mathrm{eq}}=-\frac{{\tau }_{\mathrm{leak}\mathrm{mes}}}{\left(\alpha -{\alpha }_{\mathrm{th}}^{\prime }\right)\ln \left[\frac{P_{\mathrm{leak}}-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{2}}{P_{\mathrm{val}\mathrm{out}}-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{2}}\right]}$

As discussed before, in the worst case, the max leak rate from the reservoir to the patient that can be obtained for a given R_eq is:

$Q_{\max }=\frac{\Delta P_{\mathrm{th}}}{4R_{\mathrm{eq}}}=-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{4{\tau }_{\mathrm{leak}\mathrm{mes}}}\left(\alpha -{\alpha }_{\mathrm{th}}^{\prime }\right)\ln \left[\frac{P_{\mathrm{leak}}-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{2}}{P_{\mathrm{val}\mathrm{out}}-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{2}}\right]$

Where ΔP_th is the max gradient of pressure between the inlet and the outlet that can be present without launching an alarm.

We have therefore associated a maximum leak rate, according to the worst external conditions to the measured value of τ_{leak mes}.

It is now possible to associate the specification in term of leak rate of the design input with a value of τ_{leak max DI}:

$Q_{\max \mathrm{DI}}=-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{4{\tau }_{\mathrm{leak}\max \mathrm{DI}}}\left(\alpha -{\alpha }_{\mathrm{th}}^{\prime }\right)\ln \left[\frac{P_{\mathrm{leak}}-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{2}}{P_{\mathrm{val}\mathrm{out}}-\frac{P_{\mathrm{in}\mathrm{th}}^{\prime }}{2}}\right]$

In that configuration, if τ_{leak mes}≥τ_{leak max DI}, we can ensure at 100% that the device is safe. If this criterion is too conservative, Monte Carlo simulations are desirable to determine a good trade-off between safety and false alarm rating.

To illustrate this point we propose the following numerical application:

P_leak=50 mbar

P_{in th′}=50 mbar

P_{val out}=110 mbar

α=4.8E−17 m³/Pa

bubble size threshold=10 nl

⇒α′=−1E−16 m³/Pa

Q_{max DI}=0.179 U/h

⇒τ_{leak max DI}=0.455 s

The time necessary to reduce the relative pressure by a factor 2 (i.e. from 100 to 50 mbar) is therefore 0.455 s according to these worst conditions.

Without bubbles, this time constant is only 0.148 s.

In normal conditions of pressure, the max gradient of pressure is 18.6 mbar.

We obtain:

τ_{leak max DI}=0.1254 s with bubble of 10 nl

τ_{leak max DI}=0.041 s without bubble

The analytical model can be used to determine τ_spec value that is acceptable in term of risk for the patient and that will launch too much false alarm: a high value of τ_spec is conservative in term of patient safety but the too high number of false alarm is not acceptable in term of usability.

The opposite situation with a small τ_spec is no longer acceptable because true alarms will be missed.

Leak Criterion Based on the Pumping Accuracy

Without any upstream or downstream pressure, a leak can induce a backflow that reduces the net pumped volume.

In bolus mode, we assume in a first approximation that the mean pressure during the positive or negative peak of pressure is +/−Pmax mbar during a maximum duration of T ms.

We assume a backflow at the inlet. The backflow can be determined by integrating the pressure profile and by dividing this by the fluidic resistance of the backflow Rf_backflow.

Typical Values:

Rf_backflow=4E14 Pa·s/m³.

This corresponds to a typical opening of about 1 to 1.5 um.

Since R_eq≈R_backflow we obtain:

${\tau }_{\mathrm{leak}}=-R_{\mathrm{eq}}\left(\alpha -{\alpha }^{\prime }\right)\ln \left[\frac{P_{\mathrm{leak}}}{P_{\mathrm{val}\mathrm{out}}}\right]$ $\mathrm{Using}$ $P_{\mathrm{leak}}=50\mathrm{mbar}$ $P_{\mathrm{val}\mathrm{out}}=100\mathrm{mbar}$ $\alpha =4.8E-17m^3\text{/}\mathrm{Pa}$ $\mathrm{bubble}\mathrm{size}\mathrm{threshold}=10\mathrm{nl}\Rightarrow {\alpha }^{\prime }=-1E-16m^3\text{/}\mathrm{Pa}$

We obtain

⇒τ_leak=0.041 s

During the infusion, the pressure shows a peak of pressure and after about 100 ms the pressure should be more or less equal to the outlet valve pretension. If the pressure decay is fast enough to reduce this pressure by a factor 2 in less than 41 ms, then we expect in this worst case an error on the accuracy larger than 5%.

Without bubble, this time is divided by 3, leading to a quasi instantaneous pressure release to P₀ after the actuation (less than 13.6 ms).

We can conclude that the criterion on the delivery accuracy is much easier to be met than the criterion on the leakage.

This estimation shows that we should consider the leak criterion based on the free flow and not on the back flow.

The FIG. 5 shows typical detector signals using the actuation profile given in FIG. 2 for a tight pump (bold line) and a pump having a back flow of 15% (thin line).

According to the examples provided above the fast pressure decay after actuation is very fast in presence of back flow.

4.7. LEAK DETECTION AND STATIC PRESSURE MEASUREMENT: OUT-OF-STROKE DETECTION

At slow basal rate, the pressure in the pumping chamber shall be monitored to check eventual reservoir over or under pressure.

To investigate the effect of a static pressure at the inlet, we assume that in case of constant inlet pressure, the valves are either together open or together closed.

We distinguish therefore two cases:

• • 1. P−P_out>P_{val out}
  • 2. P−P_out<P_{val out} Case 1: Static Pumping Chamber Pressure>Outlet Valve Pretension

In the case 1, because the outlet valve is open, the inlet valve is automatically open and the inlet pressure is therefore larger than P_{val in}+P_{val out}+P₀. In that configuration of large overpressure (larger than the sum of the valve pretensions) the flow is very large. We assume that the fluidic resistances of the valves are equivalent in that configuration. To estimate the max flow rate, we only consider the fluidic resistances of the valves and we do not consider singular head losses.

The FIG. 6 shows the typical maximum flow rate at 37° C. using the former approximation:

The pressure P in the pumping chamber is here the half of the inlet pressure.

Case 2: Static Pumping Chamber Pressure<Outlet Vale Pretension

The pump is in basal configuration. During the last stroke the equivalent fluidic resistance of the valves has been estimated and there is no alarm and no inlet overpressure.

We suppose the inlet pressure rises to a value P_in. The pressure in the pumping chamber is equal to P with P<100 mbar. In this configuration both valves are closed. We can assume that from the last stroke the residual leaks of the valves do not change. The equivalent fluidic resistance R_eq of the valves is therefore known.

We try to estimate in the worst case what is the max free flow Q_max for a measured value of P and a given value of R_eq.

We have already shown that for a given P_in and a given R_eq, the max flow rate is obtained when

$P_{\mathrm{in}}-P_0=\frac{P-P_0}{2}$

This rule is unfortunately not reciprocal.

The max inlet pressure is equal to P+P_{val in} (otherwise the inlet valve is open in contradiction to the discussion hereabove).

We will now use the max leak rate theorem.

Max Leak Rate Theorem

If P−P₀<P_{val out}, and for a given R_eq of the valves, the max leak rate is obtained for P_in=P+P_{val in}

This theorem is demonstrated using a proof by contradiction.

Demonstration:

We consider a system having a pressure P in the pumping chamber, an equivalent fluidic resistance of the valves R_eq and a pressure P_in<P+P_{val in} inducing a leak rate Q.

We will show that for any increase of inlet pressure δP_in from any P_in up to P+P_{val in} there is always a couple of values R_in and R_out values that keeps constant R_eq and P and that lead to a flow rate larger than Q.

We have:

$\hspace{1em}\{\begin{array}{c}Q=\frac{P_{\mathrm{in}}-P_0}{R_{\mathrm{in}}+R_{\mathrm{out}}}=\frac{P-P_0}{R_{\mathrm{out}}}\\ \mathrm{and}\\ Q^{\prime }=\frac{P_{\mathrm{in}}+\delta P_{\mathrm{in}}-P_0}{R_{\mathrm{in}}^{\prime }+R_{\mathrm{out}}^{\prime }}=\frac{P-P_0}{R_{\mathrm{out}}^{\prime }}\end{array}$

We will show that there are values R′_in and R′_out that ensure that Q′>Q.

$R_{\mathrm{eq}}=\frac{R_{\mathrm{in}}{R}_{\mathrm{out}}}{R_{\mathrm{in}}+R_{\mathrm{out}}}=\frac{R_{\mathrm{in}}^{\prime }{R}_{\mathrm{out}}^{\prime }}{R_{\mathrm{in}}^{\prime }+R_{\mathrm{out}}^{\prime }}=\frac{R_{\mathrm{in}}}{1+\varepsilon }=\frac{R_{\mathrm{in}}^{\prime }}{1+{\varepsilon }^{\prime }}=\frac{R_{\mathrm{out}}}{1+\frac{1}{\varepsilon }}=\frac{R_{\mathrm{out}}^{\prime }}{1+\frac{1}{{\varepsilon }^{\prime }}}$

With

$\hspace{1em}\{\begin{array}{c}\varepsilon =\frac{R_{\mathrm{in}}}{R_{\mathrm{out}}}=\frac{P_{\mathrm{in}}-P_0}{P-P_0}-1\\ {\varepsilon }^{\prime }=\frac{R_{\mathrm{in}}^{\prime }}{R_{\mathrm{out}}^{\prime }}=\frac{P_{\mathrm{in}}+\delta P_{\mathrm{in}}-P_0}{P-P_0}-1\end{array}$

We obtain:

$R_{\mathrm{in}}^{\prime }=\left(1+\frac{\delta P_{\mathrm{in}}}{P_{\mathrm{in}}-P_0}\right)R_{\mathrm{in}}>R_{\mathrm{in}}$ $\mathrm{And}$ $R_{\mathrm{out}}^{\prime }=\frac{\left(P_{\mathrm{in}}-P\right)}{\left(P_{\mathrm{in}}+\delta P_{\mathrm{in}}-P\right)}\times \frac{\left(P_{\mathrm{in}}-P_0+\delta P_{\mathrm{in}}\right)}{\left(P_{\mathrm{in}}-P_0\right)}{R}_{\mathrm{out}}=\frac{1+\left(\frac{\delta P_{\mathrm{in}}}{P_{\mathrm{in}}-P_0}\right)}{1+\left(\frac{\delta P_{\mathrm{in}}}{P_{\mathrm{in}}-P}\right)}{R}_{\mathrm{out}}$

For P>P₀ we check that R′_out<R_out as expected for Q′>Q.

We have therefore demonstrated that the max flow is obtained for P_in=P+P_{val in}.

The max leak rate takes the form:

$Q_{\max }=\frac{P+P_{\mathrm{val}\mathrm{in}}-P_0}{R_{\mathrm{in}}+R_{\mathrm{out}}}=\frac{P-P_0}{R_{\mathrm{out}}}$

The max flow rate is obtained for:

$\varepsilon =\frac{R_{\mathrm{in}}}{R_{\mathrm{out}}}=\frac{P_{\mathrm{val}\mathrm{in}}}{P-P_0}$

Finally, the max leak rate, for a given R_eq and a given static pressure P in the pumping chamber, takes the form:

$Q_{\max }=\frac{P-P_0}{R_{\mathrm{eq}}\left(1+\frac{P-P_0}{P_{\mathrm{val}\mathrm{in}}}\right)}=\frac{1}{R_{\mathrm{eq}}\left(\frac{1}{P-P_0}+\frac{1}{P_{\mathrm{val}\mathrm{in}}}\right)}$

We can compare the accuracy of this out-of-stroke leak detection with the in-stroke detection as described hereabove.

We consider now an in-stroke detection threshold of 50 mbar leading to a max leak rate of 0.179 U/h: we obtain R_eq=2.514E15 Pa·s/m³.

The FIG. 7 shows the max leak rate in U/h that can be detected using in-stroke and out-of-stroke detection as a function of the detection pressure threshold:

The measurement of the inner detector to check a possible inlet overpressure is mandatory. The main issue of this measurement is that the inner detector is not sensitive to inlet pressure lower than 100 mbar if the ratio

$\varepsilon =\frac{R_{\mathrm{in}}}{R_{\mathrm{out}}}$ is large. This effect is due to the inlet valve pretension. During the stroke, the inlet valve opens and the detector directly “sees” the reservoir pressure.

Even if the out-of-stroke detection of the leak is two at four times less sensitive than during a stroke, this method gives fundamental improvement in term of patient safety because of the continuous estimation of the maximum leak rate in the worst case, without additional stroke and with limited power consumption.

To summarize, the monitoring of the inner (4) and outer (13) detector signals, when the pump is not actuated, is used to detect under or over pressure onto the reservoir and to estimate the related maximum over or under infusion.

4.8. STATIC LOAD ON RESERVOIR HOUSING

Static load could be detected by the pressure sensors without actuating the pump if it results:

1. an increase of the reservoir pressure

2. or an increase of the interstitial pressure

If the static load transmits a force directly onto the reservoir membrane, the reservoir pressure increases as well as the downstream pressure according to the discussion here above. A static measurement of the inner pressure sensor (4) is used to detect the effect of the static load.

If the static load transmits a force directly onto the patient skin around the cannula, typically for patch pump, the tissue compression will increase the interstitial pressure and therefore the pressure at the pump outlet (18) because the insulin will transmit this pressure. The two pressure sensors (4 and 13) and more especially the sensor (13) at the outlet of the pump will directly see this pressure increase.

4.9. VENT CLOGGING

The first and third cavities (described in the application EP11171155.2) have venting means to prevent any pressurization. If one of said venting means get clogged, the pressure gradient between inside device and external environment may change inducing an over or under delivery.

The FIG. 8 shows the pumping device and its different ports. The inlet valve port (21) is connected to the reservoir wherein a pressure form the reservoir (“P_r”). The outlet valve port (25) is connected to the patient wherein a pressure form the patient (“P_p”). The membrane port (22), the inner detector port (23) and the outer detector port not represented here are connected to the pump controller that includes the actuator wherein a pressure (“P_pc”). The outlet valve has a specific venting port 24 which is used during functional test as described in the document WO 2010/046728.

In another embodiment, the document WO2007113708 shows for instance a pumping device wherein the reservoir and the pump controller (actuator, driving electronics and batteries) share the same venting hole towards outside.

In case of vent clogging, a positive or negative pressure may be trapped in the reservoir housing and/or in the pump controller.

The change of pressure due to clogging can be monitored using the two sensors of the pump even without actuation.

Vent Clogging Case Studies:

• • 1. clogging of reservoir vent
    • Detection using inner pressure sensor (see 4.6 to 4.8)
  • 2. clogging of pump controller vent only
    • The sensor membrane back side (which is not in contact with the liquid) will be pressurized e.g. via the port (23) for the inner detector (4), inducing a deflection of the membrane and therefore a signal change. Positive (respectively negative) pressure on the port (23) is equivalent to a negative (resp. positive) pressure in the pumping chamber (30).
  • 3. clogging of all venting ports
    • The same pressure is observed in the reservoir and in the pump controller, therefore the outer detector (13) membrane, which is connected on one side with the patient and on the other side with the pump controller, is able to detect any pressure changes in the pump controller.

The clogging of the outlet valve port (24) only will be detected during actuation if the cavity below the outlet valve is pressurized. This pressure will induce an offset on the outlet valve opening threshold and this offset can be detected according to the methods described in the document WO 2010/046728. This clogging is only possible during the mounting of the pump controller onto the reservoir.

4.10. RESERVOIR FILLING MONITORING

The reservoir should be filled with a given quantity of liquid. In case of overfilling, the device should prime the pump and actuate in order to limit the pressure in the reservoir due to this overfilling.

The activation of the inner (4) and outer (13) detectors during the filling is therefore useful to alarm the patient of any reservoir overpressure using vibrations, visual or audible alarms.

Functional pumps are characterized in production. The equivalent fluidic resistance is determined with a criterion for the minimum value allowed. Since the pump has never been actuated between the production and the filling, the minimum equivalent fluidic resistance is known. The measurement of the pressure during the filling gives therefore an indication of the flow rate through the pump. For very large overpressure, the valves open and the flowrate becomes driven by the curve shown in FIG. 6.

The alarm is triggered when the pressure in the pumping chamber is larger than a predefined value. The alarm may be triggered continuously if the pressure remains larger than this predefined value and may be stopped only once the pressure is decreased below this predefined value.

The pressure release may be performed by the patient himself who can either remove liquid by pulling on the syringe piston or simply by releasing the syringe piston.

At the end of the filling, the pressure in the reservoir may be large in case of overfilling. The pressure is therefore monitored while the pump is actuated continuously during the time necessary to reduce the pressure up to a predefined threshold value. The pump is then actuated a predefined number of cycles in order to ensure that the relative reservoir pressure is equal or very close to zero.

Claims

1. A medical device comprising a pumping device, a pumping chamber, a sensor configured to measure a pressure in the pumping chamber, a reservoir in fluid communication with the pumping chamber, a notification device, and a processing unit configured to monitor a signal of the pressure sensor during a filling of the reservoir when the pumping device is not actuated; wherein the processing unit is further configured to perform at least one of the following steps:triggering a notification with the notification device when a first threshold pressure signal is reached at the end of reservoir filling;continuously actuating the pumping device to remove a determined volume of fluid from the reservoir after the end of reservoir filling.

2. The medical device according to claim 1, wherein during the filling the pumping device is in a rest position.

3. The medical device according to claim 1, wherein the processing unit is further configured to perform a step of stopping the triggering of the notification when the signal of the sensor is lower than a predefined threshold.

4. The medical device according to claim 1, wherein the processing unit is further configured to perform a step of stopping the step of continuously actuating the pumping device when a predefined number of strokes have been reached by the step of continuously actuating.

5. The medical device according to claim 1, wherein the processing unit is further configured to perform a step of starting the continuously actuating after a predetermined time period after the end of the reservoir filling.

6. The medical device according to claim 1, wherein the processing unit is further configured to perform a step of stopping the continuously actuating when a predefined threshold for the signal of the sensor has been reached.

7. The medical device according to claim 1, wherein the reservoir includes a predefined volume.

8. The medical device according to claim 1, wherein in the continuously actuating the pumping device, the determined volume of fluid is removed from the reservoir such that a volume of fluid remaining in the reservoir reaches a predefined value.

9. The medical device according to claim 1, wherein the pumping device further includes a pumping membrane, and the sensor is arranged to be in operative connection with the pumping membrane of the pumping chamber.

10. The medical device according to claim 1, wherein the pumping device further includes a pumping membrane and an actuator for actuating the pumping membrane, wherein during the filling, the pumping membrane is in a rest position.

11. The medical device according to claim 1, wherein the pumping device further includes a pumping membrane and an actuator for actuating the pumping membrane, wherein during the filling, the actuator of the pumping membrane is not powered.