Patent Abstract:
A package testing system or apparatus that may be mounted directly onto an F/F/S machine and allows for communication with an F/F/S machine in the form of either a digital or analog signal. The communication may be implemented into a PID loop which allows for a predetermined burst pressure set point to be reached “automatically” by either the burst pressure controller or the F/F/S controller to automatically adjust the sealing parameters via the PID loop. The system may employ a novel sealing system that uses either a viscous solution or a series of laminated materials to seal either the needle entry point or the puncture side of the material in its entirety, thereby eliminating the use of known sealing patches that cover the porous webbing in testing. Methods for conducting such testing and for operating such systems are within the scope of the present disclosure.

Full Description:
CROSS-REFERENCE TO RELATED APPLICATION 
     This application claims the benefit of U.S. Provisional Application No. 61/592,735, filed Jan. 31, 2012, the disclosure of which is incorporated herein by reference in its entirety. 
    
    
     TECHNICAL FIELD 
     The present disclosure relates to package integrity testing apparatus and methods and more specifically to apparatus and methods for testing package integrity that are capable of testing porous packages. 
     BACKGROUND 
     Medical devices are commonly packaged by form fill seal or F/F/S machines to place the devices in packages in which they can be sterilized and the sterilization maintained until usage. In order to verify the package integrity, a subset of packages from each batch processed by a machine are typically pulled and subject to testing for seal completeness. For packages made of a non-porous material, such tests are typically burst tests in which a needle is used to pressurize the package until the seal or package ruptures. Properly sealed packages will require at least a known pressure before bursting. However, for packages with a porous portion, such as a plastic package with a paper top, such burst testing does not work as the injected air flows through the porous portion of the package. Prior art attempts to address this issue by utilizing a sealing patch that is manually applied to the packaging web area that is to be punctured. However, such a seal can mask issues with the web area, for example holes in the porous portion that are covered by the seal, but which would represent a breach of the package integrity. 
     Some examples of known testing devices include those disclosed in the following U.S. Pat. No. 7,810,377, U.S. Pat. No. 6,640,614, U.S. Pat. No. 4,916,936, U.S. Pat. No. 4,459,843, U.S. Pat. No. 6,038,915, U.S. Pat. No. 4,539,836, U.S. Pat. No. 4,837,707, and U.S. Pat. No. 4,733,555, the contents of each of which are incorporated by reference herein in their entirety. However, current package burst test technology does not provide a reliable method for testing different types of packages directly on the F/F/S machine. Testing devices or methods that addressed these various shortcomings would be an improvement in the art. 
     SUMMARY 
     The present disclosure includes a package testing apparatus that may be mounted directly onto an F/F/S machine. The apparatus allows for communication with an F/F/S machine in the form of either a digital or analog signal. The communication may be implemented into a PID (Proportional, Integral, Derivative) loop which allows for a predetermined burst pressure set point to be reached “automatically” by either the burst pressure controller or the F/F/S controller to automatically adjust the sealing parameters via the PID loop. This apparatus may employ a novel sealing system that uses either a viscous solution to seal the needle entry point or a series of laminated materials to seal either the needle entry point or the puncture side of the material in its entirety. This apparatus greatly reduces the time for each test by eliminating the use of the known sealing patches that cover the porous webbing whether “offline” or “in-line” in testing. 
     Methods for conducting such testing, methods for operating such devices and systems including such devices are also as part of the present disclosure. Commercial applications of the methods, systems, and devices in accordance with the present disclosure may include offline, in-line, flexible, rigid, porous, and non-porous packaging. The application may be implemented on any packaging sealing machine. 
    
    
     
       DESCRIPTION OF THE DRAWINGS 
       It will be appreciated by those of ordinary skill in the art that the various drawings are for illustrative purposes only. The nature of the present disclosure, as well as various embodiments, may be more clearly understood by reference to the following detailed description, to the appended claims, and to the several drawings. 
         FIG. 1  is a perspective view of a modular testing system in accordance with the principles of the present invention. 
         FIGS. 2A and 2B  are side and front views of a modular testing unit of the system of  FIG. 1 . 
         FIG. 3  is a partially exploded view of a lower assembly of another modular testing unit in accordance with the principles of the present disclosure. 
         FIGS. 4A and 4B  are exploded views of two embodiments of bottom sealing units for attachment to the lower assemblies of  FIGS. 2 and 3 , respectively. 
         FIG. 5  is a Data Points Hierarchy Chart for conducting a Non-Torturous Path Hole Evaluation Test. 
     
    
    
     DETAILED DESCRIPTION 
     The present disclosure relates to systems and methods for testing package integrity. It will be appreciated by those skilled in the art that the embodiments herein described, while illustrative, are not intended to so limit the scope of the appended claims. Those skilled in the art will also understand that various combinations or modifications of the embodiments discussed herein can be made without departing from the scope of this disclosure. All such alternate embodiments are within the scope of the appended claims. 
     Referring to  FIG. 1 , a modular testing apparatus  10  in accordance with the present invention is depicted. The modular testing apparatus  10  may be positioned at the end of an F/F/S machine allowing it to be actuated and test packages coming directly off the machine as may be desired. For example, at periodic intervals, such as every tenth cycles on the F/F/S machine (or other intervals as may be desired or required by an application), the modular testing apparatus  10  may be actuated to perform in-line testing of packages as they are produced. 
     A number of individual modular testing units  20  are organized into one or more rows  11 . A framework  12  supports a number of individual modular testing units  20  in each row  11 . The individual units  20  may be attached to the framework  12  by set screws or bolts  102  passing through one or more attachment slots  104 , allowing for adjustment of the position of the units  20 . It will be appreciated that for certain embodiments, only a single row  11  of individual modular testing units  20  may be used and will vary upon the particular F/F/S machine with which the system  10  will be used. The framework  12  may be positioned to the individual modular units  20  to test individual packages P as they emerge from a F/F/S machine. 
     An individual modular testing unit  20  is depicted in isolation from the row  11  in  FIGS. 2A and 2B  with a package P placed in the proper position for conducting a test. The individual modular testing unit  20  includes an upper assembly  200  and a lower assembly  250 . Upper assembly  200  includes a frame  202  in which a linear actuator  204  is disposed. An upper linear shaft  210  is connected by an intermediate plate  211  to two lower linear shafts  212 A and  212 B which extend from the upper assembly  200  to lower assembly  250  through the frame  202  lower end. The two lower linear shafts  212 A and  212 B may pass through bearing assemblies  213  in frame  202  to facilitate movement. Upon actuation by the linear actuator  204  the shafts  212 A and  212 B are extended or retracted to lower or raise the lower assembly  250 . It will be appreciated that while as depicted, the two lower shafts  212 A and  212 B may extend from intermediate plate  211  to which the actuator is linked by upper linear shaft  210 , that in alternate embodiments, more or fewer shafts may be used and intermediate plate  210  may be omitted or varied as required. It will be further appreciated that in some embodiments the shafts  212 A and  212 B may vary in size, as depicted in  FIGS. 3 and 4B . 
     A pressure transducer  208  may be disposed on the upper assembly  200  and a connection  206  thereto may similarly be disposed with a connecting line therebetween. It will be appreciated that in some embodiments a single transducer may be used to which all the modular units  20  in a row or all the modular units  20  in a system  10  may be connected, depending on the desired installation. 
     A solenoid valve  205  may also be present and in communication with an air source, the pressure transducer  208 , and/or the needles. The type of solenoid valve may vary based on desired use, as discussed further herein. In some instances, a three-way solenoid valve may be used. 
     The lower assembly  250  is depicted more clearly in  FIGS. 4A and 4B  include a needle block manifold  251  in which hollow needles  252  and  254  are installed. The needles may be threaded to allow for ready replacement. Each needle is in communication with a line allowing a gas such as air to pass therethrough, as indicated by fittings  264  and  262  for connecting to external lines. One needle  254  is connected to a source of gas via fitting  264  and the other needle  252  to the pressure transducer  208  through fitting  262 . For clarity, a line between fitting  262  and the corresponding fitting  206  on the pressure transducer has been omitted from the drawings, but it will be appreciated that any suitable tubing may be used. It is noted that the different embodiments of  3 A and  3 B reflect different locations on needle block manifold  251  for the fittings  264  and  262 , which may vary based on design for a particular use. 
     As depicted in  FIG. 4A  and lower assembly  250  includes a sealing structure  400  for making a sealing connection to the surface of a package, which may be formed from a number of layers. In the depicted embodiment, a spacer block  450  is attached to the needle block manifold  251  and allows the needles  252  and  254  to pass though apertures therein. A foam backer  454 , such as a compressible foam layer, is disposed under spacer block  450  and a seal material  456 , such as silicone or rubber mat or sealing foam is used to form a bottom seal. When the modular testing unit  20  is actuated, the seal  456  may cover the entire upper surface of a package P. This allows the testing unit to be used to perform a burst test. In other embodiments where the seal  456  does not cover the entire porous surface of a package, the test may be conducted as described further below in order to assess flow rates. 
     In another embodiment, depicted in  FIG. 4B , the sealing structure  400 A may be removable and refillable ink tank  502  having two apertures for the needles  252 ,  254  to pass therethrough. Seals  504  disposed on the bottom surface thereof contact a package surface on extension and as depicted in the appendix, may mark the package with ink as a wetted stamp, to create a visual indicator that the packages have been tested. 
     To perform a flow rate test on a porous package, the needles  252  and  254  pierce the top surface of the package P inside a sealed area. A known volume and pressure of gas are injected into the package through the “in needle” and the rate of gas flow out of the package through the “out needle” is then measured by the pressure transducer  208 . Since the porous packaging material has a known, or expected, flow rate therethough, the difference between the inflow and outflow of gas through the needles can be used to determine whether the package exhibits variation from the expected rate to thereby determine seal integrity, for example if the package has a gap or opening that allows for an increased rate of flow. 
     One application for the system  10  is to characterize the integrity of a package being made of rigid, flexible, porous, or non-porous material. The apparatus  10  may be used to find holes in packaging material of a certain size that are not of a torturous path in the packaging material. The apparatus  10  may then be used to characterize the seal strength between two materials by relating the burst pressure of the package to the seal strength of the package, following the initial test. The apparatus is meant to be either mounted directly on a form/fill/seal machine as an inline test or on a bench-top mounting system. The apparatus may be utilized as a development device for characterizing machine sealing parameters either “off-line” or “in-line”. 
     As depicted, the apparatus uses a pneumatic air supply, a pneumatic air cylinder, and a pneumatic solenoid valve to drive a puncture assembly into packaging web. It will be appreciated that the linear actuator may be mechanical rather than pneumatic, if desired. The puncture assembly may employ one needle or a series of needles that connect to a pneumatic airline for pressurizing the package, a transducer ( 208 ,  FIG. 2A ) for converting the physical internal pressure of the package into an analog signal, an electronically controlled pneumatic pressure regulator for controlling the pressure into the package, a pneumatic proportional solenoid valve for controlling the flow into the package, and an electronic pneumatic flow sensor for monitoring the pneumatic flow into and/or out the package using the signal from the transducer. The analog signal may be captured by a Programmable Logic Control (“PLC”) unit, or similar device, and converted into a digital pressure which is presented to the operator by a Human Machine Interface unit, or similar device. The needle entry point is sealed by a soft non-permeable material that surrounds the needle and is attached to the puncture assembly unit. This “sealing” layer may encompass the porous packaging material so that the porosity of the package diminishes to a negligible value, as with  FIG. 4A . The sealing layer may also be comprised of a permeable material which is saturated with a solution, as in  FIG. 4B . The solution may be of a certain desired viscosity that is complementary of the porosity of the material in which it is infused. The solution may be infused with a pigment which acts as a marking agent for “tested packages”. All electronic parts of the apparatus may be controlled by a PLC unit that employs certain algorithms to control the unit as a whole. Multiple testing units may be combined in a fashion that allows for concurrent testing of multiple packages. 
     The process for testing each package entails the puncturing of the package with the two needles followed by a procedure which varies the flow of pressurized air to one of the two puncture needles. This allows for pressurized air to flow into the package from the “in needle” and out of the package through the “out needle”. Once the pressurized air flows through the out needle, the volume is measured by an electronic pneumatic flow sensor and is then released to ambient air pressure. This value is captured by several data points and stored in the PLC for further calculation. 
     Once the “flow” data points have been collected, a second test may be initiated which entails sealing the “out needle” from ambient air pressure with a “three way” electronic solenoid valve, which is connected to a pneumatic pressure transducer. Another procedure is then executed which varies the flow of pressurized air to the “in needle” while concurrently collecting and storing a series of pressure sensor readings from the pneumatic pressure transducer. 
     The “Non-Torturous Path Hole Evaluation Test is divided into two main tests, the “Flow Test” and the “Pressure Test”, which are executed subsequently. Each main test may be broken into a number of specific data points, in one example 72 data points which are separated into 12 subsets may be used. The 12 subsets may then be divided in half leaving 2 groups. An average value for the six data points contained in each subset may then be calculated. An average value is then calculated for each group leaving one value for each group. The two values from each group may be mathematically manipulated to produce a higher statistically significant confidence in the test. Results for such a test are depicted in Table 1 and a Data Points Hierarchy Chart for conducting the test is presented in  FIG. 5 . 
     
       
         
               
             
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 1 
               
             
             
               
                   
               
               
                 TEST PARAMETERS FOR AUTO EVALUATION CYCLE, TEST PARAMETERS 
               
               
                 ARE IN PERCENTAGE OF VALVE ORIFACE OPENING 
               
             
          
           
               
                   
                 CYCLE NUMBER 
               
             
          
           
               
                   
                 1 
                 2 
                 3 
                 4 
                 5 
                 6 
                 7 
                 8 
                 9 
                 10 
                 11 
                 12 
               
               
                   
                   
               
             
          
           
               
                 TEST 
                 1 
                 65 
                 68 
                 70 
                 72 
                 74 
                 76 
                 80 
                 84 
                 88 
                 90 
                 94 
                 96 
               
               
                 NUMBER 
                 2 
                 72 
                 74 
                 76 
                 78 
                 80 
                 82 
                 74 
                 76 
                 78 
                 80 
                 84 
                 88 
               
               
                   
                 3 
                 60 
                 65 
                 70 
                 75 
                 80 
                 85 
                 90 
                 95 
                 80 
                 75 
                 70 
                 65 
               
               
                   
                 4 
                 100 
                 90 
                 80 
                 70 
                 60 
                 50 
                 70 
                 72 
                 74 
                 76 
                 78 
                 80 
               
               
                   
                 5 
                 100 
                 90 
                 80 
                 70 
                 60 
                 50 
                 80 
                 82 
                 84 
                 86 
                 88 
                 90 
               
               
                   
                 6 
                 100 
                 90 
                 80 
                 70 
                 60 
                 50 
                 90 
                 92 
                 94 
                 96 
                 98 
                 100 
               
               
                   
                 7 
                 80 
                 85 
                 90 
                 60 
                 70 
                 80 
                 65 
                 70 
                 75 
                 80 
                 85 
                 90 
               
               
                   
                 8 
                 70 
                 71 
                 72 
                 73 
                 74 
                 75 
                 85 
                 86 
                 87 
                 88 
                 89 
                 90 
               
               
                   
                 9 
                 90 
                 90 
                 90 
                 90 
                 90 
                 90 
                 70 
                 70 
                 70 
                 70 
                 70 
                 70 
               
               
                   
                 10 
                 80 
                 80 
                 80 
                 80 
                 80 
                 80 
                 80 
                 80 
                 80 
                 80 
                 80 
                 80 
               
               
                   
               
             
          
         
       
     
     Additionally, applicant notes that if tests of packages in accordance with the present invention are conducted in a solution, such as underwater, rather than in air, then the variability of the test results goes down dramatically. This is because the water acts as a weak seal by creating greater pressure outside the package. Essentially, it takes more force to break through the paper making it more porous. It also makes the paper fibers swell in paper webs which decreases the porosity. 
     While this invention has been described in certain embodiments, the present invention can be further modified with the spirit and scope of this disclosure. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practices in the art to which this invention pertains and which fall within the limits of the appended claims.

Technology Classification (CPC): 6