Permeation instruments are used to measure the transmission rate of a target analyte, such as oxygen, carbon dioxide or water vapor, through various samples, such as membranes, films, envelopes, bottles, packages, containers, etc. (hereinafter collectively referenced as “test films” for convenience). Typical test films are polymeric packaging films such as those constructed from low density polyethylene (LDPE), high density polyethylene (HDPE), oriented polypropylene (OPP), polyethylene terepthalate (PET), polyvinylidene chrloride (PVTDC), etc. Typically, the film to be tested is positioned within a test chamber to sealing separate the chamber into first and second chambers. The first chamber (commonly referenced as the driving or analyte chamber) is filled with a gas containing a known concentration of the target analyte (commonly referenced as a driving gas). The second chamber (commonly referenced as the sensing chamber) is flushed with an inert gas (commonly referenced as a carrier gas) to remove any target analyte from the cell. A sensor for the target analyte is placed in fluid communication with the sensing chamber for detecting the presence of target analyte that has migrated into the sensing chamber from the driving chamber through the test film. Exemplary permeation instruments for measuring the transmission rate of oxygen (O2), carbon dioxide (CO2) and water vapor (H2O) through test films are commercially available from Mocon, Inc. of Minneapolis, Minn. under the designations O
Permeation instruments are being used more often to measure ever decreasing concentrations of target-analyte, into the ppm or even ppb range, and are therefore extremely sensitive to even minute atmospheric contamination of the fluids used in the instrument. Permeation instruments employ an extensive network of fluid interconnections with numerous valves to achieve the desired choreographed flow of driving and carrier gas through the instrument, especially when the instrument employs a plurality of testing cells in fluid communication with a single common target-analyte sensor. Each fitting in the fluid transfer system of the instrument is a potential source of contamination as atmospheric oxygen, carbon dioxide and water vapor leak around or permeate through the seals on the fittings, especially as the seals on the fittings loosen over time.
Accordingly, a substantial need exists for a permeation instrument capable near elimination of atmospheric-induced contamination of the driving and carrier gases flowing through the instrument throughout the lifespan of the instrument.
The invention is a target-analyte permeation testing instrument characterized by a block manifold. The instrument has a target-analyte sensor and a plurality of test cells for measuring target-analyte permeation rate of a test film. Each test cell defines a testing chamber and is operable for retaining a test film to sealingly divide the testing chamber into a driving chamber and a sensing chamber. The block manifold is fixed to the plurality of cells and has a plurality of channels in fluid communication with the testing chamber of each cell, a pressurized source of driving gas, a pressurized source of inert gas, and a target-analyte sensor. The plurality of channels are configured and arranged to selectively carry driving gas from the pressurized source of driving gas to the driving chamber of each cell, carry driving gas from the driving chamber of each cell to a driving gas exit port in the manifold, selectively carry inert gas from the pressurized source of inert gas to the sensing chamber of each cell, and selectively carry inert gas from the sensing chamber of each cell to the target-analyte sensor.
The block manifold can include a refillable first water reservoir in selective fluid communication with the source of driving gas and in fluid communication with the driving chamber of each cell, and a second refillable water reservoir in selective fluid communication with the source of inert gas and in fluid communication with the sensing chamber of each cell.
Referring generally to
The block manifold 100 can include a refillable first water reservoir 50A in selective fluid communication with the source of driving gas A and in fluid communication with the driving chamber 70nA of each cell 70n, and a second refillable water reservoir 50B in selective fluid communication with the source of inert gas B and in fluid communication with the sensing chamber 70nB of each cell 70n.
An exemplary two-cell embodiment of the invention 10 is depicted in
A source of dry test gas A fluidly communicates with a first humidification system that includes a wet line 3000Awet in fluid communication with a water reservoir 50A and a dry line 3000Adry that bypasses the water reservoir 50A. A test gas RH control valve 20A controls flow of test gas through the wet line 3000Awet and dry line 3000Adry according to a duty cycle for achieving the desired humidification level of the test gas.
The test gas wet line 3000Awet enters the block manifold 100 at inlet port 101Awet. The test gas dry line 3000Adry enters the block manifold 100 at inlet port 101Adry.
Upon exiting the water reservoir 50A, humidified test gas in the wet line 3000Awet is combined with dry test gas in the dry line 3000Adry and the combined test gas directed by test gas inlet lines 3001A and 3002A to the driving chambers 701A and 702A in the first testing cell 701 and second testing cell 702 respectively. Test gas flows through and exits each of the driving chambers 701A and 702A through an outlet port (unnumbered) and is vented from the block manifold at vent ports 701Ax and 702Ax respectively.
Particle filters 40Awet and 40Adry are preferably provided in the test gas wet line 3000Awet and test gas dry line 3000Adry respectively, for removing any entrained particulate matter from the test gas before it enters the block manifold 100.
In a similar fashion, a source of dry carrier gas B fluidly communicates with a second humidification system that includes a wet line 3000Bwet in fluid communication with a water reservoir 50B and a dry line 3000Bdry that bypasses the water reservoir 50B. A carrier gas RH control valve 20B controls flow of carrier gas through the wet line 3000Bwet and dry line 3000Bdry according to a duty cycle for achieving the desired humidification level of the carrier gas.
The carrier gas wet line 3000Bwet enters the block manifold 100 at inlet port 101Bwet. The carrier gas dry line 3000Bdry enters the block manifold 100 at inlet port 101Bdry.
Upon exiting the water reservoir 50B, humidified carrier gas in the wet line 3000Bwet is combined with dry carrier gas in the dry line 3000Bdry and the combined carrier gas directed by carrier gas inlet lines 3001B and 3002B to the sensing chambers 701B and 702B in the first testing cell 701 and second testing cell 702 respectively. Carrier gas flows through and exits each of the sensing chambers 701B and 702B through an outlet port (unnumbered) and is directed by dedicated outlet channels 3001Bout and 3002Bout respectively, to a common channel 3005 in fluid communication with a target-analyte sensor 200 located external to the block manifold 100.
Common channel 3005 exits the block manifold 100 at outlet port 102.
Particle filters 40Bwet and 40Bdry are preferably provided in the carrier gas wet line 3000Bwet and carrier gas dry line 3000Bdry respectively, for removing any entrained particulate matter from the carrier gas before it enters the block manifold 100.
Target-analyte catalytic converters 30Bwet and 30Bdry are preferably provided in the carrier gas wet line 3000Bwet and carrier gas dry line 3000Bdry respectively, for converting any target-analyte in the carrier gas (e.g., O2) to a molecular species (e.g., H2O when the target analyte is O2) that will not be detected by the target-analyte sensor 200.
Capillary restrictors 601A, 602A, 601B and 602B are preferably provided in the test gas inlet lines 3001A and 3002A, and carrier gas inlet lines 3001B and 3002B respectively, for facilitating a consistent and equal flow of gas into the driving chambers 701A and 702A of the testing cells 701 and 702, and the sensing chambers 701B and 702B of the testing cells 701 and 702 respectively. The capillary restrictors 60n are preferably side mounted onto the block manifold 100.
Valves 801B and 802B are provided in the dedicated outlet channels 3001Bout and 3002Bout respectively, for selectively and mutually exclusively allowing passage of carrier gas, containing any target-analyte that has permeated through the test film F, from each of the sensing chambers 701B and 702B into sensing engagement with the sensor 200. When closed, the valves 801B and 802B vent carrier gas, containing any target-analyte that has permeated through the test film F, to atmosphere through vent ports 801Bx and 802Bx in the manifold 100. The valves 80nB are preferably side mounted onto the block manifold 100.
The instrument 10 depicted in
The instrument 10 depicted in
The rezero feature includes a rezero line 3009B upstream from the testing cells 70n for bypassing the testing cells 70n and carrying carrier gas directly to the sensor 200. A rezero valve 89B is provided in the rezero line 3009B for selectively directing carrier gas to the sensor 200 or venting carrier gas from the block manifold 100 at vent port 89Bx. The rezero valve 89B is preferably side mounted to the block manifold 100.
A capillary restrictor 609B is preferably provided in the carrier gas rezero line 3009B for facilitating a consistent and equal flow of carrier gas into the sensing chambers 701B and 702B of the testing cells 701 and 702 respectively. The capillary restrictor 609B is, as with the other capillary restrictors, preferably side mounted onto the block manifold 100.
The sensor 200 is selected to measure the appropriate target-analyte (e.g., oxygen (O2), carbon dioxide (CO2) or water vapor (H2O)). Selection of a suitable sensor 200 is well within the knowledge and expertise of a person having routine skill in the art. The sensor 200 is preferably a coulox sensor and is equipped with an exhaust valve 210 for preventing atmospheric contamination of the sensor when there is no flow of carrier gas to the sensor 200.
Filing Document | Filing Date | Country | Kind |
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PCT/US15/17193 | 2/24/2015 | WO | 00 |
Number | Date | Country | |
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61943772 | Feb 2014 | US |