Membrane removal device
US-2024423839-A1 · Dec 26, 2024 · US
US9326826B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9326826-B2 |
| Application number | US-201414185641-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 20, 2014 |
| Priority date | Oct 30, 2006 |
| Publication date | May 3, 2016 |
| Grant date | May 3, 2016 |
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A gas pressure monitor system for a pneumatically-powered surgical machine includes a first transducer, a second transducer, and a controller. The first transducer is located upstream from a filter and is configured to read a first pressure of a gas before the gas enters the filter. The second transducer is located downstream from the Filter and is configured to read a second pressure of a gas after the gas exits the filter. The controller is configured to compute a difference between the first pressure and the second pressure. A state of the filter is determined from the difference between the first pressure and the second pressure.
Opening claim text (preview).
What is claimed is: 1. A gas pressure monitor system for a pneumatically-powered surgical machine comprising: a first transducer located upstream from a filter, the first transducer configured to read a first pressure of a gas before the gas enters the filter; a second transducer located downstream from the filter, the second transducer configured to read a second pressure of a gas after the gas exits the filter; a coupling configured to accept gas from a gas source; an isolation valve located between the first transducer and the filter; a pressure relief valve located between the coupling and the first transducer; a first manifold fluidly connecting the first transducer to the isolation valve; a second manifold fluidly connecting the isolation valve to the filter; a third manifold fluidly connecting the filter to the second transducer; and a fourth manifold fluidly connecting the coupling and the pressure relief valve to the first transducer. 2. The system of claim 1 wherein when the first pressure reading is greater than a first amount, the pressure release valve is open and the isolation valve is closed. 3. The system of claim 2 wherein an indication of a high pressure condition is provided. 4. The system of claim 1 wherein when the second pressure reading is less than a second amount, the isolation valve is closed. 5. The system of claim 4 wherein an indication of a low pressure condition is provided. 6. The system of claim 1 wherein when the first pressure and second pressure are within a safe pressure range, the isolation valve is open and the pressure release valve is closed. 7. A gas pressure monitor for a pneumatic module comprising: a first transducer located upstream from a filter, the first transducer configured to read a first pressure of a gas before the gas enters the filter; a second transducer located downstream from the filter, the second transducer configured to read a second pressure of a gas after the gas exits the filter; a coupling configured to accept gas from a gas source; an isolation valve located between the first transducer and the filter; a pressure relief valve located between a coupling and the first transducer; a first manifold fluidly connecting the first transducer to the isolation valve; a second manifold fluidly connecting isolation valve to the filter; a third manifold fluidly connecting the filter to the second transducer; a fourth manifold fluidly connecting the coupling and the pressure relief valve to the first transducer; and logic configured to compute a difference between the first pressure reading and the second pressure reading; wherein when the difference between the first pressure reading and the second pressure reading is greater than a second amount, an indication that the filter needs service is provided, when the first pressure reading is greater than a first amount, the pressure release valve is opened and the isolation valve is closed, and when the second pressure reading is less than a third amount, the isolation valve is closed. 8. A method for monitoring the state of a filter in a pneumatic module of a surgical machine comprising: sensing a first pressure of a gas upstream from a filter; sensing a second pressure of a gas downstream from the filter; computing a difference between the first pressure and the second pressure; comparing the difference to a value to determine a state of the filter; determining if an unacceptable pressure drop exists across the filter; and keeping an isolation valve in a closed position if an unacceptable pressure drop exists across the filter. 9. The method of claim 8 further comprising: using the difference between the first pressure and the second pressure to determine if the filter needs service. 10. The method of claim 9 further comprising: providing an indication that the filter needs service. 11. A method for monitoring the state of a filter in a pneumatic module of a surgical machine comprising: sensing a first pressure of a gas upstream from a filter; sensing a second pressure of a gas downstream from the filter; computing a difference between the first pressure and the second pressure; comparing the difference to a value to determine a state of the filter; determining if a pressure drop across the filter is acceptable; and opening an isolation valve if the pressure drop across the filter is acceptable.
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