Medical gas insufflator with automatic gas flow control

• US 5,800,381 A
• Filed: 10/19/1995
• Issued: 09/01/1998
• Est. Priority Date: 02/25/1994
• Status: Expired due to Term

• Current Assignee: Ognier Jean-Francedillaois
• Original Assignee: Ognier Jean-Francedillaois
• Inventors: Ognier, Jean-Fran.cedilla.ois
• Primary Examiner(s): Bockelman, Mark
• Application Number:
  US08/537,892
• Time in Patent Office: 1,048 Days
• Field of Search: 604/23, 604/26, 600/560
• US Class Current: 604/26
• CPC Class Codes: A61M 13/003 Blowing gases other than for carrying powders, e.g. for inflating, dilating or rinsing
• CPC Class Codes: A61M 2202/0007 introduced into the body
• CPC Class Codes: A61M 2202/0225 Carbon oxides, e.g. Carbon dioxide
• CPC Class Codes: A61M 2205/3344 Measuring or controlling pressure at the body treatment site

Abstract

A medical insufflator has a flexible tube having a downstream end provided with a needle and an upstream end, the tube and needle forming an insufflation flow path for a neutral gas into a surgical cavity into which the needle is inserted, a supply of the neutral gas under pressure connected to the upstream end, and a flow-control valve along the flow path at the upstream end. It is operated by measuring an insufflation pressure at the upstream end of the insufflation path, continuously calculating intracavity pressure from the insufflation pressure by evaluating loss of pressure of the flow path, comparing the calculated intracavity pressure and a preset value of this intracavity pressure, and controlling the flow-control valve as a function of the result of the comparison with the above-mentioned preset value in order to continuously supply a flow of the neutral gas that is minimally sufficient to compensate for leakage of gas from the surgical cavity and to maintain the intracavity pressure generally equal to the preset value.

Claims

1. A method of operating a medical insufflator comprising:

a flexible tube having a downstream end provided with a needle and an upstream end, the tube and needle forming an insufflation flow path for a neutral gas into a surgical cavity into which the needle is inserted,

a supply of the neutral gas under pressure connected to the upstream end, and

a flow-control valve along the flow path at the upstream end,

the method comprising the steps of;

measuring an insufflation pressure at the upstream end of the insufflation path,

continuously calculating intracavity pressure from the insufflation pressure by evaluating loss of pressure of the flow path,

comparing the calculated inntracavity pressure and a preset value of this intracavity pressure,

controlling the flow-control valve as a function of the result of the comparison with the above-mentioned preset value in order to continuously supply a flow the neutral gas that is minimally sufficient to compensate for leakage of gas from the surgical cavity and to maintain the intracavity pressure generally equal to the preset value; and

compensating for leaks from surgical cavity by evaluating the derivative with respect to time of the offset between the preset pressure value and the intracavity pressure.

2. The method defined in claim 1 further comprising the steps in each of a succession of cycles of sequentially

measuring the intracavity pressure at a first instant prior to insufflation when the intracavity pressure is equal to the static pressure at the upstream end of the insufflation flow path,

displaying the measured intracavity pressure,

starting insufflation at the first instant with a flow that stays constant during the current cycle,

measuring the insufflation pressure at a second instant after the first instant,

calculating the loss of pressure of the flow path as the difference between the pressures measured at the first and second instants,

recording to memory the measured loss of pressure specific to the current cycle,

measuring the dynamic insufflation pressure at a third instant after the second instant,

measuring the intracavity pressure at the third instant, and

displaying the intracavity pressure determined at the third instant and comparing it with the preset value.

3. The method defined in claim 1, further comprising means for defining and changing a threshold of the insufflation pressure according to a linear function derived from the gas flow while maintaining this threshold at a constant level for flows above a particular flow level, insufflation being stopped in a cycle of progression of flows when the insufflation pressure exceeds said safety pressure.

4. The method defined in claim 1 wherein a downstream end of the flow path is provided with a check valve which is connected in a Y-joint from which extends a branch tube provided with a vapor filter for venting intracavity overpressures to the outside, and with a valve-type device for ensuring monitoring of the aspiration and escape via the tube either automatically or manually, no pressure measurements being done when this device is open.

5. A method of operating a medical insufflator comprising:

a flexible tube having a downstream end providing with need and an upstream end, the tube and needle forming an insufflation flow path for a neutral gas into a surgical cavity into which the needle is inserted,

a supply of neutral gas under pressure connected to the upstream end, and

a pneumatic control assembly comprised of the following in order from the gas supply to the downstream end;

primary expansion means for reducing to a low accurate pressure the pressure of the gas to be insufflated at the output of the supply of gas,

a filter,

an input safety valve,

a secondary expanding capillary creating laminar flow and to which is associated a differential pressure sensor that determines the instantaneous flow at the neutral gas,

a proportional flow-control valve that is opened electrically in accordance with the instantaneous flow and the flow,

an output safety valve, and

a gas outlet associated with measuring means for the insufflation pressure used for calculating and controlling (the) an intracavity pressure,

the method comprising the steps of;

measuring an insufflation pressure at the upstream end of the insufflation path,

continuously calculating intracavity pressure from the

insufflation pressure by evaluating loss of pressure of the flow path,

comparing the calculated intracavity pressure and a preset value of this intracavity pressure,

controlling the flow-control valve as a function of the result of the comparison with the above-mentioned preset value in order to continuously supply a flow of the neutral gas that is minimally sufficient to compensate for leakage of the surgical cavity and to maintain the intracavity pressure generally equal to the preset value.

6. The method defined in claim 5 wherein the pneumatic control assembly also has means for maintaining temperature by reheating the gas flowing through the capillary.

7. The method defined in claim 6 wherein the expanding capillary and the differential pressure sensor are formed from two coaxial cylindrical element, one mounted in the other, the capillary being formed by an annular-section space between the two cylindrical elements while two pressure taps are in the outside cylindrical element, respectively upstream and downstream from the region forming the capillary and serve to supply the differential pressure sensor that determines the instantaneous gas flow.

8. The method defined in claim 7 wherein the input safety valve is connected to the expansion capillary at a center of the inside cylindrical element.