Breathing assistance device, and method of regulation
A breathing assistance device having: a turbine for generating flow of pressurized respiratory gas, a duct for carrying pressurized gas to a patient, a mechanism to control gas pressure capable of elaborating a pressure setting for the turbine, the turbine is connected to a speed sensor for acquiring a signal corresponding to the rotation speed of a rotating element of the turbine, and the mechanism of controlling the calculation linked to the speed sensor in order to elaborate using the signal, a pressure setting sending the pressure setting to the turbine. Another aspect of the invention relates to a method for regulating the pressure of a respiratory gas delivered by a turbine to a patient, the method involving elaborating a pressure setting for the turbine, characterized in that the pressure setting is elaborated using a signal representative of the rotation speed of a rotating element of the turbine.
1. A breathing assistance device, comprising:
a turbine to generate a flow of pressurised respiratory gas, said turbine having an inertia less than about 200 g·cm 2 ,
a duct adapted to carry the pressurised gas to a patient, and
control means for controlling gas pressure capable of computing a pressure setting for the turbine,
wherein the turbine is connected to a speed sensor capable of acquiring a signal corresponding to a rotation speed of a rotating element of the turbine, and the control means includes means of calculation connected to said speed sensor to compute the pressure setting using only said speed signal and send the pressure setting to the turbine, said means of calculation being adapted to detect new inspiratory or expiratory cycles using only said speed signal, and consequently adapting a level of said pressure setting.
2. A device as claimed in claim 1 , wherein said speed sensor implements a Hall effect sensor.
3. A device as claimed in claim 1 , wherein said speed sensor is a sensor capable of acquiring a turbine speed signal directly connected to the rotation speed of the rotating element of the turbine.
4. A device as claimed in claim 1 , wherein the means of calculation computes the pressure setting according to variations in speed.
5. A device as claimed in claim 1 , further comprising a program for detecting an inspiratory cycle using a comparison between:
a speed value stored in a memory of the device, said speed value being extrapolated using recent values of measured speeds, and an actually measured instantaneous speed.
6. A device as claimed in claim 1 , further comprising a program for detecting an inspiratory cycle using a comparison between:
a speed value stored in a memory of the device, said speed value being representative of a recent speed bearing, and
an actually measured instantaneous speed.
7. A device as claimed in claim 5 , further comprising a program for detecting an inspiratory cycle using a comparison between:
a speed value stored in a memory of the device, said speed value being representative of a speed at an end of an expiratory cycle, and
an actually measured instantaneous speed.
8. A device as claimed in claim 5 , further comprising several programs for detecting an inspiratory cycle operating simultaneously, and is capable of computing a pressure setting corresponding to a start of inspiratory cycle as soon as one of said programs for detecting the inspiratory cycle has signalled a start of inspiration.
9. A device as claimed in claim 5 , wherein the program for detecting the inspiratory cycle is configured to be disabled for a determined duration following a start of a new expiratory cycle.
10. A device as claimed in claim 1 , further comprising a program for detecting an expiratory cycle.
11. A device as claimed in claim 10 , wherein said program for detecting the expiratory cycle uses a comparison between:
a maximum turbine speed stored in a memory of the device and corresponding to an inspiratory cycle, and
an actually measured instantaneous speed.
12. A device as claimed in claim 1 , wherein said means of calculation includes a microprocessor connected to the speed sensor and to a turbine pressure setting input.
13. A device as claimed in claim 1 , wherein the device further includes a pressure-regulating loop comprising:
a pressure sensor on the duct, and
a circuit receiving the pressure setting coming from the means of calculation as well as a pressure measured by the pressure sensor, said circuit being capable of computing an instantaneous rotation speed setting for the turbine, said circuit being connected to a turbine speed setting input.
14. A method for regulating a pressure of a respiratory gas delivered by a turbine to a patient, the method comprising:
providing, with a speed sensor, a signal representative of a rotation speed of a rotating element of the turbine, said turbine having an inertia less than about 200 g·cm 2 ; and
computing, with a processor, a pressure setting for the turbine based only on the signal representative of the rotation speed,
said method being adapted to detect new inspiratory or expiratory cycles using only said signal, and of consequently adapting a level of the pressure setting with the processor.
15. A method as claimed in claim 14 , wherein said signal corresponds to the rotation speed of the turbine rotor.
16. A method as claimed in claim 14 , wherein the method implements a program for detecting an inspiratory cycle using a comparison between:
a speed value stored in a memory, said speed value being extrapolated from recent values of measured speeds, and
an actually measured instantaneous speed.
17. A method as claimed in claim 14 , wherein the method implements a program for detecting an inspiratory cycle using a comparison between:
a speed value stored in a memory, said speed value being representative of a recent speed bearing, and
an actually measured instantaneous speed.
18. A method as claimed in claim 14 , wherein the method implements a program for detecting inspiratory cycles using a comparison between:
a speed value stored in a memory, said speed value being representative of a speed at the end of an expiratory cycle, and
an actually measured instantaneous speed.
19. A method as claimed in claim 16 , wherein the method implements several programs for detecting inspiratory cycles operating simultaneously, and computes the pressure setting corresponding to an inspiratory flow as soon as one of said programs for detecting the inspiratory cycles has signalled the start of inspiration.
20. A method as claimed in claim 16 , wherein the program for detecting inspiratory cycles is disabled during a determined duration following the start of a new expiratory cycle.
21. A method as claimed in claim 14 , wherein the method implements a program for detecting expiratory cycles.
22. A method as claimed in claim 21 , wherein said program for detecting expiratory cycle uses a comparison between:
a maximum turbine speed stored in a memory and corresponding to an inspiratory cycle, and
an actually measured instantaneous speed.