IP Library Granted Patent US 11,452,889
Granted Patent B2
US 11,452,889 · App. 16/253,543 · Granted Sep 27, 2022

Dosed oxygen systems with delivery tube anti-blockage features and a method for delivering respiratory gas

Inventors: Stuart David Dixon Walker (Paris, FR); Vincent Gérard Greter (Elancourt, FR)
Assignee: SAFRAN AEROTECHNICS SAS
A62B7/14A62B7/02B64D2231/025
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Quick Facts
Patent No.
US 11,452,889
App. No.
16/253,543
Granted
Sep 27, 2022
Kind
B2
Abstract

Oxygen-delivery systems are described. The systems may supply emergency respiratory gas on demand to aircraft passengers. To reduce risk of blockage of tubes delivering anti-blocking gas to the face masks worn by the passengers, the systems may be designed to provide a continuous trickle flow of respiratory gas, or one or more anti-blocking pulses of gas, into a delivery tube.

Claims (43)

1. A system for delivering respiratory gas to passengers on-board an aircraft, comprising:

(i) a source of respiratory gas,

(ii) at least a face mask for a passenger,

(iii) a delivery valve interposed between the source of respiratory gas and the face mask associated with the delivery valve, and

(iv) a pressure sensor configured to detect passenger respiration and send a respiration signal upon detection of the passenger respiration,

(v) a controller configured to control the delivery valve opening for supplying the face mask with a dose of the respiratory gas based on the passenger respiration detection, and

(vi) an anti-blocking device configured to supply the face mask with anti-blocking gas, so that blockage is removed,

wherein the anti-blocking device comprises an orifice configured to allow trickle flow of anti-blocking gas.

2. A system according to claim 1 wherein:

the pressure sensor is configured to sense a pressure away from the face mask, and

the anti-blocking device is configured to supply the face mask with the anti-blocking gas, at least between the pressure sensor and the face mask.

3. A system according to claim 1 wherein the anti-blocking device comprises a bypass bypassing the delivery valve so as to allow the trickle flow of anti-blocking gas regardless of a state of the delivery valve.

4. A system according to claim 1 wherein:

the system comprises a main delivery tube connecting the delivery valve to the face mask,

a bypass comprises a second delivery tube in parallel with the main delivery tube and terminating at the face mask,

the orifice is disposed in the second delivery tube, and

the pressure sensor communicates with the second delivery tube downstream the orifice.

5. A system according to claim 1 , wherein:

the system comprises a main delivery tube connecting the delivery valve to the face mask, and

the pressure sensor communicates with the main delivery tube downstream a bypass.

6. A method for delivering respiratory gas to passengers on-board an aircraft, comprising:

detecting respirations of a passenger in a face mask associated to the passenger,

supplying the face mask with a dose of respiratory gas based on each passenger respiration detection, and

supplying the face mask with a pulse of anti-blocking gas at a predetermined time after having supplied the face mask with the dose of respiratory gas, the predetermined time being in a range between 10 seconds and 30 seconds, so that an occurrence of blockage preventing detection of respiration is reduced.

7. A method according to claim 6 wherein pulses of the anti-blocking gas are supplied at times differing from times at which doses of the respiratory gas are supplied to the face mask.

8. A method according to claim 6 comprising supplying the face mask with pulses of the anti-blocking gas having a volume in a range between 0.2 milliliter and 3 milliliters.

9. A method according to claim 6 comprising:

acquiring statistical data relating to a breathing pattern of the associated passenger during several breathing cycles, and

supplying the face mask with the pulse of anti-blocking gas based on the acquired statistical data.

10. A method according to claim 9 comprising:

calculating at least an average time period of the breathing cycles of the associated passenger and a threshold time calculated based on the calculated average time period,

supplying the face mask with the pulse of anti-blocking gas in case the time period of the breathing cycles appears longer than the calculated threshold time.

11. A method according to claim 6 comprising:

adjusting a volume of the dose of respiratory gas based on a cabin pressure, and

supplying the face mask with pulses of the anti-blocking gas irrespective of the cabin pressure.

12. A method for delivering respiratory gas to passengers on-board an aircraft, comprising:

detecting respirations of a passenger in a face mask associated to the passenger,

supplying the face mask with a dose of respiratory gas based on each passenger respiration detection, and

comprising supplying each face mask with anti-blocking gas in case of depressurization occurrence, so that an occurrence of blockage, preventing detection of respiration, is reduced.

13. A method according to claim 12 comprising supplying the face mask with the anti-blocking gas either continuously or in a pulsed form and supplying more of the respiratory gas than the anti-blocking gas, preferably 5 times or more of a volume of the respiratory gas than the anti-blocking gas.

14. A method according to claim 12 wherein a trickle flow of the anti-blocking gas is continuously supplied to the face mask and the trickle flow is 10 milliliters per minute or less.

15. A method according to claim 12 wherein the anti-blocking gas is supplied in a pulsed form.

16. A method according to claim 15 comprising supplying the face mask with the pulse of anti-blocking gas at a predetermined time after having supplied the face mask with the dose of respiratory gas, the predetermined time being in a range between 10 seconds and 30 seconds.

Assignments (2)
CHANGE OF NAME Recorded Jun 7, 2021
From: ZODIAC AEROTECHNICS
To: SAFRAN AEROTECHNICS SAS
Reel/Frame 056495/0329 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 13, 2019
From: WALKER, STUART DAVID DIXON; GRETER, VINCENT GÉRARD
To: ZODIAC AEROTECHNICS
Reel/Frame 049459/0290 →
Continuity (2)
Provisional Application 62620562 · Jan 23, 2018
Related Publication 20190224505A1 · Jul 25, 2019