IP Library Granted Patent US 12,370,385
Granted Patent B2
US 12,370,385 · App. 17/642,182 · Granted Jul 29, 2025

System for delivering breathing gas to passengers

Inventors: Vincent Jean Pierre Marie Gillotin (Vauhallan, FR); Jean-Baptiste Philippe Delprat (Saclay, FR); Vincent Gérard Greter (Elancourt, FR); Stuart David Dixon Walker (Paris, FR)
Assignee: SAFRAN AEROTECHNICS
A62B7/14A62B9/02
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Quick Facts
Patent No.
US 12,370,385
App. No.
17/642,182
Granted
Jul 29, 2025
Kind
B2
Abstract

A system for delivering breathing gas to passengers includes: a face mask including a face part having a breathing cavity, a tube configured to be supplied by pressurized breathing gas, and a reservoir bag disposed between the tube and the face part. A passage connects the reservoir bag to the breathing cavity so that the system is configured to supply the breathing cavity through the reservoir bag. The reservoir bag includes a front portion and a back portion. The front portion is connected to the face mask, and the system has a stowed configuration and a deployed configuration. In the stowed configuration, the reservoir bag is maintained folded between a backing and the face part.

Claims (19)

1. A system for delivering breathing gas to passengers, the system comprising:

a face mask comprising a face part having a breathing cavity;

a tube configured to be supplied by pressurized breathing gas; and

a reservoir bag disposed between the tube and the face part, wherein a passage connects the reservoir bag to the breathing cavity so that the system is configured to supply the breathing cavity through the reservoir bag, wherein the reservoir bag comprises a front portion and a back portion, wherein the front portion is connected to the face mask,

wherein the system has a stowed configuration and a deployed configuration, wherein in the stowed configuration, the reservoir bag is maintained folded between a backing and the face part,

wherein the back portion comprises a protrusion, and wherein, in the stowed configuration, the protrusion is releasably retained by the face part to maintain the reservoir bag folded between the back portion and the face part.

2. The system according to claim 1 , wherein:

the system comprises an inlet valve movable between an open position and a closed position, the inlet valve closing the passage in the closed position, and

wherein the system is configured to maintain the inlet valve in the closed position while a pressure in the reservoir bag is not increased by at least 5 mbar above an ambient pressure.

3. The system according to claim 2 , wherein the system is configured to move the inlet valve to the open position when the pressure in the breathing cavity is decreased by 3 mbar or more below the ambient pressure.

4. The system according to claim 1 , wherein the system is configured to release the protrusion when the back portion is moved away from the face part.

5. The system according to claim 1 , wherein the protrusion is a bung, and in the stowed configuration the protrusion closes the passage.

6. The system according to claim 5 , wherein the system is configured to move the back portion away from the face part when the reservoir bag inflates.

7. The system according to claim 1 , wherein the protrusion has a substantially Ω cross section shape, the protrusion comprising a neck portion and an enlarged head protruding from the back portion, wherein the passage has a corresponding portion configured to cooperate with the protrusion, in order to releasably retain the enlarged head.

8. The system according to claim 7 , wherein the protrusion protrudes from a base portion and the protrusion is integral with the base portion.

9. The system according to claim 1 , wherein the reservoir bag comprises a bellow type portion and the back portion is substantially a plate.

10. The system according to claim 1 , wherein the back portion of the reservoir bag is resiliently deformable.

11. The system according to claim 10 , wherein the reservoir bag comprises a main portion having a first thickness and the back portion has a second thickness being at least three times as thick as the first thickness.

12. The system according to claim 10 , wherein the back portion of the reservoir bag comprises the backing.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE PREVIOUS RECORDED ASSIGNMENT PREVIOUSLY RECORDED AT REEL: 68238 FRAME: 929. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Apr 3, 2025
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 070721/0187 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 9, 2024
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 068238/0928 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 10, 2022
From: GILLOTIN, VINCENT; DELPRAT, JEAN-BAPTISTE; GRETER, VINCENT; WALKER, STUART
To: SAFRAN AEROTECHNICS
Reel/Frame 059230/0022 →
Priority Claims (1)
EP 19306109 · Sep 13, 2019 · regional
Continuity (1)
Related Publication 20220314039A1 · Oct 6, 2022
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