IP Library Granted Patent US 12,377,297
Granted Patent B2
US 12,377,297 · App. 17/431,679 · Granted Aug 5, 2025

Breathing equipment for an aircraft, breathing assembly and method for stowing the breathing equipment

Inventors: Jean-Philippe Sibuet (Moissy-Cramayel, FR); Alexandre Besson (Moissy-Cramayel, FR)
Assignee: SAFRAN AEROTECHNICS
A62B18/084A61F9/029A62B9/006A62B25/00B64D11/00
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Quick Facts
Patent No.
US 12,377,297
App. No.
17/431,679
Granted
Aug 5, 2025
Kind
B2
Abstract

A breathing apparatus for aircraft includes a breathing mask with an oronasal face cover and a support. The oronasal face cover has a cavity and the support supports a transparent lens and has an upper edge portion. An inflatable harness extends around the user's head opposite the shell and includes at least one rear portion. A guiding link includes an upper end linked to the upper edge portion and a lower end, the upper end being linked to the upper edge portion, the lower end being linked to the rear portion of the harness. A plate is linked to the lower end of the guiding link and has an abutment face that contacts the oronasal face cover, facing the cavity.

Claims (25)

1. A breathing apparatus for aircraft, the breathing apparatus being configured to supply a respiratory gas to a user and including:

a breathing mask comprising a shell, the shell having a cavity and being configured for contacting the user's head around the user's mouth and nose, the shell supporting a transparent lens and comprising an upper edge portion extending above the transparent lens,

an inflatable harness configured to extend around the user's head opposite the shell in order to hold the shell in contact with the user's face, the harness comprising at least one rear portion configured to be placed facing an occipital portion of the user's head,

a guiding link having an upper end and a lower end, the upper end being linked to the upper edge portion, and

a plate linked to the lower end of the guiding link and having a bearing face configured to contact the shell and to face the cavity, the plate being linked to the rear portion of the harness,

wherein the guiding link has an upper portion and a lower portion, the upper portion being rigid and the guiding link being configured to be folded with the upper portion on the plate and the lower portion between the upper portion and the plate,

wherein the upper portion has a length greater than or equal to 10 centimeters,

wherein the upper portion is rotatably mounted on the upper edge portion, and

wherein the lower portion is at least partly flexible and arranged between the upper portion and the plate.

2. The breathing apparatus according to claim 1 , wherein the guiding link has a torsional flexibility of less than half a turn.

3. The breathing apparatus according to claim 1 , wherein the guiding link has an elongate, flat shape.

4. The breathing apparatus according to claim 1 , wherein the upper portion comprises two arms extending longitudinally and laterally separated from one another by a distance greater than or equal to 3 centimeters and the breathing apparatus comprises two lower portions extending between the upper portion and the plate.

5. The apparatus according to claim 1 , wherein the lower portion comprises at least one rigid element.

6. The breathing apparatus according to claim 5 , wherein the at least one rigid element comprises a series of rigid elements hingedly connected to one another.

7. The breathing apparatus according to claim 1 , wherein the lower portion comprises a strap, the strap extending beyond the lower end forming a loop around a tube of the harness and the loop has ends held on the plate.

8. The breathing apparatus according to claim 1 , wherein the lower end of the guiding link is linked to the rear portion of the harness via the plate.

9. The breathing apparatus according to claim 1 , wherein the breathing apparatus is additionally provided with a sign for correct positioning in a stowage position.

10. The breathing apparatus according to claim 1 , wherein the shell comprises an oronasal face cover and a support, the oronasal face cover having a first cavity and being configured to contact the user's head around the user's mouth and nose, the support supporting the transparent lens and having a second cavity.

11. A breathing unit comprising the breathing apparatus according to claim 1 and a stowage box wherein:

the stowage box includes a housing configured to receive the breathing apparatus in a stowage position, said stowage box having an opening providing access to the housing.

12. A method for stowing the breathing apparatus of the breathing unit according to claim 11 in the stowage box wherein the method comprises:

a) moving the plate to be in contact with the shell,

b) pivoting the guiding link near the upper end of the guiding link with respect to the breathing mask,

c) placing the breathing apparatus in a stowed position by folding the guiding link so that the upper portion of the guiding link, the lower portion of the guiding link and the plate overlap, and

d) inserting the breathing apparatus into the stowage box.

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 Aug 17, 2021
From: SIBUET, JEAN-PHILIPPE; BESSON, ALEXANDRE
To: SAFRAN AEROTECHNICS
Reel/Frame 057208/0302 →
Priority Claims (1)
FR 1901609 · Feb 18, 2019 · national
Continuity (1)
Related Publication 20220193464A1 · Jun 23, 2022
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