IP Library Granted Patent US 8,496,005
Granted Patent B2
US 8,496,005 · App. 12/942,001 · Granted Jul 30, 2013

Breathing mask and regulator for aircraft

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Quick Facts
Patent No.
US 8,496,005
App. No.
12/942,001
Granted
Jul 30, 2013
Kind
B2
Abstract

The auxiliary breathing flow channel apparatus for an oxygen mask for pilots and crew of an airplane includes a flow control device with closed and open positions to regulate flow through an auxiliary channel. A pressure sensor such as an aneroid capsule automatically closes the auxiliary channel upon a decrease in cabin pressure. A handle also allows a user to manually move the flow regulating means to a closed position.

Claims (6)

1. An auxiliary breathing flow channel apparatus for an oxygen mask for pilots and crew of an airplane, the oxygen mask having an oronasal face seal defining an oronasal cavity, and an oxygen supply regulator, the auxiliary breathing flow channel apparatus comprising:

an ambient air flow channel defined through a portion of the oxygen mask, said ambient air flow channel being connected to ambient air and configured to deliver ambient air through said ambient air flow channel to the oxygen mask;

a flow regulating mechanism configured to regulate flow through the air flow channel, the flow regulating mechanism being movable between at least one closed position in which flow through the ambient air flow channel is blocked and an open position in which flow through the ambient air flow channel is enabled;

an aneroid capsule configured to apply a biasing force to the flow regulating mechanism to maintain the flow regulating mechanism in the at least one closed position;

an upper aneroid housing and a lower aneroid housing disposed in the upper aneroid housing, said aneroid capsule being disposed in said upper and lower aneroid housings, said upper and lower aneroid housings being configured to move the flow regulating mechanism between said open position and said at least one closed position; and

a spring retainer configured to latch said upper aneroid housing in upper and lower positions, wherein said aneroid capsule is configured to sense ambient pressure, said aneroid capsule being connected to said spring retainer and being operative to release the spring retainer upon sensing of a decrease in cabin pressure to a threshold pressure, to allow the flow regulating mechanism to revert to the closed position without intervention or action by a user upon such a decrease in cabin pressure.

Assignments (4)
RELEASE OF SECURITY INTEREST Recorded Jan 25, 2019
From: JP MORGAN CHASE BANK, N.A
To: B/E AEROSPACE, INC.
Reel/Frame 049209/0619 →
CORRECTIVE ASSIGNMENT TO CORRECT THE INCORRECT APPL. NO. 13/071,416 PREVIOUSLY RECORDED AT REEL: 031600 FRAME: 0945. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Jul 23, 2015
From: BE AEROSPACE, INC.
To: B/E AEROSPACE, INC.
Reel/Frame 036242/0530 →
SECURITY INTEREST Recorded Mar 10, 2015
From: B/E AEROSPACE, INC.
To: JPMORGAN CHASE BANK, N.A.
Reel/Frame 035176/0493 →
CHANGE OF NAME Recorded Nov 8, 2013
From: BE AEROSPACE, INC.
To: B/E AEROSPACE, INC.
Reel/Frame 031600/0945 →