Patent ID: 8496005
Filing Date: 2013-07-30
Classification: A62B,Y10S,Y10T

Abstract:
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.