System for regulating the dispensing of commercial aircraft passenger oxygen supply
View Patent ↗The aircraft emergency oxygen supply system includes one or more sources of supplemental breathable oxygen, one or more inlet valves for one or more breathing devices, connected to the inlet valves, and one or more cabin air pressure transducers. A pressure controller controls the inlet valves in response to the one or more cabin air pressure transducers. One or more second pressure transducers may connected to conduits downstream of inlet valves to be monitored, and the pressure controller may also control operation of the inlet valves in response to the one or more second pressure transducers.
1. An emergency oxygen supply system for an aircraft with a pressurizable passenger cabin comprising:
a source of supplemental breathable oxygen;
a conduit connected to said source of supplemental breathable oxygen;
an upstream first on-off inlet valve connected to said conduit downstream from said source of supplemental breathable oxygen;
a downstream second on-off inlet valve connected to said conduit downstream serially from said first on-off inlet valve;
a plurality of breathing devices connected to said conduit downstream from said downstream second on-off inlet valve;
at least one cabin air pressure transducer for generating a cabin air pressure input signal representing the cabin pressure and a corresponding altitude;
a second pressure transducer connected to said conduit between said upstream first on-off inlet valve and said downstream second on-off inlet valve, and a third pressure transducer connected to said conduit between said second on-off inlet valve and said plurality of breathing devices, said second and third pressure transducers being configured to sense a gas pressure in said conduit at locations downstream of the first and second on-off inlet valves, respectively; and
a pressure controller connected to said at least one cabin air pressure transducer for receiving said cabin air pressure input signal, said pressure controller being connected to and controlling the operation of said first and second on-off inlet valves in response to said cabin air pressure input signal received from said at least one cabin air pressure transducer, and said pressure controller being operative to control the operation of said first and second on-off inlet valves in response to said second and third pressure transducers, respectively.
2. The emergency oxygen supply system of claim 1 , wherein said inlet valve comprises a two-position solenoid valve.
3. An emergency oxygen supply system for an aircraft with a pressurizable passenger cabin comprising:
a plurality of sources of supplemental breathable oxygen;
a corresponding plurality of conduits connected to said plurality of sources of supplemental breathable oxygen, respectively;
a corresponding plurality of upstream first on-off inlet valves connected to said corresponding plurality of conduits, respectively, and a corresponding plurality of downstream second on-off inlet valves, connected to said corresponding plurality of conduits downstream serially from said plurality of first on-off inlet valves, respectively;
a corresponding plurality of sets of pluralities of breathing devices connected to said corresponding plurality of conduits downstream from said plurality of downstream second on-off inlet valves, respectively;
at least one cabin air pressure transducer for generating a cabin air pressure input signal representing the cabin pressure and a corresponding altitude;
a plurality of second pressure transducers connected to said corresponding plurality of conduits between said plurality of upstream first on-off inlet valves and said plurality of downstream second on-off inlet valves, respectively, and a plurality of third pressure transducers connected to said corresponding plurality of conduits between said plurality of downstream second on-off inlet valves and said corresponding plurality of sets of pluralities of breathing devices, respectively, said plurality of second pressure transducers being configured to sense a gas pressure in said corresponding plurality of conduits between said plurality of upstream first on-off inlet valves and said plurality of downstream second on-off inlet valves, respectively, and said plurality of third pressure transducers being configured to sense a gas pressure in said corresponding plurality of conduits between said plurality of second on-off inlet valves and said corresponding plurality of sets of pluralities of breathing devices, respectively; and
a pressure controller connected to said at least one cabin air pressure transducer for receiving said cabin air pressure input signal, said pressure controller being connected to and controlling the operation of said plurality of upstream first on-off inlet valves and said plurality of downstream second on-off inlet valves in response to said cabin air pressure input signal received from said at least one cabin air pressure transducer, and said pressure controller being operative to control the operation of said plurality of upstream first on-off inlet valves and said plurality of downstream second on-off inlet valves in response to said second and third pressure transducers, respectively.