Cockpit oxygen supply device
View Patent ↗A cockpit oxygen supply device includes at least one oxygen mask which is conductively connectable to an oxygen tank, wherein at least one throughput measurement device is arranged in the flow path of the device. A breathing activity of the pilot and/or an undesired outflow from the mask may be recognized with the help of an evaluation device.
1. A cockpit oxygen supply device comprising:
an oxygen tank;
an oxygen mask conductively connectable to said oxygen tank;
a throughput measurement device arranged in a device flow path;
a feed conduit connected at an exit side to the oxygen tank, said feed conduit having at least one conduit branching comprising a flow inlet and two flow outlets; and
a differential pressure sensor assigned to each of said flow outlets, said flow inlet and said flow outlet forming pressure chambers of said differential pressure sensor, said pressure chambers being separated from one another by a membrane.
2. A cockpit oxygen supply device according to claim 1 , further comprising:
means for detecting a breathing activity wherein the throughput measurement device is connected to said means for detecting a breathing activity and sends signals to said means for detecting a breathing activity.
3. A cockpit oxygen supply device according to claim 2 , wherein said means for detecting the breathing activity form a part of the flight control system of the aircraft.
4. A cockpit oxygen supply device according to claim 1 , further comprising:
an alarm device, wherein said throughput measurement device is connected to said alarm device and sends signals to said alarm device.
5. A cockpit oxygen supply device according to claim 1 , wherein said differential pressure sensor comprises an orifice structure arranged in said flow path.
6. A cockpit oxygen supply device comprising:
an oxygen tank;
a plurality of oxygen masks;
a pressure reducer;
a conduit line connected to said oxygen tank via said pressure reducer; and
conduit branching connected to said conduit line, at least one of said plurality of oxygen masks being connected to said conduit branching, said conduit branching including a throughput measurement device, a conduit branching flow inlet and a plurality of mask connection flow outlets, said throughput measurement device comprising a differential pressure sensor between each of mask connection flow outlets and said conduit branching flow inlet, said differential pressure sensor comprising an orifice structure arranged in said conduit branching, said differential pressure sensor being assigned to each of said mask connection flow outlets, said conduit branching flow inlet and said mask connection flow outlet forming pressure chambers of said differential pressure sensor, said pressure chambers being separated from one another by a membrane.
7. A cockpit oxygen supply device according to claim 6 , further comprising:
an evaluating device detecting a breathing activity wherein the throughput measurement device is connected to said evaluating device sends signals to said evaluating device.
8. A cockpit oxygen supply device according to claim 7 , wherein said evaluating device forms a part of the flight control system of the aircraft.
9. A cockpit oxygen supply device according to claim 7 , further comprising:
an alarm device, wherein said evaluating device is connected to said alarm device and sends signals to said alarm device.
10. A cockpit oxygen supply device comprising:
an oxygen tank;
a plurality of oxygen masks;
a pressure reducer;
a flow distributor, said pressure reducer being in fluid connection between said oxygen tank and said flow distributor;
a first conduit line connected to said flow distributor;
a second conduit line connected to said flow distributor;
a first conduit branching connected to said first conduit, at least two of said plurality of oxygen masks being connected to said first conduit branching, said first conduit branching including a first throughput measurement device, said first throughput measurement device defining a rate of volume flow between one of said at least two of said plurality of oxygen masks and said first conduit line; and
a second conduit branching connected to said second conduit, at least two other of said plurality of oxygen masks being connected to said second conduit branching, said second conduit branching including a second throughput measurement device, said second throughput measurement device defining another rate of volume flow between one of said at least two other of said plurality of oxygen masks and said second conduit line, each said throughput measurement device comprising a differential pressure sensor with an orifice structure arranged in said conduit branching and comprising a flow inlet and two flow outlets, said differential pressure sensor being assigned to each of said flow outlets, said flow inlet and said flow outlet forming pressure chambers of said differential pressure sensor, said pressure chambers being separated from one another by a membrane.
11. A cockpit oxygen supply device according to claim 10 , further comprising:
an evaluating device detecting a breathing activity wherein the throughput measurement device is connected to said evaluating device sends signals to said evaluating device, wherein said evaluating device forms a part of the flight control system of the aircraft.
12. A cockpit oxygen supply device according to claim 11 , further comprising:
an alarm device wherein said evaluating device is connected to said alarm device and sends signals to said alarm device.