Emergency oxygen system for aircraft with switching device and a method of operating an emergency oxygen system
An emergency oxygen system for aircraft comprising: a breathing gas supply circuit to be connected upstream to a source of breathing gas and downstream to at least one mask, a flow control valve configured to adjust the flow of breathing gas supplied to the mask, an electronics board configured to control the flow control valve, a power source, a switching device interposed between the power source and the electronics board, the switching device comprising a switch configured to have a first state in which power from the power source is supplied to the electronics board and a second state in which the electronics board is not supplied with power from the power source.
1. An emergency oxygen system for aircraft comprising:
a breathing gas supply circuit to be connected upstream to a source of breathing gas and downstream to at least one mask, the breathing gas supply circuit comprising a flow control valve configured to adjust a flow of breathing gas supplied to the mask,
an electronics board configured to control the flow control valve,
a power source,
a switching device interposed between the power source and the electronics board, the switching device comprising a switch configured to have a first state in which power from the power source is supplied to the electronics board and a second state in which the electronics board is not supplied with power from the power source, wherein:
the switch is an electrical or electronic switch,
the switching device further comprises an activation line,
the switching device is configured to actuate the switch to switch from the second state to the first state when an activation signal is present in the activation line,
the switching device comprises an input point, an output point and an ON point,
the power source is connected to the input point,
the electronics board is connected to the output point,
the switching device is configured to send the activation signal from the ON point to an ON line through the activation line, and
the switching device is configured to send an output signal from the output point to the ON line through an upholding line.
2. The emergency oxygen system according to claim 1 wherein the power source is a stored power source.
3. The emergency oxygen system according to claim 1 wherein:
the power source is connected to the input point,
the electronics board is connected to the output point, and
the switching device has an impedance higher than 100,000 ohm in the second state between the input point and the output point.
4. The emergency oxygen system according to claim 1 wherein the switching device is configured to uphold the switch in the first state, even if the activation signal in the activation line disappears.
5. The emergency oxygen system according to claim 1 wherein the emergency oxygen system comprises a test switch interposed between the power source and the activation line.
6. The emergency oxygen system according to claim 1 wherein the emergency oxygen system comprises a receiver configured to receive an emergency signal and send the activation signal in the activation line.
7. The emergency oxygen system according to claim 1 wherein:
the emergency oxygen system further comprises a container, at least one mask and a latching assembly,
the container includes a door movable between a closed position and an open position,
the latching assembly has a locking state and a releasing state,
in the locking state, the latching assembly is configured to secure the door in the closed position, in order to maintain the mask within the container,
in the releasing state, the latching assembly is configured to release the door,
the activation line is connected to the latching assembly, and
the latching assembly is configured to be driven in the releasing state when the activation signal is present in the activation line.
8. The emergency oxygen system according to claim 1 wherein:
the emergency oxygen system further comprises a container, at least one mask and a latching assembly,
the container includes a door movable between a closed position and an open position,
the latching assembly has a locking state and a releasing state,
in the locking state, the latching assembly is configured to secure the door in the closed position, in order to maintain the mask within the container,
in the releasing state, the latching assembly is configured to release the door, and
the electronics board is configured to control the releasing state of the latching assembly.
9. The emergency oxygen system according to claim 1 wherein:
the switching device comprises a deactivation line configured to switch the switch from the first state to the second state in case a deactivation signal is present in the deactivation line, and
the electronics board is configured to send the deactivation signal in the deactivation line.
10. A method of operating the emergency oxygen system according to claim 1 , the method including:(i) interposing the switching device between the power source and the electronics board, (ii) causing the switching device to electrically connect the power source to the electronics board, and (iii) adjusting the flow of breathing gas supplied to an aircraft passenger with the electronics board.
11. The method according to claim 10 further includes receiving the activation signal to cause the switching device to electrically connect the power source to the electronics board.
12. The method according to claim 11 further includes upholding the power source connected to the electronics board regardless of the activation signal.
13. The method according to claim 11 further includes receiving the activation signal to cause the switching device to electrically connect the power source to the electronics board and to cause the at least one mask released from a container.
14. The method according to claim 10 further includes transmitting a deactivation signal from the electronics board so as to cause the switching device to electrically disconnect the electronics board from the power source.
15. The method according to claim 14 wherein the method comprises detecting a test procedure and during an operation achieving the test procedure and then transmitting the deactivation signal from the electronics board so as to cause the switching device to electrically disconnect the electronics board from the power source.
16. An emergency oxygen system for aircraft comprising:
a breathing gas supply circuit to be connected upstream to a source of breathing gas and downstream to at least one mask, the breathing gas supply circuit comprising a flow control valve configured to adjust the flow of breathing gas supplied to the mask,
an electronics board configured to control the flow control valve,
a power source,
a switching device interposed between the power source and the electronics board, the switching device comprising a switch configured to have a first state in which power from the power source is supplied to the electronics board and a second state in which the electronics board is not supplied with power from the power source, wherein:
the switching device comprises a deactivation line configured to switch the switch from the first state to the second state in case a deactivation signal is present in the deactivation line,
the electronics board is configured to send the deactivation signal in the deactivation line,
the electronics board comprises an ambient pressure sensor configured to sense ambient pressure, and
the electronics board is configured to determine whether ambient pressure sensed by the pressure sensor is higher than a depressurization threshold and send the deactivation signal in the deactivation line in case the ambient pressure is higher than the depressurization threshold.
17. The emergency oxygen system according to claim 16 wherein the electronics board comprises a controller configured to control the flow control valve based on the ambient pressure sensed by the ambient pressure sensor.