Oxygen Pressure Relief and Ventilation System and Method
An oxygen pressure relief and ventilation system includes a flow fuse fluidly coupled downstream of a pressure regulator. The pressure regulator is operatively coupled to an oxygen tank, and the oxygen tank is located in an unpressurized compartment of an aircraft. A pressure relief valve is fluidly coupled downstream of the flow fuse. A ventilation pathway fluidly couples the unpressurized compartment with a pressurized compartment. The flow fuse and the pressure relief valve are configured to cooperatively mitigate downstream flow of pressurized oxygen if the pressure regulator fails. The ventilation pathway is configured to allow air from the pressurized compartment to pass through to the unpressurized compartment for diluting a concentrated oxygen in the unpressurized compartment.
1 . A method for protecting against a failed pressure regulator of an oxygen system, the method comprising:
partially blocking flow of a pressurized oxygen downstream of a failed pressure regulator via one or more flow fuses to isolate downstream components of the oxygen system from the pressurized oxygen;
venting flow of the pressurized oxygen into an unpressurized compartment via one or more pressure relief valves to relieve pressure from the pressurized oxygen; and
ventilating the unpressurized compartment with air from an occupied compartment via a pathway for diluting an oxygen concentration in the unpressurized compartment.
2 . The method of claim 1 , wherein the one or more flow fuses are configured for partially blocking flow of the pressurized oxygen when a threshold pressure is reached thereby protecting downstream components from a surge in pressure.
3 . The method of claim 2 , wherein the one or more pressure relief valves are configured for venting flow of the pressurized oxygen to relieve pressure upon exposure to a predetermined pressure.
4 . The method of claim 1 , wherein the pathway is configured for ventilating the unpressurized compartment with air flowing from the occupied compartment at a predetermined flow rate.
5 . A method for protecting against a failed pressure regulator of an oxygen system, the method comprising:
blocking high pressure downstream of a pressure regulator if the pressure regulator fails via a flow fuse fluidly coupled downstream of the pressure regulator, wherein the pressure regulator is operatively coupled to an oxygen tank, and the oxygen tank is located in an unpressurized compartment of an aircraft;
relieving pressure via a pressure relief valve fluidly coupled downstream of the flow fuse; and
allowing air to pass from a pressurized compartment into the unpressurized compartment via a ventilation pathway for diluting a concentrated oxygen in the unpressurized compartment.
6 . The method of claim 5 , wherein blocking high pressure comprises at least partially blocking flow of oxygen downstream of the pressure regulator if the pressure regulator fails.
7 . The method of claim 5 , wherein relieving pressure comprises opening the pressure relief valve in response to an increase in pressure.
8 . The method of claim 5 , comprising cooperatively blocking pressure via the flow fuse and relieving pressure via the pressure relief valve for protecting against all failure modes of the pressure regulator.
9 . The method of claim 5 , wherein allowing air to pass comprises releasing ventilated air from the pressurized compartment into the unpressurized compartment.
10 . The method of claim 5 , comprising venting air from the unpressurized compartment into an ambient environment outside the aircraft.
11 . The method of claim 5 , wherein blocking high pressure via the flow fuse comprises biasing a spring-loaded mechanism of the flow fuse into a first position thereby allowing flow of oxygen to pass.
12 . The method of claim 11 , comprising overcoming a force of the spring-loaded mechanism when the pressure of oxygen surpasses a predetermined pressure, thereby pushing the flow fuse into a second position that substantially blocks flow of oxygen for protecting downstream components.
13 . The method of claim 12 , comprising automatically resetting the flow fuse back to the first position when the pressure of oxygen from upstream is restored to below the predetermined pressure.
14 . The method of claim 12 , comprising allowing some pressurized oxygen to pass when the flow fuse is in the second position thereby limiting an upstream pressure while also protecting downstream components.