Inerting and venting system
An inerting and venting system for an aircraft. The inerting and venting system includes a tank containing fluid to be inerted, a mixer including an operating flow path and a mixing flow path, a vent line fluidly connecting ambient atmosphere to the operating flow path of the mixer, and an inert gas line fluidly connecting an inert gas source to the mixing flow path of the mixer. The mixing flow path and the operating flow path are arranged in a coflowing configuration such that ambient air communicated by the operating flow path mixes in a coflowing manner with inert gas communicated by the mixing flow path and the coflowed mixture is directed into the tank. The inerting and venting system may include a first valve for controlling flow of vent air from ambient atmosphere to the tank, and a second valve for controlling flow of inert gas from an inert gas source to the tank. A valve adjuster is configured to passively adjust the first and second valves in response to a pressure differential between the ambient atmosphere and the tank, and to control ratio of flow in response to oxygen concentration in the inert gas or the tank ullage gas.
1. An inerting and venting system for an aircraft, comprising:
a tank containing fluid to be inerted;
a first valve for controlling flow of vent air from ambient atmosphere to the tank;
a second valve for controlling flow of inert gas from an inert gas source to the tank; and
a valve adjuster configured to passively adjust the first and second valves in response to a pressure differential between the ambient atmosphere and the tank;
wherein the valve adjuster, the first valve, and the second valve are passively operated components that are driven mechanically by changes in atmospheric pressure and tank pressure rather than by electronic sensors.
2. The inerting and venting system of claim 1 , wherein the valve adjuster is mechanically coupled to the first and second valves to simultaneously and passively adjust the first and second valves.
3. An inerting and venting system for an aircraft, comprising:
a tank containing fluid to be inerted;
a first valve for controlling flow of vent air from ambient atmosphere to the tank;
a second valve for controlling flow of inert gas from an inert gas source to the tank; and
a valve adjuster configured to passively adjust the first and second valves in response to a pressure differential between the ambient atmosphere and the tank,
wherein the second valve is mechanically coupled to the first valve so that flow control of inert gas flow through the second valve is proportional to flow control of vent air through the first valve in response to the pressure differential between the ambient atmosphere and the tank.
4. An inerting and venting system for an aircraft, comprising:
a tank containing fluid to be inerted;
a first valve for controlling flow of vent air from ambient atmosphere to the tank;
a second valve for controlling flow of inert gas from an inert gas source to the tank; and
a valve adjuster configured to passively adjust the first and second valves in response to a pressure differential between the ambient atmosphere and the tank,
wherein the valve adjuster includes an actuator responsive to oxygen concentration in the inert gas of the tank ullage gas to change the ratio of the controlled flow of vent air and inert gas admitted through the respective first and second valves.
5. The inerting and venting system of claim 4 , wherein the actuator includes an electronic oxygen sensor for sensing oxygen concentration, and an electronic controller that controls movement of the actuator based on the sensed oxygen concentration.
6. An inerting and venting system for an aircraft, comprising:
a tank containing fluid to be inerted;
a first valve for controlling flow of vent air from ambient atmosphere to the tank;
a second valve for controlling flow of inert gas from an inert gas source to the tank; and
a valve adjuster configured to passively adjust the ratio of the controlled flow of vent air and inert gas admitted through the respective first and second valves based on one or more of an oxygen concentration in an inert gas line communicating inert gas from the inert gas source to the second valve and an oxygen concentration in an ullage space of the tank.
7. The inerting and venting system of claim 6 , wherein the valve adjuster includes an actuator responsive to oxygen concentration in the inert gas to proportionately change the controlled flow of vent air and inert gas by the respective first and second valves.
8. The inerting and venting system of claim 7 , wherein the actuator includes a stimuli sensitive material actuator.
9. The inerting and venting system of claim 8 , wherein the actuator includes an amplifier that amplifies volumetric/length changes in stimuli sensitive material of the stimuli sensitive material actuator.
10. The inerting and venting system of claim 7 , wherein the actuator includes a stimuli sensitive polymer actuator.
11. The inerting and venting system of claim 7 , wherein the actuator includes a stimuli sensitive gel actuator.
12. The inerting and venting system of claim 7 , wherein the actuator expands and contracts in response to respective increase and decrease in oxygen concentration.
13. The inerting and venting system of claim 12 , wherein the expansion and contraction respectively increases and decreases an effective flow area of the second valve.
14. The inerting and venting system of claim 12 , wherein the expansion and contraction respectively increases and decreases the proportion of inert gas flow admitted by the second valve relative to vent air flow admitted by the first valve.