Waste water air stop valve
Embodiments provide systems and methods for releasing grey water from an aircraft sink or sump using an improved waste water air stop valve. The valves described herein allow drainage of waste water, without air leakage. Additionally, if drainage in the piping is blocked, the valves are designed to ensure that water cannot flow back into the sinks or sumps.
1. A waste water air stop valve, comprising:
a housing comprising an inlet and an outlet;
a movable valve body positioned to open or close the outlet, depending upon a pressure condition differential between the inlet and the outlet;
the movable valve body comprising first and second openings, the first opening supporting a first piston and the second opening supporting a second piston,
the first and second pistons associated via a member having a first end operably connected to the first piston and a second end operably connected to the second piston, wherein raised movement of the first end of the member causes raising of the first piston and lowering of the second piston,
wherein raised movement of the second end of the member causes raising of the second piston and lowering of the first piston;
the member secured to a float at a securement point, the securement point positioned closer to the second end of the member than the first;
wherein fluid entering the inlet accumulates in a housing cavity until the fluid reaches a level that causes flotation of the float, wherein flotation of the float causes raising of the securement point end of the member, causing raised movement of the second piston, wherein raised movement of the second piston allows fluid to flow past the second piston and through the outlet.
2. The valve of claim 1 , wherein the second piston comprises a channel therethrough.
3. The valve of claim 2 , wherein fluid is allowed to pass via the first piston, the second piston, or both.
4. The valve of claim 1 , wherein both the first piston and the second piston comprise a channel therethrough.
5. The valve of claim 1 , wherein the second piston comprises an upper flange that abuts an upper shoulder of the movable valve body when the second piston is in a closed position.
6. The valve of claim 1 , wherein the movable valve body comprises a sealing member configured to abut an internal wall of the housing when the movable valve body is in a closed position.
7. The valve of claim 1 , wherein the housing comprises a lower ledge.
8. The valve of claim 7 , wherein when pressure at the inlet is equal to pressure at the outlet, the movable valve body is raised from the lower ledge.
9. The valve of claim 7 , wherein when pressure at the inlet is a greater than pressure at the outlet, the movable valve body is seated with respect to the lower ledge.
10. The valve of claim 1 , further comprising a spring to bias the movable valve body in an open position.
11. The valve of claim 10 , wherein a higher pressure at the inlet than at the outlet causes compression of the spring and movement of the movable valve body to a closed position.
12. The valve of claim 1 , further comprising a spring to cause raised and lowered movement of the movable body depending upon pressure at the inlet and outlet.
13. The valve of claim 1 , wherein the member comprises a central hinge point secured to the movable valve body.
14. The valve of claim 1 , further comprising a backflow prevention system.
15. The valve of claim 14 , wherein the backflow prevention system comprises a lower float configured to block the outlet when buoyant.
16. The valve of claim 14 , wherein the backflow system comprises an internal flange along a conduit portion of the outlet and a lower float, wherein backflow fluid applying water pressure to the lower float causes the lower float to raise and abut the internal flange, blocking the outlet.
17. The valve of claim 1 , wherein each of the first and second pistons comprises an o-ring seal.
18. The valve of claim 1 , further comprising a manual override option.
19. A method for releasing grey water from an aircraft, comprising:
providing the waste water air stop valve of claim 1 ;
draining fluid from a sink or sump into the inlet;
directing fluid leaving the outlet to an aircraft drain mast.