Fuel tank valve
View Patent ↗Some water drain valves tend to fill with water which may freeze, thereby jamming the valve. This invention provides an aircraft water drain valve comprising a passageway, a shaft, a first sealing member and a second sealing member. The shaft is moveable between an open position in which the first and second sealing members are arranged to allow free passage of fluid through the passageway, and a closed position in which both the first and second sealing members are arranged to prevent free passage of fluid through the passageway thereby preventing ingress of fluid into the region between the first and second sealing members. Thus water may be hindered from collecting and freezing in the part of the valve close to the cold wall of the fuel tank.
1. An aircraft water drain valve, the valve comprising a passageway for communicating fluid between the interior and exterior of a fuel tank, a shaft, a first sealing member and a second sealing member, wherein the first and second sealing members are mounted on the shaft and the shaft is moveable between an open position in which the first and second sealing members are arranged to allow free passage of fluid through the passageway, and a closed position in which both the first and second sealing members are arranged to prevent free passage of fluid through the passageway thereby preventing ingress of fluid into the region between the first and second sealing members.
2. A valve according to claim 1 wherein the shaft is resiliently biased towards the closed position.
3. A valve according to claim 1 wherein the second sealing member is moveable relative to the first sealing member.
4. A valve according to claim 3 wherein the second sealing member is slideably mounted on the shaft.
5. A valve according to claim 1 , wherein the second sealing member is resiliently biased towards a position in which whilst the shaft is in the closed position the second sealing member is arranged to prevent free passage of fluid through the passageway.
6. A valve according to claim 1 , further comprising a first compliant member and a second compliant member, the first and second members being arranged, whilst the shaft is in the closed position, to co-operate with the first and second sealing members respectively.
7. A valve according to claim 1 , further comprising a housing, the housing comprising a first valve seat and a second valve seat with which, whilst the shaft is in the closed position, the first and second sealing members abut respectively, wherein the portion of the housing containing the first valve seat is detachable from the remainder of the valve.
8. An aircraft fuel tank comprising a water drain valve according to claim 1 .
9. An aircraft comprising a fuel tank according to claim 8 .
10. A method of draining water from an aircraft fuel tank through a water drain valve, the method comprising the steps of:
(i) moving a shaft in the water drain valve to an open position, the shaft having first and second sealing members mounted thereon, such that movement of the shaft to the open position enables the first and the second sealing members in the water drain valve to allow free passage of fluid through a passageway in the water drain valve,
(ii) allowing water to drain from the aircraft fuel tank through the passageway, and then
(iii) allowing the first and a second sealing members to move to a position in which both the first and second sealing members are arranged to prevent free passage of fluid through the passageway thereby preventing ingress of fluid into the region between the first and second sealing members.