Overpressure protector
View Patent ↗An aircraft fuel tank assembly comprises a first fuel tank, a second fuel tank and a tank-to-tank overpressure protector therebetween. The overpressure protector has a closed state and an open state. The fuel tank assembly further comprises an indicator for indicating whether the overpressure protector is in the open or closed state, the indication of the indicator being able to be sensed at a location outside of the fuel tanks. The fuel tank assembly may comprise a test mechanism arranged to effect movement of the overpressure valve from the closed state to the open state, the test mechanism being operable from a location outside a fuel tank. The fuel tank assembly may comprise an overpressure valve re-set mechanism, the re-set mechanism being operable from a location outside the fuel tanks.
1. An aircraft fuel tank assembly, comprising: a first fuel tank, a second fuel tank, and a tank-to-tank overpressure protector, wherein the overpressure protector has a closed state for substantially preventing fluid communication between said first fuel tank and said second fuel tank through the overpressure protector, and an open state for enabling fluid communication between said first fuel tank and said second fuel tank through the overpressure protector to provide pressure relief,
wherein the fuel tank assembly further comprises a mechanical indicator for indicating whether the overpressure protector is in the open or closed state, wherein said indicator comprises a follower element which is moveable dependent on the state of the overpressure protector, wherein the indication of the indicator is generated dependent on the position of the follower element, and
wherein said open or closed state indication of the indicator is sensed at a location outside of the first and second fuel tanks.
2. A fuel tank assembly according to claim 1 , wherein the indicator is mechanically associated with the overpressure protector.
3. A fuel tank assembly according to claim 1 , wherein the indicator comprises a flag, the flag being moveable between a hidden position and a visible position dependent on the state of the overpressure protector.
4. A fuel tank assembly according to claim 1 , wherein the indicator comprises a fibre optic cable arranged to transmit an optical signal dependent on the state of the overpressure protector and being arranged to output said signal, for use as the indication, to a location outside the first and second fuel tanks.
5. A fuel tank assembly according to claim 1 , wherein the part of the indicator arranged to make the indication is wholly located outside the first and second fuel tanks.
6. A fuel tank assembly according to claim 1 , wherein the overpressure protector is in the form of an overpressure valve.
7. An aircraft fuel tank overpressure protector unit for use in the fuel tank assembly according to claim 1 , the unit comprising an overpressure protector and an indicator mechanically associated therewith, for providing an indication remote from the overpressure protector.
8. An aircraft fuel tank overpressure protector unit according to claim 7 wherein the overpressure protector is a spring-loaded overpressure valve comprising a shaft and a sealing member moveable between an open state and a closed state,
the follower element is biased against the shaft or sealing member so as to be moveable dependent on the state of the overpressure valve, and
the unit further comprises a flag, the flag being biased against the follower element so as to be moveable between a hidden position and a visible position dependent on the position of the follower element.
9. An aircraft fuel tank overpressure protector unit according to claim 7 , further comprising a fibre optic cable arranged to transmit an optical signal dependent on the state of the overpressure protector.
10. In combination, an aircraft and a fuel tank assembly, wherein said fuel tank assembly comprising a first fuel tank, a second fuel tank and a tank-to-tank overpressure protector between said first fuel tank and said second fuel tank, wherein the overpressure protector has a closed state for substantially preventing fluid communication between said first fuel tank and said second fuel tank through the overpressure protector, and an open state for enabling fluid communication between said first fuel tank and said second fuel tank through the overpressure protector to provide pressure relief,
wherein the fuel tank assembly further comprises a mechanical indicator for indicating whether the overpressure protector is in the open or closed state, wherein said indicator comprises a follower element which is moveable dependent on the state of the overpressure protector, wherein the indication of the indicator is generated dependent on the position of the follower element, and
wherein said open or closed state indication of the indicator is sensed at a location outside of the first and second fuel tanks.
11. The combination according to claim 10 , wherein the indication of the indicator is able to be sensed in the aircraft cockpit.
12. The combination according to claim 10 , wherein the indication of the indicator is operable to be visible on the exterior of the aircraft wing.
13. In combination, an aircraft wing and a fuel tank assembly, wherein said fuel tank assembly comprising a first fuel tank, a second fuel tank, and a tank-to-tank overpressure protector between said first fuel tank and said second fuel tank, wherein said overpressure protector has a closed state for substantially preventing fluid communication between said first fuel tank and said second fuel tank through the overpressure protector, and an open state for enabling fluid communication between said first fuel tank and said second fuel tank through the overpressure protector to provide pressure relief, and a mechanical indicator for indicating whether the overpressure protector is in the open or closed state, wherein said indicator comprises a follower element which is moveable dependent on the state of the overpressure protector, wherein the indication of the indicator is generated dependent on the position of the follower element, and
wherein said open or closed state indication is sensed at a location outside of the first and second fuel tanks.
14. A method of detecting the open state or closed state of an overpressure protector on an aircraft, comprising the steps of:
providing a fuel tank assembly having a first fuel tank and a second fuel tank,
providing a tank-to-tank overpressure protector between said first fuel tank and said second fuel tank, wherein the overpressure protector has a closed state for substantially preventing fluid communication between said first fuel tank and said second fuel tank through the overpressure protector, and an open state for enabling fluid communication between said first fuel tank and said second fuel tank through the overpressure protector to provide pressure relief,
providing a mechanical indicator for indicating whether the overpressure protector is in the open or closed state, wherein said indicator comprises a follower element which is moveable dependent on the state of the overpressure protector, and wherein the indication of the indicator is generated dependent on the position of the follower element,
sensing said open or closed state indication of the indicator at a location outside of the first and second fuel tanks.