Aircraft fuel tank assembly
View Patent ↗An aircraft fuel tank assembly includes a tank for holding fuel, a canister and a fuel pump assembly. The fuel pump assembly includes: an electric motor, a pump and an electronics unit. The electronics unit and canister are arranged so that, in use, a dry bay is defined between the electronics unit and the canister.
1. An aircraft fuel tank assembly, comprising
a tank for holding fuel,
a canister in the fuel tank,
a fuel pump assembly, said fuel pump assembly being provided in the canister and comprising:
an electric motor,
a pump to be driven by the motor, and
an electronics unit electrically coupled to the motor for controlling the motor, and
a dry bay between the electronics unit and the canister.
2. An aircraft fuel tank assembly according to claim 1 , wherein the dry bay comprises a witness drain on an outer wall of the fuel tank for visual indication of a breach of the dry bay.
3. An aircraft fuel tank assembly according to claim 1 , wherein the electronics unit is adjacent to an inside surface of a wall of the fuel tank.
4. An aircraft fuel tank assembly according to claim 1 , wherein the pump is adjacent to an inside surface a wall of the fuel tank.
5. An aircraft fuel tank assembly according to claim 1 , wherein the canister is adapted to be, in use, partly fuel flooded.
6. An aircraft fuel tank assembly according to claim 1 , wherein the fuel pump assembly is removably located within the canister.
7. An aircraft fuel tank assembly according to claim 1 , wherein the electronics unit is arranged to be cooled by fuel that is passed through the electronics unit.
8. An aircraft fuel tank assembly according to claim 1 , wherein the motor is arranged to be cooled by fuel that is passed through the motor.
9. An aircraft fuel tank assembly according to claim 1 , wherein the pump is a remote inlet pump.
10. An aircraft fuel tank assembly according to claim 1 , wherein the pump is a direct inlet pump.
11. In an aircraft, the improvement comprising a fuel tank assembly according to claim 1 .
12. An aircraft fuel tank assembly according to claim 1 , wherein the dry bay is filled with air or a gas.
13. A aircraft fuel tank assembly according to claim 1 , wherein the electronics unit comprises a housing, the canister and the electronics unit housing together defining the dry bay.
14. A aircraft fuel tank assembly according to claim 1 , wherein the dry bay is configured for withstanding the force of any ignitions or explosions which may occur if fuel or fuel vapor is present within the dry bay.
15. An aircraft fuel tank assembly according to claim 1 , wherein the dry bay is filled with air and is configured for withstanding the force of any ignitions or explosions which may occur if fuel or fuel vapor is present within the air space surrounding the electronics unit.
16. An aircraft fuel tank assembly according to claim 1 , wherein the motor is placed in the dry bay.
17. A kit for forming a fuel tank assembly, the kit comprising:
a canister installable in a fuel tank, and
an electronics unit for use with a fuel pump assembly, said fuel pump assembly being installable in the canister and comprising an electric motor and a pump to be driven by the motor, said electronics unit being electrically connectable to the motor for controlling the motor,
said electronics unit being assemble in said canister with a dry bay between the electronics unit and the canister.
18. A kit according to claim 17 further comprising said pump.
19. A kit according to claim 17 , further comprising said electric motor.
20. A kit according to claim 19 , wherein said motor is installable in said dry bay together with said electronics unit.