초록

A fuel system for an aircraft includes a fuel collector downstream of a boost pump and upstream of an engine fuel pump.

대표청구항 ▼

1. A fuel system for an aircraft comprising: a boost pump;an engine fuel pump; anda fuel collector downstream of said boost pump and upstream of said engine fuel pump, wherein said engine fuel pump is spaced from said fuel collector, wherein said fuel collector operates at a near-ambient fuel tank u

1. A fuel system for an aircraft comprising: a boost pump;an engine fuel pump; anda fuel collector downstream of said boost pump and upstream of said engine fuel pump, wherein said engine fuel pump is spaced from said fuel collector, wherein said fuel collector operates at a near-ambient fuel tank ullage pressure and said engine fuel pump is located outward from an outer surface of said fuel collector. 2. The system as recited in claim 1, wherein said fuel collector is mounted within a fuel tank. 3. The system as recited in claim 2, wherein said boost pump is mounted within said fuel tank, with said boost pump upstream of said fuel collector. 4. The system as recited in claim 3, further comprising a foot valve upstream of said boost pump. 5. The system as recited in claim 4, further comprising a fuel line section which communicates with said boost pump and extends through a base of said fuel collector. 6. The system as recited in claim 5, further comprising a second fuel line section which extends into an open top of said fuel collector. 7. The system as recited in claim 4, further comprising a fuel line section which communicates with said boost pump and extends through a side wall of said fuel collector. 8. The system as recited in claim 7, further comprising a second fuel line section which extends through a base of said fuel collector, said second fuel line section extends through a side-wall of said fuel tank. 9. The system as recited in claim 1, further comprising an inverted fuel collector adjacent said fuel collector to collect fuel under negative g operations, said fuel collector and said inverted fuel collector within said fuel tank. 10. The system as recited in claim 1, wherein said fuel collector is mounted external to a fuel tank. 11. The system as recited in claim 10, wherein said fuel collector is directly downstream of said boost pump. 12. The system as recited in claim 10, further comprising a fuel return line which communicates fuel from said fuel collector to said fuel tank. 13. The system as recited in claim 12, further comprising an anti-siphon vent line which communicates between a vent line in communication with said fuel tank and said fuel collector. 14. The system as recited in claim 10, wherein said boost pump is mounted external to said fuel tank, said boost pump upstream of said fuel collector. 15. The system as recited in claim 1, wherein said boost pump is spaced from said fuel collector. 16. The system as recited in claim 1, wherein said boost pump is located outward from an outer surface of said fuel collector. 17. The system as recited in claim 1, wherein said fuel collector forms an enclosure and said engine fuel pump is spaced from said enclosure. 18. The system as recited in claim 1, wherein said engine fuel pump is spaced from said boost pump. 19. The system as recited in claim 1, wherein the fuel collector includes a fuel inlet and a fuel outlet and the fuel outlet is located on an opposite side of the collector from the fuel inlet. 20. The system as recited in claim 1, wherein a fuel outlet is adjacent an upper portion of the fuel collector. 21. The system as recited in claim 1, wherein the fuel collector defines a cavity and the engine fuel pump is located outward of the cavity. 22. The system as recited in claim 1, including a second fuel collector spaced from the fuel collector and inverted relative to the fuel collector and a fluid passaged defined by an inner surface of the second fuel collector and an outer surface of the fuel collector. 23. A method of communicating fuel within an aircraft comprising: offsetting a fuel collector from a fuel tank bottom surface;receiving fuel pumped by a boost pump into the fuel collector, wherein said boost pump is spaced from the fuel collector;operating the fuel collector at a near-ambient fuel tank ullage pressure; andlocating an engine fuel pump outward from an outer surface of said fuel collector. 24. The method as recited in claim 23, locating the fuel collector within the fuel tank. 25. The method as recited in claim 23, locating the fuel collector external to the fuel tank, the boost pump which maintains the boost pressure, directly upstream of the fuel collector.