초록 ▼

A fuel jettison system which provides pilot-initiated automatic operation to jettison fuel down to a 60 minute useable fuel remaining level while the manual operation, requiring the pilot to hold down the jettison panel switch, jettisons fuel down to a 20-minute useable fuel remaining level. The pil

A fuel jettison system which provides pilot-initiated automatic operation to jettison fuel down to a 60 minute useable fuel remaining level while the manual operation, requiring the pilot to hold down the jettison panel switch, jettisons fuel down to a 20-minute useable fuel remaining level. The pilot can interrupt jettisoning at any time. This termination sequence operates in either automatic or manual mode. The port and starboard main fuel tanks jettison fuel independently through independent shutoff valves and associated circuit logic to thereby maintain aircraft balance.

대표청구항 ▼

What is claimed is: 1. An aircraft fuel jettison system comprising: a fuel tank; a fuel pump; a fuel conduit in communication with said fuel tank and said fuel pump; a shutoff valve having an inward vent within said fuel conduit; and an overboard fuel jettison conduit in communication with said fue

What is claimed is: 1. An aircraft fuel jettison system comprising: a fuel tank; a fuel pump; a fuel conduit in communication with said fuel tank and said fuel pump; a shutoff valve having an inward vent within said fuel conduit; and an overboard fuel jettison conduit in communication with said fuel pump, said inward vent operable to vent said overboard fuel jettison conduit to permit operation of said fuel pump after said shutoff valve has closed to purge fuel from said overboard fuel jettison conduit at completion of a fuel jettison event. 2. The system as recited in claim 1, wherein said shutoff valve movable between an open position and a closed position, said shutoff valve biased to said closed position. 3. The system as recited in claim 2, further comprising a fuel jettison controller to independently operate said fuel shutoff valve in response to a fuel quantity gauging system. 4. The aircraft as recited in claim 1, further comprising a dip conduit in communication with said fuel conduit, said dip conduit defining an opening at a minimum useable fuel remaining level within said fuel tank, said fuel conduit penetrates into said fuel tank at a penetration level greater than said first useable fuel remaining level. 5. The aircraft as recited in claim 4, further comprising a fuel jettison controller in communication with said fuel pump, said fuel jettison controller providing pilot-initiated one-time activation automatic operation to said penetration level and a continuous activation manual operation to jettison fuel to said minimum useable fuel remaining level less than said penetration level. 6. The system as recited in claim 1, further comprising a dip conduit in communication with said fuel conduit, said dip conduit defining an opening at a minimum useable fuel remaining level within said fuel tank. 7. The system as recited in claim 6, wherein said dip conduit is in communication with said fuel conduit through a self sealing break away valve. 8. The system as recited in claim 6, wherein said minimum useable fuel remaining level within said fuel tank is a twenty minute useable fuel remaining level. 9. The aircraft as recited in claim 8, further comprising a fuel jettison controller in communication with said fuel pump, said fuel jettison controller providing pilot-initiated one-time actuation automatic operation to said penetration level and a continuous activation manual operation to jettison fuel to a minimum fuel remaining level less than said predefined useable fuel remaining level. 10. The system as recited in claim 8, wherein said fuel conduit penetrates into said fuel tank at a penetration level greater than said twenty minute useable fuel remaining level and less than a 120 minute useable fuel remaining level. 11. The system as recited in claim 10, wherein said fuel conduit penetration level is at an approximately 60 minute useable fuel remaining level. 12. An aircraft fuel jettison system comprising: a fuel tank; a fuel pump; a fuel conduit in communication with said fuel tank and said fuel pump, said fuel conduit penetrates into said fuel tank at a penetration level; an overboard fuel jettison conduit in communication with said fuel pump; a dip conduit in communication with said fuel conduit, said dip conduit defining an opening at a minimum useable fuel remaining level within said fuel tank; and a fuel jettison controller in communication with said fuel pump, said fuel jettison controller operable to provide a pilot-initiated one-time activation automatic operation to jettison fuel to said penetration level and a pilot-initiated continuous activation manual operation to jettison fuel to said minimum useable fuel remaining level less than said penetration level. 13. The system as recited in claim 12, wherein said penetration level is an approximately 60 minute useable fuel remaining level. 14. The system as recited in claim 12, wherein said penetration level is a 120 minute useable fuel remaining level. 15. The system as recited in claim 12, wherein said minimum useable fuel remaining level is a twenty minute useable fuel remaining level. 16. The system as recited in claim 12, further comprising a shutoff valve having an inward vent within said fuel conduit, said inward vent operable to vent said overboard fuel jettison conduit to permit operation of said fuel pump after said shutoff valve has closed to purge fuel from said overboard fuel jettison conduit at completion of a fuel jettison event. 17. The system as recited in claim 12, wherein said pilot-initiated one-time activation automatic operation is provide through a one-time actuation of a fuel jettison switch to jettison fuel down to said penetration level. 18. The system as recited in claim 17, wherein said pilot-initiated continuous activation manual operation is provided through continued actuation of said fuel jettison switch to jettison fuel to said minimum useable fuel remaining level. 19. The system as recited in claim 18, wherein said pilot-initiated manual operation stops when said continuous actuation of said fuel jettison switch is interrupted.