초록 ▼

A fuel inerting system, comprising a first supply means ( 2 ) to supply an inert gas to a fuel tank ( 8 ) to scrub the fuel therein when the ullage ( 16 ) of the fuel tank is inert, and a second supply means ( 4 ) to supply the inert gas to scrub the fuel ( 6 ) therein when the ullage of the fuel ta

A fuel inerting system, comprising a first supply means ( 2 ) to supply an inert gas to a fuel tank ( 8 ) to scrub the fuel therein when the ullage ( 16 ) of the fuel tank is inert, and a second supply means ( 4 ) to supply the inert gas to scrub the fuel ( 6 ) therein when the ullage of the fuel tank is not inert, the first and second supply means ( 2, 4 ) being individually operable by means of a valve arrangement ( 10 ), in such a manner that only one of the supply means is operable at any given time. The inert gas consists of nitrogen enriched air, produced by passing air from a pressurized area of the aircraft through a nitrogen separator located within, but removable from, the aircraft.

대표청구항 ▼

1. A fuel inerting system comprising:a first supply means to supply an inert gas to a fuel tank to scrub the fuel therein when the ullage of the fuel tank is not inert,a second supply means to supply the inert gas to scrub the fuel therein when the ullage of the fuel tank is inert,an oxygen sensor l

1. A fuel inerting system comprising:a first supply means to supply an inert gas to a fuel tank to scrub the fuel therein when the ullage of the fuel tank is not inert,a second supply means to supply the inert gas to scrub the fuel therein when the ullage of the fuel tank is inert,an oxygen sensor linked to the second supply means and located within the fuel tank ullage to measure the oxygen concentration; anda valve arrangement, responsive to said oxygen sensor, for interconnecting said first supply means to said fuel tank and for interconnecting said second supply means to said fuel tank, wherein only one of the first supply means and second supply means is operable at any given time, wherein the second supply means is automatically operated with regard to an output of the oxygen sensor. 2. A fuel inerting system according to claim 1, wherein the valve arrangement consists of a pressure-actuated priority valve. 3. A fuel inerting system according to claim 2, wherein the first supply means consists of a mixer drawing the inert gas from the ullage. 4. A fuel inerting system according to claim 3, wherein the second supply means consists of a supply of pressurised inert gas. 5. A fuel inerting system according to claim 1, further comprising means for producing the inert gas from air taken from within an aircraft pressurised area. 6. A fuel inerting system according to claim 5, wherein the air is taken from a pressurised cargo bay. 7. A fuel inerting system according to claim 5, wherein the inert gas is produced by means of a nitrogen separator located within, but removable from, the aircraft. 8. A fuel inerting system according to claim 1, further comprising means for storing the pressurised inert gas. 9. A fuel inerting system according to claim 8, wherein the storage means is located within, but removable from, the aircraft. 10. A fuel inerting system according to claim 1, wherein the first and second supply means may be operated manually. 11. A fuel inerting system according to claim 1, wherein the inert gas consists of nitrogen enriched air.