초록 ▼

A fuel injection system for a gas trubine engine combustion chamber comprises at least one pilot fuel injector having a fuel discharge passage communicated to the combustion chamber and at least one secondary fuel injector having a fuel discharge passage communicated to the combustion chamber and a

A fuel injection system for a gas trubine engine combustion chamber comprises at least one pilot fuel injector having a fuel discharge passage communicated to the combustion chamber and at least one secondary fuel injector having a fuel discharge passage communicated to the combustion chamber and a fuel purging passage communicated to a higher pressure region upstream of the combustion chamber. A fuel flow control device supplies metered fuel flow to the pilot fuel injector under all regimes of engine operation and to the secondary fuel injector under certain, intermittent regimes of engine operation requiring fuel flow above a selected level. A shuttle valve is movable to a first position to provide fuel flow communication between the fuel control device and the fuel discharge passage of the secondary fuel injector for fuel injection to the combustion chamber. The shuttle valve also is movable to a second position to communicate the fuel discharge passage and the fuel purging passage of the secondary injector to the higher pressure region to purge fuel from the fuel discharge passage to the combustion chamber.

대표청구항 ▼

[ I claim:] [1.] A fuel injection system for a gas turbine engine combustion chamber, comprisingat least one pilot fuel injector communicated to said combustion chamber for discharging fuel thereto,at least one secondary fuel injector having a fuel discharge passage communicated to said combustion c

[ I claim:] [1.] A fuel injection system for a gas turbine engine combustion chamber, comprisingat least one pilot fuel injector communicated to said combustion chamber for discharging fuel thereto,at least one secondary fuel injector having a fuel discharge passage communicated to said combustion chamber for discharging fuel thereto and a fuel purging passage communicated to a purge air source,fuel flow control means for supplying fuel flow to said pilot fuel injector under all regimes of engine operation and to said secondary fuel injector under regimes of engine operation requiring fuel flow above a selected level, anda purge valve movable between a first injection position to provide fuel flow communication between said fuel control means and said fuel discharge passage of said secondary fuel injector for fuel injection to said combustion chamber and to a second purging position to communicate said fuel discharge passage of said secondary injector and said fuel purging passage to purge fuel from said fuel discharge passage to said combustion chamber, the purge valve being biased by spring means toward the second purging position, said purge valve being communicated to fuel return pressure when fuel flow to said secondary injector exceeds said selected level such that secondary fuel pressure on said purge valve overcomes said spring means and said fuel return pressure to position said purge valve at the first injection position and being communicated to fuel supply pressure and biased by said spring means in a manner to position said purge valve at the second purging position when fuel flow to said secondary injector is controlled below said selected level.