Fuel injector

Claim 2

A fuel injector suitable for a gas turbine engine comprising a main body portion having an upstream end and a downstream end, said upstream end being operationally in communication with a region of air at high pressure, said main body portion having at least one passage therin interconnecting said upstream and downstream ends thereof so as to provide an air flow through said main body portion which exhausts from said downstream end thereof, means adapted to direct fuel into said air flow so as to provide intermixing therewith, and steam injection means located in the region of the upstream end of said main body portion, said steam injection means being so configured and arranged as to operationally permit said air flow through said at least one passage from said region of air at high pressure and optionally direct steam into said at least one passage, the total exhaust area of said stem injection means being less than the total inlet area of said at least one passage and the total pressure of steam at the exhaust outlet of said steam injection means when steam is exhausted therefrom being higher than the pressure operationally within said at least one passage so that at least the majority of steam so directed enters said at least one passage, a portion of said injector main body cooperating with said steam injection means to define said steam outlet from said steam injector.

Claim 3

A fuel injector as claimed in claim 1 wherein said at least one passage is of annular cross-sectional shape.

Claim 4

A fuel injector as claimed in claim 1 wherein said steam injection means is of annular form.

Claim 5

A fuel injector as claimed in claim 1 wherein the downstream end of said at least one passage has a radially outwardly directed component with respect to the longitudinal axis of said fuel injector.

Claim 6

A fuel injector as claimed in claim 1 wherein said injector is so arranged that sufficient steam is operationally directed into said at least one passage to provide that the air content within said at least one passage is not greater than 20% by weight.

Claim 7

A fuel injector suitable for a gas turbin engine comprising a main body portion having an upstream end and a downstream end, said upstream end bein operationally in communication with a region of air at high pressure, said main body portion having at least one passage therein interconnecting said upstream and downstream ends thereof so as to provide an air flow through said main body portion which exhausts from said downstream end thereof, means adapted to direct fuel into said air flow so as to provide intermixing therewith, and steam injection means located in the region of the upstream end of said main body portion, said steam injection means including an exhaust outlet, said steam injection means being so configured and arranged as to operationally permit said air flow through said at least one passage from said region of air at high pressure and optionally direct steam into said least one passage, the total exhaust area of said steam injection means being less than the total inlet area of said at least one passage and the total pressure of steam at the exhaust outlet of said steam injection means when steam is exhausted therefrom being higher than the pressure operationally within said at least one passage so that at least the majority of steam so directed enters said at least one passsage, said means adapted to direct fuel into said air flow being situated internally of said main body portion and being adapted to direct fuel into said at least one passage, said fuel injector beinig provided with two of said passages interconnecting said upstream and downstreams ends of said main body portion and additional fuel injection means being situated on said downstream end of said main body portion, said additional fuel injection means being adapted to direct fuel into the air flow exhausted from the passage which does not have fuel injected thereinto.

Claim 8

A fuel injector suitable for a gas turbin engine comprising a main body portion having an upstream end and a downstream end, said upstream end bein operationally in communication with a region of air at high pressure, said main body portion having at least one passage therein interconnecting said upstream and downstream ends thereof so as to provide an air flow through said main body portion which exhausts from said downstream end thereof, means adapted to direct fuel into said air flow so as to provide intermixing therewith, and steam injection means located in the region of the upstream end of said main body portion, said steam injection means including an exhaust outlet, said steam injection means being so configured and arranged as to operationally permit said air flow through said at least one passage from said region of air at high pressure and optionally direct steam into said least one passage, the total exhaust area of said steam injection means being less than the total inlet area of said at least one passage and the total pressure of steam at the exhaust outlet of said steam injection means when steam is exhausted therefrom being higher than the pressure operationally within said at least one passage so that at least the majority of steam so directed enters said at least one passsage, said means adapted to direct fuel into said air flow being situated internally of said main body portion and being adapted to direct fuel into said at least one passage, said fuel injector beinig provided with two of said passages interconnecting said upstream and downstreams ends of said main body portion and additional fuel injection means being situated on said downstream end of said main body portion, said additional fuel injection means being adapted to direct fuel into the air flow exhausted from the passage which does not have fuel injected thereinto.