Fuel inlet with crescent shaped passage for gas turbine engines

Details Fuel inlet with crescent shaped passage for gas turbine engines Fuel inlet with crescent shaped passage for gas turbine engines

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/22 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2638541

An inlet tube within a gas turbine engine which includes a primary fuel channel and a secondary fuel channel formed in a cylindrical tube body. The secondary channel has a substantially crescent shaped cross-sectional area which is complementary in shape to the primary fuel channel, such as to maximize the combined fuel flow area through the primary and secondary fuel channels relative to an outer diameter of the cylindrical tube body.

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