F - Mech Eng,Light,Heat,Weapons – 23 – R
Patent
F - Mech Eng,Light,Heat,Weapons
23
R
F23R 3/34 (2006.01) F02C 7/22 (2006.01) F23R 3/10 (2006.01) F23R 3/16 (2006.01)
Patent
CA 2597846
A mixer assembly (67) for a gas turbine engine (10), including: a primary fuel injector (110) having a central axis (120) for injecting a primary fuel spray into a primary air stream, wherein fuel is provided at a desired rate and droplets of the fuel spray are within a desired size range; a secondary fuel injector (128) positioned radially outwardly of the primary fuel injector (110) for injecting a secondary fuel spray into a secondary air stream spaced radially outwardly of and surrounding the primary air stream; and, a primary air jet positioned between the primary fuel injector (110) and the secondary fuel injector (128) to direct a portion of an incoming air stream between the primary air stream and the secondary air stream.
Mancini Alfred Albert
Mongia Hukam Chand
Company General Electric
Craig Wilson And Company
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