Aero-slinger combustor

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 9/00 (2006.01) F23R 3/14 (2006.01) F23R 3/28 (2006.01) F23R 3/30 (2006.01) F23R 3/34 (2006.01)

Patent

CA 2076102

A combustor includes radially spaced apart outer and inner liners joined together at upstream ends through an annular dome disposed coaxially about a longitudinal centerline axis. A plurality of circumferentially spaced apart fuel injectors are disposed adjacent to an arcuate a splashplate for injecting fuel thereagainst, the splashplate being arcuate about the centerline axis. Primary air is channeled along the splashplate for mixing with the injected fuel for forming a fuel/air mixture dischargeable from the splashplate into a combustion zone defined between the liners and the dome.

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