Angled Radial Fuel/Air Delivery System for Combustor

Kim, Wookyung [Inventor]Dai, Zhongtao [Inventor]Kopp-Vaughan, Kristin [Inventor]

关键词: GAS TURBINE ENGINES;    COMBUSTION CHAMBERS;    FUEL SYSTEMS;    PATENTS;   

RP-ID  :  US-Patent-10,060,629, US-Patent-Appl-SN-14/627,709

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

A combustor is provided. The combustor may comprise an axial fuel delivery system, and a radial fuel delivery system aft of the axial fuel delivery system. The radial fuel delivery system may be configured to direct fuel at least partially towards the axial fuel delivery system. A radial fuel delivery system is also provided. The system may comprise a combustor including a combustor liner, a mixer coupled to the combustor liner, and a nozzle disposed within the mixer, wherein the mixer and the nozzle are configured to direct fuel in a direction at least partially forward.