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Angled Radial Fuel/Air Delivery System for CombustorA 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.
Document ID
20180005312
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
Authors
Kim, Wookyung
Dai, Zhongtao
Kopp-Vaughan, Kristin
Date Acquired
September 15, 2018
Publication Date
August 28, 2018
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-10,060,629
Patent Application Number: US-Patent-Appl-SN-14/627,709
Funding Number(s)
TASK: NNC13TA45T
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-10,060,629
Patent Application
US-Patent-Appl-SN-14/627,709

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