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Fuel premixing module for gas turbine engine combustorA fuel-air premixing module is designed to reduce emissions from a gas turbine engine. In one form, the premixing module includes a central pilot premixer module with a main premixer module positioned thereround. Each of the portions of the fuel-air premixing module include an axial inflow swirler with a plurality of fixed swirler vanes. Fuel is injected into the main premixer module between the swirler vanes of the axial inflow swirler and at an acute angle relative to the centerline of the premixing module.
Document ID
20080005032
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
Authors
Chin, Jushan
Rizk, Nader K.
Razdan, Mohan K.
Marshall, Andre W.
Date Acquired
August 24, 2013
Publication Date
November 29, 2005
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-423135
Patent Number: US-PATENT-6,968,692
Funding Number(s)
CONTRACT_GRANT: NAS3-27725
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,968,692
Patent Application
US-PATENT-APPL-SN-423135
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