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Nonlinearly stacked low noise turbofan statorA nonlinearly stacked low noise turbofan stator vane having a characteristic curve that is characterized by a nonlinear sweep and a nonlinear lean is provided. The stator is in an axial fan or compressor turbomachinery stage that is comprised of a collection of vanes whose highly three-dimensional shape is selected to reduce rotor-stator and rotor-strut interaction noise while maintaining the aerodynamic and mechanical performance of the vane. The nonlinearly stacked low noise turbofan stator vane reduces noise associated with the fan stage of turbomachinery to improve environmental compatibility.
Document ID
20090043145
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
Authors
Schuster, William B.
Kontos, Karen B.
Weir, Donald S.
Nolcheff, Nick A.
Gunaraj, John A.
Date Acquired
August 24, 2013
Publication Date
June 16, 2009
Subject Category
Mechanical Engineering
Funding Number(s)
CONTRACT_GRANT: NAS3-01136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,547,186
Patent Application
US-Patent-Appl-SN-11/166,668
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