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Low-noise fan exit guide vanesLow-noise fan exit guide vanes are disclosed. According to the present invention a fan exit guide vane has an outer shell substantially shaped as an airfoil and defining an interior cavity. A porous portion of the outer shell allows communication between the fluctuations in the air passing over the guide vane and the interior cavity. At least one acoustically resonant chamber is located within the interior cavity. The resonant chamber is in communication with the porous portion of the outer perimeter. The resonant chamber is configured to reduce the noise generated at a predetermined frequency. In various preferred embodiments, there is a plurality of acoustically resonant chambers located within the interior cavity. The resonant chambers can be separated by one or more partitions within the interior cavity. In these embodiments, the resonant chambers can be configured to reduce the noise generated over a range of predetermined frequencies.
Document ID
20080020317
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Jones, Michael G.
Parrott, Tony L.
Heidelberg, Laurence J.
Envia, Edmane
Date Acquired
August 24, 2013
Publication Date
February 26, 2008
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-7,334,998
Patent Application Number: US-Patent-Appl-SN-11/005,624
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,334,998
Patent Application
US-Patent-Appl-SN-11/005,624
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