Integrated turbine exhaust struts and mixer of turbofan engine
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United States of America Patent
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Sep 12, 2017
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app pub date -
Oct 23, 2014
filing date -
May 26, 2014
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Abstract
A turbine exhaust case (TEC) of a turbofan aeroengine includes a mixer in an annular wavy configuration having alternate crests and valleys, and a plurality of radial deswirling struts interconnecting an annular hub positioned within the mixer and selected valleys of the mixer. A plurality of secondary trailing edge struts smaller than the deswirling struts in average chord dimensions interconnect the annular hub and other selected valleys free of connection with the deswirling struts.
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