| CPC F01D 9/041 (2013.01) [F02C 7/24 (2013.01); F05D 2240/12 (2013.01); F05D 2260/96 (2013.01)] | 20 Claims |

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1. A turbofan engine including outlet guide vanes comprising: a bypass duct having a radially inward wall and a radially outward wall; and a plurality of non-uniform outlet guide vanes disposed between the radially inward wall and the radially outward wall of the bypass duct, wherein the plurality of non-uniform outlet guide vanes includes at least one first integral outlet guide vane coupled to a pylon of the turbofan engine, wherein chord lengths of two or more of the plurality of non-uniform outlet guide vanes at a base adjacent the radially inward wall are different, wherein the plurality of non-uniform outlet guide vanes includes the at least one first integral outlet guide vane, at least one structural outlet guide vane, at least one cut-out outlet guide vane, and at least one non-structural outlet guide vane.
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