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Aircraft engine driveshaft vessel assembly and method of assembling the same

  • US 9,657,646 B2
  • Filed: 04/19/2013
  • Issued: 05/23/2017
  • Est. Priority Date: 04/25/2012
  • Status: Active Grant
First Claim
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1. A driveshaft vessel assembly for a gas turbine engine comprising an axis of rotation, said assembly comprising:

  • a driveshaft vessel configured to house at least a portion of a radial driveshaft, said driveshaft vessel including a forward face, an aft face, and opposing side faces; and

    an outlet guide vane including a leading edge and a trailing edge, wherein said trailing edge includes a length substantially equal to a length of said forward face such that said trailing edge of said outlet guide vane is faired into said forward face of said driveshaft vessel.

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