Auxiliary power unit intake duct with aero-acoustic guide vanes

Details Auxiliary power unit intake duct with aero-acoustic guide vanes Auxiliary power unit intake duct with aero-acoustic guide vanes

B - Operations, Transporting

64

D

B64D 33/02 (2006.01)

Patent

CA 2531699

An auxiliary power unit intake duct for an aircraft, comprising an internal straight portion 1a, an internal first bend portion 1b and an internal second bend portion 1c, extending between an air inlet 2 and a plenum entry 3 of the auxiliary power unit, a plurality of acoustic guides vanes 4,5 located in the straight portion la of the intake duct 1, extending horizontally between opposite side portions of the straight portion 1a; and a plurality of curved aerodynamic guide vanes 6,7 located in the second bend portion 1c proximate to said plenum inlet 3, extending vertically between a top portion and a bottom portion of the second bend portion 1c, each of the curved aerodynamic guide vanes 6,7 being concentric with said bend curvature of the second bend portion 1c.

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