| 摘要 |
A turbine engine comprising a compressor section having an intake, a core vane assembly positioned upstream of said compressor section and encircling a central longitudinal axis and having a plurality of core vanes each extending radially between an inner hub and an outer band wherein said core vane assembly extends along said central longitudinal axis between a first forward end and a first aft end, a bypass vane assembly disposed on a radially opposite side of said outer band relative to said plurality of core vanes, said bypass vane assembly including at least one bypass vane extending radially outward from a platform and said bypass vane assembly extending along said central longitudinal axis between a second forward end and a second aft end; and wherein said bypass vane assembly includes a plurality of bosses fixed with said outer band and the plurality of bosses engages said bypass vane assembly proximate to said second forward end, wherein said plurality of bosses includes a first set of bosses and a second set of bosses arranged in an alternating relation about the central longitudinal axis and the first set of bosses and the second set of bosses are differently shaped from one another. |
