CPC F01D 9/041 (2013.01) [F05D 2230/60 (2013.01); F05D 2240/12 (2013.01); F05D 2300/175 (2013.01); F05D 2300/6033 (2013.01)] | 8 Claims |
1. An assembly for a gas turbine engine comprising:
a vane disposed about an axis and having a radially outer platform, a flange projecting radially outwardly from the radially outer platform, and a notch extending axially through the flange such that the notch opens at forward and aft flange faces of the flange; and
a ring located radially outward of the radially outer platform, the ring having axially forward and aft ring faces and a lug extending axially from the forward ring face, the lug extending axially through the notch on the flange and limiting circumferential movement of the vane.
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