CPC F04D 29/329 (2013.01) [B29B 11/16 (2013.01); F01D 5/26 (2013.01); F01D 5/282 (2013.01); F01D 5/3007 (2013.01); F02K 3/06 (2013.01); F04D 29/023 (2013.01); F04D 29/34 (2013.01); F04D 29/646 (2013.01); B29L 2031/08 (2013.01); F05D 2220/36 (2013.01); Y02T 50/60 (2013.01)] | 20 Claims |
1. A blade for a turbine engine, the blade comprising:
a blade root;
an airfoil portion extending upwards from the blade root;
a platform made of composite material and extending transversely to the airfoil portion at a junction between the blade root and the airfoil portion, wherein the platform extends from the blade root along a first axis; and
an attachment portion provided on a lower surface of the platform at a distal end of the platform, configured to cooperate with a first hook of the turbine engine, wherein the attachment portion is at a furthest position of the platform on the first axis away from the blade root.
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