A GUIDE VANE MADE OF COMPOSITE MATERIAL FOR A GAS TURBINE ENGINE, AND IT'S METHOD OF FABRICATION

A guide vane for a gas turbine engine, the guide vane including an airfoil made of composite material having fiber reinforcement densified by a matrix, the fiber reinforcement being obtained from pre-impregnated long fibers agglomerated in the form of a mat, the airfoil being provided at least on a leading edge with a reinforcing strip, the reinforcing strip being made from a single strip of unidirectional fabric or of textile, or by stacking a plurality of pre-impregnated plies of unidirectional fabric or of textile made of carbon fibers or of glass fibers, and at least one platform positioned at a radial end of the airfoil, the platform being made of composite material having fiber reinforcement densified by a matrix, the fiber reinforcement being obtained from pre-impregnated long fibers.


» Number: US2017254212A1 (A1)

» Publication Date: 07/09/2017

» Applicant: SAFRAN AIRCRAFT ENGINES?[FR]; SAFRAN?[FR]

» Inventor: PAUTARD SÉBASTIEN?[FR]; BRIEND MAXIME?[FR] (2)

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This project has received funding from the European Union's Horizon 2020 research and innovation programme under grant agreement Nº 768737


                   




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