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filingDate 2012-10-23^^<http://www.w3.org/2001/XMLSchema#date>
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inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_aac9ba5aaee01777e844c3392bfb669c
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publicationDate 2017-10-10^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-9784113-B2
titleOfInvention Method of fabricating a turbine or compressor guide vane sector made of composite material for a turbine engine, and a turbine or a compressor incorporating such guide vane sectors
abstract Single-airfoil vanes each having an inner platform, an outer platform, and an airfoil are obtained by three-dimensionally weaving a fiber blank in a single piece, by shaping the fiber blank to obtain a single-piece fiber preform, and by densifying the preform with a matrix to obtain a vane of composite material forming a single piece with inner and outer platforms incorporated therein. A plurality of vanes is assembled together at an intermediate stage of densification to form a multi-airfoil composite material guide vane sector for a turbine nozzle or a compressor diffuser and the assembled-together vanes are bonded together.
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