http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2014058502-A2

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publicationDate 2014-04-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber WO-2014058502-A2
titleOfInvention Ceramic centerbody and method of making
abstract A ceramic centerbody (120) for an aircraft gas turbine engine. The ceramic centerbody (120) comprises an interlaced fiber structure having fibers oriented in a substantially transverse directions and a ceramic matrix surrounding the ceramic fiber structure. The ceramic fiber and matrix are formed into a conical shape having a fore end (128) and an aft end (126). The centerbody includes a means for mechanical attachment (130) circumferentially oriented around the fore end of the centerbody. The fore end further includes additional plies oriented in a third preselected direction, thereby providing additional strength to for mechanical attachment.
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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2017138219-A1
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