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公开(公告)号:US11879358B2
公开(公告)日:2024-01-23
申请号:US17772176
申请日:2020-11-27
Applicant: EXONETIK TURBO INC.
Inventor: Benoit Picard , Jean-Sebastien Plante , Mathieu Picard
CPC classification number: F01D5/284 , C04B35/44 , C04B35/48 , F01D5/08 , F01D5/18 , F01D5/288 , F01D25/12 , C04B2235/3222 , C04B2235/3225 , C04B2235/3246 , C04B2235/9607 , C04B2237/121 , C10M2201/0613 , F05D2230/90
Abstract: A rim-rotor assembly has an annular structure including a composite rim and a hub. Blades project from the hub, tips of the blades contacting the annular structure, the blades configured to be loaded in compression against the annular structure. A thermal barrier is in the annular structure, the thermal barrier defining at least part of a radially inward surface of the annular structure. The tips of the blades contact the thermal barrier, the thermal barrier being a thermal barrier coating.