发明名称 Rotor assembly of a turbomachine fan
摘要 <p>The assembly has blades (20) fixed to rotor discs (18) by feet (22) of the blades, and extending outside from the disc. Interblade platforms (30) extend between the adjacent blades, and define an inner profile for fluid flowing through a fan. The adjacent blades form bulge guides (25) on lateral surfaces (20A), where the guides are located outside the disc and limits radial movement of the platforms toward outside. The platforms have C-shaped section, an outer wall (30E), and inner walls (30I) that are located in extension of side walls (30L) and bent towards center of the platforms.</p>
申请公布号 EP1972757(B1) 申请公布日期 2012.07.18
申请号 EP20080153131 申请日期 2008.03.20
申请人 SNECMA 发明人 BRAULT, MICHEL;ROUSSELIN, STEPHANE
分类号 F01D11/00 主分类号 F01D11/00
代理机构 代理人
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