发明名称 複合材翼形部組立体
摘要 A composite blade assembly (10) for mounting on a turbine wheel includes a ceramic airfoil (12) and an airfoil platform (14). The ceramic airfoil (12) is formed with an airfoil portion (16), a blade shank portion (18) and a blade dovetail tang (20). The metal platform (14) includes a platform shank (22) and a radially inner platform dovetail. The ceramic airfoil (12) is captured within the metal platform (14), such that in use, the ceramic airfoil is held within the turbine wheel independent of the metal platform. A turbine rotor wheel and a corresponding method of assembling a composite blade are also provided.
申请公布号 JP6043154(B2) 申请公布日期 2016.12.14
申请号 JP20120238468 申请日期 2012.10.30
申请人 ゼネラル・エレクトリック・カンパニイ 发明人 アンドレス・ホセ・ガルシア−クレスポ
分类号 F01D5/30;F01D5/14;F01D5/28;F01D25/00;F02C7/00 主分类号 F01D5/30
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