发明名称 TIP SHROUDS OF TURBINE ROTOR BLADES AND METHODS OF MANUFACTURE RELATED THERETO
摘要 A rotor blade for use in a turbine of a turbine engine is described. The rotor blade may include an airfoil that extends from a connection with a root. The airfoil may include a pressure sidewall and a suction sidewall that define an outer periphery and an outboard tip. The rotor blade may further include a tip shroud assembly disposed at the outboard tip of the airfoil. The tip shroud assembly includes a non-integral tip shroud.
申请公布号 US2014255194(A1) 申请公布日期 2014.09.11
申请号 US201213725649 申请日期 2012.12.21
申请人 General Electric Company 发明人 Jones Mark Andrew
分类号 F01D5/22 主分类号 F01D5/22
代理机构 代理人
主权项 1. A rotor blade for use in a turbine of a turbine engine, the rotor blade comprising an airfoil that extends from a connection with a root, the airfoil including a pressure sidewall and a suction sidewall that define an outer periphery and an outboard tip, the rotor blade further comprising: a tip shroud assembly disposed at the outboard tip of the airfoil; wherein the tip shroud assembly includes a non-integral tip shroud.
地址 US