发明名称 VARIABLE-PITCH ROTOR WITH REMOTE COUNTERWEIGHTS
摘要 A pitch control mechanism includes: a rotor structure configured for rotation about a longitudinal axis; a row of blades carried by the rotor structure, each blade having an airfoil and a trunnion mounted for pivoting movement relative to the rotor structure, about a trunnion axis which is perpendicular to the longitudinal axis; a unison ring interconnecting the blades; an actuator connected to the unison ring and the rotor structure, operable to move the unison ring relative to the rotor structure; at least one moveable counterweight carried by the rotor structure, remote from the blades; and an interconnection between the blades and the counterweight, such that movement of the counterweight causes a change in the pitch angle of the blades.
申请公布号 US2016032740(A1) 申请公布日期 2016.02.04
申请号 US201514708353 申请日期 2015.05.11
申请人 General Electric Company 发明人 NIERGARTH Daniel Alan;MILLER Brandon Wayne;BRADLEY Donald Albert
分类号 F01D7/02;F01D5/02;F02C3/04 主分类号 F01D7/02
代理机构 代理人
主权项 1. A pitch control mechanism, comprising: a rotor structure configured for rotation about a longitudinal axis; a row of blades carried by the rotor structure, each blade having an airfoil and a trunnion mounted for pivoting movement relative to the rotor structure, about a trunnion axis which is perpendicular to the longitudinal axis; a unison ring interconnecting the blades; an actuator connected to the unison ring and the rotor structure, operable to move the unison ring relative to the rotor structure; at least one moveable counterweight carried by the rotor structure, remote from the blades; and an interconnection between the blades and the counterweight, such that movement of the counterweight causes a change in the pitch angle of the blades.
地址 Schenectady NY US