发明名称 Propeller Blade With Relatively Movable Counterweight
摘要 A propeller rotor has a hub mounting a plurality of blades. A counterweight is movably mounted on the blade. A pitch change mechanism for changing an angle of incidence of an airfoil is associated with each of the blades. The counterweight twists the blades toward an increased pitch direction should the pitch change mechanism fail. A stop member stops rotation of the counterweight as the blade moves to a feather position.
申请公布号 US2014193253(A1) 申请公布日期 2014.07.10
申请号 US201313735419 申请日期 2013.01.07
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 Carvalho Paul A.
分类号 F01D7/00 主分类号 F01D7/00
代理机构 代理人
主权项 1. A propeller rotor comprising: a rotor mounting a plurality of blades, said blades having a root mounted in a hub of said rotor and a counterweight movably mounted on said blades; a pitch change mechanism for changing an angle of incidence of an airfoil associated with said blades and said counterweight for biasing said blades toward an increased pitch direction should said pitch change mechanism fail; and a stop member for stopping rotation of said counterweight and said counterweight with said blade as said blade moves to a feathered position.
地址 Windsor Locks CT US