发明名称 STRAIN AMPLIFICATION STRUCTURE AND SYNTHETIC JET ACTUATOR
摘要 A strain amplification structure has a frame with a hexagonal structure incorporating a plurality of rigid beams that are connected to opposing end beams by a plurality of flexible joints. A piezoceramic actuator assembly is connected to the opposing end beams having a collar including an opening. A shaft providing an output is connected to the plurality of rigid beams with flexible joints and passes through the opening in the collar for non-interfering motion orthogonal to the actuator assembly.
申请公布号 US2015097467(A1) 申请公布日期 2015.04.09
申请号 US201414569464 申请日期 2014.12.12
申请人 The Boeing Company 发明人 Griffin Steven F.;Haar Shawn
分类号 H01L41/09;H01L41/25;H01L41/053 主分类号 H01L41/09
代理机构 代理人
主权项 1. A strain amplification structure comprising: a frame having a hexagonal structure incorporating a plurality of rigid beams that are connected to opposing end beams by a plurality of flexible joints; a piezoceramic actuator assembly connected to the opposing end beams; a collar in the piezoceramic actuator assembly, said collar including an opening; and a shaft providing an output and connected to the plurality of rigid beams with flexible joints, said shaft passing through said opening.
地址 Chicago IL US