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 |