
基本信息:
- 专利标题: Airfoil performance modification using synthetic jet actuators
- 专利标题(中):使用合成射流执行器进行翼型性能改进
- 申请号:US11263504 申请日:2005-10-31
- 公开(公告)号:US20070095987A1 公开(公告)日:2007-05-03
- 发明人: Ari Glezer , Michael DeSalvo
- 申请人: Ari Glezer , Michael DeSalvo
- 主分类号: B64C23/06
- IPC分类号: B64C23/06
摘要:
Systems and methods for modifying fluid flowing over solid bodies are provided. A representative system incorporates a vorticity concentration-producing component and a synthetic jet actuator. The vorticity concentration-producing component is disposed on a pressure side of the solid body. The fluid flowing over the solid body remains attached to a surface of the solid body in a vicinity of the vorticity concentration-producing component. The synthetic jet actuator includes a jet housing that incorporates an internal chamber with a volume of fluid and an opening in the jet housing connecting the internal chamber to an external environment having the fluid. The synthetic jet actuator is operative to periodically change the volume within the internal chamber such that a synthetic jet stream comprising a series of fluid vortices is generated and projected in the external environment out from the opening of the jet housing resulting in a reduction in pressure drag of the solid body compared to the pressure drag exhibited by the solid body without operation of the synthetic jet actuator.
摘要(中):
提供了用于改变在固体上流动的流体的系统和方法。 代表性的系统包括产生涡度浓度的组分和合成射流致动器。 涡旋浓度产生组分设置在固体的压力侧。 在固体上流动的流体保持附着在固体的表面附近的涡度产生组分附近。 合成射流致动器包括喷射壳体,其包括具有一定体积流体的内部腔室和喷射壳体中的开口,其将内部腔室连接到具有流体的外部环境。 合成射流致动器可操作以周期性地改变内部腔室内的体积,从而产生包含一系列流体旋涡的合成射流,并在外部环境中从射流壳体的开口突出,导致压力阻力减小 的固体与固体的表现的压力阻力相比,而不需要合成射流致动器的操作。
公开/授权文献:
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64C | 飞机;直升飞机 |
------B64C23/00 | 其他类目不包含的影响流经飞机表面的空气流 |
--------B64C23/06 | .通过产生旋涡 |