| 发明名称 | Fluidic traverse actuator | ||
| 摘要 | A system and methods for a self-rotating fluidic traverse actuator are presented. A turbine rotates in response to a fluid flow, and an outer cylinder with a longitudinal slot that ejects the fluid flow. An inner cylinder rotates inside the outer cylinder in response to a rotation of the turbine and at least one helical slot of the inner cylinder ejects the fluid flow into the longitudinal slot. | ||
| 申请公布号 | US9511849(B2) | 申请公布日期 | 2016.12.06 |
| 申请号 | US201213662466 | 申请日期 | 2012.10.27 |
| 申请人 | The Boeing Company | 发明人 | Shmilovich Arvin;Kent Steven Richard |
| 分类号 | F03B3/12;B64C21/04 | 主分类号 | F03B3/12 |
| 代理机构 | McDonnell Boehnen Hulbert & Berghoff LLP | 代理人 | McDonnell Boehnen Hulbert & Berghoff LLP |
| 主权项 | 1. A self-rotating fluidic traverse actuator for an aircraft comprising: a turbine operable to rotate in response to a fluid flow; an outer cylinder comprising a longitudinal slot operable to eject the fluid flow; and an inner cylinder operable to rotate inside the outer cylinder in response to a rotation of the turbine, wherein the turbine is operable to introduce the fluid flow into the inner cylinder, and wherein the inner cylinder comprises at least one helical slot operable to eject the fluid flow into the longitudinal slot. | ||
| 地址 | Chicago IL US | ||