|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 7|
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.
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; andan 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, andwherein the inner cylinder comprises at least one helical slot operable to eject the fluid flow into the longitudinal slot. 2. The self-rotating fluidic...