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특허 상세정보

Active systems and methods for controlling an airfoil vortex

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06   
미국특허분류(USC) 244/1993; 244/208
출원번호 US-0747112 (2007-05-10)
등록번호 US8016244 (2011-08-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 5  인용 특허 : 56
초록

Active systems and methods for controlling aircraft vortices are disclosed. An apparatus in accordance with one embodiment is directed to an aircraft system that includes an airfoil having first and second oppositely facing flow surfaces and a tip. The system can further include a vortex dissipation device carried by the airfoil, with the vortex dissipation device including an orifice positioned to direct a flow of fluid outwardly from the tip, an actuator operatively coupled to the fluid flow orifice and positioned to change a manner in which flow is di...

대표
청구항

We claim: 1. An aircraft system, comprising:an airfoil having a root and a tip; anda vortex dissipation device carried by the airfoil, the vortex dissipation device including:a plurality of fluid flow orifices positioned to direct fluid outwardly from the tip;a plurality of actuators, individual actuators being operatively coupled to individual fluid flow orifices, the actuators being positioned to actuate an interior surface within individual orifices to create alternating positive and negative pressures within the individual orifices; anda controller o...

이 특허에 인용된 특허 (56)

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