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특허 상세정보

Plasma optimized aerostructures for efficient flow control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-029/00    F15D-001/00    B64C-021/00   
출원번호 US-0710750 (2007-02-26)
등록번호 US-9541106 (2017-01-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kolkowski, Brian
인용정보 피인용 횟수 : 1  인용 특허 : 28
초록

The present invention relates to a method of designing or optimizing a control surface for use with plasma actuators for controlling an aircraft, missile, munition or automobile, and more particularly to controlling fluid flow across their surfaces or other surfaces using plasma actuators, which would benefit from such a method. The various embodiments provide the steps to increase the efficiency of aircraft, missiles, munitions and automobiles. The method of flow control also provides a means for reducing aircraft, missile's, munition's and automobile's...

대표
청구항

1. An aircraft, missile, projectile, munition, or automobile comprising at least one surface over which air flow occurs, the at least one surface having a leading edge and a trailing edge, the at least one surface comprising a modified contour, the modified contour being designed to create a surface flow disturbance along the surface beyond a specific location on the surface, andat least one plasma actuator being positioned on the surface to affect the created surface flow disturbance along the surface when actuated,wherein the at least one plasma actuat...

이 특허에 인용된 특허 (28)

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