发明名称 Dynamically controlled cross flow instability inhibiting assembly
摘要 A cross flow instability inhibiting assembly generates periodic aerodynamic disturbances on a swept wing. The cross flow instability inhibiting assembly is dynamic in that it can be selectively turned on and off as needed. The cross flow instability inhibiting assembly is a strip of material separating a set of electrodes from a set of electrodes. When energized, the fields created between the electrodes and electrodes create plasma disturbances around the electrodes. The electric fields and plasma create heating and body force disturbances on the air or surrounding fluid. These plasma generated disturbances disrupt development of unstable voriticity due to cross flow, inhibiting transition to turbulent flow of the wing to which it is attached. The electrodes may be connected to electrical power in series or they may be connected to an alternating configuration. The system allows for various uses based on the design of the wing and the conditions in which the host aircraft is flying.
申请公布号 US8636254(B2) 申请公布日期 2014.01.28
申请号 US20100893618 申请日期 2010.09.29
申请人 HANSEN CRAIG M.;MCCLURE PAUL D.;MACHERET SERGEY;LOCKHEED MARTIN CORPORATION 发明人 HANSEN CRAIG M.;MCCLURE PAUL D.;MACHERET SERGEY
分类号 B64C23/00 主分类号 B64C23/00
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