发明名称 Articulated control surface
摘要 An articulated control surface for flight control utilizes a moldable control surface that is shaped by contracting and elongating shape memory alloys embedded within the control surface. The shape memory alloys contract when heated via an applied electric current and elongate when cooled, i.e., the electric current is removed. The resulting control surface is capable of generating a curved control surface without any electro/mechanical or hydraulic control systems.
申请公布号 US5114104(A) 申请公布日期 1992.05.19
申请号 US19900591532 申请日期 1990.10.01
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 CINCOTTA, MANUEL;NADOLINK, RICHARD H.
分类号 B64C3/48 主分类号 B64C3/48
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