发明名称 Shape memory alloy actuated adaptive exhaust nozzle for jet engine
摘要 The proposed adaptive exhaust nozzle features an innovative use of the shape memory alloy (SMA) actuators for actively control of the opening area of the exhaust nozzle for jet engines. The SMA actuators remotely control the opening area of the exhaust nozzle through a set of mechanism. An important advantage of using SMA actuators is the reduction of weight of the actuator system for variable area exhaust nozzle. Another advantage is that the SMA actuator can be activated using the heat from the exhaust and eliminate the need of other energy source. A prototype has been designed and fabricated. The functionality of the proposed SMA actuated adaptive exhaust nozzle is verified in the open-loop tests.
申请公布号 US8245516(B2) 申请公布日期 2012.08.21
申请号 US20090539242 申请日期 2009.08.11
申请人 SONG GANGBING;MA NING;UNIVERSITY OF HOUSTON 发明人 SONG GANGBING;MA NING
分类号 F02K1/00;B05B12/00;B63H11/10 主分类号 F02K1/00
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