发明名称 MORPHING AEROFOIL
摘要 A morphing aerofoil comprising: a leading edge; a trailing edge; and upper and lower surfaces extending between the leading and trailing edges. An upper thermal actuation member is provided proximate the upper surface; and a lower thermal actuation member is provided proximate the lower surface opposite the upper thermal actuator. The upper and lower thermal actuation members have different thermal expansion coefficients and are positioned such that they cause the trailing edge to deflect when they expand or contract by different amounts in response to a change in ambient temperature, thereby changing a camber of the aerofoil.
申请公布号 US2015122951(A1) 申请公布日期 2015.05.07
申请号 US201314397990 申请日期 2013.04.26
申请人 AIRBUS OPERATIONS LIMITED 发明人 Wood Norman
分类号 B64C3/44 主分类号 B64C3/44
代理机构 代理人
主权项 1. A morphing aerofoil comprising: a leading edge; a trailing edge; upper and lower surfaces extending between the leading and trailing edges; an upper thermal actuation member proximate the upper surface; and a lower thermal actuation member proximate the lower surface opposite the upper thermal actuator, wherein the upper and lower thermal actuation members have different thermal expansion coefficients and are positioned such that they cause the trailing edge to deflect when they expand or contract by different amounts in response to a change in ambient temperature, thereby changing a camber of the aerofoil.
地址 Bristol GB