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公开(公告)号：US10518865B2
公开(公告)日：2019-12-31
申请号：US15593241
申请日：2017-05-11
摘要： In one embodiment, a horizontal stabilizer comprises an airfoil structure configured to be mounted to an aircraft at a horizontal orientation. The airfoil structure comprises a leading edge, a trailing edge, a top surface, and a bottom surface. Moreover, the airfoil structure is cambered, wherein a camber of the airfoil structure forms a concave slope on the top surface and a convex slope on the bottom surface.
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公开(公告)号：US20180327079A1
公开(公告)日：2018-11-15
申请号：US15593304
申请日：2017-05-11
CPC分类号： B64C5/06 , B64C27/82 , B64C2027/8272 , B64C2027/8281
摘要： In one embodiment, a vertical stabilizer comprises an airfoil structure configured to be mounted to an aircraft at a vertical orientation. The airfoil structure comprises a leading edge and a trailing edge, wherein the trailing edge is configured to form a blunt shaped edge. The airfoil structure further comprises a root end and a tip end, wherein the airfoil structure is tapered from the root end to the tip end. The airfoil structure is also cambered. Finally, the airfoil structure is further configured to be mounted with a rotor, and is also further configured to house one or more internal components associated with the aircraft.
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公开(公告)号：US20180327078A1
公开(公告)日：2018-11-15
申请号：US15593241
申请日：2017-05-11
CPC分类号： B64C5/02 , B64C27/06 , B64C27/82 , B64C2003/142 , B64C2027/8272 , B64C2027/8281
摘要： In one embodiment, a horizontal stabilizer comprises an airfoil structure configured to be mounted to an aircraft at a horizontal orientation. The airfoil structure comprises a leading edge, a trailing edge, a top surface, and a bottom surface. Moreover, the airfoil structure is cambered, wherein a camber of the airfoil structure forms a concave slope on the top surface and a convex slope on the bottom surface.
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