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公开(公告)号：US5884863A
公开(公告)日：1999-03-23
申请号：US548771
申请日：1995-10-26
IPC分类号： B64C31/028 , B64C31/02
CPC分类号： B64C31/0285 , Y10S244/901
摘要： The deployable wing of the present invention comprises an internal structure having diverging leading edge spars attached to a keel spar and cross spars to form a delta wing configuration. This internal structure is enclosed within a volume defined by a fabric sail having an upper section, a lower section, and fabric ribs disposed therebetween. This fabric sail volume is internally pressurized through a ram air intake at the nose stagnation point. This deployable wing can be folded, extracted from an aircraft and deployed in the air.
摘要翻译： 本发明的可部署翼包括内部结构，其具有连接到龙骨翼梁上的分叉的前缘翼梁和交叉翼梁以形成三角翼构型。 该内部结构封闭在由具有上部，下部和布置在其间的织物肋条的织物帆布限定的体积内。 这种织物帆布体积在鼻部停滞点处通过压头进气口内部加压。 这种可部署的机翼可以折叠，从飞机上提取并部署在空中。
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公开(公告)号：US5878979A
公开(公告)日：1999-03-09
申请号：US552160
申请日：1995-11-02
IPC分类号： B64C31/028 , B64D17/80
CPC分类号： B64C31/0285 , B64D17/80
摘要： The deployable wing of the present invention comprises an internal structure having diverging leading edge spars attached to a keel spar and cross spars to form a delta wing configuration. This internal structure is enclosed within a volume defined by a fabric sail having an upper section and a lower section. This fabric sail volume is internally pressurized through a ram air intake at the nose stagnation point. This deployable wing can be folded closed, extracted from an aircraft, deployed in the air and landed with the aid of parachutes.
摘要翻译： 本发明的可部署翼包括内部结构，其具有连接到龙骨翼梁上的分叉的前缘翼梁和交叉翼梁以形成三角翼构型。 该内部结构封闭在由具有上部和下部的织物帆布限定的体积内。 这种织物帆布体积在鼻部停滞点处通过压头进气口内部加压。 这种可部署的机翼可以折叠封闭，从飞机上提取，部署在空中并借助降落伞降落。
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公开(公告)号：US5474257A
公开(公告)日：1995-12-12
申请号：US156322
申请日：1993-11-23
IPC分类号： B64C31/028 , B64C3/56
CPC分类号： B64C31/028 , Y10S244/901 , Y10S244/904
摘要： The deployable wing of the present invention comprises an internal structure having diverging leading edge spars attached to a keel spar and cross spars to form a delta wing configuration. This internal structure is enclosed within a volume defined by a fabric sail having an upper section, a lower section, and fabric ribs disposed therebetween. This fabric sail volume is internally pressurized through a ram air intake at the nose stagnation point. This deployable wing can be folded and deployed in the air.
摘要翻译： 本发明的可部署翼包括内部结构，其具有连接到龙骨翼梁上的分叉的前缘翼梁和交叉翼梁以形成三角翼构型。 该内部结构封闭在由具有上部，下部和布置在其间的织物肋条的织物帆布限定的体积内。 这种织物帆布体积在鼻部停滞点处通过压头进气口内部加压。 这种可部署的机翼可以折叠和部署在空中。
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公开(公告)号：US06283409B1
公开(公告)日：2001-09-04
申请号：US09420260
申请日：1999-10-18
申请人： Dennis Van Dam
发明人： Dennis Van Dam
IPC分类号： B64C356
CPC分类号： B64C31/028
摘要： The openings in the fabric ribs of a deployable wing made from fabric sail material is automatically closed by use of a zipper mounted adjacent each of the openings that is actuated by movement of the cross spars of the deployable wing which serves to prevent the airfoil surface to the wing to bulge and cause a drag to the deployable wing when in flight.
摘要翻译： 由织物帆布材料制成的可展开翼片的织物肋条中的开口通过使用安装在每个开口附近的拉链来自动关闭，该拉链由可展开翼片的十字形翼片的运动致动，用于防止翼面表面 机翼在飞行中凸起并造成可部署机翼的拖动。
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