公开(公告)号：US20100243795A1

公开(公告)日：2010-09-30

申请号：US12675165

申请日：2008-08-29

申请人： William R McDonnell

发明人： William R McDonnell

IPC分类号： B64C39/10 ,  B64C3/00 ,  B64C17/10

CPC分类号： B64C3/10 ,  B64C30/00 ,  B64C39/10 ,  B64C2039/105 ,  Y02T50/12

摘要： An oblique wing aircraft (1) designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment (27) on one side of the wing and an aft swept wing segment (29) on the opposite side of the wing. A center oblique airfoil section (25) connects the forward and aft swept wing segments. The center oblique airfoil section has a larger chord near its centerline than the chords of either of the forward or aft swept wing segments. The chord of the center oblique airfoil section tapers down more rapidly than the forward or aft wing segments as the center oblique airfoil section extends outboard toward the forward and aft swept wings. The center oblique airfoil section is not shaped solely to function as a circular fairing to fill the gap between an oblique wing and a fuselage at different oblique wing angles, nor is it a second wing in an X wing configuration. Preferably, the aircraft is an all-wing aircraft.

摘要翻译： 斜翼飞机（1）设计用于减小表面积与体积比。 飞机具有斜翼，其包括在机翼的一侧上的向前扫掠翼段（27）和在翼的相对侧上的后扫掠翼段（29）。 中心斜翼部分（25）连接前掠翼部和后掠翼部。 中心斜翼型部分的中心线附近的弦杆比前方或后掠翼段的和弦更大。 中心倾斜翼型部分的和弦比前翼或后翼部分的下降更快，因为中心倾斜翼型部分朝向前后扫掠的翼部向外延伸。 中心斜翼型部分的形状不仅仅是作为圆形整流罩，以不同的倾斜翼角填充斜翼和机身之间的间隙，也不是X翼构型中的第二翼。 飞机最好是全翼飞机。

公开(公告)号：US08408490B2

公开(公告)日：2013-04-02

申请号：US12675165

申请日：2008-08-29

申请人： William R McDonnell

发明人： William R McDonnell

IPC分类号： B64C3/10

CPC分类号： B64C3/10 ,  B64C30/00 ,  B64C39/10 ,  B64C2039/105 ,  Y02T50/12

摘要： An oblique wing aircraft (1) designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment (27) on one side of the wing and an aft swept wing segment (29) on the opposite side of the wing. A center oblique airfoil section (25) connects the forward and aft swept wing segments. The center oblique airfoil section has a larger chord near its centerline than the chords of either of the forward or aft swept wing segments. The chord of the center oblique airfoil section tapers down more rapidly than the forward or aft wing segments as the center oblique airfoil section extends outboard toward the forward and aft swept wings. The center oblique airfoil section is not shaped solely to function as a circular fairing to fill the gap between an oblique wing and a fuselage at different oblique wing angles, nor is it a second wing in an X wing configuration. Preferably, the aircraft is an all-wing aircraft.

摘要翻译： 斜翼飞机（1）设计用于减小表面积与体积比。 飞机具有斜翼，其包括在机翼的一侧上的向前扫掠翼段（27）和在翼的相对侧上的后扫掠翼段（29）。 中心斜翼部分（25）连接前掠翼部和后掠翼部。 中心斜翼型部分的中心线附近的弦杆比前方或后掠翼段的和弦更大。 中心倾斜翼型部分的和弦比前翼或后翼部分的下降更快，因为中心倾斜翼型部分朝向前后扫掠的翼部向外延伸。 中心斜翼型部分的形状不仅仅是作为圆形整流罩，以不同的倾斜翼角填充斜翼和机身之间的间隙，也不是X翼构型中的第二翼。 飞机最好是全翼飞机。