公开(公告)号：US4860970A

公开(公告)日：1989-08-29

申请号：US935733

申请日：1986-11-28

Applicant: Auro Roselli

Inventor： Auro Roselli

IPC: B64C31/036

CPC classification number: B64C31/036 ,  Y10S244/90 ,  Y10S244/902

Abstract: An aircraft includes a nonrigid dynamically inflated airfoil wing which carries an operator. The operator is suspended by a plurality of shrouds which interconnect the wing to a control stick. The control stick position is varied to change the angle of attack of the wing. A transverse control bar is connected to the wing tips for direction control. The center of gravity of the total aircraft is rearward of the center of lift. The wing includes air intake orifices at its leading edge and at least one trailing edge exhaust aperture for inflation by airspeed relative to the wing. A spanwise tubular plenum may be employed for air flow control through the wing.

Abstract translation: 一架飞机包括一个非刚性的动态充气翼型机翼，它运送操作员。 操作者被将翅片连接到控制棒上的多个护罩悬挂。 控制杆位置是变化的，以改变机翼的迎角。 横向控制杆连接到翼尖以进行方向控制。 总飞机的重心位于电梯中心的后方。 机翼包括在其前缘的进气孔和至少一个后缘排气孔，用于相对于机翼的空速进行充气。 可以采用翼展式管状增压室，用于通过机翼进行气流控制。

公开(公告)号：US4261534A

公开(公告)日：1981-04-14

申请号：US951080

申请日：1978-10-13

Applicant: Auro Roselli

Inventor： Auro Roselli

IPC: B64C1/34 ,  B64C3/30 ,  B64C39/00 ,  B64C33/00 ,  B64D1/04

CPC classification number: B64C3/30 ,  B64C1/34 ,  B64C39/00 ,  B64B2201/00

Abstract: An aircraft is constructed of an airfoil shaped inflated involucrum of lightweight gas-impervious plastic film. The airfoil is maneuverable to attain forward self-propulsion upon ascent as well as descent. The gases contained in the involucrum are heated by solar radiation to reduce craft density with the upper surface of the airfoil being translucent and the lower surface of the airfoil interior mirrored for concentration of the radiant energy upon an interior cylindrical black spar. A honeycomb reradiation barrier is provided beneath the translucent surface. In one embodiment a large volume involucrum is changeable in camber to maximize forward propulsion. The craft may be utilized to suspend a large fog broom for the purpose of condensation of water vapor. In a further embodiment a manpowered inflatable craft is formed with a flexible longitudinal medial fold which separates the airfoil into wing segments. Each segment includes a passive trailing zone. When the wing segments are oscillated about the medial fold, the craft is propelled by ciliary thrust.

Abstract translation: 一架飞机是由一个轻型不透气塑料薄膜的翼型充气基座构成的。 机翼可以在上升和下降时获得自主推进。 包含在叶片中的气体被太阳辐射加热以降低机翼密度，翼型件的上表面是半透明的，并且翼型件内部的下表面被镜像以将辐射能集中在内部圆柱形黑色翼梁上。 在半透明表面之下提供蜂窝再辐射屏障。 在一个实施例中，大的体积内壁可以在外倾角变化以最大化向前推进。 为了冷凝水蒸气，该工艺可用于悬挂大型扫帚。 在另一个实施例中，人力充气的可飞行艇形成有将翼型件分成翼段的柔性纵向内侧折叠。 每个段包括一个被动尾随区。 当翼段围绕内侧折叠振荡时，飞行物被睫毛推动推动。