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公开(公告)号:WO2008060717A3
公开(公告)日:2008-11-13
申请号:PCT/US2007071822
申请日:2007-06-21
Applicant: INFORMATION SYSTEMS LAB INC
Inventor: BOSCHMA JAMES H JR , MCDANIEL WILLIAM DOUGLAS , MCNABB MICHAEL , RYDER MICHAEL , SULLIVAN CALLUM R , TIERNEY GLENN MARTIN , VAN STAAGEN PETER K
IPC: B64B1/40
CPC classification number: G09F21/06
Abstract: A device for deploying an aerostat includes a cylindrical shaped container having an open end and a closed end and a center tube axially oriented in the container. A tapered disc is mounted for axial movement on the center tube, and it has a taper of increasing diameter in an axial direction from the closed end toward the open end of the container. In its operation, the tapered disc is held in a first position while a portion of the aerostat is loaded into the container. It is then moved to a second position wherein the tapered disc holds the loaded portion of the aerostat in the container. Thereafter, the disc is moved to a release position wherein the disc directs deployment of the aerostat from the container.
Abstract translation: 用于部署空气净化器的装置包括具有开口端和封闭端的圆柱形容器和在容器中轴向定向的中心管。 锥形盘被安装成用于在中心管上轴向运动,并且其具有从容器的封闭端朝向开口端的轴向方向上增加的直径的锥形。 在其操作中,锥形盘保持在第一位置,同时一部分空气稳定器被装载到容器中。 然后将其移动到第二位置,其中锥形盘保持容器中的空气稳定器的装载部分。 此后,盘被移动到释放位置,其中盘指示空气调节器从容器的展开。
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公开(公告)号:WO2007021361A3
公开(公告)日:2009-04-16
申请号:PCT/US2006023376
申请日:2006-06-16
Applicant: INFORMATION SYSTEMS LAB INC
Inventor: TIERNEY GLENN MARTIN
CPC classification number: B64C39/005 , B64B1/30 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102 , B64C2201/104 , B64C2201/165
Abstract: A system and method for moving an aerial vehicle along a flight path includes rotatable hubs mounted on opposite sides of the vehicle. Elongated airfoils are mounted on the hubs parallel to a common hub axis for rotation about the hub axis on a blade path. Each airfoil defines a chord line and the system includes a gear assembly changeable, during hub rotation, between a first modality wherein airfoil chord lines remain tangential to the blade path (curtate flight), and a second modality wherein airfoil chord lines remain parallel to the flight path of the vehicle (prolate flight). Also, rotation of the hub can be stopped and the airfoils used for fixed wing flight.
Abstract translation: 沿着飞行路径移动飞行器的系统和方法包括安装在车辆的相对侧上的可旋转轮毂。 细长的翼型件平行于公共轮毂轴线安装在轮毂上,以便在叶片路径上围绕轮毂轴线旋转。 每个翼型件限定弦线,并且该系统包括齿轮组件,在轮毂旋转期间,在第一形式之间,其中翼型弦线保持与叶片路径相切的第一模态(压头飞行),以及第二模态,其中翼型弦线保持平行于 车辆的飞行路线(长跑)。 此外,轮毂的旋转可以停止,翼型件用于固定翼飞行。
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