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    • 13. 发明授权
    • Packaging for fragile items
    • US06840381B2
    • 2005-01-11
    • US10210408
    • 2002-07-31
    • Thomas Stephens
    • Thomas Stephens
    • B65D5/50B65D25/10B65D81/02
    • B65D25/107B65D5/503
    • One or more unique hinges are provided within panels of a fragility packaging article for use in retaining one or more fragile articles within a container (e.g., a corrugated box). The unique hinges provide predicted deformation paths that assist in protecting one or more fragile items stored in the container. One of the unique hinges is a diamond shaped hinge that provides at least two predicted deformation paths. Other unique hinges of the present invention includes a gusset hinge, a step hinge, and a v-hinge, each of which provides at least one predicted deformation path. The predicted deformation paths reduce permanent deformation and provide for improved overall cushioning, thereby increasing protection of fragile items and significantly reducing damage that may occur to the fragile items. The unique hinges of the present invention also improve the cosmetic appearance of a fragility packing article because a majority of crushing occurs along the unique hinges, preventing random unsightly crush points from occurring throughout the packaging article.
    • 14. 发明授权
    • Reusable and recyclable packaging for shock and static sensitive objects
    • 可重复使用和可回收的包装,用于冲击和静电敏感物体
    • US5249685A
    • 1993-10-05
    • US916194
    • 1992-07-17
    • Thomas Stephens
    • Thomas Stephens
    • B65D81/02B65D85/30
    • B65D81/02Y02W30/807
    • The invention provides a dissembleable and reusable package is provided for static, debris and shock sensitive objects. The package comprises a folding box of single piece static dissipative corrugated plastic interlocking configuration. The box has an interlocking bottom, an open top and two pairs of parallel opposite sides. A shock absorbing pad structure fits against the central portions of the sides. The pad structure is a solid self-skinning plastic foam which is static dissipative. It is detachably attachable against the sides utilizing fasteners. A shock absorbing plastic bottom pad fits inside of the box atop its bottom. An open top static dissipative plastic bag fits within the box atop the shock absorbing bottom pad and substantially lines the box. A sensitive object holding structure includes first and second pluralities of static dissipative corrugated plastic walls which interlock with one another, the pluralities of walls being mutually perpendicular. The walls are releasably interlockable with one another and, when interlocked, define a plurality of cavities, each of which is adapted to closely hold one of the sensitive objects. The sensitive object holding structure is of a size to fit within the bag and, when the bag is pushed within the box, is of a size such that the respective opposite ends of the walls are closely adjacent the interiors of the sides of the box.
    • 本发明提供了一种可拆卸且可重复使用的包装,用于静电,碎片和冲击敏感物体。 该包装包括单件静电消散波纹塑料互锁配置的折叠盒。 该箱具有互锁的底部,敞开的顶部和两对平行的相对侧。 减震垫结构与侧面的中心部分相配合。 垫结构是固体自剥皮塑料泡沫,它是静电耗散的。 它使用紧固件可拆卸地抵靠两侧。 吸震塑料底垫适合底部顶部的盒子内部。 一个开放的顶部静电消散塑料袋装在吸震底垫顶部的盒子中,并且基本上排成一排。 敏感物体保持结构包括彼此互锁的第一和第二多个静电消散波纹状塑料壁,多个壁相互垂直。 壁可释放地彼此互锁,并且当互锁时限定多个空腔,每个空腔适于紧密地保持敏感物体之一。 敏感物体保持结构具有适合于袋内的尺寸,并且当袋被推入箱内时,其尺寸使得壁的相应相对端紧密靠近箱体侧面的内部。
    • 20. 发明申请
    • Rotary wing aircraft
    • 旋翼飞机
    • US20070164146A1
    • 2007-07-19
    • US11411540
    • 2006-04-26
    • Thomas Stephens
    • Thomas Stephens
    • B64C27/26
    • B64C39/008
    • A rotary wing aircraft is provided with longitudinally oriented counter-rotating rotors with circumferentially spaced variable pitch rotor blades connected to rotatable support rings mounted on the aircraft fuselage. Rotor downwash may be guided laterally and longitudinally by respective sets of moveable guide vanes. Propulsion may be obtained by an engine providing thrust and power take-off for driving the rotors. An auxiliary or second engine may be drivingly connected to the rotors. One embodiment includes rotors with lift or blade pitch angle control mechanism for changing the resultant lift forces for providing aircraft lateral movement and movement about a yaw axis. A wind driven power turbine includes a similar pitch angle control mechanism.
    • 旋翼飞机设置有纵向定向的反向旋转转子,其具有连接到安装在飞行器机身上的可旋转支撑环的周向间隔可变桨距转子叶片。 转子下洗可以由相应的可移动导向叶片横向和纵向引导。 可以通过提供用于驱动转子的推力和动力输出的发动机获得推进。 辅助或第二发动机可以驱动地连接到转子。 一个实施例包括具有提升或叶片俯仰角控制机构的转子,用于改变所产生的升力以提供飞行器侧向运动和围绕偏转轴的运动。 风力动力涡轮机包括相似的俯仰角控制机构。