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21. 发明申请

US20100003889A1 FLEXIBLE MECHANICAL APPENDAGE 审中-公开
标题翻译：柔性机械附件
公开(公告)号：US20100003889A1
公开(公告)日：2010-01-07
申请号：US12498753
申请日：2009-07-07
申请人： Peter Greenley , Nick Grisolia
发明人： Peter Greenley , Nick Grisolia
IPC分类号： A63H3/20
CPC分类号： A63H31/06 , A63H3/46 , A63H31/10
摘要： A flexible mechanical appendage is provided to include a predetermined length positioned between head and tail ends, and having two sides disposed along the length. Arms extending outwardly from both sides of the flexible spine, and having an aperture positioned through each arm. A cable extends along both sides of the flexible spine through each of the apertures and terminates about the tail end of the flexible spine. A pulley system is positioned about the head end and has a spool rotatably driven by a reciprocating motor. The spool has a fastener for securing the cable thereto, wherein when the pulley system rotates the spool in a single direction reeling on cable, one side of the flexible spine bends in an arc.
摘要翻译：提供灵活的机械附件以包括位于头端和尾端之间的预定长度，并且沿着长度设置有两侧。臂从柔性脊椎的两侧向外延伸，并且具有通过每个臂定位的孔。电缆沿着柔性脊柱的两侧延伸穿过每个孔，并且围绕柔性脊柱的尾端终止。皮带轮系统围绕头端定位，并具有由往复式马达旋转驱动的线轴。卷线轴具有用于将电缆固定到其上的紧固件，其中当滑轮系统沿单个方向旋转卷轴时，柔性脊柱的一侧弯曲成弧形。

22. 发明申请

US20080223994A1 MOVEABLE WINGS ON A FLYING/HOVERING VEHICLE 有权
标题翻译：飞行/悬挂车辆上的可移动的翅膀
公开(公告)号：US20080223994A1
公开(公告)日：2008-09-18
申请号：US12045207
申请日：2008-03-10
申请人： Peter Greenley
发明人： Peter Greenley
IPC分类号： B64C39/00
CPC分类号： A63H27/02 , A63H30/04 , B64C2201/088
摘要： The present invention includes an embodiment defined as a flying vehicle having a pair of wings and a transition assembly partially housed within each of the pair of wings. The transition assembly has ends rotatable with respect to each other and separately secured to the wing in which the end is housed. The transition assembly has a first position defined as having each wing positioned at an angle offset from a substantial horizontal orientation and oriented in an opposite direction from the other wing. When the transition assembly is in the first position the vehicle spins and will fly in a substantially hovering vertical orientation. The transition assembly has a second position defined as having each wing positioned in a substantial horizontal position. When the transition assembly is in the second position the vehicle will fly in a substantially horizontal orientation.
摘要翻译：本发明包括被定义为具有一对翼的飞行器的实施例和部分地容纳在所述一对翼中的每一翼内的过渡组件。过渡组件具有相对于彼此可旋转的端部，并且单独地固定到其中容纳端部的翼部。过渡组件具有第一位置，该第一位置被定义为使每个翼定位成与实质水平取向偏移的角度并且朝向与另一翼相反的方向定向。当过渡组件处于第一位置时，车辆旋转并将以大致悬停的垂直方向飞行。过渡组件具有第二位置，该第二位置被定义为使每个翼位于基本水平位置。当过渡组件处于第二位置时，车辆将以基本上水平的方向飞行。

23. 发明授权

US08574022B2 Toy vehicle 有权
标题翻译：玩具车
公开(公告)号：US08574022B2
公开(公告)日：2013-11-05
申请号：US13247204
申请日：2011-09-28
申请人： Nick Grisolia , Peter Greenley , Gerry Dean Cody, Jr. , Chan Hok Yat
发明人： Nick Grisolia , Peter Greenley , Gerry Dean Cody, Jr. , Chan Hok Yat
IPC分类号： A63H17/00
CPC分类号： A63H17/262 , A63H17/004
摘要： In one embodiment there is provided a toy car that includes four wheels which have a weight that is at least 40%, 50%, 70% or 80% of the total weight of the car. In another aspect each wheel has a center point, with a combined weight such that a horizontally planar center of gravity defined by the car and measured from a lowest point on an outer edge of the four wheels towards a center of the body is positioned substantially about the center point of the four wheels. In either embodiment, the body may include an upper outer portion and the upper outer portion includes a finger detent.
摘要翻译：在一个实施例中，提供了一种玩具车，其包括四个车轮，其重量为轿厢总重量的至少40％，50％，70％或80％。在另一方面，每个车轮具有中心点，具有组合的重量，使得由轿厢限定的水平平面重心从四个车轮的外边缘上的最低点朝向身体的中心测量，其基本上围绕四轮的中心点。在任一实施例中，主体可以包括上部外部部分，并且上部外部部分包括手指卡爪。

24. 发明授权

US08382547B2 Toy projectile and launcher 有权
标题翻译：玩具射弹和发射器
公开(公告)号：US08382547B2
公开(公告)日：2013-02-26
申请号：US12941532
申请日：2010-11-08
申请人： Nick Grisolia , Peter Greenley , John Vanderbeek
发明人： Nick Grisolia , Peter Greenley , John Vanderbeek
IPC分类号： A63H27/14
CPC分类号： A63H33/16 , A63H27/007 , A63H27/02 , A63H27/14 , A63H33/18
摘要： A projectile and a compact carrying and launching case in combination. The projectile includes foldable wings which when unfolded resemble a plane. The compact carrying and launching case includes a two piece housing that is pivotally attached to each other about a hinge/launching mechanism. When closed, the two piece housing encloses the plane in its folded position. When opened, the hinge/launching mechanism can be pulled to a cocked position and then released forcibly moves the projectile such that it releases from the launching mechanism and is capable of flying.
摘要翻译：组合弹丸和小型携带和发射箱。抛射体包括可折叠的翼，当展开类似于飞机时。紧凑的携带和发射箱包括两个壳体，其围绕铰链/发射机构彼此枢转地附接。当关闭时，两件式的外壳将平面包围在折叠位置。当打开时，铰链/发射机构可以被拉到一个俯冲的位置，然后释放强制地移动射弹，使其从发射机构释放并且能够飞行。

25. 发明申请

US20120115391A1 TOY PROJECTILE AND LAUNCHER 有权
标题翻译：玩具项目和开奖
公开(公告)号：US20120115391A1
公开(公告)日：2012-05-10
申请号：US12941532
申请日：2010-11-08
申请人： Nick Grisolia , Peter Greenley , Jon Vanderbeek
发明人： Nick Grisolia , Peter Greenley , Jon Vanderbeek
IPC分类号： A63H27/14
CPC分类号： A63H33/16 , A63H27/007 , A63H27/02 , A63H27/14 , A63H33/18
摘要： A projectile and a compact carrying and launching case in combination. The projectile includes foldable wings which when unfolded resemble a plane. The compact carrying and launching case includes a two piece housing that is pivotally attached to each other about a hinge/launching mechanism. When closed, the two piece housing encloses the plane in its folded position. When opened, the hinge/launching mechanism can be pulled to a cocked position and then released forcibly moves the projectile such that it releases from the launching mechanism and is capable of flying.
摘要翻译：组合弹丸和小型携带和发射箱。抛射体包括可折叠的翼，当展开类似于飞机时。紧凑的携带和发射箱包括两个壳体，其围绕铰链/发射机构彼此枢转地附接。当关闭时，两件式的外壳将平面包围在折叠位置。当打开时，铰链/发射机构可以被拉到一个俯冲的位置，然后释放强制地移动射弹，使其从发射机构释放并且能够飞行。

26. 发明授权

US08142254B1 Toy vehicle 有权
标题翻译：玩具车
公开(公告)号：US08142254B1
公开(公告)日：2012-03-27
申请号：US12548026
申请日：2009-08-26
申请人： Peter Greenley , Nick Grisolia
发明人： Peter Greenley , Nick Grisolia
IPC分类号： A63H17/36 , A63H17/00
CPC分类号： A63H17/262 , A63H29/22
摘要： A vehicle having a chassis and motor. An electronic controller and receiver for receiving control signals from a remote control. A pair of ground-engaging front and rear wheels mounted to a front and rear portions of the chassis, and being freely rotatably mounted to the chassis. A ground-engaging center drive wheel operably coupled to the drive motor, the center drive wheel being mounted on a rotatable platform positioned on the chassis within a perimeter defined by the front and rear wheels, the rotatable platform rotating with respect to the chassis to allow the central drive wheel to steer the vehicle in different directions, the central drive wheel having a coefficient of friction higher than the front and rear wheels to aid in driving the vehicle in different direction.
摘要翻译：具有底盘和电机的车辆。一种用于从遥控器接收控制信号的电子控制器和接收器。一对地面接合的前轮和后轮安装到底盘的前部和后部，并且可自由旋转地安装在底盘上。可操作地联接到驱动马达的接地中心驱动轮，所述中心驱动轮安装在位于由所述前轮和后轮限定的周边内的所述底盘上的可旋转平台上，所述可旋转平台相对于所述底盘旋转以允许所述中央驱动轮以不同方向转向所述车辆，所述中央驱动轮的摩擦系数高于前轮和后轮，以帮助车辆沿不同方向驾驶。

27. 发明授权

US07997526B2 Moveable wings on a flying/hovering vehicle 有权
标题翻译：飞行/悬停车辆上的可动翼
公开(公告)号：US07997526B2
公开(公告)日：2011-08-16
申请号：US12045207
申请日：2008-03-10
申请人： Peter Greenley
发明人： Peter Greenley
IPC分类号： B64C27/22 , B64C15/12 , B64C3/38 , A63H27/127
CPC分类号： A63H27/02 , A63H30/04 , B64C2201/088
摘要： The present invention includes an embodiment defined as a flying vehicle having a pair of wings and a transition assembly partially housed within each of the pair of wings. The transition assembly has ends rotatable with respect to each other and separately secured to the wing in which the end is housed. The transition assembly has a first position defined as having each wing positioned at an angle offset from a substantial horizontal orientation and oriented in an opposite direction from the other wing. When the transition assembly is in the first position the vehicle spins and will fly in a substantially hovering vertical orientation. The transition assembly has a second position defined as having each wing positioned in a substantial horizontal position. When the transition assembly is in the second position the vehicle will fly in a substantially horizontal orientation.
摘要翻译：本发明包括被定义为具有一对翼的飞行器的实施例和部分地容纳在所述一对翼中的每一翼内的过渡组件。过渡组件具有相对于彼此可旋转的端部，并且单独地固定到其中容纳端部的翼部。过渡组件具有第一位置，该第一位置被定义为使每个翼定位成与实质水平取向偏离的角度并且朝向与另一翼相反的方向定向。当过渡组件处于第一位置时，车辆旋转并将以大致悬停的垂直方向飞行。过渡组件具有第二位置，其被定义为使每个翼定位在基本水平位置。当过渡组件处于第二位置时，车辆将以基本上水平的方向飞行。

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