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91. 发明申请

US20080076320A1 Toy Helicopter 有权
标题翻译：玩具直升机
公开(公告)号：US20080076320A1
公开(公告)日：2008-03-27
申请号：US11953826
申请日：2007-12-10
申请人： Alexander Jozef Van De Rostyne
发明人： Alexander Jozef Van De Rostyne
IPC分类号： A63H27/133
CPC分类号： A63H27/12
摘要： A helicopter has a main rotor with propeller blades which is driven by a rotor shaft and which is hinge-mounted to this rotor shaft. The angle between the surface of rotation of the main rotor and the rotor shaft may vary. A swinging manner on an oscillatory shaft is essentially transverse to the rotor shaft of the main rotor and is directed transversally to the longitudinal axis of the vanes. The main rotor and the auxiliary rotor are connected to each other by a mechanical link. The swinging motions of the auxiliary rotor controls the angle of incidence (A) of at least one of the propeller blades of the main rotor. There are wings from the body and a stabilizer at the tail.
摘要翻译：直升机具有主转子，其具有由转子轴驱动的螺旋桨叶片，并且铰链安装在该转子轴上。主转子和转子轴的旋转表面之间的角度可以变化。振荡轴上的摆动方式基本上横向于主转子的转子轴，横向于叶片的纵向轴线。主转子和辅助转子通过机械连接相互连接。辅助转子的摆动运动控制主转子至少一个螺旋桨叶片的入射角（A）。身上有翅膀和尾巴的稳定器。

92. 发明申请

US20070221781A1 HELICOPTER 有权
标题翻译：直升机
公开(公告)号：US20070221781A1
公开(公告)日：2007-09-27
申请号：US11754752
申请日：2007-06-14
申请人： Alexander Van de Rostyne
发明人： Alexander Van de Rostyne
IPC分类号： B64C27/52
CPC分类号： A63H27/12
摘要： A helicopter has a main rotor with propeller blades which is driven by a rotor shaft and which is hinge-mounted to this rotor shaft. The angle between the surface of rotation of the main rotor and the rotor may vary. A swinging manner on an oscillatory shaft is essentially transverse to the rotor shaft of the main rotor and is directed transversally to the longitudinal axis of the vanes. The main rotor and the auxiliary rotor are connected to each other by a mechanical link. The swinging motions of the auxiliary rotor controls the angle of incidence (A) of at least one of the propeller blades of the main rotor. There are wings from the body and a stabilizer at the tail.
摘要翻译：直升机具有主转子，其具有由转子轴驱动的螺旋桨叶片，并且铰链安装在该转子轴上。主转子和转子的旋转表面之间的角度可以变化。振荡轴上的摆动方式基本上横向于主转子的转子轴，横向于叶片的纵向轴线。主转子和辅助转子通过机械连接相互连接。辅助转子的摆动运动控制主转子至少一个螺旋桨叶片的入射角（A）。身上有翅膀和尾巴的稳定器。

93. 发明授权

US07274868B2 Method and apparatus for creating aerial panoramic photography 失效
标题翻译：用于创建空中全景摄影的方法和设备
公开(公告)号：US07274868B2
公开(公告)日：2007-09-25
申请号：US11253338
申请日：2005-10-18
申请人： Mark Segal , Jeff Jones
发明人： Mark Segal , Jeff Jones
IPC分类号： G03B39/00
CPC分类号： G03B15/006 , A63H27/12 , A63H30/04 , G03B37/00
摘要： An aerial photography apparatus that comprises a remote controlled piloted aircraft, a platform, a camera, and a remote wireless transmitter for operating and controlling the apparatus. The remote controlled piloted aircraft is attached to the top side of the platform. The camera is attached to the bottom side of the platform using a rigid member having a rotatable joint. The remote controlled piloted aircraft lifts and moves the apparatus to a desired location at a specific altitude above a particular property where the panoramic aerial photograph is to be taken. Depending upon the wind forces exerted upon the remote controlled piloted aircraft and the resulting orientation of the aircraft to maintain the camera at the desired location, the rotatable joint enables the gravitational weight of the camera to naturally gravitate to a vertical orientation or position relative to the ground. Alternatively, cushions in the platform or a suspension system may be used to achieve this position for the camera. A counterbalance weight is provided on the camera to counter the weight of the lens for maintaining the camera in a level balance while rotating through the three hundred and sixty degree rotation when creating the desired panoramic aerial photograph
摘要翻译：一种航空摄影装置，包括遥控驾驶飞机，平台，相机和用于操作和控制该装置的远程无线发射机。遥控飞行员被安装在平台的顶部。相机使用具有可旋转接头的刚性构件附接到平台的底侧。遥控驾驶飞行器将设备升降并移动到要采集全景航空照片的特定属性上方特定高度的所需位置。根据施加在遥控驾驶飞行器上的风力和飞机维持摄像机到达所需位置的方位，可旋转接头可使照相机的重力自然地垂直于垂直方位或相对于地面。或者，可以使用平台或悬架系统中的垫子来实现相机的该位置。在相机上提供平衡重量以抵抗透镜的重量，以在创建期望的全景航空照片时旋转360度旋转，以保持相机处于水平平衡

94. 发明申请

US20070164148A1 HELICOPTER 审中-公开
标题翻译：直升机
公开(公告)号：US20070164148A1
公开(公告)日：2007-07-19
申请号：US11462177
申请日：2006-08-03
申请人： Alexander Jozef Magdalena Van De Rostyne
发明人： Alexander Jozef Magdalena Van De Rostyne
IPC分类号： B64C27/82
CPC分类号： B64C27/43 , A63H27/06 , A63H27/12 , A63H30/04 , B64C27/82
摘要： A helicopter has a main rotor with propeller blades which is driven by a rotor shaft and which is hinge-mounted to this rotor shaft. The angle between the surface of rotation of the main rotor and the rotor shaft may vary. A swinging manner on an oscillatory shaft is essentially transverse to the rotor shaft of the main rotor and is directed transversally to the longitudinal axis of the vanes. The main rotor and the auxiliary rotor are connected to each other by a mechanical link. The swinging motions of the auxiliary rotor controls the angle of incidence (A) of at least one of the propeller blades of the main rotor.
摘要翻译：直升机具有主转子，其具有由转子轴驱动的螺旋桨叶片，并且铰链安装在该转子轴上。主转子和转子轴的旋转表面之间的角度可以变化。振荡轴上的摆动方式基本上横向于主转子的转子轴，横向于叶片的纵向轴线。主转子和辅助转子通过机械连接相互连接。辅助转子的摆动运动控制主转子至少一个螺旋桨叶片的入射角（A）。

95. 发明申请

US20060083501A1 Method and apparatus for creating aerial panoramic photography 失效
标题翻译：用于创建空中全景摄影的方法和设备
公开(公告)号：US20060083501A1
公开(公告)日：2006-04-20
申请号：US11253338
申请日：2005-10-18
申请人： Mark Segal , Jeff Jones
发明人： Mark Segal , Jeff Jones
IPC分类号： G03B39/00
CPC分类号： G03B15/006 , A63H27/12 , A63H30/04 , G03B37/00
摘要： An aerial photography apparatus that comprises a remote controlled piloted aircraft, a platform, a camera, and a remote wireless transmitter for operating and controlling the apparatus. The remote controlled piloted aircraft is attached to the top side of the platform. The camera is attached to the bottom side of the platform using a rigid member having a rotatable joint. The remote controlled piloted aircraft lifts and moves the apparatus to a desired location at a specific altitude above a particular property where the panoramic aerial photograph is to be taken. Depending upon the wind forces exerted upon the remote controlled piloted aircraft and the resulting orientation of the aircraft to maintain the camera at the desired location, the rotatable joint enables the gravitational weight of the camera to naturally gravitate to a vertical orientation or position relative to the ground. Alternatively, cushions in the platform or a suspension system may be used to achieve this position for the camera. A counterbalance weight is provided on the camera to counter the weight of the lens for maintaining the camera in a level balance while rotating through the three hundred and sixty degree rotation when creating the desired panoramic aerial photograph
摘要翻译：一种航空摄影装置，包括遥控驾驶飞机，平台，相机和用于操作和控制该装置的远程无线发射机。遥控飞行员被安装在平台的顶部。相机使用具有可旋转接头的刚性构件附接到平台的底侧。遥控驾驶飞行器将设备升降并移动到要采集全景航空照片的特定属性上方特定高度的所需位置。根据施加在遥控驾驶飞行器上的风力和飞机维持摄像机到达所需位置的方位，可旋转接头可使照相机的重力自然地垂直于垂直方位或相对于地面。或者，可以使用平台或悬架系统中的垫子来实现相机的该位置。在相机上提供平衡重量以抵抗透镜的重量，以在创建期望的全景航空照片时旋转360度旋转，以保持相机处于水平平衡

96. 发明授权

US06960112B2 Airfoil blade with cushioned edge for powered toy aircraft 有权
公开(公告)号：US06960112B2
公开(公告)日：2005-11-01
申请号：US10778369
申请日：2004-02-13
申请人： David Vincent Helmlinger , Gregory Gilbert Garneau , Lee Chun Wah , Chung Zhi Jie
发明人： David Vincent Helmlinger , Gregory Gilbert Garneau , Lee Chun Wah , Chung Zhi Jie
IPC分类号： A63H20060101 , A63H27/00 , A63H27/127 , A63H27/133
CPC分类号： A63H27/12
摘要： An airfoil blade in a powered toy aircraft has a body with a cushioned edge. The body has a first end adjoining a hub, a second opposing end, a forward edge, and an opposing trailing edge. The cushioned leading edge is attached mechanically to the body and extends along the forward edge so as to form a cushioned leading edge of the blade or along the second end to form a cushioned blade tip or both. The body is formed from a first resiliently flexible polymer plastic material. The cushioned edge is formed from a second noticeably softer material such as an elastomer.

97. 发明申请

US20040162001A1 Ornamental design for a flying toy 有权
标题翻译：飞行玩具的装饰设计
公开(公告)号：US20040162001A1
公开(公告)日：2004-08-19
申请号：US10647930
申请日：2003-08-26
发明人： Steven Davis
IPC分类号： A63H001/00
CPC分类号： A63H27/04 , A63H27/12 , A63H30/04 , A63H33/18
摘要： A rotating toy may then include a hub having a central axis and a lower portion; a plurality of counter rotating blades extending outwardly from the lower portion of the hub, the plurality of counter rotating blades having a tip connected to an outer ring; a single means for rotating the hub and blades sufficiently quickly to generate a major portion of the lift generated by the aircraft through the single rotating means; and the hub having an upper portion above the plurality of counter rotating blades and above the single rotating means such that the aircraft includes a center of gravity above the plurality of counter rotating blades to provide a self-stabilizing rotating toy. In furtherance thereto the single rotating means may be secured on the central axis and positioned below the counter rotating blades.
摘要翻译：然后，旋转玩具可以包括具有中心轴线和下部分的轮毂; 多个反向旋转叶片，其从所述轮毂的下部向外延伸，所述多个反转叶片具有连接到外圈的尖端; 用于使轮毂和叶片足够快地旋转以产生飞行器通过单个旋转装置产生的升力的主要部分的单个装置; 并且所述轮毂在所述多个反转叶片上方具有上部并且在所述单个旋转装置上方，使得所述飞行器在所述多个反向旋转叶片之上包括重心以提供自稳定旋转玩具。为了促进这一点，单个旋转装置可以固定在中心轴线上并且位于反转叶片下方。

98. 发明授权

US06599161B2 Airfoil launching system 失效
标题翻译：翼型发射系统
公开(公告)号：US06599161B2
公开(公告)日：2003-07-29
申请号：US10000274
申请日：2001-11-02
申请人： John W. Hunter
发明人： John W. Hunter
IPC分类号： A63H27127
CPC分类号： F41B3/02 , A63H27/12 , A63H27/14
摘要： An airfoil launching system having a rod with a structure attached to a first end of the rod. A pusher holds a ring airfoil and has a sufficient coefficient of friction that the ring airfoil will generally rotate with the pusher and is rotatably and slidably mounted on the rod. Propulsive force is provided by resilient bands connected to the structure outward from the rod and to the pusher outward from the central aperture of the pusher. A string guide is rotatably attached to the rod and has apertures through which generally non-resilient cords, the first ends of which are attached to the pusher outward from the central aperture, pass. The second ends of the generally non-resilient cords are connected to each other, preferably with a pliable grip.
摘要翻译：一种翼型发射系统，其具有杆，该杆具有连接到杆的第一端的结构。推动器保持环形翼片并且具有足够的摩擦系数，使得环形翼片通常将与推动器一起旋转并且可旋转并可滑动地安装在杆上。推进力由从杆的外部连接到结构的弹性带和从推动器的中心孔向外推动的推动器提供。线引导件可旋转地附接到杆上并具有孔，通孔将第一端附接到推动器上的大致无弹性的帘线通过。通常非弹性帘线的第二端彼此连接，最好用柔软的手柄连接。

99. 发明申请

US20030096552A1 Modular and adjustable autorotative flyer 审中-公开
标题翻译：模块化和可调式自动传单
公开(公告)号：US20030096552A1
公开(公告)日：2003-05-22
申请号：US10267616
申请日：2002-10-08
发明人： William Ernest Nicholson
IPC分类号： A63H027/00
CPC分类号： A63H27/00 , A63H27/12
摘要： An apparatus is disclosed for a modular and adjustable autorotative flying toy comprising: a planar, quasi tear-drop shaped wing having a substantially linear leading edge; an elongated cylindrical spine adapted to receive the wing; and a root constructed from elastomeric material, adapted to receive the spine, one end of the spine is inserted into an aperture in the root and fixed there by the root's elastomeric properties. The spine's cylindrical surface has a slit running parallel to its elongated axis from its distal end towards the root. The slit receives the linear leading edge of the wing, securing it relative to the spine and the root. The flight and rotational characteristics of the flyer may be adjusted by interchanging its components for alternative components that have different size, shape or weight; and by slidably adjusting the wing's position within the slit in the spine.
摘要翻译：公开了一种用于模块化和可调节自动飞行玩具的装置，包括：具有基本线性前缘的平面准泪液形翼; 适于接收机翼的细长圆柱形脊柱; 以及由弹性体材料构成的根部，其适于接收脊柱，脊柱的一端插入根部的孔中，并通过根部的弹性体固定在那里。脊柱的圆柱形表面具有从其远端朝向根平行于其细长轴线延伸的狭缝。狭缝接收翼的线性前缘，使其相对于脊柱和根固定。可以通过将具有不同尺寸，形状或重量的替代部件的组件相互交换来调整飞行物的飞行和旋转特性; 并且通过可滑动地调节机翼在脊椎缝隙内的位置。

100. 发明授权

US06550715B1 Miniature vertical takeoff and landing aircraft 失效
标题翻译：微型垂直起降飞机
公开(公告)号：US06550715B1
公开(公告)日：2003-04-22
申请号：US10005746
申请日：2001-12-07
申请人： John Reynolds , Eric P. Young , Joseph Wurts , Eric Knutson
发明人： John Reynolds , Eric P. Young , Joseph Wurts , Eric Knutson
IPC分类号： B64C2706
CPC分类号： B64C39/028 , A63H27/12 , B64C27/20 , B64C2201/027 , B64C2201/042 , B64C2201/108
摘要： A vertical takeoff and landing aircraft is disclosed that includes a support structure having a motor mounted vertically thereto, with the motor having a propeller for rotation in a horizontal plane. A power supply for the motor is mounted to the support structure below the motor and electrical coupled thereto. A plurality of fins are attached by their first end to the power and extending radially outward therefrom. Vertical posts have there first ends attached to the second end of the fins and extend upward to the plane of rotation of the propeller. A ring is mounted horizontally to the second ends of the plurality of vertical posts surrounding the propeller. The torque produced by the drag of fins as the aircraft rotates in the opposite direction reacting the torque of the propeller equal to the torque of the propeller necessary to achieve hover. The rotational inertia of aircraft is made equal to the rotational inertia of the propeller.
摘要翻译：公开了一种垂直起降飞机，其包括具有垂直安装的马达的支撑结构，电动机具有用于在水平面中旋转的螺旋桨。用于电动机的电源安装到电动机下方的电气耦合的支撑结构上。多个翅片通过其第一端附接到动力并从其径向向外延伸。垂直柱的第一端附接到翅片的第二端，并向上延伸到螺旋桨的旋转平面。环绕水平地安装在围绕螺旋桨的多个垂直柱的第二端。当飞机沿相反方向旋转时，翼片拖动产生的扭矩使螺旋桨的扭矩等于实现悬停所需螺旋桨的扭矩。使飞机的转动惯量等于螺旋桨的旋转惯量。

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