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1. 发明授权

US6089940A Model airplane kit 失效
标题翻译：型号飞机套件
公开(公告)号：US6089940A
公开(公告)日：2000-07-18
申请号：US942378
申请日：1997-10-01
申请人： Rodney K. Farrar
发明人： Rodney K. Farrar
IPC分类号： A63H27/00 , A63H27/16 , A63H27/18 , B26F3/12
CPC分类号： A63H27/02 , A63H27/00 , A63H27/001 , B26F3/12
摘要： A model airplane, airplane kit, and method of making a model airplane. The kit of the present invention enables children and adults to easily make a well-flying model airplane using recycled plastic foam moldings such as polystyrene food trays well known as 10-S in the food packaging arts.
摘要翻译：模型飞机，飞机套件和制造模型飞机的方法。本发明的试剂盒使儿童和成年人能够使用回收的塑料泡沫塑料模制品（例如在食品包装领域中称为10-S的聚苯乙烯食品托盘）轻松制作飞行良好的模型飞机。

2. 发明授权

US5853312A Model airplane for scientific education and competition 失效
标题翻译：模型飞机用于科学教育和竞争
公开(公告)号：US5853312A
公开(公告)日：1998-12-29
申请号：US597276
申请日：1996-02-06
申请人： Danny H. Y. Li
发明人： Danny H. Y. Li
IPC分类号： A63H27/00 , A63H27/18
CPC分类号： A63H27/00
摘要： The present invention relates to an improved model airplane for purposes of scientific education and competition. Model airplanes in the prior art are either bad at flying, or do not look like real airplanes; and all are short of a collision prevention device. By means of some special positioning adapters for fixing the wing section firmly to the body and by adding a collision buffer piece to the nose, the model airplane according to the present invention is not only good at flying, but also safe and durable to use. The model airplane according to this invention is, therefore, best suitable for the above-mentioned purposes.
摘要翻译：本发明涉及一种用于科学教育和竞争的改进型飞机。现有技术中的模型飞机在飞行中不好，或者看起来不像真实的飞机; 并且都缺少防撞装置。通过一些特殊的定位适配器，用于将机翼部分牢固地固定在车身上，并且通过在鼻子上添加碰撞缓冲件，根据本发明的模型飞机不仅飞行良好，而且安全耐用。因此，根据本发明的模型飞机最适合于上述目的。

3. 发明授权

US4714444A Drink can glider 失效
标题翻译：喝可以滑翔
公开(公告)号：US4714444A
公开(公告)日：1987-12-22
申请号：US862265
申请日：1986-05-12
申请人： Robert D. Rendel
发明人： Robert D. Rendel
IPC分类号： A63H27/00 , B65D81/36 , A63H27/18
CPC分类号： B65D81/365 , A63H27/00
摘要： This invention is an unmanned aircraft which utilizes commonly available drink cans as a fuselage and central connecting point. The aircraft can be used with any pop top-type can, is easy to assemble without tools or adhesive materials, and gives above average performance relative to comparable sized craft. The wings are of break away type to prevent damage in landings or striking of other objects and the can fuselage which takes the brunt of landings can be readily replaced.
摘要翻译：本发明是一种无人驾驶飞机，它使用通常可用的饮料罐作为机身和中心连接点。该飞机可以与任何流行顶级罐一起使用，易于组装而不用工具或粘合剂材料，并且相对于相当尺寸的工艺提供了高于平均性能。机翼是脱离型的，以防止着陆或其他物体的撞击造成损坏，并且能够轻易更换首要的着陆能力的机身机身。

4. 发明授权

US4494940A Model aircraft 失效
标题翻译：模型飞机
公开(公告)号：US4494940A
公开(公告)日：1985-01-22
申请号：US369567
申请日：1982-04-19
申请人： Charles Gretz
发明人： Charles Gretz
IPC分类号： A63H27/00 , A63H27/18
CPC分类号： A63H27/02
摘要： A model aircraft, such as a glider, includes a clip for connecting separable wing members thereof to the fuselage. The clip has a resilient bridge portion and spaced depending limbs. The clip fits over an arch section of the fuselage with the limbs having a friction fit in openings in the wings, whereby the wings and fuselage are secured together. The wings may fit in a wing slot in the fuselage with inboard sections of the wings having recesses locating against tabs within the slot. The arch section of the fuselage may be recessed so that the clip when assembled is flush with adjacent surfaces of the fuselage, whereby the appearance and aerodynamic characteristics of the aircraft are unimpaired. The clip connection may allow for vertical hinging of the wings upon impact to absorb impact forces and prevent wing separation.
摘要翻译：诸如滑翔机的示范飞机包括用于将其可分离的翼构件连接到机身的夹子。夹子具有弹性桥接部分和间隔开的四肢。该夹子装配在机身的拱形部分上，其四肢具有与机翼中的开口中的摩擦配合，由此机翼和机身固定在一起。机翼可以装配在机身中的机翼槽中，机翼的内侧部分具有定位在槽内的突出部的凹部。机身的拱形部分可以是凹进的，使得组装时的夹子与机身的相邻表面齐平，从而飞机的外观和空气动力学特性不受损害。夹子连接可以允许在冲击时机翼的垂直铰接以吸收冲击力并防止机翼分离。

5. 发明授权

US4266366A Prefabricated airplane model kit 失效
标题翻译：预制飞机模型套件
公开(公告)号：US4266366A
公开(公告)日：1981-05-12
申请号：US2202
申请日：1979-01-09
申请人： Philippe Lapierre
发明人： Philippe Lapierre
IPC分类号： A63H27/18 , B65D81/36 , A63H27/00 , A63H27/02
CPC分类号： B65D81/365 , A63H27/02
摘要： An airplane model kit comprises one or more wings, integrally formed with temporary frames which are joined to the wings at their periphery, which frames are intended to avoid any deformation of the wings and are provided with imprints and lugs for easy and accurate positioning of the wing with respect to the fuselage or the rest of the model. The frames further comprise a planar surface for ensuring that the frame-wing assembly does not twist and for ensuring the accurate positioning of the different wings with respect to one another.
摘要翻译：飞机模型套件包括一个或多个翼片，其一体形成有临时框架，该临时框架在其周边处连接到翼片，该框架旨在避免翼的任何变形，并且设置有印记和凸耳，以便容易且准确地定位相对于机身或模型的其余部分。这些框架还包括一个平坦的表面，用于确保框架翼组件不扭曲并且用于确保不同翼片相对于彼此的准确定位。

6. 发明授权

US4233773A Attachments in model airplanes 失效
标题翻译：模型飞机附件
公开(公告)号：US4233773A
公开(公告)日：1980-11-18
申请号：US952114
申请日：1978-10-17
申请人： Robert S. Jones
发明人： Robert S. Jones
IPC分类号： A63H27/18
CPC分类号： A63H27/02
摘要： The present invention is directed to a positive removable mounting of a wing and, if desired, the tail assemblage. This attachment provides a spring biased mounting means at one side of the mounted member and one or two pins or dowels are inserted into receiving holes provided. The opposite side is brought to fixed hole portions and one or more fixed pins or dowels are placed in these holes. The wing or tail assembly is rearwardly moved with and by bias to retain the wing or tail in position until moved forwardly. This forward movement is produced by a crash or sudden stop or by the operator when he wishes to disassemble the craft.
摘要翻译：本发明涉及一种机翼的正面可拆卸安装，如果需要的话，还可以是尾部组合件。该附件在安装的构件的一侧提供弹簧偏压的安装装置，并且将一个或两个销或销钉插入到设置的接收孔中。将相对侧带到固定孔部分，并将一个或多个固定销或销钉放置在这些孔中。机翼或尾翼组件通过偏压向后移动以将机翼或尾部保持在适当位置，直到向前移动。这种向前的运动是由于碰撞或突然停止或操作人员在拆卸工艺时产生的。

7. 发明授权

US4202132A Hollow structural element 失效
标题翻译：空心结构件
公开(公告)号：US4202132A
公开(公告)日：1980-05-13
申请号：US913081
申请日：1978-06-06
申请人： Artur Fischer
发明人： Artur Fischer
IPC分类号： A63H27/18 , A63H33/06 , A63H33/08 , A63H33/00 , A63H27/00 , A63H33/10
CPC分类号： A63H33/06
摘要： A hollow structural element has a hollow member having a circumferential wall and a side wall which closes one of the axial ends of the circumferential wall, a cover member arranged to close the other end of the circumferential wall of the hollow member and connecting elements for connecting the structural element with other structural elements. The connecting elements include an undercut projection provided in the cover member and arranged for inserting into an undercut groove of another structural element, and an undercut lateral slot provided in the side wall of the hollow member and arranged for engaging with an undercut projection of a further structural element. The lateral slot has a first enlarged portion through which the projection of the further structural element can pass, and a second reduced portion extending from the first portion toward the axis of the circumferential wall and dimensioned so that the projection of the further structural element engages in the reduced portion.
摘要翻译：中空构件具有中空构件，该中空构件具有周壁和侧壁，该侧壁闭合周壁的轴向端部之一;盖构件，其设置成封闭中空构件的周壁的另一端和用于连接的连接元件结构元件与其他结构元件。连接元件包括设置在盖构件中并设置成插入到另一结构元件的底切槽中的底切突起和设置在中空构件的侧壁中的底切侧向槽，并且布置成与另外的底切突起接合结构元素。横向狭槽具有第一扩大部分，另外的结构元件的突出部可穿过该第一扩大部分，以及从第一部分朝向周向壁的轴线延伸的第二缩小部分，其尺寸使得其他结构元件的突出部接合缩小部分。

8. 发明授权

US07503826B2 Flying apparatus 有权
标题翻译：飞行器具
公开(公告)号：US07503826B2
公开(公告)日：2009-03-17
申请号：US11425971
申请日：2006-06-22
申请人： David Howard
发明人： David Howard
IPC分类号： A63H27/18 , A63H27/00
CPC分类号： A63H27/001
摘要： This invention provides a small lightweight glider that is hollow and made from a molded thin film material. Typically the glider is formed in the shape of a bird or a plane. The body of the glider comprises top half and a lower half, which form a hollow fuselage, a left wing and a right wing extending laterally from the fuselage. The glider also comprises a ballast weight, a stiffener, and optionally an interior skeleton. The interior of the glider is open to the outside atmosphere and requires no inflation.
摘要翻译：本发明提供一种小型轻型滑翔机，其是中空的并且由模制的薄膜材料制成。通常，滑翔机形成为鸟或飞机的形状。滑翔机的主体包括上半部和下半部，其形成中空的机身，左翼和从机身横向延伸的右翼。滑翔机还包括压载重量，加强件和任选的内部骨架。滑翔机的内部对外界气氛开放，不需要通风。

9. 发明申请

US20080090487A1 Inflatable plastic articles with sealed internal illumination 审中-公开
标题翻译：具有密封内部照明的充气塑料制品
公开(公告)号：US20080090487A1
公开(公告)日：2008-04-17
申请号：US11705922
申请日：2007-02-13
申请人： James W. Randall
发明人： James W. Randall
IPC分类号： A63H27/18
CPC分类号： A63H27/10 , A63H33/22 , A63H2027/1058
摘要： An inflatable blimp replica formed of thin plastic sheet, includes: a. an inflatable main chamber having walls which define the perimeter of the air space within the main chamber, and a gondola extending downward from the bottom wall, b. an inner chamber having a central part an open top part, and a closed bottom part, wherein the top part intersects and is heat sealed in an air tight manner to the top wall, the central part extends downward through the main body, and the bottom part extends into the gondola, such that the main chamber can be closed and inflatable notwithstanding the intersection of the inner chamber through the top wall, and c. an illumination sub-assembly within the inner chamber including at least one LED, a replaceable electric battery at the top part, and control means for controlling when the LED is switched on and off.
摘要翻译：由薄塑料薄片制成的充气飞轮复制品包括：a。一个可充气的主室具有限定主室内的空气空间的周边的壁，以及从底壁向下延伸的吊篮。具有中心部分为开放顶部的内室和封闭的底部部分，其中顶部部分以气密的方式相交并热密封到顶壁，中心部分向下延伸通过主体，底部部分延伸到吊舱中，使得主室可以被封闭并且可充气，尽管内室通过顶壁的相交，c。所述内部室内的照明子组件包括至少一个LED，顶部的可替换电池，以及用于控制所述LED何时被接通和断开的控制装置。

10. 发明申请

US20050082425A1 EMPENNAGE ASSEMBLY AND ATTACHMENT MECHANISM FOR A MODEL AIRPLANE 有权
标题翻译：一种模型飞机的装配大会和附件机制
公开(公告)号：US20050082425A1
公开(公告)日：2005-04-21
申请号：US10690065
申请日：2003-10-21
申请人： Miguel Frontera Castaner
发明人： Miguel Frontera Castaner
IPC分类号： A63H27/00 , A63H27/18 , B64C9/00 , B64C9/02
CPC分类号： A63H27/02
摘要： An empennage assembly for a model aircraft. The empennage assembly includes a fuselage having a bottom portion with an opening and a housing positioned in the opening in the bottom portion of the fuselage. The housing has a first end defining an opening and a second end. A rod extends from an underside of a vertical stabilizer, and a horizontal stabilizer having a hole is aligned with the opening in the bottom portion of the fuselage, the housing and the rod, whereby the rod is positioned within the opening in the first end of the housing to secure the vertical and horizontal stabilizers to the fuselage. A method and device for attaching an empennage assembly to a model aircraft are also disclosed.
摘要翻译：模型飞机的尾翼装配。尾翼组件包括具有开口的底部的机身和位于机身底部的开口中的壳体。壳体具有限定开口的第一端和第二端。杆从垂直稳定器的下侧延伸，并且具有孔的水平稳定器与机身，壳体和杆的底部中的开口对准，由此杆位于开口内的第一端外壳可将垂直和水平稳定器固定在机身上。还公开了一种用于将尾翼组件附接到模型飞机的方法和装置。

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