公开(公告)号：US2366652A

公开(公告)日：1945-01-02

申请号：US46386542

申请日：1942-10-30

申请人： RIEGER JAMES H

发明人： RIEGER JAMES H

IPC分类号： A63H27/18 ,  B64C31/02

CPC分类号： A63H27/02

公开(公告)号：US08246414B2

公开(公告)日：2012-08-21

申请号：US12820294

申请日：2010-06-22

申请人： Masaki Suzuki

发明人： Masaki Suzuki

IPC分类号： A63H27/18 ,  A63H27/30

CPC分类号： A63H27/02 ,  A63H30/04

摘要： The present invention provides an unconventional and proprietary radio control (RC) or infrared remote control (IR) toy model/airplane which can intentionally shift or change its center of gravity (COG) to different positions along the longitudinal centerline of the aircraft or fuselage. The incremental shifting or moving of the COG from front to rear or vice versa incrementally changes the “angle of attack” of the wing, thereby producing a variable range of viable flight attitudes and resultant terminal velocities (top speeds). Therefore, users can easily select an appropriate speed for the airplane to fly in limited indoor spaces or in larger outdoor areas. Additionally, the COG shifting of the present invention can be applied not only to RC and IR controlled toy models/aircrafts but may also be implemented into real aircrafts including manned and unmanned aircraft for civilian and/or military applications.

摘要翻译： 本发明提供了一种非常规和专有的无线电控制（RC）或红外遥控（IR）玩具模型/飞机，其可以有意地将其重心（COG）移动或改变到沿飞机或机身的纵向中心线的不同位置。 COG从前到后的增量移动或移动反过来逐渐改变机翼的“迎角”，从而产生可行的飞行姿态和最终的最终速度（最高速度）的可变范围。 因此，用户可以轻松地选择合适的速度使飞机在有限的室内空间或较大的户外区域内飞行。 此外，本发明的COG转移不仅可以应用于RC和IR控制的玩具模型/飞机，而且还可以被实现为真正的飞机，包括用于民用和/或军事应用的载人和无人飞行器。

公开(公告)号：US20050106987A1

公开(公告)日：2005-05-19

申请号：US10895164

申请日：2004-07-20

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.

公开(公告)号：US5868597A

公开(公告)日：1999-02-09

申请号：US256235

申请日：1994-06-27

申请人： John Youngfu Chen

发明人： John Youngfu Chen

IPC分类号： A63H1/32 ,  A63H27/18 ,  A63H33/18 ,  C08L51/00 ,  C08L53/00 ,  C08L53/02 ,  A63H27/00

CPC分类号： C08L53/02 ,  A63H1/32 ,  A63H33/185 ,  C08L51/00 ,  C08L53/00 ,  C08L53/025

摘要： A novel rotating aerodynamic toy made of a ultra-elastic gel airfoil which is suitable for launch in light or heavy wind conditions and capable of performing various aerodynamic effects including climb, stall, return, straight-line flight and other aerobatics. The ultra-elastic properties of the airfoil allow the airfoil to transform by at least 50% extension of its aerodynamic profile at launch and; while in flight; one or more preselected sized cavities and holes, slots and holes, cavities, slots and holes and cavities, slots, or holes provide handling, elastic control of airfoil profile stretching for flight, and flight stability.

摘要翻译： PCT No.PCT / US94 / 07314 Sec。 371日期1994年6月27日第 102（e）日期1994年6月27日PCT提交1994年6月27日PCT公布。 公开号WO96 / 00118 日期1996年1月4日一种由超弹性凝胶翼型制成的新型旋转空气动力学玩具，适用于轻型或重型风力条件下的发射，能够执行各种空气动力学效果，包括爬升，失速，返回，直线飞行和其他特技飞行 。 翼型的超弹性特性允许翼型在发射时转变其空气动力学特性的至少50％的延伸; 在飞行中 一个或多个预选的尺寸的空腔和孔，槽和孔，空腔，狭槽和孔以及空腔，狭槽或孔提供了用于飞行的翼型轮廓的弹性控制和飞行稳定性。

公开(公告)号：US5676580A

公开(公告)日：1997-10-14

申请号：US489805

申请日：1995-06-12

申请人： Rodney Farrar

发明人： Rodney Farrar

IPC分类号： A63H27/00 ,  A63H27/18 ,  B26F3/12 ,  A63H33/00 ,  H05B3/00

CPC分类号： B26F3/12 ,  A63H27/00 ,  A63H27/001 ,  A63H27/02

摘要： A model airplane, airplane kit, method of making a model airplane, a plastic foam cutter useful for making the model airplane and a method for making the plastic foam cutter. 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，制造模型飞机的方法，用于制造模型飞机的塑料泡沫切割机和制造塑料泡沫切割机的方法。 本发明的试剂盒使得儿童和成年人能够使用回收塑料泡沫塑料模制品（例如食品包装领域众所周知的10-S的聚苯乙烯食品托盘）轻松制作飞行良好的模型飞机。

公开(公告)号：US5655947A

公开(公告)日：1997-08-12

申请号：US705096

申请日：1991-05-23

申请人： John Youngfu Chen

发明人： John Youngfu Chen

IPC分类号： A61C15/04 ,  A63H27/18 ,  A63H33/18 ,  C08K5/01 ,  C08L51/00 ,  C08L53/00 ,  C08L53/02 ,  A63H27/00

CPC分类号： C08L53/02 ,  A61C15/041 ,  A63H33/185 ,  C08K5/01 ,  C08L51/00 ,  C08L53/00 ,  C08L53/025

摘要： A novel rotating aerodynamic toy in the form of a ultra-elastic gel airfoil which is suitable for launch in light or heavy wind conditions and capable of performing various aerodynamic effects including climb, stall, return, straight-line flight and other aerobatics. The ultra-elastic properties of the airfoil allow the airfoil to transform its aerodynamic profile at launch and while in flight.

摘要翻译： 一种新型的旋转空气动力学玩具，它是一种超弹性凝胶翼型，适用于轻型或重型风力发射，能够执行各种空气动力学效果，包括爬升，失速，返回，直线飞行和其他特技飞行。 翼型的超弹性特性允许机翼在发射时和飞行中改变其空气动力学特性。

公开(公告)号：US5324222A

公开(公告)日：1994-06-28

申请号：US876118

申请日：1992-04-29

申请人： John Y. Chen

发明人： John Y. Chen

IPC分类号： A61C15/04 ,  A63H27/18 ,  A63H33/18 ,  C08K5/01 ,  C08L51/00 ,  C08L53/00 ,  C08L53/02 ,  A63H27/00 ,  A63H3/00 ,  A63H27/14

CPC分类号： A61C15/041 ,  A63H33/185 ,  C08K5/01 ,  C08L51/00 ,  C08L53/00 ,  C08L53/02 ,  C08L53/025 ,  C08L91/00

摘要： A novel rotating aerodynamic toy comprising a ultra-elastic gel airfoil which is suitable for launch in light or heavy wind conditions and capable of performing various aerodynamic effects including climb, stall, return, straight-line flight and other aerobatics. The ultra-elastic properties of the airfoil allow the airfoil to transform its aerodynamic profile at launch and while in flight.

摘要翻译： 一种新颖的旋转空气动力学玩具，其包括超弹性凝胶翼型件，其适合于在轻或强风条件下发射，并且能够执行各种空气动力学效果，包括爬升，失速，返回，直线飞行和其他特技飞行。 翼型的超弹性特性允许机翼在发射时和飞行中改变其空气动力学特性。

公开(公告)号：US5281179A

公开(公告)日：1994-01-25

申请号：US48470

申请日：1993-04-16

申请人： Hans Wu

发明人： Hans Wu

IPC分类号： A63H27/00 ,  A63H27/14 ,  A63H27/18

CPC分类号： A63H27/14 ,  A63H27/00

摘要： A toy aircraft capable of circling in changeable radius which includes a fuselage and two rudders disposed on the wings, wherein multiple weight-adjusting recesses are longitudinally arranged on a top portion of the fuselage and arranged on upper rear positions of the wings at predetermined intervals, whereby multiple weight-adjusting ball members can be placed in the recesses and the locations or weight of the ball members can be changed to freely adjust the weight and gravitational center of the toy aircraft, at least one of the rudders being slightly inclined, making the shot aircraft fly in a circling pattern with the circling radius changeable.

摘要翻译： 一种能够以可变半径盘绕的玩具飞机，其包括设置在机翼上的机身和两个方向舵，其中多个重量调节凹部纵向地布置在机身的顶部上并以预定间隔布置在机翼的后部后部位置， 由此能够将多个重量调节球部件放置在凹部中，并且可以改变球部件的位置或重量以自由地调节玩具飞机的重量和重力中心，至少一个方向舵稍微倾斜，使得 射击飞机以盘旋的方式飞行，圆盘半径可变。

公开(公告)号：US5145439A

公开(公告)日：1992-09-08

申请号：US734524

申请日：1991-07-23

申请人： Claus W. Wagener

发明人： Claus W. Wagener

IPC分类号： A63H27/00 ,  A63H27/18

CPC分类号： A63H27/00

摘要： The invention discloses a fuselage which is subdivided into a fuselage lower part (1) and a shell-shaped upper fuselage portion (3) where the upper fuselage portion (3) is provided with windows arranged in rows (12, 13), the windows being formed by inserted pieces (8) with the fuselage moulded around them, the windows being formed on an integral insert part (7). It is desirable that, on the one hand, the upper fuselage portion including the injection-moulded window pieces be of simpler construction and, on the other hand, should have a continuous external fuselage surface extending continuously without any conspicuous joint line down to the joint with the fuselage lower part. This is accomplished in that the upper fuselage portion (7) is of single-piece construction down to the joint (2) to the fuselage lower part (1) with the windows being surrounded by said upper fuselage portion, and in that the elongated insert part (7) of shell-shaped construction continuously lines the upper fuselage portion piece (3) on the inside. The simplified single piece construction of the upper fuselage portion provided with windows is achieved by the use of the insert part which is conveniently made by injection moulding.

摘要翻译： 本发明公开了一种机身，其分为机身下部（1）和壳体上机身部分（3），其中机身上部（3）设置有排列成行（12,13）的窗口，窗口 由其上模制的机身的插入件（8）形成，窗口形成在整体插入件（7）上。 理想的是，一方面，包括注射成型的窗件的上部机身部分的结构更简单，另一方面，应该具有连续的外部机身表面，而连续的外部机身表面连续地延伸，而没有任何显着的接合线向下延伸到接头 与机身下部。 这是通过上机身部分（7）具有单件结构向下到机身下部（1）的接头（2），其中窗口被所述上部机身部分包围，并且细长插入件 壳体构造的部分（7）将机体上部部分（3）连续地排列在内侧。 通过使用方便地通过注射成型制造的插入部件来实现设置有窗户的上部机身部分的简化单件结构。

公开(公告)号：US5096452A

公开(公告)日：1992-03-17

申请号：US641936

申请日：1991-01-16

申请人： Claus Wagener

发明人： Claus Wagener

IPC分类号： A63H17/26 ,  A63H17/267 ,  A63H27/00 ,  A63H27/18 ,  A63H27/32

CPC分类号： A63H27/02

摘要： In a model airplane having a landing gear 5 provided on a fuselage 1 or wing made as a zinc-alloy die-casting where a bearing member 19 is suspended from a strut 18, it is desirable that the manufacture of an accurately modelled landing gear be simplified. This is achieved in that a landing gear 8 formed with two clasp member arms 10 made of elastically bendable plastic forms the bearing member 19 and at least partially the strut 18 with a tenon 11 being inserted and glued into a cast cavity 12 in the fuselage 1/wing wherein the clasp member 8 bears against the zinc-alloy die-casting with a thickening shoulder 17. The clasp member being a plastic moulding permits a finely engraved realistic appearance of the strut and bearing member while simplifying assembly of the wheel pair and reducing the scrapping rate.

摘要翻译： 在具有设置在机身1上的起落架5的模型飞机或由支承构件19从支柱18悬挂而形成为锌合金压铸件的机翼上，希望制造精确建模的起落架为 简化了 这是通过形成有由弹性可弯曲塑料制成的两个搭扣构件臂10的起落架8形成轴承构件19，并且至少部分地具有支柱18，其中榫头11被插入并粘合到机身1中的铸造空腔12中 /翼，其中扣环构件8用增厚肩部17抵靠锌合金压铸。作为塑料模制件的扣环构件允许支柱和支承构件的精细雕刻的现实外观，同时简化车轮对的组装并且减小 报废率。