公开(公告)号：WO2008045901A2

公开(公告)日：2008-04-17

申请号：PCT/US2007/080864

申请日：2007-10-09

Applicant: IYC PRODUCTS

IPC: A63H27/10

CPC classification number: A63H27/10 ,  A63H27/14 ,  A63H2027/1008

Abstract: This covers a game kit, system, method, and device for the balloon games. A game kit for the Balloon Stomper/ popping/ hitting/ kicking/ bursting game. The kit consists of a balloon, a tether for the balloon, and a device for attaching the balloon to a player, as an example. As one example, the game involves tying a balloon to the ankle of each player. Then the players try to stomp on each other's balloons, while protecting their own balloon. The winner is the last person or team with a balloon that has not been popped. There are many other variations for the game/ rules as explained here in more details. One problem with the game is that preparing a large number of game set-ups is time consuming and labor intensive. This is intended to make both set-up and clean-up of the balloon stomper game simpler. It also deals with the balloon weight setup and system.

Abstract translation: 这涵盖了气球游戏的游戏套件，系统，方法和设备。 气球狙击手/弹出/打/踢/爆破游戏的游戏工具包。 作为示例，该套件包括气球，气球系绳和用于将气球附接到玩家的装置。 例如，游戏涉及将气球绑在每个玩家的脚踝上。 然后玩家试图踩在对方的气球上，同时保护自己的气球。 获胜者是最后一个没有弹出气球的人或团队。 游戏/规则还有许多其他的变体，这里有更详细的解释。 游戏的一个问题是，准备大量的游戏设置是耗时且劳动密集型的。 这是为了使气球踩踏游戏的设置和清理更简单。 它还涉及气球重量设置和系统。

公开(公告)号：WO2004071608A3

公开(公告)日：2005-11-24

申请号：PCT/US2004004051

申请日：2004-02-11

Applicant: RHINO TOYS INC ,  SIVERGLATE DAVID

Inventor： SIVERGLATE DAVID

IPC: A63H5/00 ,  A63H27/00 ,  A63H27/14 ,  A63H33/18

CPC classification number: A63H33/18 ,  A63H5/00 ,  A63H27/14

Abstract: A flying toy apparatus (10) is provided. The flying toy apparatus typically includes a body (12) having an elongate channel (20) formed therein, the channel extending in a longitudinal direction along the body. The flying toy apparatus also typically includes an elastic launch member (14) coupled to the body and configured to be stretched forward in the longitudinal direction by a digit of a user. The channel is typically configured to accommodate passage of the digit therein during launch of the body over the digit. A foam nose member (17) may be coupled to a leading portion of the body to soften impact and/or guide the digit into the channel. A grip (21) may be provided on the body for the user to securely hold the apparatus during launch. Fins (19) may also be provided on the body.

Abstract translation: 提供一种飞行玩具装置（10）。 飞行玩具装置通常包括具有形成在其中的细长通道（20）的主体（12），该通道沿主体沿纵向方向延伸。 飞行玩具装置通常还包括弹性发射构件（14），弹性发射构件（14）联接到主体并构造成通过使用者的数字在纵向方向上向前伸展。 该通道通常被配置为在身体在数字上方的发射期间容纳数字在其中的通过。 泡沫鼻构件（17）可以联接到身体的引导部分，以软化冲击和/或引导数字进入通道。 可以在身体上设置手柄（21），供使用者在发射期间牢固地固定装置。 鳍（19）也可以在身体上提供。

公开(公告)号：WO2004112922A2

公开(公告)日：2004-12-29

申请号：PCT/US2004/019323

申请日：2004-06-18

Applicant: ABESHOUSE, Matthew

Inventor： ABESHOUSE, Matthew

IPC: A63F

CPC classification number: A63H33/18 ,  A63H27/14

Abstract: An aerodynamic toy is disclosed comprising a flying airplane configured to launch into flight by being thrown from a wing portion of the airplane, the airplane including a weighted nose portion, a generally horizontal wing portion, and a rearwardly extending generally vertical portion. A tossable toy flier is also disclosed having a first body portion that is generally flat extends along a first plane, the first body portion being of a single piece of material; a weight fixed to a nose portion of the first body portion adjacent said front end; and a second body portion being generally flat and extending along a second plane. The first plane and the second plane intersect along a line that extends longitudinally from said front end to a tail end of the first body portion. The second body portion comprises the tail and extends from a point behind a midpoint of the first body portion towards a rear end portion of the first body portion.

Abstract translation: 公开了一种空气动力学玩具，其包括飞行飞机，其构造成通过从飞机的翼部投掷而发射到飞行中，所述飞机包括加权的鼻部，大致水平的翼部和向后延伸的大致垂直的部分。 还公开了一种可折叠的玩具飞行器，其具有第一主体部分，该第一主体部分大致平坦地沿着第一平面延伸，第一主体部分是单个材料; 固定到所述第一主体部分的与所述前端相邻的鼻部的重物; 并且第二主体部分大致平坦并且沿第二平面延伸。 第一平面和第二平面沿着从第一主体部分的所述前端纵向延伸到尾端的线相交。 第二主体部分包括尾部并且从第一主体部分的中点之后的点朝向第一主体部分的后端部延伸。

公开(公告)号：WO1997035650A1

公开(公告)日：1997-10-02

申请号：PCT/US1997004867

申请日：1997-03-25

Applicant: ALBRECHT, Glenn, C.

IPC: A63H27/01

CPC classification number: A63H27/14

Abstract: This toy is a launcher (20) and one or more gliders (10). The dihedral of the glider is achieved with two parallel creases (12, 13) that run front to back down the center (11) of the glider. Near the leading edge of the wing surfaces (36, 38) self-adhesive strips of flat magnetic sheet stock can be applied to the top and bottom of each wing to provide a proper weight to initiate desirable trim to the glider and to provide a force to separate the nested planes after launching, i.e., magnetic repulsion. For a multiple launch, the gliders are stacked on top of one another and placed upside down and mounted on a launching stick. Using a vertical upward force, wind resistance will induce the glider wings to collapse upon themselves, facilitating a higher launch. At the peak of the launch, the combination of magnetic repulsion and the spring-back of the glider wings to their designed high glide ratio configuration permits each glider to successfully separate and glide to earth.

Abstract translation: 这个玩具是一个发射器（20）和一个或多个滑翔机（10）。 滑翔机的二面体通过从滑翔机的中心（11）向前运行的两个平行的折痕（12,13）实现。 在机翼表面（36,38）的前缘附近，平板磁性片材的自粘带可以施加到每个翼的顶部和底部，以提供适当的重量以启动对滑翔机的期望的修剪并提供力 在发射后分离嵌套飞机，即磁力排斥。 对于多次发射，滑翔机堆叠在另一个顶部，并倒置放置在发射棒上。 使用垂直向上的力量，抗风能力将导致滑翔机翼自身崩溃，从而有助于更高的发射。 在发射的高峰期，磁力排斥与滑翔机翼的回弹与其设计的高滑行比配置的组合允许每个滑翔机成功地分离并滑动到地球。

公开(公告)号：WO1995028212A1

公开(公告)日：1995-10-26

申请号：PCT/CA1995000208

申请日：1995-04-12

Applicant: ROBINSON, Allan, Brooks ,  ROBINSON, Russel, Victor ,  ROBINSON, Kelly, Thomas

IPC: A63H27/00

CPC classification number: A63H27/14 ,  A63H27/00

Abstract: The toy is composed of a projectile and a tube for lauching the projectile into the air. The projectile has a pair of wings symmetrically disposed about a longitudinal axis. The leading edges of the wings normally extend outwardly at an oblique angle from a nose which defines the forward end of the projectile. In that position the projectile will fly through the air. The wings are spring-biased into the position for flying. When a manual force opposed to the biasing means is applied to the wings, they fold inwardly with resulting pivoting of the leading edges toward each other. When the wings are closed the projectile is in a pre-lauching position. The projectile is launched into the air by means of a tube which is hollow and open at one end through which the projectile exists from the tube.

Abstract translation: 玩具由射弹和管子组成，用于将射弹向空中扬扬。 射弹具有一对围绕纵向轴线对称设置的翼。 机翼的前缘通常以与定义射弹前端的鼻角呈倾斜角向外延伸。 在那个位置上，射弹会飞过空中。 翅膀被弹簧偏置到飞行位置。 当将与偏置装置相对的手动力施加到翼部时，它们向内折叠，从而使前缘朝向彼此枢转。 当机翼关闭时，射弹处于预先的位置。 射弹通过管子被引入空气，管子在一端是空心的，在管的一端存在射弹。

公开(公告)号：WO1993014848A1

公开(公告)日：1993-08-05

申请号：PCT/US1992006742

申请日：1992-08-13

Applicant: MATTEL, INC.

Inventor： MATTEL, INC. ,  SAFFER, Gary, M. ,  PUGH, Robert, V. ,  ASBAGHI, Ahmed

IPC: A63H29/16

CPC classification number: A63H27/14 ,  A63H17/008 ,  A63H29/16

Abstract: As shown, the toy vehicle launcher (10) includes a hollow base unit (11) and a collapsible bellows (12) combined to form a pressurization air chamber. The base unit (11) includes a launch tube (33) extending therefrom which provides an air passage for the expulsion of pressurized air from the interior housing. The launched tube (33) defines a noncircular cross section which in its preferred form is rectangular to properly align a to-be-launched vehicle (25) with respect to the launcher (10). A pair of safety ribs (36, 37) are supported within the launch tube to preclude the insertion of hazardous objects into the launch tube by the child user. In an alternate embodiment, an angled adapter (70) is provided which is received upon the launch tube (33) and terminates in an upwardly angled launch portion (73).

Abstract translation: 如图所示，玩具车辆发射器（10）包括中空基座单元（11）和组合形成加压空气室的可折叠波纹管（12）。 基座单元（11）包括从其延伸的发射管（33），其提供用于从内部壳体排出加压空气的空气通道。 推出的管（33）限定非圆形横截面，其在其优选形式中是矩形的，以相对于发射器（10）正确对准待发射的车辆（25）。 发射管内支持一对安全肋（36,37），以防止儿童使用者将危险物品插入发射管。 在替代实施例中，提供成角度的适配器（70），其接收在发射管（33）上并且终止于向上成角度的发射部分（73）。

公开(公告)号：WO2017158234A1

公开(公告)日：2017-09-21

申请号：PCT/FI2017/050161

申请日：2017-03-13

Applicant: SKYCAT OY

Inventor： HIISILÄ, Henri

IPC: B64D17/70 ,  B64D1/12 ,  B64D1/06

CPC classification number: B64F1/04 ,  A63H27/14 ,  B64C2201/08

Abstract: An object of the invention is a launching device for launching an object from a launch pad, wherein said apparatus comprises a frame (1) affixed to the launch pad, a push element (2) for pushing an object detached from the launch pad, a flexible force storing element (3) for turning the push element (2) in relation to the frame (1), a casing (4) for holding the launchable object in place against the push element (2), and a lock element (6) for locking the casing (4) in standby position and for bringing the launching device in a position of ready to operate such that the frame (1) and the push element (2) are superposed and connected to each other substantially at one edge of the device, the frame (1) and the push element (2) being substantially parallel, force being stored in the force storing element (3) for displacing the push element (2) and that said stored force being releasable at a moment of launch. The force storing element (3) is composed of at least one spring (3`) or elastic band (3``) or an extension spring functioning as an elastic band, and the casing (4) has been attached fixedly to the frame (1) at its fixing point (9).

Abstract translation: 本发明的目的是一种用于从发射台发射物体的发射装置，其中所述装置包括固定到发射台的框架（1），推动元件（2） （2）相对于框架（1）转动的柔性力存储元件（3），用于将可发射物体保持就位以抵靠推动元件（2）的壳体（4） ）和用于将壳体（4）锁定在备用位置并且使发射装置处于准备工作位置的锁定元件（6），使得框架（1）和推动元件（2）叠置并连接 所述框架（1）和所述推动元件（2）基本上是平行的，存储在所述力存储元件（3）中的力用于移动所述推动元件（2）并且所述存储在所述存储元件 部队在发射时可以释放。 力存储元件（3）由至少一个弹簧（3'）或弹性带（3“）或用作弹性带的拉伸弹簧构成，并且壳体（4）固定地连接到框架 1）在其固定点（9）。

公开(公告)号：WO2014176263A1

公开(公告)日：2014-10-30

申请号：PCT/US2014/035006

申请日：2014-04-22

Applicant: SIEVERS, Roger

Inventor： SIEVERS, Roger

IPC: A63B65/12 ,  A63B69/40

CPC classification number: F41B3/005 ,  A01K15/025 ,  A63B65/122 ,  A63H27/14 ,  A63H33/18 ,  F41B3/03 ,  F41B3/04

Abstract: Throwing devices are described. In one embodiment, a throwing device includes a spring-actuated throwing arm wherein a cup member is disposed at an end of the throwing arm and is adapted to allow a user to pick up an object to be thrown by the throwing device without touching the object. In another embodiment, a throwing device includes a tension adjustment member, by which a user can adjust the tension applied to the launching spring, thereby adjusting the launch range of the throwing device.

Abstract translation: 描述投掷设备。 在一个实施例中，抛掷装置包括弹簧致动的投掷臂，其中杯构件设置在投掷臂的端部，并且适于允许使用者拾取被投掷装置投掷的物体而不接触物体 。 在另一个实施例中，投掷装置包括张力调节构件，通过该张力调节构件，使用者可以调节施加到发射弹簧的张力，从而调节投掷装置的发射范围。

公开(公告)号：WO2006135606A1

公开(公告)日：2006-12-21

申请号：PCT/US2006/021906

申请日：2006-06-06

Applicant: HONEYWELL INTERNATIONAL INC. ,  MANTYCH, Glen, A. ,  GOOSSEN, Emray, R.

Inventor： MANTYCH, Glen, A. ,  GOOSSEN, Emray, R.

IPC: B64C39/00 ,  A63H27/133

CPC classification number: A63H27/02 ,  A63H27/12 ,  A63H27/14 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/108

Abstract: Self-leveling legs (30, 32) are used to accommodate landing a ducted fan hovercraft (20) on a sloped surface (52) such as a roof-top. These legs (30, 32) move to accommodate a variation of slope within their range of motion irrespective to the azimuth of the vehicle body (38). The configuration and operation of the landing legs (30, 32) allow the hovercraft (20) to land in a stable fashion with the hovercraft (20) vehicle body (38) maintained in a vertical orientation. The basic kinematics of the present invention is the displacement of one landing leg (30) upwards is connected by a horizontal member (46) to the opposite leg and displaces it downwards (32), and visa-versa. Planar surface contact is accomplished by the unique curvature of the legs (30, 32) and the splay of the legs from the vehicle body (38).

Abstract translation: 自调平腿（30,32）用于容纳在诸如屋顶的倾斜表面（52）上的管道风扇气垫船（20）的落地。 这些腿（30,32）移动以适应在其运动范围内的斜率变化，而与车体（38）的方位角无关。 着陆腿（30,32）的构造和操作允许气垫船（20）以气垫船（20）车身（38）保持垂直方向稳定地着陆。 本发明的基本运动学是一个着陆腿（30）向上的位移通过水平构件（46）连接到相对的腿并向下移位（32），反之亦然。 平面表面接触通过腿部（30,32）的独特曲率和来自车身（38）的腿部的张开来实现。

公开(公告)号：WO2002072221A1

公开(公告)日：2002-09-19

申请号：PCT/US2002/007939

申请日：2002-03-14

Applicant: WILKINSON, William, T.

Inventor： WILKINSON, William, T. ,  BART, Phil

IPC: A63H11/06

CPC classification number: A63H11/06 ,  A63H13/10 ,  A63H27/14

Abstract: A jumping toy (60) comprising a projectile (10) comprising a cushioned head (16), a propulsion mechanism (30), a base (14), and, in some embodiments, a releasable catch mechanism (20) that prevents the propulsion mechanism (30) from activating until the catch mechanism is released. In various embodiments, the propulsion mechanism (30) may comprise a spring (12) with the cushioned head (64) attached to the spring (12); the base (14) may comprise a launching tube (156) into which the spring (12) is compressed; the toy (60) may comprise an article (152) with a spring (154) mounted in an inner compartment; or the toy may comprise a launching apparatus (600) comprising a projectile interface and a base (606), wherein movement of the projectile interface relative to the base creates stored energy that is subsequently converted to kinetic energy and transferred to the projectile.

Abstract translation: 一种跳跃玩具（60），包括弹丸（10），包括缓冲头（16），推进机构（30），基座（14），并且在一些实施例中是可释放的止动机构（20），其防止推进 机构（30）从启动直到捕获机构被释放。 在各种实施例中，推进机构（30）可以包括弹簧（12），其中缓冲头（64）附接到弹簧（12）; 基座（14）可以包括弹簧（12）被压缩在其中的发射管（156）; 玩具（60）可以包括具有安装在内部隔间中的弹簧（154）的物品（152） 或者玩具可以包括包括射弹界面和基座（606）的发射装置（600），其中射弹界面相对于基座的运动产生存储的能量，其随后被转换成动能并被转移到射弹。