JP2007130146A - Radio-controlled flying toy - Google Patents

Radio-controlled flying toy Download PDF

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Publication number
JP2007130146A
JP2007130146A JP2005324666A JP2005324666A JP2007130146A JP 2007130146 A JP2007130146 A JP 2007130146A JP 2005324666 A JP2005324666 A JP 2005324666A JP 2005324666 A JP2005324666 A JP 2005324666A JP 2007130146 A JP2007130146 A JP 2007130146A
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Japan
Prior art keywords
radio
propellers
flying toy
transmitter
propeller
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JP2005324666A
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Japanese (ja)
Inventor
Takeo Goto
武雄 後藤
Yoshiaki Oe
善明 大江
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Taiyo Kogyo Co Ltd
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Taiyo Kogyo Co Ltd
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Priority to JP2005324666A priority Critical patent/JP2007130146A/en
Priority to US11/378,801 priority patent/US20070105474A1/en
Publication of JP2007130146A publication Critical patent/JP2007130146A/en
Pending legal-status Critical Current

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    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys
    • A63H27/12Helicopters ; Flying tops
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys
    • A63H27/02Model aircraft
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H30/00Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
    • A63H30/02Electrical arrangements
    • A63H30/04Electrical arrangements using wireless transmission

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Toys (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a radio-controlled flying toy allowing a user to easily float a body and to easily control the traveling direction. <P>SOLUTION: The radio-controlled flying toy comprises the rectangular plate-like body 11 with a flat bottom on the lower side, first to fourth propellers 16a, 16b, 16c and 16d disposed at least at four corners forming a quadrangle on the lower side of the body 11 for floating the body 11 by blowing air to the bottom side, first to fourth driving means 17a, 17b, 17c and 17d for driving the first to fourth propellers 16a, 16b, 16c and 16d respectively, a control part 20 for controlling the driving output of the first to fourth driving means 17a, 17b, 17c and 17d independently, a transmitter 30 for transmitting control signals for flying to the control part 20 from outside, and a battery 21 for feeding the power supply to the first to fourth driving means 17a, 17b, 17c and 17d and to the control part 20. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

本発明は、機体の底面側へ空気を送風することで機体を平坦な走行面上を浮上させて、自由に飛行できる無線操縦飛行玩具に関するものである。   The present invention relates to a radio-controlled flying toy that can fly freely by blowing air to the bottom side of the aircraft to float the aircraft on a flat running surface.

従来、地面効果機として、機体の底面と下部側の地面や水面等の走行面との間に封じ込めたエアクッションの揚力、または翼の地面効果を利用して航行する乗物として、ホバークラフト(商標名)あるいはエアクッション機等が一般に知られている。このような地面効果機の原理を利用して遠隔操縦により航行する玩具として、本出願人は、本体の下部周縁に膨張・収縮自在な袋状に形成したスカート部を取付け、本体内に搭載した浮上用送風機により空気を外部から吸引してスカート部で囲まれた本体底部へ導入するとともにスカート部内へ導入して膨張させることで、本体を浮上させ、また本体の上部に推進用送風機を設けたエアクッション機玩具に関する技術を開示している(例えば、特許文献1参照。)。
実公平6−20559号公報(第2〜6ページ、図1〜9)。
Conventionally, as a ground effect aircraft, a hovercraft (trade name) is used as a vehicle that navigates using the lift of an air cushion confined between the bottom surface of the aircraft and a traveling surface such as the ground or water surface on the lower side, or the ground effect of a wing. ) Or an air cushion machine or the like is generally known. As a toy that navigates by remote control using the principle of such a ground effect machine, the present applicant attaches a skirt formed in a bag shape that can be expanded and contracted to the lower peripheral edge of the main body, and mounts it in the main body. Air was sucked from the outside by a levitation blower, introduced into the bottom of the main body surrounded by the skirt, and introduced into the skirt to inflate it, so that the main body was levitated, and a propulsion blower was provided at the top of the main body The technique regarding an air cushion machine toy is disclosed (for example, refer patent document 1).
Japanese Utility Model Publication No. 6-20559 (pages 2-6, FIGS. 1-9).

従来のエアクッション機玩具は、本体内に搭載した浮上用送風機により、本体下部周縁に設けたスカート部に送風して膨張させ、スカート部で囲まれた本体の底部へ送風し、膨張したスカート部の下部側と地面等の走行面との間に空気を流通させることで機体を走行面から浮上させているため、均一なスカート部の膨張や浮上に要する空気の流通のために大きな出力を有する浮上用送風機が必要であった。また、本体を走行させたり自由に方向を変更するために、本体の上部に2台の推進用送風機を設けたり、あるいは1台の推進用送風機により送風方向を可変にする機構等を搭載する必要があった。そのため、これらの浮上用送風機や推進用送風機を駆動するために大きな駆動電源が必要となり、消費電力が大きくなり長時間の飛行ができないおそれがあった。   Conventional air cushion machine toys are blown to the skirt part provided at the lower periphery of the main body by the levitation blower installed in the main body, and blown to the bottom part of the main body surrounded by the skirt part. Since the aircraft is levitated from the running surface by circulating air between the lower side of the vehicle and the running surface such as the ground, it has a large output for the air flow required for uniform expansion and levitation of the skirt A levitation blower was required. Also, in order to run the main body and change the direction freely, it is necessary to install two propulsion fans at the top of the main body, or to install a mechanism to change the air blowing direction with one propulsion fan was there. Therefore, a large drive power source is required to drive these levitation blowers and propulsion blowers, and there is a possibility that power consumption increases and long-time flight cannot be performed.

本発明は上記事情に鑑みなされたもので、機体の浮上を容易にでき走行方向の制御も簡単にできる無線操縦飛行玩具を提供することを目的とする。   The present invention has been made in view of the above circumstances, and an object of the present invention is to provide a radio controlled flying toy that can easily float the aircraft and easily control the traveling direction.

上記目的を達成するために請求項1に記載の発明にあっては、低部側が平坦な底面を有する矩形板状に形成された機体と、該機体の低部側の少なくとも4辺形を形成する4隅に設けられ底面側へ送風して前記機体を浮上させる第1〜4のプロペラと、前記第1〜4のプロペラをそれぞれ駆動する第1〜4の駆動手段と、前記第1〜4の駆動手段の駆動出力をそれぞれ個別に制御する制御部と、飛行のための制御信号を外部から前記制御部へ送信する送信機と、前記第1〜4の駆動手段及び制御部へ電源を供給する電池とを備えたことを特徴とするものである。送信機から飛行のための制御信号を制御部へ送信し、この制御部で第1〜4の駆動手段の駆動出力をそれぞれ個別に制御して第1〜4のプロペラの回転速度を変えることで、機体の浮上を容易にでき走行方向の制御も簡単にできる。   In order to achieve the above object, in the first aspect of the present invention, a machine body formed in a rectangular plate shape having a flat bottom surface on the lower side and at least a quadrilateral on the lower side of the machine is formed. The first to fourth propellers that are provided at the four corners and blown toward the bottom surface side to float the airframe, the first to fourth driving means for driving the first to fourth propellers, and the first to fourth, respectively. A control unit for individually controlling the driving output of the driving means, a transmitter for transmitting a control signal for flight to the control unit from the outside, and supplying power to the first to fourth driving means and the control unit It is characterized by having a battery. By transmitting a control signal for flight from the transmitter to the control unit, and by controlling the drive outputs of the first to fourth driving means individually by the control unit, the rotational speed of the first to fourth propellers is changed. The aircraft can be easily lifted and the direction of travel can be easily controlled.

請求項2に記載の発明にあっては、前記機体は、前記制御部及び電池を収納する上部本体と、この上部本体の下部に設けられた矩形板状に形成された下部本体とから構成され、前記下部本体の4辺形を形成する4隅の位置にそれぞれ取付け孔が開口され、該取付け孔に前記第1〜第4のプロペラが配置されていることを特徴とするものである。下部本体の4辺形を形成する4隅の位置に開口させた取付け孔に第1〜第4のプロペラを配置することが簡単にできる。   According to a second aspect of the present invention, the airframe is composed of an upper body that houses the control unit and the battery, and a lower body that is formed in a rectangular plate shape and is provided at the lower portion of the upper body. The mounting holes are opened at the four corners forming the quadrilateral of the lower body, and the first to fourth propellers are arranged in the mounting holes. It is possible to easily arrange the first to fourth propellers in the mounting holes opened at the positions of the four corners forming the quadrilateral shape of the lower body.

請求項3に記載の発明にあっては、前記第1〜4のプロペラは、前記機体の4辺形を形成する4隅の一方の対角線上に位置する一対のプロペラが一方方向に回転駆動され、他方の対角線上に位置する一対のプロペラが異なる他方方向に回転駆動されることを特徴とするものである。一方の対角線上に位置する一対のプロペラと他方の対角線上に位置する一対のプロペラとを互いに反対方向に回転させることで、前進、後退、左右への旋回を制御することができる。   According to a third aspect of the present invention, the first to fourth propellers are configured such that a pair of propellers positioned on one diagonal line of the four corners forming the quadrilateral of the airframe are rotationally driven in one direction. The pair of propellers positioned on the other diagonal line are rotationally driven in different other directions. By rotating the pair of propellers located on one diagonal line and the pair of propellers located on the other diagonal line in opposite directions, forward, backward, and left / right turning can be controlled.

請求項4に記載の発明にあっては、前記第1〜4のプロペラは、前記機体の4辺形を形成する4隅の右側に位置する一対のプロペラが一方方向に回転駆動され、左側に位置する一対のプロペラが異なる他方方向に回転駆動されることを特徴とするものである。4隅の右側に位置する一対のプロペラと左側に位置する一対のプロペラとを互いに反対方向に回転させることで、前進、後退、左右への旋回を制御することができる。   In a fourth aspect of the invention, the first to fourth propellers are configured such that a pair of propellers positioned on the right side of the four corners forming the quadrilateral shape of the airframe are rotationally driven in one direction, and on the left side. A pair of positioned propellers are rotationally driven in different directions. By rotating the pair of propellers located on the right side of the four corners and the pair of propellers located on the left side in opposite directions, it is possible to control forward, backward, and left / right turning.

請求項5に記載の発明にあっては、前記送信機は、前記第1〜4の駆動手段の駆動出力をそれぞれ個別に上昇又は下降制御する信号を生成するための操作レバーを有することを特徴とするものである。操作レバーにより第1〜4の駆動手段の駆動出力を個別に上昇又は下降制御する信号を生成することができる。   According to a fifth aspect of the present invention, the transmitter has an operation lever for generating a signal for individually controlling the driving output of the first to fourth driving means to be raised or lowered. It is what. A signal for individually raising or lowering the drive output of the first to fourth drive means can be generated by the operation lever.

請求項6に記載の発明にあっては、前記操作レバーは、垂直な状態から一方側及び他方側へ回動操作する右の操作レバー及び左の操作レバーを有し、それぞれの前記右の操作レバー及び左の操作レバーの一方側及び他方側への回動操作に対応させて、前記第1〜4の駆動手段のいずれか1つの駆動出力を個別に上昇又は下降制御する信号を生成するものであることを特徴とするものである。右の操作レバー及び左の操作レバーの操作により走行制御を簡単に行うことができる。   According to a sixth aspect of the present invention, the operation lever includes a right operation lever and a left operation lever that are rotated from the vertical state to the one side and the other side, and each of the right operation levers. A signal for individually raising or lowering the drive output of any one of the first to fourth drive means in response to the turning operation of the lever and the left operation lever to one side and the other side. It is characterized by being. Travel control can be easily performed by operating the right control lever and the left control lever.

請求項7に記載の発明にあっては、前記送信機は、前記第1〜4の駆動手段の駆動出力をそれぞれ個別に上昇又は下降制御する信号を生成するための操作ボタンを有することを特徴とするものである。操作ボタンにより第1〜4の駆動手段の駆動出力を個別に上昇又は下降制御する信号を生成することが可能になる。   In a seventh aspect of the present invention, the transmitter has an operation button for generating a signal for individually raising or lowering the driving output of the first to fourth driving means. It is what. It becomes possible to generate a signal for individually controlling the driving output of the first to fourth driving means to be raised or lowered by the operation button.

請求項8に記載の発明にあっては、前記操作ボタンは、それぞれ前後左右の前記第1〜4の駆動手段に対応させた4つの操作ボタンを有することを特徴とするものである。4つの操作ボタンの操作により走行制御を簡単に行うことが可能になる。   According to an eighth aspect of the present invention, the operation buttons include four operation buttons respectively corresponding to the first to fourth driving means on the front, rear, left and right sides. Travel control can be easily performed by operating the four operation buttons.

本発明では、、低部側が平坦な底面を有する矩形板状に形成された機体と、機体の低部側の少なくとも4辺形を形成する4隅に設けられ底面側へ送風して機体を浮上させる第1〜4のプロペラと、第1〜4のプロペラをそれぞれ駆動する第1〜4の駆動手段と、第1〜4の駆動手段の駆動出力をそれぞれ個別に制御する制御部と、飛行のための制御信号を外部から制御部へ送信する送信機と、第1〜4の駆動手段及び制御部へ電源を供給する電池とを備えたことで、送信機から飛行のための制御信号を制御部へ送信し、この制御部で第1〜4の駆動手段の駆動出力をそれぞれ個別に制御して第1〜4のプロペラの回転速度を変えることで、機体の浮上を容易にでき走行方向の制御も簡単にできる。   In the present invention, the airframe is formed in a rectangular plate shape having a flat bottom surface on the lower portion side, and is provided at four corners forming at least four sides on the lower portion side of the airframe to float the airframe to the bottom surface side. First to fourth propellers to be driven, first to fourth drive means for driving the first to fourth propellers, a control unit for individually controlling drive outputs of the first to fourth drive means, The control signal for the flight is controlled from the transmitter by including a transmitter that transmits a control signal for external control to the control unit, and a battery that supplies power to the first to fourth driving units and the control unit. The control unit controls the drive outputs of the first to fourth drive units individually to change the rotation speed of the first to fourth propellers, thereby making it easy to float the aircraft. Control is also easy.

以下、本発明を図示の一実施形態により具体的に説明する。図1〜図7は本発明の第1実施形態の無線操縦飛行玩具の構成を説明する図であり、図1は無線操縦飛行玩具の斜視図、図2は無線操縦飛行玩具の平面図、図3は図2の無線操縦飛行玩具のA―A線断面図、図4は無線操縦飛行玩具の背面図、図5は無線操縦飛行玩具の側面図、図6は無線操縦飛行玩具の底面図、図7は無線操縦飛行玩具の制御動作を説明するブロック図である。   Hereinafter, the present invention will be specifically described with reference to an illustrated embodiment. 1 to 7 are diagrams for explaining the configuration of the radio controlled flying toy according to the first embodiment of the present invention. FIG. 1 is a perspective view of the radio controlled flying toy. FIG. 2 is a plan view of the radio controlled flying toy. 3 is a cross-sectional view of the radio-controlled flying toy of FIG. 2 taken along line AA, FIG. 4 is a rear view of the radio-controlled flying toy, FIG. 5 is a side view of the radio-controlled flying toy, and FIG. FIG. 7 is a block diagram for explaining the control operation of the radio controlled flying toy.

これらの図において、本発明の第1実施形態の無線操縦飛行玩具10は、屋外における地面や水面、あるいは屋内における床面等の平坦な走行面1上を浮上して自由に飛行させ、楽しむことができる飛行玩具である。この無線操縦飛行玩具10は、機体11と、この機体11の低部側の4辺形を形成する4隅の位置に下方の走行面1側へ向けて送風するように設けらた第1〜第4のプロペラ16a,16b,16c,16dと、これら第1〜第4のプロペラ16a,16b,16c,16dをそれぞれ駆動する第1〜4の駆動手段17a,17b,17c,17dと、これら第1〜4の駆動手段17a,17b,17c,17dの駆動出力をそれぞれ個別に制御する機体11に搭載された制御部20と、飛行のための制御信号を外部から制御部20へ送信するための送信機30と、第1〜4の駆動手段17a,17b,17c,17d及び制御部20へ電源を供給する電池21等とを備えている。   In these figures, the radio controlled flying toy 10 of the first embodiment of the present invention floats freely on a flat traveling surface 1 such as the ground or water surface outdoors, or a floor surface indoors, and can freely fly and enjoy it. It is a flying toy. This radio-controlled flying toy 10 is provided with a body 11 and first to first air blown toward the lower traveling surface 1 side at the positions of four corners forming the lower quadrilateral of the body 11. Fourth propellers 16a, 16b, 16c, 16d, first to fourth driving means 17a, 17b, 17c, 17d for driving the first to fourth propellers 16a, 16b, 16c, 16d, respectively, The control unit 20 mounted on the airframe 11 that individually controls the drive outputs of the first to fourth drive units 17a, 17b, 17c, and 17d, and a control signal for flight to the control unit 20 from the outside The transmitter 30 includes first to fourth driving units 17a, 17b, 17c, and 17d, a battery 21 that supplies power to the control unit 20, and the like.

機体11は、上部本体12と、この上部本体12の下部に設けられた下部本体13とから構成され、例えば、それぞれ軽量なプラスチック材料等により成形されている。この上部本体12は、走行方向に沿った前後に細長いケース状に形成され、その内部には制御部20を構成する回路基板及び電池21等が収納され、後部側の上部には受信用のアンテナ22が取り付けられている。下部本体13は、低部側が走行面1に平行な平坦な底面14を有し、走行方向の前側の左右部分がそれぞれ半円形状に前方へ突出され、また、走行方向の後側の左右部分が半円形状にそれぞれ後方へ突出され、全体として矩形板状に形成されている。この下部本体13の中央部上面に、上部本体12が取り付けられている。この矩形板状に形成された下部本体13の4辺形を形成する前側及び後側の左右の4隅の位置には、円形状の取付け孔15a,15b,15c,15dが開口されている。これらの取付け孔15a,15b,15c,15dには、それぞれ走行面1側へ送風するための第1〜第4のプロペラ16a,16b,16c,16dが配置されている。これらの第1〜第4のプロペラ16a,16b,16c,16dは、それぞれ第1〜4の駆動手段17a,17b,17c,17dにより駆動されるようになっている。これらの第1〜4の駆動手段17a,17b,17c,17dは、例えば、取付け孔15a,15b,15c,15dの中心位置において駆動軸を下方に向けて突出させて配置された電動モータであり、それぞれの駆動軸に第1〜第4のプロペラ16a,16b,16c,16dが取付けられている。これらの第1〜4の駆動手段17a,17b,17c,17dは、例えば、板状に形成された複数本の取付け部材18a,18b,18c,18dにより、それぞれ下部本体13の対応する取付け孔15a,15b,15c,15dに取付けられている。すなわち、これらの第1〜4の駆動手段17a,17b,17c,17dは、それぞれの第1〜第4のプロペラ16a,16b,16c,16dが取付けられる出力軸を、対応する取付け孔15a,15b,15c,15dの中心において垂直に下方に向けた位置に取付けられている。また、図2に示すように、機体11の4辺形を形成する4隅の一方の対角線上に位置する一対の第1のプロペラ16a及び第4のプロペラ16dは、同じ右方向に回転駆動され、他方の対角線上に位置する一対の第2プロペラ16b及び第3のプロペラ16cは、同じ左方向に回転駆動されるようになっている。   The body 11 is composed of an upper body 12 and a lower body 13 provided at the lower part of the upper body 12, and is formed of, for example, a lightweight plastic material. The upper main body 12 is formed in a long and narrow case shape in the front and rear direction along the traveling direction, and a circuit board and a battery 21 constituting the control unit 20 are housed therein, and a receiving antenna is disposed in the upper part on the rear side. 22 is attached. The lower body 13 has a flat bottom surface 14 whose lower side is parallel to the running surface 1, the left and right parts on the front side in the running direction project forward in a semicircular shape, and the left and right parts on the rear side in the running direction Are projected rearward in a semicircular shape, and are formed in a rectangular plate shape as a whole. The upper main body 12 is attached to the upper surface of the central portion of the lower main body 13. Circular mounting holes 15a, 15b, 15c, and 15d are opened at the positions of the four left and right corners on the front side and the rear side that form the quadrilateral shape of the lower body 13 formed in the rectangular plate shape. In these mounting holes 15a, 15b, 15c, and 15d, first to fourth propellers 16a, 16b, 16c, and 16d for blowing air toward the traveling surface 1 are disposed. These first to fourth propellers 16a, 16b, 16c and 16d are driven by first to fourth driving means 17a, 17b, 17c and 17d, respectively. These first to fourth drive means 17a, 17b, 17c, 17d are, for example, electric motors that are arranged with the drive shaft protruding downward at the center position of the mounting holes 15a, 15b, 15c, 15d. The first to fourth propellers 16a, 16b, 16c, and 16d are attached to the respective drive shafts. These first to fourth driving means 17a, 17b, 17c, and 17d are, for example, a plurality of mounting members 18a, 18b, 18c, and 18d formed in a plate shape, and corresponding mounting holes 15a of the lower body 13 respectively. , 15b, 15c, 15d. In other words, the first to fourth driving means 17a, 17b, 17c, and 17d have output shafts to which the first to fourth propellers 16a, 16b, 16c, and 16d are attached, corresponding mounting holes 15a and 15b. , 15c, 15d are attached at positions vertically downward. Further, as shown in FIG. 2, the pair of first propeller 16a and fourth propeller 16d located on one diagonal line of the four corners forming the quadrilateral of the body 11 are rotationally driven in the same right direction. The pair of second propeller 16b and the third propeller 16c located on the other diagonal line are rotationally driven in the same left direction.

制御部20は、上部本体12の内部に配置された走行制御のための回路基板であり、図7に示すように、電源スイッチ19と、送信機30から送信されてくる制御信号をアンテナ22を介して受信する受信回路23と、この受信回路23で受信された信号に基づき制御信号を生成する制御回路24と、この制御回路24の制御信号に基づいて第1〜4の駆動手段17a,17b,17c,17dの駆動出力を制御する駆動回路25等とから構成されている。また、上部本体12の内部に配置された電池21は、受信回路23、制御回路24、駆動回路25及び第1〜4の駆動手段17a,17b,17c,17dへ電源を供給する。   The control unit 20 is a circuit board for traveling control disposed inside the upper main body 12. As shown in FIG. 7, the control signal transmitted from the power switch 19 and the transmitter 30 is transmitted to the antenna 22. A receiving circuit 23 received via the control circuit 24, a control circuit 24 for generating a control signal based on the signal received by the receiving circuit 23, and first to fourth driving means 17a, 17b based on the control signal of the control circuit 24. , 17c, 17d, and the like. The battery 21 disposed inside the upper body 12 supplies power to the receiving circuit 23, the control circuit 24, the driving circuit 25, and the first to fourth driving units 17a, 17b, 17c, and 17d.

送信機30は、走行のための制御信号を制御部20へ送信する部分であり、例えば、電源スイッチ36と、走行制御のための操作を行う操作部33と、この操作部33の操作に基づく信号を生成する信号生成回路34と、この信号生成回路34からの信号を電波等として送信する送信回路31と、送信用のアンテナ35と、信号生成回路34や送信回路31へ電源を供給する電池32等とから構成されている。また、この送信機30は、図1に示すように、送信用のアンテナ35が設けられた人が手に持って操作するケース部を有し、その操作部33は、指先で操作する右の操作レバー37及び左の操作レバー38がケース部表面に垂直に突出するように設けられている。これらの右の操作レバー37及び左の操作レバー38は、それぞれアンテナ35が設けられた側(上側)及び反対側(下側)に垂直な状態からスプリング等の付勢力に抗して指先で上下に回動操作させることができるものである。右の操作レバー37は、下部本体14の右側に位置する第2の駆動手段17b及び第4の駆動手段17dの駆動出力を制御するためのレバーであり、左の操作レバー38は、下部本体14の左側に位置する第1の駆動手段17a及び第3の駆動手段17cの駆動出力を制御するためのレバーである。この右の操作レバー37は、上側に回動操作したときには、第4の駆動手段17dの駆動出力を通常の60%から100%程度まで上昇させ、下側に回動操作したときには、第2の駆動手段17bの駆動出力を通常の60%から100%程度まで上昇させるものである。また、左の操作レバー38は、上側に回動操作したときには、第3の駆動手段17cの駆動出力を通常の60%から100%程度まで上昇させ、下側に回動操作したときには、第1の駆動手段17aの駆動出力を通常の60%から100%程度まで上昇させるものである。   The transmitter 30 is a part that transmits a control signal for traveling to the control unit 20. For example, the transmitter 30 is based on a power switch 36, an operation unit 33 that performs an operation for traveling control, and an operation of the operation unit 33. A signal generation circuit 34 that generates a signal, a transmission circuit 31 that transmits a signal from the signal generation circuit 34 as a radio wave, a transmission antenna 35, and a battery that supplies power to the signal generation circuit 34 and the transmission circuit 31 32 etc. Further, as shown in FIG. 1, the transmitter 30 has a case part that is operated by a person provided with an antenna 35 for transmission, and the operation part 33 has a right part operated by a fingertip. An operation lever 37 and a left operation lever 38 are provided so as to protrude perpendicularly to the surface of the case portion. The right operating lever 37 and the left operating lever 38 are moved up and down with a fingertip against a biasing force of a spring or the like from a state perpendicular to the side (upper side) and the opposite side (lower side) where the antenna 35 is provided. Can be rotated. The right operation lever 37 is a lever for controlling the drive output of the second drive means 17b and the fourth drive means 17d located on the right side of the lower body 14, and the left operation lever 38 is the lower body 14 It is a lever for controlling the drive output of the 1st drive means 17a and the 3rd drive means 17c which are located in the left side. When the right operating lever 37 is rotated upward, the drive output of the fourth driving means 17d is raised from the normal 60% to about 100%, and when it is rotated downward, the second operating lever 37d The drive output of the drive means 17b is raised from the normal 60% to about 100%. When the left operating lever 38 is turned upward, the drive output of the third driving means 17c is raised from the normal 60% to about 100%, and when it is turned downward, the first operating lever 38 The drive output of the drive means 17a is increased from the normal 60% to about 100%.

次に、上記構成の無線操縦飛行玩具10の動作を説明する。図8〜図14は本発明の第1実施形態の無線操縦飛行玩具の動作を説明する図であり、図8は無線操縦飛行玩具が浮上する状態を説明する図、図9は無線操縦飛行玩具が前進する状態を説明する図、図10は無線操縦飛行玩具が浮上するときの送信機の操作を説明する図、図11は無線操縦飛行玩具が前進するときの送信機の操作を説明する図、図12は無線操縦飛行玩具が後退するときの送信機の操作を説明する図、図13は無線操縦飛行玩具が右旋回するときの送信機の操作を説明する図、図14は無線操縦飛行玩具が左旋回するときの送信機の操作を説明する図である。   Next, the operation of the radio controlled flying toy 10 having the above configuration will be described. 8 to 14 are views for explaining the operation of the radio controlled flying toy according to the first embodiment of the present invention. FIG. 8 is a view for explaining the state of the radio controlled flying toy. FIG. FIG. 10 is a diagram for explaining the operation of the transmitter when the radio controlled flying toy rises. FIG. 11 is a diagram for explaining the operation of the transmitter when the radio controlled flying toy moves forward. FIG. 12 is a diagram for explaining the operation of the transmitter when the radio-controlled flying toy moves backward, FIG. 13 is a diagram for explaining the operation of the transmitter when the radio-controlled flying toy turns right, and FIG. It is a figure explaining operation of a transmitter when a flying toy turns left.

まず、無線操縦玩具10を動作させるためには、その下部本体13の平坦な底面14を走行面1上に配置する。続いて、電源スイッチ19をオンにしたとき、制御部20の駆動回路25により、第1〜4の駆動手段17a,17b,17c,17dが全て60%の同一の駆動出力で駆動され、それぞれの出力軸に取付けられている第1〜第4のプロペラ16a,16b,16c,16dが全て同一の速度で回転し、それぞれの取付け孔15a,15b,15c,15dから下方の走行面1側へ向けて空気が送られる。これらの取付け孔15a,15b,15c,15dから下方へ向けて送られた空気は、図8に示すように、下部本体13の平坦な底面14と走行面1との間に送られ、下部本体13の周囲に向けて流れることで、下部本体13の底面14と走行面1との間に空気の流れる空間が生じ、機体11が停止状態で走行面1上に浮上する。このとき、一方の対角線上に位置する一対の第1プロペラ16a及び第4のプロペラ16dと、他方の対角線上に位置する第2プロペラ16b及び第3のプロペラ16cとが互いに反対方向に同一速度で駆動されるため、それぞれの第1〜第4のプロペラ16a,16b,16c,16dの回転による機体11を反転させる力がバランスして、機体11は左右に旋回することなくその場で走行面1上に浮上する。このとき、電源スイッチ36をオンにした送信機30は、図10に示すように、操作部33の右の操作レバー37及び左の操作レバー38は、指先で操作していない垂直な状態になっている。   First, in order to operate the radio controlled toy 10, the flat bottom surface 14 of the lower main body 13 is disposed on the traveling surface 1. Subsequently, when the power switch 19 is turned on, the drive circuit 25 of the control unit 20 drives all of the first to fourth drive means 17a, 17b, 17c, and 17d with the same drive output of 60%. The first to fourth propellers 16a, 16b, 16c, 16d attached to the output shaft all rotate at the same speed, and are directed from the respective attachment holes 15a, 15b, 15c, 15d to the lower running surface 1 side. Air is sent. The air sent downward from these mounting holes 15a, 15b, 15c, 15d is sent between the flat bottom surface 14 of the lower body 13 and the running surface 1, as shown in FIG. By flowing toward the periphery of 13, a space in which air flows is created between the bottom surface 14 of the lower main body 13 and the traveling surface 1, and the body 11 floats on the traveling surface 1 in a stopped state. At this time, the pair of first propeller 16a and the fourth propeller 16d located on one diagonal line and the second propeller 16b and the third propeller 16c located on the other diagonal line are at the same speed in opposite directions. Since the first to fourth propellers 16a, 16b, 16c, and 16d are rotated, the forces for reversing the airframe 11 are balanced, so that the airframe 11 does not turn left and right, and the traveling surface 1 on the spot. Rise to the top. At this time, in the transmitter 30 with the power switch 36 turned on, as shown in FIG. 10, the right operation lever 37 and the left operation lever 38 of the operation unit 33 are in a vertical state where they are not operated with the fingertips. ing.

次に、無線操縦玩具10を浮上させた状態から前進させるときには、図11に示すように、送信機30の操作部33において右の操作レバー37及び左の操作レバー38を指先で同時にアンテナ35側(上側)へ回動操作させると、信号生成回路34において第3の駆動手段17c及び第4の駆動手段17dの駆動出力を60%から100%へ上昇させる信号が生成され、その信号が送信回路31からアンテナ35を介して送信される。この前進のための信号は、制御部20のアンテナ22から受信回路23で受信され、さらに制御回路24から駆動回路25へ伝達され、対応する第3の駆動手段17c及び第4の駆動手段17dの駆動出力が60%から100%へ上昇する。これら第3の駆動手段17c及び第4の駆動手段17dの駆動出力の上昇により、後部側の左右に配置された第3のプロペラ16c及び第4のプロペラ16dの回転速度が上昇し、図9に示すように、機体11の後部側の送風量が増加することで、機体11が前進する。このとき、後部側の左右の第3のプロペラ16c及び第4のプロペラ16dの回転速度が上昇しても、互いに反対方向に回転しているため、機体11を反転させる力がバランスして、機体11は左右に旋回することなく前進させることができる。   Next, when the radio controlled toy 10 is moved forward from the floated state, the right operating lever 37 and the left operating lever 38 are simultaneously operated with the fingertips on the antenna 35 side in the operating unit 33 of the transmitter 30, as shown in FIG. When rotating upward (upward), the signal generation circuit 34 generates a signal for increasing the drive output of the third drive unit 17c and the fourth drive unit 17d from 60% to 100%, and the signal is transmitted to the transmission circuit. 31 through the antenna 35. The signal for forward movement is received by the receiving circuit 23 from the antenna 22 of the control unit 20, and further transmitted from the control circuit 24 to the driving circuit 25, and the corresponding third driving means 17c and fourth driving means 17d. The drive output increases from 60% to 100%. By increasing the drive outputs of the third drive means 17c and the fourth drive means 17d, the rotational speeds of the third propeller 16c and the fourth propeller 16d arranged on the left and right sides on the rear side increase, and FIG. As shown, the airframe 11 moves forward by increasing the air flow rate on the rear side of the airframe 11. At this time, even if the rotational speeds of the left and right third propeller 16c and fourth propeller 16d on the rear side are increased, they rotate in opposite directions, so that the forces for reversing the airframe 11 balance and the airframe 11 can be advanced without turning left and right.

次に、無線操縦玩具10を浮上させた状態から後退させるときには、図12に示すように、送信機30の操作部33において右の操作レバー37及び左の操作レバー38を指先で同時にアンテナ35と反対側(下側)へ回動操作させると、上記と同様に信号生成回路34で第1の駆動手段17a及び第2の駆動手段17bの駆動出力を60%から100%へ上昇させる信号が生成される。この信号を受信した制御部20の駆動回路25は、第1の駆動手段17a及び第2の駆動手段17bの駆動出力を上昇させ、前部側の左右に配置された第1のプロペラ16a及び第2のプロペラ16bの回転速度が上昇し、図12に示すように、機体11の前部側の左右の送風量が増加することで、機体11が後退する。このとき、前進の場合と同様に、第1のプロペラ16a及び第2のプロペラ16bの回転速度が上昇しても、互いに反対方向に回転しているため、機体11を反転させる力がバランスして、機体11は左右に旋回することなく後退させることができる。   Next, when the radio controlled toy 10 is retracted from the floated state, as shown in FIG. 12, the right operating lever 37 and the left operating lever 38 are simultaneously connected to the antenna 35 with the fingertips in the operating unit 33 of the transmitter 30. When rotating to the opposite side (downward), the signal generation circuit 34 generates a signal for increasing the drive output of the first drive means 17a and the second drive means 17b from 60% to 100% as described above. Is done. Receiving this signal, the drive circuit 25 of the control unit 20 increases the drive outputs of the first drive unit 17a and the second drive unit 17b, and the first propeller 16a and the first propeller 16a arranged on the left and right of the front side. The rotational speed of the second propeller 16b is increased, and as shown in FIG. 12, the left and right blast volumes on the front side of the body 11 are increased, so that the body 11 moves backward. At this time, as in the case of the forward movement, even if the rotation speeds of the first propeller 16a and the second propeller 16b are increased, the forces that reverse the airframe 11 are balanced because they rotate in opposite directions. The airframe 11 can be moved backward without turning left and right.

次に、無線操縦玩具10を浮上させた状態から右旋回させるときには、図13に示すように、送信機30の操作部33において右の操作レバー37を下側へ指先で回動させ、左の操作レバー38を指先で上側へ回動操作させると、それぞれのレバーに対応した第2の駆動手段17b及び第3の駆動手段17cの駆動出力の上昇に従って、右前の第2プロペラ16b及び左後の第3のプロペラ16cの回転速度が上昇する。これらの第2のプロペラ16b及び第3のプロペラ16cは、図2に示すように、同一の方向で左回転しているため、それらの回転速度の上昇が、機体11を右旋回させる力を生じさせる。従って、図13に示すレバー操作により、機体11を浮上させた状態から右旋回させることができる。なお、第2のプロペラ16b及び第3のプロペラ16cの回転速度の上昇に伴う送風量の増加は、互いに打ち消す力を生じ右旋回させる動作に大きな影響を与えないことが確認された。   Next, when the radio controlled toy 10 is turned right from the state where the radio controlled toy 10 is lifted, as shown in FIG. 13, the right operation lever 37 is rotated downward with the fingertip in the operation unit 33 of the transmitter 30, and the left When the operation lever 38 is rotated upward with the fingertip, the right front second propeller 16b and the left rear are increased in accordance with the increase in the drive output of the second drive means 17b and the third drive means 17c corresponding to each lever. The rotational speed of the third propeller 16c increases. Since these second propeller 16b and third propeller 16c are rotating counterclockwise in the same direction, as shown in FIG. 2, an increase in their rotational speed causes a force to turn the body 11 to the right. Cause it to occur. Therefore, the lever 11 shown in FIG. 13 can be turned to the right from the state where the body 11 is lifted. In addition, it was confirmed that the increase in the amount of air flow accompanying the increase in the rotation speed of the second propeller 16b and the third propeller 16c does not greatly affect the operation of turning right by generating a force to cancel each other.

次に、無線操縦玩具10を浮上させた状態から左旋回させるときには、図14に示すように、送信機30の操作部33において右の操作レバー37を上側へ指先で回動させ、左の操作レバー38を指先で下側へ回動操作させると、それぞれのレバーに対応した第4の駆動手段17d及び第1の駆動手段17aの駆動出力の上昇に従って、右後の第4のプロペラ16d及び左前の第1のプロペラ16aの回転速度が上昇する。これらの第4のプロペラ16d及び第1のプロペラ16aは、図2に示すように、同一の方向で右回転しているため、それらの回転速度の上昇が、機体11を左旋回させる力を生じさせる。従って、図14に示すレバー操作により、無線操縦玩具10を浮上させた状態から左旋回させることができる。なお、前記の右旋回の場合と同様に、第4のプロペラ16d及び第1のプロペラ16aの回転速度の上昇に伴う送風量の増加は、左旋回させる動作に大きな影響を与えないことが確認された。   Next, when the radio controlled toy 10 is turned left from the state where it is levitated, as shown in FIG. 14, in the operation unit 33 of the transmitter 30, the right operation lever 37 is rotated upward with the fingertip, and the left operation is performed. When the lever 38 is turned downward with the fingertip, the right rear fourth propeller 16d and the left front are increased in accordance with the increase in the drive output of the fourth drive means 17d and the first drive means 17a corresponding to each lever. The rotational speed of the first propeller 16a increases. Since the fourth propeller 16d and the first propeller 16a rotate rightward in the same direction as shown in FIG. 2, the increase in their rotational speed generates a force for turning the airframe 11 counterclockwise. Let Therefore, by the lever operation shown in FIG. 14, the radio controlled toy 10 can be turned left from the state where it is levitated. As in the case of the right turn described above, it is confirmed that the increase in the air flow rate accompanying the increase in the rotation speed of the fourth propeller 16d and the first propeller 16a does not significantly affect the left turn operation. It was done.

以上説明した通り、本発明の第1実施形態の無線操縦飛行玩具10では、機体11の低部側の4隅のそれぞれに下方の走行面1側へ送風するように設けた第1〜第4のプロペラ16a,16b,16c,16dを、それぞれ第1〜4の駆動手段17a,17b,17c,17dにより駆動させ、4隅の4辺形を形成する一方の対角線上に位置する一対の第1プロペラ16a及び第4のプロペラ16dと、他方の対角線上に位置する第2プロペラ16b及び第3のプロペラ16cとを互いに反対方向に回転させ、送信機30から送信される信号に基づいて、制御部20によりそれぞれ第1〜4の駆動手段17a,17b,17c,17dの駆動出力を制御している。そして、浮上させるときには第1〜第4のプロペラ16a,16b,16c,16dを同一の60%程度の低速度で回転させ、前進させるときには後部側の左右の第3のプロペラ16c及び第4のプロペラ16dの回転速度を上昇させ、後退させるときには前部側の左右の第1のプロペラ16a及び第2のプロペラ16bの回転速度を上昇させ、右旋回するときには第2のプロペラ16b及び第3のプロペラ16cの回転速度を上昇させ、左旋回するときには第1プロペラ16a及び第4のプロペラ16dの回転速度を上昇させている。従って、本実施形態の無線操縦玩具10では、構造も簡単になり、従来のエアクッション機玩具等のように浮上用送風機や推進用送風機を駆動するために大きな駆動電源を必要とせず、消費電力を小さくでき長時間の飛行が可能になり、平坦な走行面1上を浮上して自由に飛行させて楽しむことができる。   As described above, in the radio controlled flying toy 10 according to the first embodiment of the present invention, the first to fourth parts are provided so as to blow to the lower traveling surface 1 side at each of the four corners on the lower part side of the body 11. The propellers 16a, 16b, 16c, and 16d are driven by the first to fourth driving means 17a, 17b, 17c, and 17d, respectively, and a pair of firsts positioned on one diagonal line that forms a quadrilateral of four corners. Based on the signal transmitted from the transmitter 30, the propeller 16 a and the fourth propeller 16 d and the second propeller 16 b and the third propeller 16 c located on the other diagonal are rotated in opposite directions. 20 controls the drive outputs of the first to fourth drive means 17a, 17b, 17c and 17d, respectively. Then, the first to fourth propellers 16a, 16b, 16c, 16d are rotated at the same low speed of about 60% when levitating, and the left and right third propellers 16c and fourth propellers are moved forward. The rotational speed of 16d is increased, and when rotating backward, the rotational speeds of the left and right first propellers 16a and 16b are increased, and when turning right, the second propeller 16b and the third propeller are rotated. The rotational speed of 16c is increased, and the rotational speed of the first propeller 16a and the fourth propeller 16d is increased when turning left. Therefore, in the radio-controlled toy 10 of the present embodiment, the structure is simplified, and a large driving power source is not required for driving the levitation blower and the propulsion blower unlike the conventional air cushion toy and the power consumption. It is possible to make the flight smaller and to fly for a long time, so that the user can fly freely on the flat running surface 1 and enjoy it.

上記の第1実施形態の無線操縦飛行玩具10では、一方の対角線上に位置する一対の第1のプロペラ16a及び第4のプロペラ16dが右方向に回転駆動され、他方の対角線上に位置する一対の第2のプロペラ16b及び第3のプロペラ16cが左方向に回転駆動される例で説明したが、一方側を左方向に、他方側を右方向に回転駆動させるようにしてもよく、このような場合には、前進及び後退のレバー操作は同一であるが右旋回と左旋回の操作は反対になる。また、送信機30のレバー操作に対応させて、第1〜4の駆動手段17a,17b,17c,17dの駆動出力を60%から100%へ上昇させているが、駆動出力を逆に100%から60%へ下降させるようにしても走行制御ができ、このような場合には、同じレバー操作による走行動作も異なってくる。さらに、右の操作レバー37または左の操作レバー38の一方側のみを回動させることで、旋回動作をさせることができる。   In the radio controlled flying toy 10 of the first embodiment, the pair of first propeller 16a and the fourth propeller 16d positioned on one diagonal line are rotationally driven in the right direction and the pair positioned on the other diagonal line. The second propeller 16b and the third propeller 16c are driven to rotate leftward, but one side may be rotated leftward and the other side rotated rightward. In this case, the forward and backward lever operations are the same, but the right and left turn operations are opposite. Further, the drive output of the first to fourth drive means 17a, 17b, 17c, and 17d is increased from 60% to 100% corresponding to the lever operation of the transmitter 30, but the drive output is 100% on the contrary. The traveling control can be performed even when the vehicle is lowered to 60%. In such a case, the traveling operation by the same lever operation is different. Furthermore, the turning operation can be performed by rotating only one side of the right operation lever 37 or the left operation lever 38.

図15及び図16は本発明の第2実施形態の無線操縦飛行玩具の構成を説明する図であり、図15は無線操縦飛行玩具の斜視図、図16は無線操縦飛行玩具の平面図である。なお、第1実施形態に対応する部分及び部材は同一の符号を記し詳細の説明を省略する。   15 and 16 are views for explaining the configuration of the radio controlled flying toy according to the second embodiment of the present invention. FIG. 15 is a perspective view of the radio controlled flying toy, and FIG. 16 is a plan view of the radio controlled flying toy. . Note that portions and members corresponding to the first embodiment are denoted by the same reference numerals, and detailed description thereof is omitted.

本発明の第2実施形態の無線操縦飛行玩具40は、第1実施形態と同様に、機体11の低部側の下部本体13の4辺形を形成する4隅のそれぞれに、第1〜第4のプロペラ16a,16b,16c,16dと、これら第1〜第4のプロペラ16a,16b,16c,16dをそれぞれ駆動する第1〜4の駆動手段17a,17b,17c,17dと、これら第1〜4の駆動手段17a,17b,17c,17dの駆動出力をそれぞれ個別に制御する制御部20と、第1〜4の駆動手段17a,17b,17c,17d及び制御部20へ電源を供給する電池21等とを備え、ボタン操作による飛行のための制御信号を外部から制御部20へ送信するための送信機50を備えたものである。また、この無線操縦飛行玩具40は、第1実施形態と異なり、図16に示すように、左側の第1のプロペラ16a及び第3のプロペラ16cが同一の左方向に回転駆動され、右側の第2のプロペラ16b及び第4のプロペラ16dが同一の右方向に回転駆動されている。送信機50は、図15に示すように、送信用のアンテナ35が設けられた人が手に持って操作するケース部を有し、その操作部33は、左右上下に指先で操作する4つの操作ボタン51,52,53,54が設けられている。これらの操作ボタン51,52,53,54は、それぞれを個別に押す操作を行うことで、対応する第1〜4の駆動手段17a,17b,17c,17dの駆動出力を通常の60%から100%程度まで上昇させる信号を送信するものであり、その他の回路構成は第1実施形態の送信機30と同様である。   The radio-controlled flying toy 40 according to the second embodiment of the present invention is similar to the first embodiment in each of the four corners forming the quadrilateral of the lower main body 13 on the lower side of the body 11. Four propellers 16a, 16b, 16c, 16d, first to fourth driving means 17a, 17b, 17c, 17d for driving the first to fourth propellers 16a, 16b, 16c, 16d, respectively, and the first The control unit 20 that individually controls the drive outputs of the fourth to fourth drive units 17a, 17b, 17c, and 17d, and the battery that supplies power to the first to fourth drive units 17a, 17b, 17c, and 17d and the control unit 20 21 and the like, and a transmitter 50 for transmitting a control signal for flying by button operation from the outside to the control unit 20. Also, unlike the first embodiment, the radio-controlled flying toy 40 is configured such that the left first propeller 16a and the third propeller 16c are rotationally driven in the same left direction as shown in FIG. The two propellers 16b and the fourth propeller 16d are rotationally driven in the same right direction. As shown in FIG. 15, the transmitter 50 has a case part that a person provided with an antenna 35 for transmission holds and operates, and the operation part 33 includes four parts that are operated with a fingertip in the left, right, up and down directions. Operation buttons 51, 52, 53, and 54 are provided. These operation buttons 51, 52, 53, 54 are operated by individually pressing them, so that the drive outputs of the corresponding first to fourth drive means 17 a, 17 b, 17 c, 17 d are reduced from the normal 60% to 100%. The other circuit configuration is the same as that of the transmitter 30 of the first embodiment.

次に、上記構成の無線操縦飛行玩具40の動作を説明する。図17〜図21は本発明の第2実施形態の無線操縦飛行玩具の動作を説明する図であり、図17は無線操縦飛行玩具が浮上するときの送信機の操作を説明する図、図18は無線操縦飛行玩具が前進するときの送信機の操作を説明する図、図19は無線操縦飛行玩具が後退するときの送信機の操作を説明する図、図20は無線操縦飛行玩具が右旋回するときの送信機の操作を説明する図、図21は無線操縦飛行玩具が左旋回するときの送信機の操作を説明する図である。   Next, the operation of the radio controlled flying toy 40 having the above configuration will be described. 17 to 21 are diagrams for explaining the operation of the radio controlled flying toy according to the second embodiment of the present invention, and FIG. 17 is a diagram for explaining the operation of the transmitter when the radio controlled flying toy floats. Is a diagram for explaining the operation of the transmitter when the radio controlled flying toy moves forward, FIG. 19 is a diagram for explaining the operation of the transmitter when the radio controlled flying toy moves backward, and FIG. FIG. 21 is a diagram illustrating the operation of the transmitter when the radio-controlled flying toy makes a left turn.

まず、無線操縦玩具40を動作させるためには、第1実施形態と同様に、電源スイッチ19をオンにしたとき、第1〜4の駆動手段17a,17b,17c,17dが全て60%の同一の駆動出力で駆動されて、第1〜第4のプロペラ16a,16b,16c,16dが全て同一の速度で回転し、底面14と走行面1との間に空気の流れる空間が生じ、機体11が停止状態で走行面1上に浮上する。このとき、左側の第1のプロペラ16a及び第3のプロペラ16cが左側に回転駆動され、右側の第2のプロペラ16b及び第4のプロペラ16dが右側に回転駆動されるため、機体11を反転させる力がバランスして、機体11は左右に旋回することなくその場で浮上する。このとき、送信機50は、図17に示すように、操作部33の操作ボタン51,52,53,54を操作していない(押していない)状態になっている。   First, in order to operate the radio controlled toy 40, as in the first embodiment, when the power switch 19 is turned on, the first to fourth driving means 17a, 17b, 17c, 17d are all 60% identical. The first to fourth propellers 16a, 16b, 16c, and 16d are all rotated at the same speed, and a space through which air flows between the bottom surface 14 and the traveling surface 1 is generated. Floats on the running surface 1 in a stopped state. At this time, the left first propeller 16a and the third propeller 16c are driven to rotate leftward, and the right second propeller 16b and the fourth propeller 16d are driven to rotate rightward, so that the airframe 11 is reversed. The force balances and the airframe 11 rises on the spot without turning left and right. At this time, as shown in FIG. 17, the transmitter 50 is in a state where the operation buttons 51, 52, 53, and 54 of the operation unit 33 are not operated (not pressed).

次に、無線操縦玩具40を浮上させた状態から前進させるときには、図18に示すように、送信機50の操作部33において下側の操作ボタン53,54を指先で同時に操作する(図18において操作するボタンを矢印で示している。以下の図面におけるボタン操作の説明も同様とする)。このボタン操作により、対応する第3の駆動手段17c及び第4の駆動手段17dの駆動出力が60%から100%へ上昇し、後部側の左右に配置された第3のプロペラ16b及び第4のプロペラ16dの回転速度が上昇し、第1実施形態と同様に機体11が前進する。このとき、後部側の左右の第3のプロペラ16c及び第4のプロペラ16dの回転速度が上昇しても、互いに反対方向に回転しているため、機体11を反転させる力がバランスして、機体11は旋回することなく前進させることができる。   Next, when the radio controlled toy 40 is moved forward from the state where it floats, the lower operation buttons 53 and 54 are simultaneously operated with the fingertips in the operation unit 33 of the transmitter 50 as shown in FIG. 18 (in FIG. 18). The buttons to be operated are indicated by arrows, and the same applies to the button operations in the following drawings). By this button operation, the drive output of the corresponding third drive means 17c and fourth drive means 17d increases from 60% to 100%, and the third propeller 16b and the fourth The rotational speed of the propeller 16d increases, and the airframe 11 moves forward as in the first embodiment. At this time, even if the rotational speeds of the left and right third propeller 16c and fourth propeller 16d on the rear side are increased, they rotate in opposite directions, so that the forces for reversing the airframe 11 balance and the airframe 11 can be advanced without turning.

次に、無線操縦玩具40を浮上させた状態から後退させるときには、図19に示すように、送信機50の操作部33において上側の操作ボタン51,52を指先で同時に操作する。このボタン操作により、対応する第1の駆動手段17a及び第2の駆動手段17bの駆動出力が60%から100%へ上昇し、前部側の左右に配置された第1のプロペラ16a及び第2のプロペラ16bの回転速度が上昇し、第1実施形態と同様に機体11が後退する。このとき、前部側の左右の第1のプロペラ16a及び第2のプロペラ16bの回転速度が上昇しても、互いに反対方向に回転しているため、機体11を反転させる力がバランスして、機体11は旋回することなく後退させることができる。   Next, when the radio controlled toy 40 is retracted from the state where it is lifted, the upper operation buttons 51 and 52 are simultaneously operated with the fingertips in the operation unit 33 of the transmitter 50 as shown in FIG. By this button operation, the driving output of the corresponding first driving means 17a and second driving means 17b is increased from 60% to 100%, and the first propeller 16a and the second propeller 16a arranged on the left and right on the front side The rotation speed of the propeller 16b increases, and the airframe 11 moves backward as in the first embodiment. At this time, even if the rotational speeds of the left and right first propellers 16a and 16b on the front side are increased, they are rotating in opposite directions, so the forces to reverse the airframe 11 are balanced, The airframe 11 can be retracted without turning.

次に、無線操縦玩具40を浮上させた状態から右旋回させるときには、図20に示すように、送信機30の操作部33において左側の操作ボタン51,53の両方又はいずれか一方、例えば、下側の操作ボタン53を指先で操作する。このボタン操作により、対応する第3の駆動手段17cの駆動出力が60%から100%へ上昇し、第3のプロペラ16cの回転速度が上昇する。この第3のプロペラ16cの回転速度の上昇により、機体11には第3のプロペラ16cの左回転方向と反対方向の右旋回させる力を生じさせる。従って、図20に示すように、ボタン操作により、無線操縦玩具40を浮上させた状態から右旋回させることができる。このとき第3のプロペラ16cの回転速度の上昇に伴う送風量の増加により、機体11を移動させる力も同時に加わるため第1実施形態の右旋回と異なる動作をする。なお、左側の操作ボタン51,53の両方を操作する場合には、左側の第1のプロペラ16a及び第3のプロペラ16cの回転速度の上昇に伴う送風量の増加により、機体11が右側へ移動した後に右旋回する動作が確認された。   Next, when the radio controlled toy 40 is turned rightward from the state where it is levitated, as shown in FIG. 20, in the operation unit 33 of the transmitter 30, both or one of the left operation buttons 51 and 53, for example, The lower operation button 53 is operated with a fingertip. By this button operation, the drive output of the corresponding third drive means 17c increases from 60% to 100%, and the rotation speed of the third propeller 16c increases. Due to the increase in the rotation speed of the third propeller 16c, the airframe 11 generates a force for turning right in the direction opposite to the left rotation direction of the third propeller 16c. Therefore, as shown in FIG. 20, the radio-controlled toy 40 can be turned rightward from the state where the radio-controlled toy 40 is levitated by a button operation. At this time, an increase in the amount of blown air accompanying an increase in the rotational speed of the third propeller 16c also adds a force for moving the airframe 11, so that the operation differs from the right turn of the first embodiment. When both the left operation buttons 51 and 53 are operated, the airframe 11 moves to the right side due to an increase in the amount of air flow accompanying an increase in the rotation speed of the first propeller 16a and the third propeller 16c on the left side. It was confirmed that the vehicle turns right after

次に、無線操縦玩具40を浮上させた状態から左旋回させるときには、図21に示すように、送信機30の操作部33において左側の操作ボタン52,54の両方又はいずれか一方、例えば、下側の操作ボタン54を指先で操作する。このボタン操作により、対応する第4の駆動手段17dの駆動出力が60%から100%へ上昇し、第4のプロペラ16dの回転速度が上昇する。この第4のプロペラ16dの回転速度の上昇により、機体11には第4のプロペラ16dの右回転方向と反対方向の左旋回させる力を生じさせる。従って、図21に示すように、ボタン操作により、無線操縦玩具40を浮上させた状態から左旋回させることができる。このとき第4のプロペラ16dの回転速度の上昇に伴う送風量の増加により、機体11を移動させる力も同時に加わるため第1実施形態の左旋回と異なる動作をする。なお、右側の操作ボタン52,54の両方を操作する場合には、右側の第2のプロペラ16b及び第4のプロペラ16dの回転速度の上昇に伴う送風量の増加により、機体11が左側へ移動した後に左旋回する動作が確認された。   Next, when the radio controlled toy 40 is turned left from the state where it floats, as shown in FIG. 21, in the operation unit 33 of the transmitter 30, both or one of the left operation buttons 52 and 54, for example, the lower The operation button 54 on the side is operated with a fingertip. By this button operation, the drive output of the corresponding fourth drive means 17d increases from 60% to 100%, and the rotation speed of the fourth propeller 16d increases. Due to the increase in the rotational speed of the fourth propeller 16d, the airframe 11 is caused to turn counterclockwise in the direction opposite to the right rotation direction of the fourth propeller 16d. Therefore, as shown in FIG. 21, the radio-controlled toy 40 can be turned left from the state where the radio-controlled toy 40 is levitated by a button operation. At this time, a force that moves the airframe 11 is also applied at the same time due to an increase in the amount of blown air accompanying an increase in the rotational speed of the fourth propeller 16d. When both the right operation buttons 52 and 54 are operated, the airframe 11 moves to the left side due to an increase in the amount of air flow accompanying an increase in the rotational speed of the right second propeller 16b and the fourth propeller 16d. After turning left, it was confirmed to turn left.

以上説明した通り、本発明の第2実施形態の無線操縦飛行玩具40では、第1実施形態と同様の機体11の低部側の4隅に、第1〜4の駆動手段17a,17b,17c,17dにより駆動される第1〜第4のプロペラ16a,16b,16c,16dを配置し、また、送信機50は、4つの操作ボタン51,52,53,54により対応する第1〜4の駆動手段17a,17b,17c,17dの駆動出力を通常の60%から100%程度まで上昇させるようにしている。したがって、操作ボタン51,52,53,54により、それぞれ個別に第1〜4の駆動手段17a,17b,17c,17dの駆動出力を変えることで、前進、後退及び左右旋回を行うことができ、第1実施形態と同様に、平坦な走行面1上を浮上して自由に飛行させて楽しむことができる。   As described above, in the radio controlled flying toy 40 according to the second embodiment of the present invention, the first to fourth driving means 17a, 17b, and 17c are provided at the four corners on the lower portion side of the airframe 11 similar to the first embodiment. , 17d driven by the first to fourth propellers 16a, 16b, 16c, 16d, and the transmitter 50 includes the corresponding first to fourth propellers by the four operation buttons 51, 52, 53, 54. The drive output of the drive means 17a, 17b, 17c, 17d is increased from the normal 60% to about 100%. Therefore, the operation buttons 51, 52, 53, 54 can be used to move forward, backward, and turn left and right by individually changing the drive outputs of the first to fourth drive means 17a, 17b, 17c, 17d, Similar to the first embodiment, the user can enjoy flying and flying freely on the flat running surface 1.

上記の第2実施形態の無線操縦飛行玩具40では、左側の第1のプロペラ16a及び第3のプロペラ16cが同一の左方向に回転駆動され、右側の第2のプロペラ16b及び第4のプロペラ16dが同一の右方向に回転駆動される例で説明したが、左側を同一の右方向に、右側を同一の左方向に回転駆動させるようにしてもよく、このような場合には、前進及び後退のボタン操作は同一であるが右旋回と左旋回の操作は反対になる。また、送信機30のレバー操作に対応させて、第1〜4の駆動手段17a,17b,17c,17dの駆動出力を60%から100%へ上昇させているが、駆動出力を逆に100%から60%へ下降させるようにしてもよく、このような場合には、同じレバー操作による走行動作も異なってくる。   In the radio controlled flying toy 40 of the second embodiment described above, the left first propeller 16a and the third propeller 16c are rotationally driven in the same left direction, and the right second propeller 16b and the fourth propeller 16d. However, the left side may be rotationally driven in the same right direction, and the right side may be rotationally driven in the same left direction. The button operations are the same, but the right and left turn operations are opposite. Further, the drive output of the first to fourth drive means 17a, 17b, 17c, and 17d is increased from 60% to 100% corresponding to the lever operation of the transmitter 30, but the drive output is 100% on the contrary. May be lowered to 60%. In such a case, the traveling operation by the same lever operation is different.

なお、上記の第1及び第2実施形態において、機体11は、低部側が走行面1に平行な平坦な底面14を有し、全体として矩形板状に形成され、4辺形を形成する4隅のそれぞれに第1〜第4のプロペラ16a,16b,16c,16dが配置されるものであれば、任意の形状にすることができる。また、第1実施形態の送信機30の操作レバー37,38、及び第2実施形態の送信機50の操作ボタン51,52,53,54は、それぞれを操作することで対応する第1〜4の駆動手段17a,17b,17c,17dの駆動出力が上昇又は下降するように構成されていればよい。さらに、第1の実施形態の無線操縦玩具10を第2の実施形態と同様の送信機50で操作することができ、第2の実施形態の無線操縦玩具40を第1と同様の実施形態の送信機30で操作することもできる。   In the first and second embodiments, the airframe 11 has a flat bottom surface 14 whose lower side is parallel to the running surface 1 and is formed in a rectangular plate shape as a whole, and forms a quadrilateral shape 4. Any shape can be used as long as the first to fourth propellers 16a, 16b, 16c, and 16d are arranged in each corner. Further, the operation levers 37 and 38 of the transmitter 30 of the first embodiment and the operation buttons 51, 52, 53, and 54 of the transmitter 50 of the second embodiment correspond to the first to fourth corresponding to each by operating them. What is necessary is just to be comprised so that the drive output of the drive means 17a, 17b, 17c, 17d may rise or fall. Furthermore, the radio controlled toy 10 of the first embodiment can be operated by the transmitter 50 similar to that of the second embodiment, and the radio controlled toy 40 of the second embodiment of the same embodiment as that of the first embodiment. It can also be operated by the transmitter 30.

機体の底面側へ空気を送風することで機体を平坦な走行面上を浮上させて、自由に飛行できる無線操縦飛行玩具に利用することができる。   By blowing air to the bottom side of the airframe, the airframe can float on a flat running surface and can be used for a radio controlled flying toy that can fly freely.

本発明第1実施形態の無線操縦飛行玩具の斜視図である。It is a perspective view of the radio controlled flight toy of a 1st embodiment of the present invention. 本発明第1実施形態の無線操縦飛行玩具の平面図である。It is a top view of the radio controlled flight toy of 1st Embodiment of this invention. 本発明第1実施形態の図2の無線操縦飛行玩具のA―A線断面図である。It is the sectional view on the AA line of the radio controlled flight toy of FIG. 2 of 1st Embodiment of this invention. 本発明第1実施形態の無線操縦飛行玩具の背面図である。It is a rear view of the radio controlled flight toy of 1st Embodiment of this invention. 本発明第1実施形態の無線操縦飛行玩具の側面図である。It is a side view of the radio controlled flight toy of 1st Embodiment of this invention. 本発明第1実施形態の無線操縦飛行玩具の底面図である。It is a bottom view of the radio controlled flight toy of 1st Embodiment of this invention. 本発明第1実施形態の無線操縦飛行玩具の制御動作を説明するブロック図である。It is a block diagram explaining the control operation | movement of the radio controlled flight toy of 1st Embodiment of this invention. 本発明第1実施形態の無線操縦飛行玩具が浮上する状態を説明する図である。It is a figure explaining the state which the radio controlled flight toy of 1st Embodiment of this invention floats up. 本発明第1実施形態の無線操縦飛行玩具が前進する状態を説明する図である。It is a figure explaining the state which the radio controlled flight toy of 1st Embodiment of this invention advances. 本発明第1実施形態の無線操縦飛行玩具が浮上するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of the 1st embodiment of the present invention floats up. 本発明第1実施形態の無線操縦飛行玩具が前進するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 1st embodiment of the present invention advances. 本発明第1実施形態の無線操縦飛行玩具が後退するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 1st embodiment of the present invention retreats. 本発明第1実施形態の無線操縦飛行玩具が右旋回するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of the 1st embodiment of the present invention turns right. 本発明第1実施形態の無線操縦飛行玩具が左旋回するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 1st embodiment of the present invention turns to the left. 本発明第2実施形態の無線操縦飛行玩具の斜視図である。It is a perspective view of the radio controlled flight toy of 2nd Embodiment of this invention. 本発明第2実施形態の無線操縦飛行玩具の平面図である。It is a top view of the radio controlled flight toy of 2nd Embodiment of this invention. 本発明第2実施形態の無線操縦飛行玩具が浮上するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 2nd embodiment of the present invention floats up. 本発明第2実施形態の無線操縦飛行玩具が前進するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 2nd embodiment of the present invention advances. 本発明第2実施形態の無線操縦飛行玩具が後退するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 2nd embodiment of the present invention retreats. 本発明第2実施形態の無線操縦飛行玩具が右旋回するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 2nd embodiment of the present invention turns right. 本発明第2実施形態の無線操縦飛行玩具が左旋回するときの送信機の操作を説明する図である。It is a figure explaining operation of a transmitter when the radio controlled flight toy of a 2nd embodiment of the present invention turns to the left.

符号の説明Explanation of symbols

1 走行面
10,40 無線操縦飛行玩具
11 機体
12 上部本体
13 下部本体
14 底面
15a,15b,15c,15d 取付け孔
16a,16b,16c,16d プロペラ
17a,17b,17c,17d 駆動手段
18a,18b,18c,18d 取付け部材
19 電源スイッチ
20 制御部
21 電池
22 アンテナ
23 受信回路
24 制御回路
25 駆動回路
30,50 送信機
31 送信回路
32 電池
33 操作部
34 信号生成回路
35 アンテナ
36 電源スイッチ
37,38 操作レバー
51,52,53,54 操作ボタン
DESCRIPTION OF SYMBOLS 1 Running surface 10,40 Radio control flying toy 11 Airframe 12 Upper body 13 Lower body 14 Bottom surface 15a, 15b, 15c, 15d Mounting hole 16a, 16b, 16c, 16d Propeller 17a, 17b, 17c, 17d Drive means 18a, 18b, 18c, 18d Mounting member 19 Power switch 20 Control unit 21 Battery 22 Antenna 23 Reception circuit 24 Control circuit 25 Drive circuit 30, 50 Transmitter 31 Transmission circuit 32 Battery 33 Operation unit 34 Signal generation circuit 35 Antenna 36 Power switch 37, 38 Operation Lever 51, 52, 53, 54 Operation buttons

Claims (8)

低部側が平坦な底面を有する矩形板状に形成された機体と、該機体の低部側の少なくとも4辺形を形成する4隅に設けられ底面側へ送風して前記機体を浮上させる第1〜4のプロペラと、前記第1〜4のプロペラをそれぞれ駆動する第1〜4の駆動手段と、前記第1〜4の駆動手段の駆動出力をそれぞれ個別に制御する制御部と、飛行のための制御信号を外部から前記制御部へ送信する送信機と、前記第1〜4の駆動手段及び制御部へ電源を供給する電池とを備えたことを特徴とする無線操縦飛行玩具。 A machine body formed in a rectangular plate shape having a flat bottom surface on the lower part side, and a first body which is provided at four corners forming at least a quadrilateral on the lower part side of the machine body and floats by blowing air to the bottom surface side. -4 propellers, first to fourth drive means for driving the first to fourth propellers, a control unit for individually controlling drive outputs of the first to fourth drive means, and for flight A radio-controlled flying toy comprising: a transmitter that transmits a control signal of the above to the control unit; and a battery that supplies power to the first to fourth driving units and the control unit. 前記機体は、前記制御部及び電池を収納する上部本体と、この上部本体の下部に設けられた矩形板状に形成された下部本体とから構成され、前記下部本体の4辺形を形成する4隅の位置にそれぞれ取付け孔が開口され、該取付け孔に前記第1〜第4のプロペラが配置されていることを特徴とする請求項1記載の無線操縦飛行玩具。 The airframe is composed of an upper main body that houses the control unit and the battery, and a lower main body formed in a rectangular plate shape provided at a lower portion of the upper main body, and forms a quadrilateral of the lower main body 4. The radio-controlled flying toy according to claim 1, wherein a mounting hole is opened at each corner position, and the first to fourth propellers are disposed in the mounting hole. 前記第1〜4のプロペラは、前記機体の4辺形を形成する4隅の一方の対角線上に位置する一対のプロペラが一方方向に回転駆動され、他方の対角線上に位置する一対のプロペラが異なる他方方向に回転駆動されることを特徴とする請求項1記載の無線操縦飛行玩具。 In the first to fourth propellers, a pair of propellers positioned on one diagonal line of four corners forming the quadrilateral of the airframe are rotationally driven in one direction, and a pair of propellers positioned on the other diagonal line The radio-controlled flying toy according to claim 1, wherein the radio-controlled flying toy is driven to rotate in another different direction. 前記第1〜4のプロペラは、前記機体の4辺形を形成する4隅の右側に位置する一対のプロペラが一方方向に回転駆動され、左側に位置する一対のプロペラが異なる他方方向に回転駆動されることを特徴とする請求項1記載の無線操縦飛行玩具。 In the first to fourth propellers, a pair of propellers positioned on the right side of the four corners forming the quadrilateral of the airframe are driven to rotate in one direction, and a pair of propellers positioned on the left side are driven to rotate in different directions. The radio controlled flying toy according to claim 1, wherein: 前記送信機は、前記第1〜4の駆動手段の駆動出力をそれぞれ個別に上昇又は下降制御する信号を生成するための操作レバーを有することを特徴とする請求項1記載の無線操縦飛行玩具。 The radio-controlled flying toy according to claim 1, wherein the transmitter includes an operation lever for generating a signal for individually raising or lowering the driving output of the first to fourth driving means. 前記操作レバーは、垂直な状態から一方側及び他方側へ回動操作する右の操作レバー及び左の操作レバーを有し、それぞれの前記右の操作レバー及び左の操作レバーの一方側及び他方側への回動操作に対応させて、前記第1〜4の駆動手段のいずれか1つの駆動出力を個別に上昇又は下降制御する信号を生成するものであることを特徴とする請求項5記載の無線操縦飛行玩具。 The operating lever includes a right operating lever and a left operating lever that are rotated from a vertical state to one side and the other side, and one side and the other side of each of the right operating lever and the left operating lever. 6. A signal for individually raising or lowering the drive output of any one of the first to fourth drive means in correspondence with the turning operation to the position. Radio controlled flying toy. 前記送信機は、前記第1〜4の駆動手段の駆動出力をそれぞれ個別に上昇又は下降制御する信号を生成するための操作ボタンを有することを特徴とする請求項1記載の無線操縦飛行玩具。 The radio-controlled flying toy according to claim 1, wherein the transmitter has operation buttons for generating signals for individually raising or lowering the driving outputs of the first to fourth driving means. 前記操作ボタンは、それぞれ前後左右の前記第1〜4の駆動手段に対応させた4つの操作ボタンを有することを特徴とする請求項7記載の無線操縦飛行玩具。 8. The radio-controlled flying toy according to claim 7, wherein the operation buttons include four operation buttons respectively corresponding to the first to fourth driving means on the front, rear, left and right sides.
JP2005324666A 2005-11-09 2005-11-09 Radio-controlled flying toy Pending JP2007130146A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013510760A (en) * 2009-11-13 2013-03-28 パロット Navigation electronic card support for drone drones
JP2013139256A (en) * 2012-01-05 2013-07-18 Parrot Method for piloting rotary wing drone to photographing by onboard camera while minimizing disturbing movement
KR101626495B1 (en) * 2015-02-06 2016-06-01 동의과학대학 산학협력단 Air-cushion vehicle for amusement
JP5997338B1 (en) * 2015-09-15 2016-09-28 京商株式会社 Multicopter controller and multicopter control method
WO2018061246A1 (en) * 2016-09-27 2018-04-05 正 星野 Air cushion device toy
US10095226B1 (en) 2008-02-12 2018-10-09 Drone-Control, Llc Radio controlled aircraft, remote controller and methods for use therewith

Families Citing this family (68)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7407424B2 (en) * 2005-01-10 2008-08-05 Silverlit Toys Manufactory, Ltd. Spatial navigation system and method for programmable flying objects
GB2452533B (en) * 2007-09-07 2011-12-14 Alien Technology Ltd Flying toy apparatus
US8109802B2 (en) 2007-09-15 2012-02-07 Mattel, Inc. Toy helicopter having a stabilizing bumper
US8702466B2 (en) * 2008-07-02 2014-04-22 Asian Express Holdings Limited Model helicopter
US8473143B2 (en) * 2008-12-02 2013-06-25 Caterpillar Inc. System and method for accident logging in an automated machine
GB0905027D0 (en) * 2009-03-24 2009-05-06 Allen Technology Ltd Flying apparatus
US20110201246A1 (en) * 2010-02-17 2011-08-18 Masaki Suzuki Ground effect model
MY173920A (en) * 2010-06-04 2020-02-27 Univ Malaysia Perlis A flying apparatus for aerial agricultural application
US8844860B2 (en) * 2012-07-06 2014-09-30 Lapcad Engineering, Inc. Foldable rise and stare vehicle
US20140231582A1 (en) * 2012-10-03 2014-08-21 Sean Headrick Methods and Systems of Constructing a Multi Rotor Aircraft Fuselage
US9004973B2 (en) * 2012-10-05 2015-04-14 Qfo Labs, Inc. Remote-control flying copter and method
DE202013012547U1 (en) * 2012-11-15 2017-07-03 SZ DJI Technology Co., Ltd. Unmanned aerial vehicle with multiple rotors
US20140323009A1 (en) * 2013-04-24 2014-10-30 Top Notch Toys Limited Protective ring for toy helicopter
CN105938369B (en) 2013-06-25 2018-11-02 深圳市大疆创新科技有限公司 Flight control and control method
US9650155B2 (en) 2013-06-25 2017-05-16 SZ DJI Technology Co., Ltd Aircraft control apparatus, control system and control method
CN105555375B (en) 2013-08-15 2018-06-08 特拉克赛卡斯公司 Gyroplane with integrated light pipe supporting member
WO2015100754A1 (en) * 2014-01-06 2015-07-09 林日壮 Remotely controlled toy helicopter with double-propeller empennage
CN103752020A (en) * 2014-02-08 2014-04-30 吴士明 Disc type flying toy
CN103861291B (en) * 2014-03-31 2016-02-03 王丽芸 The four-axle aircraft toy of automatic omnidirectional tracking target and control method thereof
USD772991S1 (en) * 2014-04-02 2016-11-29 Parrot Drones Flying toy
USD770572S1 (en) 2014-04-16 2016-11-01 Parrot Drones Flying toy
USD751490S1 (en) * 2014-06-12 2016-03-15 SZ DJI Technology Co., Ltd. Aircraft
USD751025S1 (en) * 2014-06-13 2016-03-08 Bcb International Limited Unmanned aerial vehicle
USD761690S1 (en) * 2014-11-06 2016-07-19 Dronesmith Technologies, Inc. Unmanned aerial vehicle
USD759764S1 (en) * 2014-11-18 2016-06-21 Thunder Tiger Corporation Quadcopter
USD827723S1 (en) 2015-09-28 2018-09-04 Traxxas Lp Quadrotor model helicopter
USD827724S1 (en) 2015-09-28 2018-09-04 Traxxas Lp Set of supporting arms for a quadrotor model helicopter
USD819749S1 (en) * 2015-10-01 2018-06-05 Parrot Drones Remote-controlled flying drone
USD797859S1 (en) * 2015-10-01 2017-09-19 Parrot Drones Remote-controlled flying toy with bumpers
US10094669B2 (en) * 2015-10-29 2018-10-09 Horizon Hobby, LLC Systems and methods for inertially-instituted binding of a RC vehicle
US10258888B2 (en) 2015-11-23 2019-04-16 Qfo Labs, Inc. Method and system for integrated real and virtual game play for multiple remotely-controlled aircraft
USD843266S1 (en) 2016-01-26 2019-03-19 SZ DJI Technology Co., Ltd. Aerial vehicle
USD782365S1 (en) * 2016-03-17 2017-03-28 XDynamics Limited Unmanned aerial vehicle
USD779595S1 (en) * 2016-04-06 2017-02-21 Guangdong Syma Model Aircraft Industrial Co., Ltd Toy aircraft
GB2552344A (en) * 2016-07-19 2018-01-24 Alexander Scott Curtis-Oliver Damian Flying toy
US11141673B1 (en) * 2016-09-28 2021-10-12 Traxxas Lp Model rotorcraft with light pipe support members
USD846441S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD846442S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD846440S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD846443S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD847019S1 (en) * 2016-10-18 2019-04-30 Samsung Electronics Co., Ltd. Drone
USD847021S1 (en) * 2016-10-18 2019-04-30 Samsung Electroncis Co., Ltd. Drone
USD846439S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD846438S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD847020S1 (en) * 2016-10-18 2019-04-30 Samsung Electronics Co., Ltd. Drone
USD846444S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD847018S1 (en) * 2016-10-18 2019-04-30 Samsung Electronics Co., Ltd. Drone
USD847017S1 (en) * 2016-10-18 2019-04-30 Samsung Electronics Co., Ltd. Drone
USD846437S1 (en) * 2016-10-18 2019-04-23 Samsung Electronics Co., Ltd. Drone
USD862359S1 (en) 2016-10-27 2019-10-08 SZ DJI Technology Co., Ltd. Aerial vehicle
USD816581S1 (en) * 2016-12-06 2018-05-01 Jianjia Zhao Quadcopter
USD851540S1 (en) * 2017-06-07 2019-06-18 MerchSource, LLC Drone
USD825380S1 (en) * 2017-06-27 2018-08-14 MerchSource, LLC Drone for kids
USD852091S1 (en) * 2017-07-20 2019-06-25 MerchSource, LLC Drone
US10894219B1 (en) * 2017-09-05 2021-01-19 David Thomas Parker Finger flying hover toy
USD875021S1 (en) * 2017-09-11 2020-02-11 Brendon G. Nunes Airbike
USD875023S1 (en) * 2017-11-03 2020-02-11 Sang Hyun Lee Aircraft with multiple rotors
USD867470S1 (en) * 2017-12-01 2019-11-19 Horizon Hobby, LLC Quadcopter
USD906170S1 (en) * 2018-02-13 2020-12-29 Skydio, Inc. Unmanned aerial vehicle
USD862361S1 (en) * 2018-04-16 2019-10-08 FanFlyer Inc. Ducted fan flying machine
USD872004S1 (en) * 2018-05-15 2020-01-07 Brendon G. Nunes Multicopter
USD865637S1 (en) * 2018-09-06 2019-11-05 AEE Aviation Technology Company Aircraft with camera
USD925399S1 (en) * 2019-04-17 2021-07-20 Shenzhen Aee Aviation Technology Co., Ltd. Pocket drone
USD943457S1 (en) * 2020-03-16 2022-02-15 Zero Zero Robotics Inc. Unmanned aerial vehicle
USD944117S1 (en) * 2020-03-16 2022-02-22 Zero Zero Robotics Inc. Unmanned aerial vehicle
US11260312B1 (en) * 2020-10-01 2022-03-01 MerchSource, LLC Wall riding vehicle
JP1701070S (en) * 2020-12-11 2021-11-29
USD1001682S1 (en) * 2023-06-16 2023-10-17 Tongwei Wang Toy aircraft

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1749471A (en) * 1924-03-29 1930-03-04 Bothezat George De Helicopter
US2954614A (en) * 1957-12-02 1960-10-04 Curtiss Wright Corp Flight training apparatus for hovering type aircraft
US2951661A (en) * 1957-12-30 1960-09-06 Harley A Dorman Aircraft having a plurality of annular wings
US2987272A (en) * 1959-04-29 1961-06-06 Curtiss Wright Corp Aircraft with a tiltable rotor system
US3201068A (en) * 1963-07-08 1965-08-17 Gen Motors Corp Plural propeller pitch change control system
US4770371A (en) * 1968-12-09 1988-09-13 Karl Eickmann Fluid motor driven multi propeller aircraft
CA967538A (en) * 1973-07-13 1975-05-13 Paul Horsdal Flying machine
US4161843A (en) * 1978-09-01 1979-07-24 Hui Danny C T Electrically powered toy aircraft
JPH0620559Y2 (en) * 1989-01-31 1994-06-01 大陽工業株式会社 Air cushion machine toy
US6260796B1 (en) * 1997-03-04 2001-07-17 Wallace Neil Klingensmith Multi-thrustered hover craft
FR2809026B1 (en) * 2000-05-18 2003-05-16 Philippe Louvel ELECTRIC FLYING SAUCER, PILOTED AND REMOTELY POWERED
US6688936B2 (en) * 2001-03-28 2004-02-10 Steven Davis Rotating toy with directional vector control
WO2002098732A2 (en) * 2001-06-04 2002-12-12 Romeo Yankee Ltd. Vehicles particularly useful as vtol vehicles
JP3861224B2 (en) * 2001-12-07 2006-12-20 有限会社新科学開発研究所 Aerial vehicle
US7581608B2 (en) * 2003-02-07 2009-09-01 St Louis Daniel Mark Levitating platform
US7946526B2 (en) * 2004-11-05 2011-05-24 Nachman Zimet Rotary-wing vehicle system
US20060226281A1 (en) * 2004-11-17 2006-10-12 Walton Joh-Paul C Ducted fan vertical take-off and landing vehicle
US7407424B2 (en) * 2005-01-10 2008-08-05 Silverlit Toys Manufactory, Ltd. Spatial navigation system and method for programmable flying objects
JP4343167B2 (en) * 2005-11-10 2009-10-14 株式会社タイヨー Radio controlled helicopter toy
JP4685620B2 (en) * 2005-12-19 2011-05-18 Npo法人ぺんぎん Drawing sets and how to use them

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10095226B1 (en) 2008-02-12 2018-10-09 Drone-Control, Llc Radio controlled aircraft, remote controller and methods for use therewith
US10248117B2 (en) 2008-02-12 2019-04-02 Drone-Control, Llc Radio controlled aircraft, remote controller and methods for use therewith
US11281205B2 (en) 2008-02-12 2022-03-22 Drone-Control, Llc Radio controlled aircraft, remote controller and methods for use therewith
JP2013510760A (en) * 2009-11-13 2013-03-28 パロット Navigation electronic card support for drone drones
JP2013139256A (en) * 2012-01-05 2013-07-18 Parrot Method for piloting rotary wing drone to photographing by onboard camera while minimizing disturbing movement
KR101626495B1 (en) * 2015-02-06 2016-06-01 동의과학대학 산학협력단 Air-cushion vehicle for amusement
JP5997338B1 (en) * 2015-09-15 2016-09-28 京商株式会社 Multicopter controller and multicopter control method
JP2017055911A (en) * 2015-09-15 2017-03-23 京商株式会社 Controller for multicopter and control method of multicopter
WO2018061246A1 (en) * 2016-09-27 2018-04-05 正 星野 Air cushion device toy

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