WO2015100754A1 - Remotely controlled toy helicopter with double-propeller empennage - Google Patents

Remotely controlled toy helicopter with double-propeller empennage Download PDF

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Publication number
WO2015100754A1
WO2015100754A1 PCT/CN2014/070191 CN2014070191W WO2015100754A1 WO 2015100754 A1 WO2015100754 A1 WO 2015100754A1 CN 2014070191 W CN2014070191 W CN 2014070191W WO 2015100754 A1 WO2015100754 A1 WO 2015100754A1
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Prior art keywords
propeller
tail
double
toy helicopter
empennage
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PCT/CN2014/070191
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French (fr)
Chinese (zh)
Inventor
林日壮
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林日壮
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Priority to PCT/CN2014/070191 priority Critical patent/WO2015100754A1/en
Publication of WO2015100754A1 publication Critical patent/WO2015100754A1/en

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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

Abstract

A remotely controlled toy helicopter with a double-propeller empennage comprises a helicopter body (100), a power supply, a control circuit board (110), a main propeller device (200) and a tail propeller device (300); the power supply and the control circuit board (110) are arranged inside the helicopter body (100), the main propeller device (200) and the tail propeller device (300) are electrically connected with the control circuit board (110), the tail propeller device (300) comprises a left propeller (320) and a right propeller (310), and the left propeller (320) and the right propeller (310) are arranged on the tail of the helicopter body (100) in a left-right symmetrical manner. Thus, left-lateral and right-lateral force is provided by the left propeller and the right propeller so as to ensure directional control such that unhindered steering and transverse flight can be achieved, and further, the remotely controlled toy helicopter with a double-propeller empennage can move forward and backward in a faster way.

Description

一种尾翼双螺旋浆遥控玩具直升飞机 技术领域  Tail double propeller remote control toy helicopter
本发明属于玩具领域, 尤其涉及一种遥控玩具直升飞机。 背景技术  The invention belongs to the field of toys, and in particular relates to a remote control toy helicopter. Background technique
遥控玩具直升飞机, 由于其可在空中实现遥控飞行, 所以深受广大儿童的喜 爱。 然而, 由于目前的遥控玩具直升飞机主要动力来源于设置于机身中部的主螺 旋浆装置, 通过主螺旋浆装置内共轴的两个螺旋浆之间的差速或等速转动实现左 右转向及上下飞行, 而依靠后方的一个尾翼螺旋浆, 控制其前后飞行, 而不能自 如地进行转弯或左右横向飞行, 所以玩耍时缺乏新颖性,趣味性不够强,难以满足 广大儿童的玩耍要求。 发明内容  The remote-controlled toy helicopter is popular among children because of its ability to fly remotely in the air. However, since the current main power of the remote control toy helicopter is derived from the main propeller device installed in the middle of the fuselage, the left and right steering is realized by differential or constant speed rotation between the two propellers in the main propeller device. And flying up and down, and relying on a rear tail propeller to control the flight before and after, but can not freely turn or fly laterally, so the lack of novelty in play, the interest is not strong enough, it is difficult to meet the children's play requirements. Summary of the invention
本发明的目的在于, 提供一种尾翼双螺旋浆遥控玩具直升飞机 , 其能够自如 地进行转弯和左右横向飞行。  SUMMARY OF THE INVENTION It is an object of the present invention to provide a tail twin propeller remote control toy helicopter that is capable of freely turning and laterally flying laterally.
本发明通过如下技术方案实现: 一种尾翼双螺旋浆遥控玩具直升飞机, 所述 尾翼双螺旋浆遥控玩具直升飞机包括机体、 电源、 控制电路板、 主螺旋桨装置及 尾部螺旋桨装置, 电源和控制电路板设置在所述机体内, 所述主螺旋桨装置和所 述尾部螺旋桨装置与所述控制电路板电连接, 所述尾部螺旋桨装置包括左螺旋桨 和右螺旋桨, 所述左螺旋桨和所述右螺旋桨以左右对称的方式设置在所述机体的 尾部。  The invention is realized by the following technical solutions: a tail twin propeller remote control toy helicopter, the tail double propeller remote control toy helicopter comprises a body, a power source, a control circuit board, a main propeller device and a tail propeller device, a power source and a control circuit board disposed in the body, the main propeller device and the tail propeller device being electrically connected to the control circuit board, the tail propeller device including a left propeller and a right propeller, the left propeller and the right The propeller is disposed at the tail of the body in a bilaterally symmetrical manner.
作为上述技术方案的进一步改进, 所述主螺旋桨装置包括一对共轴的两个竖 直向上设置的螺旋浆。  As a further improvement of the above technical solution, the main propeller device comprises a pair of coaxial two propellers arranged vertically upward.
作为上述技术方案的进一步改进, 优选所述左螺旋桨和所述右螺旋桨竖直向 上设置, 当然也可以采用竖直向上、 向外倾斜 45度向上设置等左右对称设置。  As a further improvement of the above technical solution, it is preferable that the left propeller and the right propeller are vertically disposed, and of course, the left and right symmetrical arrangement may be adopted such that the vertical propeller is inclined upward by 45 degrees.
作为上述技术方案的进一步改进, 所述左螺旋桨和所述右螺旋桨均包括桨叶 及驱动桨叶的驱动马达组件, 通过控制电路板控制左螺旋桨和右螺旋桨转动的方 向及转速, 实现向前向后或左右横向飞行。 作为上述技术方案的进一步改进, 所述机体 ( 100 )的尾部中央还设置有一螺 旋浆。 As a further improvement of the above technical solution, the left propeller and the right propeller each include a driving motor assembly of the blade and the driving blade, and the direction and the rotation speed of the left propeller and the right propeller are controlled by the control circuit board to realize the forward direction. Fly laterally or left and right. As a further improvement of the above technical solution, a propeller is disposed in the center of the tail of the body (100).
本发明的有益效果是: 本发明的尾翼双螺旋浆遥控玩具直升飞机包括机体、 主螺旋桨装置及尾部螺旋桨装置, 所述尾部螺旋桨装置包括左螺旋桨和右螺旋桨, 所述左螺旋桨和所述右螺旋桨以左右对称的方式设置在所述机体的尾部, 由此, 不但可以通过左螺旋桨和右螺旋桨提供向左右方向侧部的力而掌握方向, 自如地 进行转弯和左右横向飞行, 还可以更加快速地前进和后退。  The beneficial effects of the present invention are: The empennage double propeller remote control toy helicopter of the present invention comprises a body, a main propeller device and a tail propeller device, the tail propeller device comprising a left propeller and a right propeller, the left propeller and the right The propeller is disposed at the tail of the body in a bilaterally symmetrical manner, thereby not only providing the force to the left and right side by the left propeller and the right propeller, but also grasping the direction, freely turning and laterally flying, and also being faster. Advance and retreat.
附图说明 DRAWINGS
图 1 是根据本发明的一个具体实施例的尾翼双螺旋浆遥控玩具直升飞机的示 意图。  BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a schematic illustration of a tail twin propeller remote control toy helicopter in accordance with an embodiment of the present invention.
图 2是图 1的尾翼双螺旋浆遥控玩具直升飞机的剖切示意图。 具体实施方式  2 is a cross-sectional view of the tail rotor double propeller remote control toy helicopter of FIG. detailed description
以下结合附图对本发明的具体实施方式进行进一步的说明。  The specific embodiments of the present invention are further described below in conjunction with the accompanying drawings.
如图 1和图 2所示, 本实施例的尾翼双螺旋浆遥控玩具直升飞机 1000包括机 体 100、 电源、 控制电路板 110、 主螺旋桨装置 200及尾部螺旋桨装置 300。 电源 和控制电路板 110设置在所述机体 100内, 电源用于给尾翼双螺旋浆遥控玩具直 升飞机 1000供电。 所述主螺旋桨装置 200和所述尾部螺旋桨装置 300与所述控制 电路板 110电连接。 其中, 所述尾部螺旋桨装置 300包括左螺旋桨 320和右螺旋 桨 310。所述左螺旋桨 320和所述右螺旋桨 310以左右对称的方式设置在所述机体 100的尾部。优选地, 所述左螺旋桨 320和所述右螺旋桨 310对称竖直向上设置在 所述机体 100的尾部。 而且, 本实施例中, 所述左螺旋桨 320和所述右螺旋桨 310 结构相同。  As shown in Figs. 1 and 2, the tail twin propeller remote control toy helicopter 1000 of the present embodiment includes a body 100, a power source, a control circuit board 110, a main propeller device 200, and a tail propeller device 300. A power and control circuit board 110 is disposed within the body 100 for powering the tail twin propeller remote control toy helicopter 1000. The main propeller device 200 and the tail propeller device 300 are electrically connected to the control circuit board 110. Wherein the tail propeller device 300 includes a left propeller 320 and a right propeller 310. The left propeller 320 and the right propeller 310 are disposed at the tail of the body 100 in a bilaterally symmetrical manner. Preferably, the left propeller 320 and the right propeller 310 are symmetrically disposed vertically upward at the tail of the body 100. Moreover, in this embodiment, the left propeller 320 and the right propeller 310 have the same structure.
主螺旋桨装置 200具有一对共轴的两个竖直向上设置的上螺旋桨 210、下螺旋 桨 220、 旋转轴结构 230及驱动机构 240。 驱动机构 240包含驱动马达、 齿轮减速 机构等。 驱动机构 240的动力经旋转轴结构 230传递给上螺旋桨 210和下螺旋桨 220, 通过控制电路板 110控制主螺旋浆装置 200内共轴的两个螺旋浆 210、 220 之间的差速或等速转动实现左右转向及上下飞行。如图 2所示, 所述左螺旋桨 320 和所述右螺旋桨 310均包括桨叶 302及驱动桨叶 302的驱动马达组件 304。所述左 螺旋桨 320和所述右螺旋桨 310由所述控制电路板 110控制其转向及转速。 当然, 也可以根据需要, 通过所述控制电路板 110将所述左螺旋桨 320和所述右螺旋桨 310控制成桨叶转向相反。 驱动马达组件 304可以包括驱动马达和 /或减速机构等。 另外, 驱动机构 240和驱动马达组件 304通过手持遥控器(未示出)遥控控制。 The main propeller device 200 has a pair of coaxially disposed two upper vertical propellers 210, a lower propeller 220, a rotating shaft structure 230, and a drive mechanism 240. The drive mechanism 240 includes a drive motor, a gear reduction mechanism, and the like. The power of the driving mechanism 240 is transmitted to the upper propeller 210 and the lower propeller 220 via the rotating shaft structure 230, and the differential or constant speed between the two propellers 210, 220 coaxial in the main propeller device 200 is controlled by the control circuit board 110. Rotate to achieve left and right steering and flying up and down. As shown in FIG. 2, the left propeller 320 and the right propeller 310 each include a paddle 302 and a drive motor assembly 304 that drives the paddle 302. The left The propeller 320 and the right propeller 310 are controlled by the control circuit board 110 for their steering and rotational speed. Of course, the left propeller 320 and the right propeller 310 may be controlled to be opposite to the blade turning by the control circuit board 110 as needed. Drive motor assembly 304 can include a drive motor and/or a speed reduction mechanism or the like. Additionally, drive mechanism 240 and drive motor assembly 304 are remotely controlled by a hand held remote control (not shown).
在本实施例的尾翼双螺旋浆遥控玩具直升飞机 1000中, 通过控制电路板 110 控制左螺旋桨 320、 右螺旋桨 310的驱动马达的转速和转向, 例如: 当左螺旋桨 320、 右螺旋桨 310同向正转时, 抬升尾部, 使整个遥控玩具直升飞机向前飞行; 左螺旋桨 320、 右螺旋桨 310同向反转时, 压低尾部, 使整个遥控玩具直升飞机向 后飞行;左螺旋桨 320、右螺旋桨 310反向转动时,则使机体向左或向右一侧倾斜, 从而使整个遥控玩具直升飞机朝左右侧横向飞行。 这样尾部上的双螺旋浆可以使 整个遥控玩具直升飞机自如地进行转弯和左右横向飞行, 增加了玩耍的趣味性, 而且还可以利用左螺旋桨 320和右螺旋桨 310使尾翼双螺旋浆遥控玩具直升飞机 1000更加快速地前进和后退。  In the empennage double propeller remote control toy helicopter 1000 of the present embodiment, the rotational speed and steering of the driving motors of the left propeller 320 and the right propeller 310 are controlled by the control circuit board 110, for example: when the left propeller 320 and the right propeller 310 are in the same direction When turning forward, lift the tail to make the whole remote toy helicopter fly forward; when the left propeller 320 and the right propeller 310 reverse in the same direction, lower the tail to make the whole remote toy helicopter fly backward; left propeller 320, right When the propeller 310 is rotated in the reverse direction, the body is tilted to the left or right side, so that the entire remote control toy helicopter flies laterally to the left and right sides. The double-spiral slurry on the tail can make the whole remote-controlled toy helicopter freely turn and laterally fly, which increases the fun of play, and can also use the left propeller 320 and the right propeller 310 to make the tail double-propeller remote control toy straight. The aircraft 1000 advances and retreats more quickly.
以上具体实施方式对本发明进行了详细的说明, 但这些并非构成对本发明的 限制。 本发明的保护范围并不以上述实施方式为限, 但凡本领域普通技术人员根 据本发明所揭示内容所作的等效修饰或变化, 皆应纳入权利要求书中记载的保护 范围内。  The present invention has been described in detail in the above embodiments, but these are not intended to limit the invention. The scope of the present invention is not limited to the above-described embodiments, and equivalent modifications or variations made by those skilled in the art in light of the present invention are included in the scope of the claims.

Claims

权 利 要 求 书 Claims
1、 一种尾翼双螺旋浆遥控玩具直升飞机, 其特征在于, 所述尾翼双螺旋浆遥控玩 具直升飞机( 1000) 包括机体(100)、 电源、 控制电路板(110)、 主螺旋桨装置 A tail rotor double propeller remote control toy helicopter, characterized in that the tail rotor double propeller remote control toy helicopter (1000) comprises a body (100), a power supply, a control circuit board (110), a main propeller device
( 200 )及尾部螺旋桨装置 ( 300 ), 电源和控制电路板 (110)设置在所述机体 ( 100 ) 内, 所述主螺旋桨装置(200)和所述尾部螺旋桨装置(300)与所述控制电路板(200) and a tail propeller device (300), a power supply and control circuit board (110) disposed in the body (100), the main propeller device (200) and the tail propeller device (300) and the control Circuit board
(110)电连接,所述尾部螺旋桨装置( 300 )包括左螺旋桨( 320 )和右螺旋桨( 310 ), 所述左螺旋桨(320)和所述右螺旋桨(310) 以左右对称的方式设置在所述机体(110) electrically connected, the tail propeller device (300) includes a left propeller (320) and a right propeller (310), and the left propeller (320) and the right propeller (310) are disposed in a bilaterally symmetric manner Body
(100)的尾部, 通过控制电路板控制左螺旋桨(320)和所述右螺旋桨(310)转 动的方向及转速。 At the tail of (100), the direction and rotation speed of the left propeller (320) and the right propeller (310) are controlled by a control circuit board.
2、 根据权利要求 1所述的尾翼双螺旋浆遥控玩具直升飞机, 其特征在于, 所述主 螺旋桨装置(200) 包括一对共轴的两个竖直向上设置的螺旋浆(210、 220), 通 过控制电路板控制两个螺旋浆转速。  2. The empennage double propeller remote control toy helicopter according to claim 1, wherein said main propeller device (200) comprises a pair of coaxial two vertically upwardly disposed propellers (210, 220) ), control the two propeller speeds through the control board.
3、 根据权利要求 2所述的尾翼双螺旋浆遥控玩具直升飞机, 其特征在于, 所述左 螺旋桨(320)和所述右螺旋桨(310)竖直向上设置。  The empennage double propeller remote control toy helicopter according to claim 2, wherein the left propeller (320) and the right propeller (310) are vertically arranged upward.
4、 根据权利要求 2所述的尾翼双螺旋浆遥控玩具直升飞机, 其特征在于, 所述左 螺旋桨(320)和所述右螺旋桨(310)竖直向下设置。  The empennage double propeller remote control toy helicopter according to claim 2, wherein the left propeller (320) and the right propeller (310) are vertically disposed downward.
5、 根据权利要求 2所述的尾翼双螺旋浆遥控玩具直升飞机, 其特征在于, 所述左 螺旋桨(320)和所述右螺旋桨(310)向外倾斜 45度向上设置。  The empennage double propeller remote control toy helicopter according to claim 2, wherein the left propeller (320) and the right propeller (310) are inclined upward by 45 degrees.
6、 根据权利要求 1至 5任一权利要求所述的尾翼双螺旋浆遥控玩具直升飞机, 其 特征在于, 所述左螺旋桨(320)和所述右螺旋桨(310)结构相同。  The empennage double propeller remote control toy helicopter according to any one of claims 1 to 5, wherein the left propeller (320) and the right propeller (310) are identical in structure.
7、 根据权利要求 6所述的尾翼双螺旋浆遥控玩具直升飞机, 其特征在于, 所述左 螺旋桨(320)和所述右螺旋桨(310) 均包括桨叶(302)及驱动桨叶 (302) 的 驱动马达组件(304)。  7. The empennage double propeller remote control toy helicopter according to claim 6, wherein the left propeller (320) and the right propeller (310) each comprise a paddle (302) and a drive paddle ( 302) Drive motor assembly (304).
8、 根据权利要求 7所述的尾翼双螺旋浆遥控玩具直升飞机, 其特征在于, 所述机 体(100)的尾部中央还设置有一螺旋浆。  The empennage double propeller remote control toy helicopter according to claim 7, characterized in that a propeller is further disposed at the center of the tail of the body (100).
PCT/CN2014/070191 2014-01-06 2014-01-06 Remotely controlled toy helicopter with double-propeller empennage WO2015100754A1 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109143854A (en) * 2018-07-27 2019-01-04 南京航空航天大学 It is a kind of solve helicopter tail rotor clamping stagnation after safe landing procedures numerical value emulation method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5836545A (en) * 1994-04-25 1998-11-17 Paul E. Arlton Rotary wing model aircraft
US20070105474A1 (en) * 2005-11-09 2007-05-10 Taiyo Kogyo Co., Ltd. Radio control flying toy
DE202006020254U1 (en) * 2006-12-15 2008-03-13 Silverlit Toys Inc., Walnut helicopter
CN201101892Y (en) * 2007-06-27 2008-08-20 倪康汉 Telecontrolled model helicopter
JP2010075568A (en) * 2008-09-26 2010-04-08 Nikko:Kk Helicopter toy
CN201744174U (en) * 2010-01-21 2011-02-16 罗之洪 Model airplane vertically taking off and landing

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5836545A (en) * 1994-04-25 1998-11-17 Paul E. Arlton Rotary wing model aircraft
US20070105474A1 (en) * 2005-11-09 2007-05-10 Taiyo Kogyo Co., Ltd. Radio control flying toy
DE202006020254U1 (en) * 2006-12-15 2008-03-13 Silverlit Toys Inc., Walnut helicopter
CN201101892Y (en) * 2007-06-27 2008-08-20 倪康汉 Telecontrolled model helicopter
JP2010075568A (en) * 2008-09-26 2010-04-08 Nikko:Kk Helicopter toy
CN201744174U (en) * 2010-01-21 2011-02-16 罗之洪 Model airplane vertically taking off and landing

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109143854A (en) * 2018-07-27 2019-01-04 南京航空航天大学 It is a kind of solve helicopter tail rotor clamping stagnation after safe landing procedures numerical value emulation method

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