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WO2009018708A1 - A remote control helicopter - Google Patents

A remote control helicopter Download PDF

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Publication number
WO2009018708A1
WO2009018708A1 PCT/CN2008/000418 CN2008000418W WO2009018708A1 WO 2009018708 A1 WO2009018708 A1 WO 2009018708A1 CN 2008000418 W CN2008000418 W CN 2008000418W WO 2009018708 A1 WO2009018708 A1 WO 2009018708A1
Authority
WO
WIPO (PCT)
Prior art keywords
shaft
remote control
tube
control helicopter
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/CN2008/000418
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French (fr)
Chinese (zh)
Inventor
Wenyu Xu
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Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of WO2009018708A1 publication Critical patent/WO2009018708A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys
    • A63H27/12Helicopters ; Flying tops

Definitions

  • the present invention relates to a toy, and more particularly to a remote control helicopter that utilizes the up and down pairs of rotors to rotate forward and backward to produce lift changes and direction changes.
  • the RC helicopter features: two pairs of rotors on the same axis, one pair being a positively rotating rotor and the other pair being a counter-rotating rotor, thereby counteracting the counter-rotation generated by the rotation of the two pairs of rotors.
  • two pairs of rotors accelerate or decelerate at the same time, the helicopter rises or falls.
  • one pair of rotors accelerates and the other pair of blades decelerates, the helicopter turns.
  • the present invention overcomes the above technical deficiencies and provides a remote control helicopter with stable flight stability and strong impact resistance.
  • the invention relates to a remote control helicopter, comprising an organic shell, a base, an upper rotor and a lower rotor, a motor, a transmission gear set and a controller connected to the motor, and the motor and the transmission gear set are mounted on the base, and the base is mounted thereon a rotating shaft and a tube, the lower part of the shaft is set in the tube, and the shaft and the tube are respectively connected with the above-mentioned transmission gear set, and the following features:
  • the rotor is fixedly connected to the tube;
  • the upper rotor movable set is at the upper end of the shaft, and a balance hammer device is movably connected to the upper part of the shaft, and a connecting rod connecting structure is arranged between the balance cymbal device and the upper rotor, and the connecting structure of the connecting rod includes
  • the crossbar of the balance hammer device is fixedly connected, the connecting block on the upper rotor, and the double-hole ball joint link with one end of the movable ferr
  • the remote control helicopter as described above is characterized in that the base is composed of an upper seat portion and a lower seat portion which are spaced apart from each other, and the lower seat portion is combined with the upper seat portion by a peripheral support portion, and a center portion of the upper seat portion is provided with a through hole.
  • a shaft hole, a center of the lower seat portion correspondingly provided with a counterbore, the lower end of the tube passing through the shaft hole and fixedly connected with the counter-rotating gear on the transmission gear set, the shaft passing through the tube and the transmission gear set
  • the positive rotation gear is fixedly connected, the lower end of the shaft is inserted in the above-mentioned counterbore, and a small steel ball with a buffering function is placed at the bottom of the counterbore;
  • the RC helicopter as described above is characterized in that the counterbore is provided with a steel sleeve of a stable shaft, and the lower end of the shaft is inserted into the steel sleeve;
  • the RC helicopter as described above is characterized in that the shaft is a hollow shaft, and a hollow tube is fixedly connected to the shaft hole of the upper seat portion, and the tube is set in the hollow tube;
  • the RC helicopter as described above is characterized in that the upper part of the shaft is sleeved with a protective sleeve, the upper end of the protective sleeve is a "ten" shape, the rib of the "ten” character is provided with a reinforcing rib, and the upper end of the protective sleeve is convexly mounted on the upper rotor Inside the "ten" word slot at the center;
  • the RC helicopter as described above characterized in that the sheath of the protective sleeve is screwed on the wall, and the shaft is provided with a positioning groove, and the front end of the screw is locked in the positioning groove;
  • the remote control helicopter as described above characterized in that the counterweight device comprises a balance frame that is slidably sleeved on the protective cover and two balance hammers fixedly connected to the balance frame, and the outer port of the balance hammer hammer bar is provided with an anti-hammer Body detachment rib;
  • a remote control helicopter as described above, characterized in that the counterweight and the balance frame are The connecting parts are screwed with screws, and the screws pass through the screw holes on the balance frame and are caught in the card slots on the balance hammer rod;
  • the remote control helicopter as described above is characterized in that the rear of the casing is provided with a protective frame, and the protective frame is composed of upper and lower clamping plates, and the tail of the casing is sandwiched between the upper and lower clamping plates, and the two ends of the upper clamping plate are Separate boards are provided;
  • the RC helicopter as described above is characterized in that the casing is internally provided with a carbon fiber rod, and the carbon fiber rod is located at the tail of the casing.
  • the upper rotor and the balanced hammer device with balance function are connected by connecting rods, which solves the stable relationship between the balance hammer device and the upper rotor.
  • the lever connecting structure formed by the active connection of the upper ball and the balance hammer device improves the stability of the upper rotor, thereby improving the flight stability of the remote control helicopter;
  • the components on the balance hammer device and the balance hammer device and the protective sleeve are connected by screws.
  • the front end of the connecting screw is stuck in the corresponding slot, and the connection is firm, which greatly improves the flight stability and impact resistance of the remote control helicopter;
  • the lower side of the shaft fixedly connected with the upper rotor is placed with a small steel ball with a buffering effect.
  • the small steel ball disperses the axial downward impact force in different directions, avoiding the shaft colliding with the support point and causing the shaft to be on the shaft.
  • the positive rotation gear is separated from the motor gear, which improves the flight stability and impact resistance of the remote control helicopter;
  • the upper and lower rotors are made of anti-fall and tough plastic, which is light and durable.
  • FIG. 1 is an exploded view of the present invention
  • Figure 2 is an enlarged view of A in Figure 1;
  • Figure 3 is a perspective view of the present invention
  • Figure 4 is a cross-sectional view showing the assembly structure of the components at the upper rotor of the present invention
  • Figure 5 is a cross-sectional view showing the assembly structure of the components of the second group of upper rotors of the present invention
  • Figure 6 is a cross-sectional view showing the assembly structure of the components of the third group of upper rotors of the present invention
  • Figure 7 is a schematic view showing the assembly of the internal mechanism and the rotor of the present invention
  • Figure 8 is a cross-sectional view showing the assembled structure of the internal mechanism and the rotor of the present invention.
  • Figure 9 is an enlarged view of B in Figure 8.
  • the RC helicopter includes an organic casing 11, a base 12, an upper rotor 13 and a lower rotor 14 made of anti-falling tough plastic, a motor 15, a transmission gear set 16 and a controller connected to the motor 15. 17.
  • the motor 15 and the drive gear set 16 are mounted on the base 12, the base 12 is provided with a rotatable shaft 18 and a tube 19, the lower portion of the shaft 18 is fitted within the tube 19, and the shaft 18 and the tube 19 are respectively coupled to the transmission gear set 16
  • the lower rotor 14 is fixedly connected to the tube 19;
  • the upper rotor 13 is movably fitted on the upper end of the shaft 18, and the upper part of the shaft 18 is sleeved with a protective sleeve 4, and the lower end of the protective sleeve 4 is sleeved on the tube 19, so that the shaft 18 is secured
  • the shaft 18 can be effectively prevented from being bent and deformed; the slee
  • a balance hammer device 2 is movably connected to the upper portion of the shaft 18, and a link connecting structure is disposed between the counterweight device 2 and the upper rotor 13.
  • the link connecting structure includes a cross bar 20 fixedly connected to the counterweight device 2, located at The connecting block 130 at the center of the upper rotor 13 and the double-hole ball joint link 8 with the movable ferrule at the outer end of the crossbar 20 and the other end of the movable ferrule on the connecting block 130.
  • the counterweight device 2 includes a balance frame 21 movably sleeved on the protective cover 4 and two balance hammers 22 fixedly connected to the balance frame 21, and the outer balance port of the balance hammer 22 There is a rib 220 that prevents the hammer from flying off.
  • a screw is screwed to the connecting portion of the counterweight 22 and the balance frame 21, and the screw passes through the screw hole on the balance frame 21 and is caught in the slot 23 of the hammer of the counterweight 22 to prevent the fast-rotating balance hammer 22 from being disengaged.
  • the connection is firm and practical.
  • Two motors 15 are fixedly connected to the lower portion of the base 12, and the gears on the main shafts of the two motors 15 respectively mesh with the counter-rotating gear 161 and the ortho-rotary gear 162 on the transmission gear set 16, and the shafts 18 and 19 are longitudinally movable.
  • the base 12 is composed of an upper seat portion 121 and a lower seat portion 122 which are spaced apart from each other.
  • the reverse gear 161 and the orbiting gear 162 are located between the upper seat portion 121 and the lower seat portion 122, and the counter-rotor gear 161 is located at the orbiting gear 162.
  • the lower seat portion 122 is coupled to the upper seat portion 121 by a peripheral support portion 123.
  • the upper seat portion 121 is provided with a through hole 124 in the center.
  • the center of the lower seat portion 122 is correspondingly provided with a counterbore 125 having a truncated cone shape.
  • the lower end passes through the shaft hole 124 and is fixedly connected to the counter-rotating gear 161.
  • the shaft 18 is fixedly connected to the orbiting gear 162 through the tube 19, and the lower end of the shaft 18 is inserted into the counterbore 125.
  • a small steel ball 126 with a buffering effect is placed at the bottom of the counterbore 125.
  • the shaft 18 moves downward in the axial direction, is pressed against the small steel ball 126, and the small steel ball 126 is forced to be unoriented. Rotating, thereby dispersing the downward impact force of the shaft 18 into different directions, prevents the shaft 18 from damaging the support point and disengaging the ortho-rotor gear 162 on the shaft 18 from the gear on the motor 15.
  • a steel sleeve 127 for stabilizing the shaft 18 is also provided in the counterbore 125, and the lower end of the shaft 18 is inserted into the steel sleeve 127.
  • the shaft 18 is a hollow shaft, and the hollow hole 3 is fixedly connected to the shaft hole 124 of the upper seat portion 121.
  • the tube 19 is set in the hollow tube 3, and the hollow tube 3 functions to cover the tube 19 and the tube 19.
  • the shaft 18 enhances the impact resistance of the RC helicopter of the present invention.
  • a protective frame 9 is provided at the tail portion thereof.
  • the protective frame 9 is composed of upper and lower clamping plates 91, 92 and two side plates 93, and the tail portion of the casing 11 is sandwiched between the upper and lower clamping plates 91. Between 92 and 92, the upper and lower splints 91 and 92 are respectively stuck at the two ends. It is installed in the hole 930 of the two side plates 93; a carbon fiber rod 10 is inserted into the tail portion of the casing 11 to improve the impact resistance of the tail portion of the casing 11.

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  • Toys (AREA)

Abstract

A remote control helicopter includes a cover (11), a base (12), a motor (15), a gear assembly (16), a controller (17), the mask (18) and the coaxial pipe (19) which rotate concentrically in the opposite direction driven by the gear assembly (16), the upper rotor (13) connected at the upper end of the mask (18), the lower rotor (14) connected at the upper end of the pipe (19), the stabilizing hammer device (2) connected at the upside of the mask (18), the rod linking structure connecting the upper rotor (13) and the stabilizing hammer device (2). The rod linking structure includes a level rod (20) fixed on the stabilizing hammer device (2), alink block (130) on the upper rotor (13), the two-hole bulb rod with two end hinging the level rod (20) and the link block (130).

Description

遥控直升机 技术领域  Remote control helicopter

本发明涉及一种玩具, 进一步说的是一种利用上下两对旋翼 作正反旋转而产生升力变化和方向变动的遥控直升机。  The present invention relates to a toy, and more particularly to a remote control helicopter that utilizes the up and down pairs of rotors to rotate forward and backward to produce lift changes and direction changes.

背景技术 Background technique

双翼遥控直升机的特点在于: 同在一条轴线上的两对旋翼, 一对为正旋转旋翼, 另一对为反旋转旋翼, 由此抵消两对旋翼旋 转时产生的反旋力。 当两对旋翼同时加速或减速时, 直升机上升 或下降。 当一对旋翼加速、 另一对旋翼减速时, 直升机就转向。  The RC helicopter features: two pairs of rotors on the same axis, one pair being a positively rotating rotor and the other pair being a counter-rotating rotor, thereby counteracting the counter-rotation generated by the rotation of the two pairs of rotors. When two pairs of rotors accelerate or decelerate at the same time, the helicopter rises or falls. When one pair of rotors accelerates and the other pair of blades decelerates, the helicopter turns.

目前市场上销售的双翼遥控直升机多为较大型的油动力共轴 双翼遥控直升机, 因危险大、 造价高、 生产量低、 工艺复杂而不 能形成大量销售; 电动力双翼遥控直升机采用无线控制, 直升机 可自由地飞行, 娱乐性强, 但是电动力遥控直升机因双翼旋转不 稳定, 使得直升机在飞行过程中很不稳定, 摇摆大; 同时, 由于 电动直升机在实际使用中不可避免地与硬性物体碰撞, 如降落时 与地面碰撞, 飞行时与墙等阻挡物碰撞, 往往因碰撞而破坏。 因 此, 有必要改进现有直升机的结构, 以增强其实用性能。  Most of the two-wing RC helicopters currently on the market are larger oil-powered coaxial two-wing RC helicopters, which cannot be mass-produced due to high risk, high cost, low production volume and complicated process. Electric-powered two-wing RC helicopters use wireless control, helicopters. It is free to fly and entertaining, but the electric-powered remote-controlled helicopter is unstable due to the rotation of the wings, making the helicopter unstable and swaying during flight. At the same time, because the electric helicopter inevitably collides with hard objects in actual use, If it collides with the ground when landing, it collides with obstacles such as walls during flight, and is often destroyed by collision. Therefore, it is necessary to improve the structure of existing helicopters to enhance their practical performance.

发明内容 Summary of the invention

本发明克服了上述技术不足, 提供一种飞行稳定、 抗撞击性 能强的遥控直升机。  The present invention overcomes the above technical deficiencies and provides a remote control helicopter with stable flight stability and strong impact resistance.

为实现上述目的, 本发明采用了下列技术方案:  In order to achieve the above object, the present invention adopts the following technical solutions:

本发明涉及的遥控直升机, 包括有机壳、 机座、 上旋翼和下 旋翼、 电机、 与电机相连的传动齿轮组和控制器, 电机和传动齿 轮组安装在机座上, 机座上装有可旋转的轴和管, 轴下部套装在 管内, 轴和管分别与上述传动齿轮组相连, 其特征在于: 所述下 旋翼与所述管固定相连; 所述上旋翼活动套装在所述轴上端, 轴 上部活动连接有平衡锤装置, 平衡倕装置与上旋翼之间有连杆连 接结构, 连杆连接结构包括与所述平衡锤装置固定相连的横杆、 上旋翼上的连接块以及一端活动卡套在横杆外端且另一端活动卡 套在连接块上的双孔球头连杆; The invention relates to a remote control helicopter, comprising an organic shell, a base, an upper rotor and a lower rotor, a motor, a transmission gear set and a controller connected to the motor, and the motor and the transmission gear set are mounted on the base, and the base is mounted thereon a rotating shaft and a tube, the lower part of the shaft is set in the tube, and the shaft and the tube are respectively connected with the above-mentioned transmission gear set, and the following features: The rotor is fixedly connected to the tube; the upper rotor movable set is at the upper end of the shaft, and a balance hammer device is movably connected to the upper part of the shaft, and a connecting rod connecting structure is arranged between the balance cymbal device and the upper rotor, and the connecting structure of the connecting rod includes The crossbar of the balance hammer device is fixedly connected, the connecting block on the upper rotor, and the double-hole ball joint link with one end of the movable ferrule at the outer end of the crossbar and the other end of the movable ferrule on the connecting block;

如上所述的遥控直升机, 其特征在于所述的机座由上、 下相 距的上座部和下座部组成, 下座部通过周边的支撑部与上座部组 合, 该上座部中央设有一贯通的轴孔, 下座部中央对应设有一沉 孔, 所述管下端穿过上述轴孔并与所述传动齿轮组上的反旋齿轮 固定相连, 所述轴穿过管与所述传动齿轮组上的正旋齿轮固定相 连, 轴下端插装在上述沉孔内, 在沉孔底部放置有一起緩冲作用 的小钢珠;  The remote control helicopter as described above is characterized in that the base is composed of an upper seat portion and a lower seat portion which are spaced apart from each other, and the lower seat portion is combined with the upper seat portion by a peripheral support portion, and a center portion of the upper seat portion is provided with a through hole. a shaft hole, a center of the lower seat portion correspondingly provided with a counterbore, the lower end of the tube passing through the shaft hole and fixedly connected with the counter-rotating gear on the transmission gear set, the shaft passing through the tube and the transmission gear set The positive rotation gear is fixedly connected, the lower end of the shaft is inserted in the above-mentioned counterbore, and a small steel ball with a buffering function is placed at the bottom of the counterbore;

如上所述的遥控直升机, 其特征在于所述的沉孔内套装有稳 定轴的钢套, 所述轴下端插装在钢套内;  The RC helicopter as described above is characterized in that the counterbore is provided with a steel sleeve of a stable shaft, and the lower end of the shaft is inserted into the steel sleeve;

如上所述的遥控直升机, 其特征在于所述的轴为空心轴, 所 述上座部的轴孔处固定连接有空心管, 所述管套装在上述空心管 内;  The RC helicopter as described above is characterized in that the shaft is a hollow shaft, and a hollow tube is fixedly connected to the shaft hole of the upper seat portion, and the tube is set in the hollow tube;

如上所述的遥控直升机, 其特征在于所述的轴上部套设有防 护套, 防护套上端为 "十" 字形, "十" 字夹角处设有加强筋, 防 护套上端凸装在上旋翼中心处的 "十" 字槽内;  The RC helicopter as described above is characterized in that the upper part of the shaft is sleeved with a protective sleeve, the upper end of the protective sleeve is a "ten" shape, the rib of the "ten" character is provided with a reinforcing rib, and the upper end of the protective sleeve is convexly mounted on the upper rotor Inside the "ten" word slot at the center;

如上所述的遥控直升机, 其特征在于所述的防护套套壁上旋 接有螺钉, 所述轴上开有定位槽, 所述螺钉前端卡装在上述定位 槽内;  The RC helicopter as described above, characterized in that the sheath of the protective sleeve is screwed on the wall, and the shaft is provided with a positioning groove, and the front end of the screw is locked in the positioning groove;

如上所述的遥控直升机, 其特征在于所述的平衡锤装置包括 活动套接在防护套上的平衡架以及固定连接在平衡架上的两个平 衡锤, 平衡锤锤杆外端口设有防止锤体飞脱的挡边;  The remote control helicopter as described above, characterized in that the counterweight device comprises a balance frame that is slidably sleeved on the protective cover and two balance hammers fixedly connected to the balance frame, and the outer port of the balance hammer hammer bar is provided with an anti-hammer Body detachment rib;

如上所述的遥控直升机, 其特征在于所述的平衡锤与平衡架 连接部位均旋接有螺钉, 螺钉穿过平衡架上的螺孔并卡在平衡锤 锤杆上的卡槽内; a remote control helicopter as described above, characterized in that the counterweight and the balance frame are The connecting parts are screwed with screws, and the screws pass through the screw holes on the balance frame and are caught in the card slots on the balance hammer rod;

如上所述的遥控直升机, 其特征在于所述的机壳尾部装有防 护架, 防护架由上、 下夹板组成, 所述机壳尾部夹制在上、 下夹 板之间, 上夹板两端部分别设有两侧板;  The remote control helicopter as described above is characterized in that the rear of the casing is provided with a protective frame, and the protective frame is composed of upper and lower clamping plates, and the tail of the casing is sandwiched between the upper and lower clamping plates, and the two ends of the upper clamping plate are Separate boards are provided;

如上所述的遥控直升机, 其特征在于所述的机壳内插有一碳 纤杆, 该碳纤杆位于所述机壳尾部。  The RC helicopter as described above is characterized in that the casing is internally provided with a carbon fiber rod, and the carbon fiber rod is located at the tail of the casing.

本发明的有益效果是:  The beneficial effects of the invention are:

1、上旋翼和起平衡作用的平衡锤装置采用连杆连接,解决了 平衡锤装置对上旋翼的稳定关系, 当上旋翼不稳定时, 能很容易 地被平衡锤装置纠正, 这种用双孔球头连杆活动连接上旋翼和平 衡锤装置形成的杠杆连接结构提高了上旋翼的稳定性, 从而提高 了遥控直升机的飞行稳定性能;  1. The upper rotor and the balanced hammer device with balance function are connected by connecting rods, which solves the stable relationship between the balance hammer device and the upper rotor. When the upper rotor is unstable, it can be easily corrected by the balance hammer device. The lever connecting structure formed by the active connection of the upper ball and the balance hammer device improves the stability of the upper rotor, thereby improving the flight stability of the remote control helicopter;

2、平衡锤装置上各部件以及平衡锤装置与防护套之间采用螺 钉连接, 连接螺钉的前端卡在对应的槽内, 连接牢固, 大大提高 了遥控直升机飞行稳定性能及抗撞击性能;  2. The components on the balance hammer device and the balance hammer device and the protective sleeve are connected by screws. The front end of the connecting screw is stuck in the corresponding slot, and the connection is firm, which greatly improves the flight stability and impact resistance of the remote control helicopter;

3、 与上旋翼固定相连的轴下端放置有一起緩沖作用的小钢 珠, 当遥控飞机降落时, 小钢珠将轴向下沖击力分散到不同方向, 避免轴撞坏支撑点而使轴上的正旋齿轮与电机齿轮脱离, 提高了 遥控直升机的飞行稳定性能及抗撞击性能;  3. The lower side of the shaft fixedly connected with the upper rotor is placed with a small steel ball with a buffering effect. When the remote control plane is lowered, the small steel ball disperses the axial downward impact force in different directions, avoiding the shaft colliding with the support point and causing the shaft to be on the shaft. The positive rotation gear is separated from the motor gear, which improves the flight stability and impact resistance of the remote control helicopter;

4、 上下两旋翼采用抗摔强韧性塑料制成, 既轻巧又耐用。 附图说明  4. The upper and lower rotors are made of anti-fall and tough plastic, which is light and durable. DRAWINGS

下面结合附图与本发明的实施方式作进一步详细的描述: 图 1为本发明的爆炸图;  The embodiments of the present invention will be further described in detail below with reference to the accompanying drawings: FIG. 1 is an exploded view of the present invention;

图 2为图 1中 A处放大图;  Figure 2 is an enlarged view of A in Figure 1;

图 3为本发明的立体图;  Figure 3 is a perspective view of the present invention;

图 4为本发明上旋翼处各部件组装结构剖视图; 图 5为本发明第二组上旋翼处各部件组装结构剖视图; 图 6为本发明第三组上旋翼处各部件组装结构剖视图; 图 7为本发明内部机构与旋翼组装示意图; Figure 4 is a cross-sectional view showing the assembly structure of the components at the upper rotor of the present invention; Figure 5 is a cross-sectional view showing the assembly structure of the components of the second group of upper rotors of the present invention; Figure 6 is a cross-sectional view showing the assembly structure of the components of the third group of upper rotors of the present invention; Figure 7 is a schematic view showing the assembly of the internal mechanism and the rotor of the present invention;

图 8为本发明内部机构与旋翼组装结构剖视图;  Figure 8 is a cross-sectional view showing the assembled structure of the internal mechanism and the rotor of the present invention;

图 9为图 8中 B处放大图。  Figure 9 is an enlarged view of B in Figure 8.

具体实施方式 detailed description

如图所示, 遥控直升机, 包括有机壳 11、 机座 12、 采用抗摔 强韧性塑料制成的上旋翼 13和下旋翼 14、 电机 15、 与电机 15 相连的传动齿轮组 16和控制器 17, 电机 15和传动齿轮组 16安 装在机座 12上, 机座 12上装有可旋转的轴 18和管 19, 轴 18下 部套装在管 19内, 轴 18和管 19分别与传动齿轮组 16相连, 下 旋翼 14与管 19固定相连;上旋翼 13活动套装在所述轴 18上端, 轴 18上部套设有防护套 4, 防护套 4的下端套在管 19上, 这样, 在保证轴 18和管 19同旋转轴心的基础上,可有效防止轴 18弯曲 变形; 防护套 4套壁上旋接有螺钉 5, 螺钉 5前端卡装在轴 18上 的定位槽 180内; 防护套 4上端为 "十" 字形, "十" 字夹角处设 有加强筋 41, 防护套 4上端凸装在上旋翼 13中心处的 "十" 字 槽 131内, 加强筋 41可以提高防护套 4抗扭转性能。  As shown in the figure, the RC helicopter includes an organic casing 11, a base 12, an upper rotor 13 and a lower rotor 14 made of anti-falling tough plastic, a motor 15, a transmission gear set 16 and a controller connected to the motor 15. 17. The motor 15 and the drive gear set 16 are mounted on the base 12, the base 12 is provided with a rotatable shaft 18 and a tube 19, the lower portion of the shaft 18 is fitted within the tube 19, and the shaft 18 and the tube 19 are respectively coupled to the transmission gear set 16 Connected, the lower rotor 14 is fixedly connected to the tube 19; the upper rotor 13 is movably fitted on the upper end of the shaft 18, and the upper part of the shaft 18 is sleeved with a protective sleeve 4, and the lower end of the protective sleeve 4 is sleeved on the tube 19, so that the shaft 18 is secured On the basis of the same axis of rotation of the tube 19, the shaft 18 can be effectively prevented from being bent and deformed; the sleeve of the sleeve 4 is screwed with a screw 5, and the front end of the screw 5 is fitted in the positioning groove 180 on the shaft 18; the upper end of the protective sleeve 4 For the "ten" character shape, the "ten" character is provided with a rib 41 at the corner, and the upper end of the protective sleeve 4 is convexly mounted in the "ten" slot 131 at the center of the upper rotor 13, and the rib 41 can improve the protection sleeve 4 against twisting. performance.

所述轴 18上部活动连接有平衡锤装置 2, 平衡锤装置 2与上 旋翼 13之间有连杆连接结构,该连杆连接结构包括与所述平衡锤 装置 2固定相连的横杆 20、 位于上旋翼 13中心处的连接块 130, 以及一端活动卡套在横杆 20外端且另一端活动卡套在连接块 130 上的双孔球头连杆 8。 当上旋翼 13不稳定时, 通过横杆 20、 双孔 球头连杆 8形成的杠杆关系, 平衡锤装置 2可很容易地纠正上旋 翼 13, 使上旋翼 13快速恢复稳定。  A balance hammer device 2 is movably connected to the upper portion of the shaft 18, and a link connecting structure is disposed between the counterweight device 2 and the upper rotor 13. The link connecting structure includes a cross bar 20 fixedly connected to the counterweight device 2, located at The connecting block 130 at the center of the upper rotor 13 and the double-hole ball joint link 8 with the movable ferrule at the outer end of the crossbar 20 and the other end of the movable ferrule on the connecting block 130. When the upper rotor 13 is unstable, the balance weight device 2 can easily correct the upper rotor 13 by the lever relationship formed by the crossbar 20 and the double-hole ball joint link 8, so that the upper rotor 13 is quickly restored and stabilized.

平衡锤装置 2包括活动套接在防护套 4上的平衡架 21以及固 定连接在平衡架 21上的两个平衡锤 22, 平衡锤 22锤杆外端口设 有防止锤体飞脱的挡边 220。 平衡锤 22与平衡架 21连接部位均 旋接有螺钉, 螺钉穿过平衡架 21上的螺孔并卡在平衡锤 22锤杆 上的卡槽 23内, 避免快速旋转的平衡锤 22甩脱, 连接牢固, 实 用性好。 The counterweight device 2 includes a balance frame 21 movably sleeved on the protective cover 4 and two balance hammers 22 fixedly connected to the balance frame 21, and the outer balance port of the balance hammer 22 There is a rib 220 that prevents the hammer from flying off. A screw is screwed to the connecting portion of the counterweight 22 and the balance frame 21, and the screw passes through the screw hole on the balance frame 21 and is caught in the slot 23 of the hammer of the counterweight 22 to prevent the fast-rotating balance hammer 22 from being disengaged. The connection is firm and practical.

所述机座 12下部固定连接有两个电机 15, 两电机 15主轴上 的齿轮分别与传动齿轮组 16上的反旋齿轮 161、正旋齿轮 162啮 合, 轴 18和管 19沿纵向活动插装在机座 12上。 机座 12由上、 下相距的上座部 121和下座部 122组成, 反旋齿轮 161、 正旋齿 轮 162位于上座部 121和下座部 122之间, 且反旋齿轮 161位于 正旋齿轮 162上方。 下座部 122通过周边的支撑部 123与上座部 121结合, 该上座部 121中央设有一贯通的轴孔 124, 下座部 122 中央对应设有一截面为圆台形的沉孔 125, 所述管 19下端穿过上 述轴孔 124并与反旋齿轮 161固定相连, 轴 18穿过管 19与正旋 齿轮 162固定相连, 轴 18下端插装在上述沉孔 125内。  Two motors 15 are fixedly connected to the lower portion of the base 12, and the gears on the main shafts of the two motors 15 respectively mesh with the counter-rotating gear 161 and the ortho-rotary gear 162 on the transmission gear set 16, and the shafts 18 and 19 are longitudinally movable. On the base 12. The base 12 is composed of an upper seat portion 121 and a lower seat portion 122 which are spaced apart from each other. The reverse gear 161 and the orbiting gear 162 are located between the upper seat portion 121 and the lower seat portion 122, and the counter-rotor gear 161 is located at the orbiting gear 162. Above. The lower seat portion 122 is coupled to the upper seat portion 121 by a peripheral support portion 123. The upper seat portion 121 is provided with a through hole 124 in the center. The center of the lower seat portion 122 is correspondingly provided with a counterbore 125 having a truncated cone shape. The lower end passes through the shaft hole 124 and is fixedly connected to the counter-rotating gear 161. The shaft 18 is fixedly connected to the orbiting gear 162 through the tube 19, and the lower end of the shaft 18 is inserted into the counterbore 125.

在沉孔 125底部放置有一起緩沖作用的小钢珠 126, 当本发 明的遥控直升机降落时, 轴 18 沿轴向向下移动, 顶压在小钢珠 126上, 小钢珠 126受力后作不定向转动, 从而将轴 18向下的沖 击力分散到不同方向, 避免轴 18撞坏支撑点而使轴 18上的正旋 齿轮 162与电机 15上的齿轮脱离。沉孔 125内还套装有用来稳定 轴 18的钢套 127, 轴 18下端插装在钢套 127内。  A small steel ball 126 with a buffering effect is placed at the bottom of the counterbore 125. When the RC helicopter of the present invention is lowered, the shaft 18 moves downward in the axial direction, is pressed against the small steel ball 126, and the small steel ball 126 is forced to be unoriented. Rotating, thereby dispersing the downward impact force of the shaft 18 into different directions, prevents the shaft 18 from damaging the support point and disengaging the ortho-rotor gear 162 on the shaft 18 from the gear on the motor 15. A steel sleeve 127 for stabilizing the shaft 18 is also provided in the counterbore 125, and the lower end of the shaft 18 is inserted into the steel sleeve 127.

所述轴 18为空心轴,所述上座部 121的轴孔 124处固定连接 有空心管 3, 所述管 19套装上述空心管 3内, 空心管 3的作用在 于套住管 19及管 19内的轴 18,提高本发明的遥控直升机的抗撞 击能力。  The shaft 18 is a hollow shaft, and the hollow hole 3 is fixedly connected to the shaft hole 124 of the upper seat portion 121. The tube 19 is set in the hollow tube 3, and the hollow tube 3 functions to cover the tube 19 and the tube 19. The shaft 18 enhances the impact resistance of the RC helicopter of the present invention.

考虑到机壳 11尾部较为细弱, 在其尾部装有防护架 9, 防护 架 9由上、 下夹板 91、 92和两侧板 93组成, 所述机壳 11尾部夹 制在上、 下夹板 91、 92之间, 上、 下夹板 91、 92两端部分别卡 装在两侧板 93上的卡孔 930内; 在机壳 11尾部内还插有一碳纤 杆 10, 以提高机壳 11尾部抗撞击能力。 Considering that the tail portion of the casing 11 is relatively thin, a protective frame 9 is provided at the tail portion thereof. The protective frame 9 is composed of upper and lower clamping plates 91, 92 and two side plates 93, and the tail portion of the casing 11 is sandwiched between the upper and lower clamping plates 91. Between 92 and 92, the upper and lower splints 91 and 92 are respectively stuck at the two ends. It is installed in the hole 930 of the two side plates 93; a carbon fiber rod 10 is inserted into the tail portion of the casing 11 to improve the impact resistance of the tail portion of the casing 11.

Claims

Figure imgf000009_0001
Figure imgf000009_0001
1. 遥控直升机, 包括有机壳( 11 )、 机座( 12 )、 上旋翼( 13 ) 和下旋翼( 14 )、 电机( 15 )、与电机( 15 )相连的传动齿轮组( 16 ) 和控制器( 17 ), 电机( 15 )和传动齿轮组( 16 )安装在机座( 12 ) 上, 机座(12)上装有可旋转的轴(18)和管 (19), 轴(18)下 部套装在管 (19) 内, 轴 (18) 和管 (19)分别与上述传动齿轮 组 (16)相连, 其特征在于: 所述下旋翼 (14) 与所述管 (19) 固定相连; 所述上旋翼(13) 活动套装在所述轴 (18) 上端, 轴 ( 18 )上部活动连接有平衡锤装置( 2 ), 平衡锤装置( 2 )与上旋 翼 (13)之间有连杆连接结构, 连杆连接结构包括与所述平衡锤 装置(2)固定相连的横杆(20)、 上旋翼(13)上的连接块(130) 以及一端活动卡套在横杆(20) 外端且另一端活动卡套在连接块 (130) 上的双孔球头连杆(8)。 1. a remote control helicopter comprising an organic casing (11), a base (12), an upper rotor (13) and a lower rotor (14), a motor (15), a transmission gear set (16) coupled to the motor (15), and The controller (17), the motor (15) and the transmission gear set (16) are mounted on the base (12), and the base (12) is provided with a rotatable shaft (18) and a tube (19), the shaft (18) The lower part is disposed in the tube (19), and the shaft (18) and the tube (19) are respectively connected to the transmission gear set (16), wherein the lower rotor (14) is fixedly connected with the tube (19); The upper rotor (13) is movably fitted on the upper end of the shaft (18), and a balance hammer device (2) is movably connected to the upper portion of the shaft (18), and a link is arranged between the balance hammer device (2) and the upper rotor (13). The connecting structure, the connecting rod connecting structure comprises a cross bar (20) fixedly connected with the counterweight device (2), a connecting block (130) on the upper rotor (13), and a movable ferrule at one end outside the crossbar (20) The other end of the movable sleeve is a double-hole ball joint (8) that is sleeved on the connecting block (130). 2. 根据权利要求 1 所述的遥控直升机, 其特征在于所述的 机座( 12 ) 由上、 下相距的上座部( 121 )和下座部( 122 )组成, 下座部 (122)通过周边的支撑部 (123) 与上座部 (121) 结合, 该上座部 (121) 中央设有一贯通的轴孔(124), 下座部 (122) 中央对应设有一沉孔( 125 ),所述管( 19 )下端穿过上述轴孔( 124 ) 并与所述传动齿轮组(16)上的反旋齿轮(161) 固定相连, 所述 轴( 18 )穿过管( 19 )与所述传动齿轮组( 16 )上的正旋齿轮( 162 ) 固定相连, 轴(18)下端插装在上述沉孔(125)内, 在沉孔(125) 底部放置有一起緩冲作用的小钢球(126)。  2. The remote control helicopter according to claim 1, wherein the base (12) is composed of an upper seat portion (121) and a lower seat portion (122) spaced apart from each other, and the lower seat portion (122) passes a peripheral support portion (123) is coupled to the upper seat portion (121), a central shaft hole (124) is formed in the center of the upper seat portion (121), and a counterbore (125) is disposed in the center of the lower seat portion (122). a lower end of the tube (19) passes through the shaft hole (124) and is fixedly coupled to a counter-rotating gear (161) on the transmission gear set (16), the shaft (18) passing through the tube (19) and the transmission The ortho-rotary gear ( 162 ) on the gear set ( 16 ) is fixedly connected, the lower end of the shaft ( 18 ) is inserted into the counterbore ( 125 ) , and a small steel ball with a buffering function is placed at the bottom of the counterbore ( 125 ) ( 126). 3. 根据权利要求 2 所述的遥控直升机, 其特征在于所述的 沉孔(125) 内套装有稳定轴 (18) 的钢套(127), 所述轴 (18) 下端插装在钢套(127) 内。  3. The remote control helicopter according to claim 2, characterized in that the counterbore (125) is provided with a steel sleeve (127) for stabilizing the shaft (18), and the lower end of the shaft (18) is inserted into the steel sleeve (127) inside. 4. 根据权利要求 2 所述的遥控直升机, 其特征在于所述轴 (18) 为空心轴, 所述上座部 (121) 的轴孔(124) 处固定连接 有空心管 (3), 所述管 (19)套装上述空心管 (3) 内。 4. The remote control helicopter of claim 2, wherein the axle (18) is a hollow shaft, a hollow tube (3) is fixedly connected to the shaft hole (124) of the upper seat portion (121), and the tube (19) is fitted in the hollow tube (3). 5. 根据权利要求 1 所述的遥控直升机, 其特征在于所述轴 (18) 上部套设有防护套(4), 防护套(4) 上端为 "十" 字形, "十" 字夹角处设有加强筋 (41), 防护套(4) 上端凸装在上旋 翼 (13) 中心处的 "十" 字槽 (131) 内。  The remote control helicopter according to claim 1, characterized in that the upper part of the shaft (18) is sleeved with a protective sleeve (4), and the upper end of the protective sleeve (4) is a "ten" shape, and the angle of the "ten" character is A rib (41) is provided, and the upper end of the protective sleeve (4) is protruded into the "ten" slot (131) at the center of the upper rotor (13). 6. 根据权利要求 5 所述的遥控直升机, 其特征在于所述的 防护套( 4 )套壁上旋接有螺钉( 5 ), 所述轴( 18 )上开有定位槽 6. The remote control helicopter according to claim 5, characterized in that the sheath (4) is screwed to the sleeve (5), and the shaft (18) is provided with a positioning groove. (180), 所述螺钉(5) 前端卡装在上述定位槽 (180) 内。 (180), the front end of the screw (5) is fitted in the positioning groove (180). 7. 根据权利要求 5 所述的遥控直升机, 其特征在于所述的 平衡锤装置 (2) 包括活动套接在防护套(4) 上的平衡架 (21) 以及固定连接在平衡架( 21 )上的两个平衡锤 ( 22 ), 平衡锤( 22 ) 锤杆外端口设有防止锤体飞脱的挡边(220)。  7. The remote control helicopter according to claim 5, characterized in that the counterweight device (2) comprises a gimbal (21) movably sleeved on the protective cover (4) and fixedly connected to the gimbal (21) The upper two balancing hammers (22), the counterweight (22), the outer port of the hammer bar is provided with a rib (220) for preventing the hammer from flying off. 8. 根据权利要求 7 所述的遥控直升机, 其特征在于所述的 平衡锤(22) 与平衡架 (21)连接部位均旋接有螺钉, 螺钉穿过 平衡架 (21) 上的螺孔并卡在平衡锤(22)锤杆上的卡槽 (23) 内。  8. The remote control helicopter according to claim 7, wherein the balance weight (22) and the balance frame (21) are screwed to the joint portion of the balance frame (21), and the screw passes through the screw hole on the balance frame (21). It is caught in the slot (23) on the hammer of the counterweight (22). 9. 根据权利要求 1 所述的遥控直升机, 其特征在于所述的 机壳(11)尾部装有防护架(9), 防护架(9)由上、 下夹板(91、 92)组成, 所述机壳 (11)尾部夹制在上、 下夹板(91、 92)之 间, 上夹板(91) 两端部分别设有两侧板(93)。  9. The remote control helicopter according to claim 1, wherein the casing (11) is provided with a protective frame (9) at the rear, and the protective frame (9) is composed of upper and lower clamping plates (91, 92). The tail of the casing (11) is sandwiched between the upper and lower clamping plates (91, 92), and the two ends of the upper clamping plate (91) are respectively provided with two side plates (93). 10. 根据权利要求 1所述的遥控直升机, 其特征在于所述的 机壳( 11 ) 内插有一碳纤杆( 10 ), 该碳纤杆( 10 )位于所述机壳 10. The remote control helicopter according to claim 1, wherein the casing (11) is internally provided with a carbon fiber rod (10), and the carbon fiber rod (10) is located in the casing. (11)尾部。 (11) The tail.
PCT/CN2008/000418 2007-08-08 2008-02-29 A remote control helicopter Ceased WO2009018708A1 (en)

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CN101972548B (en) * 2010-09-09 2012-07-04 倪康汉 Convenient assembling and disassembling axis structure of coaxial double-paddle reversal model helicopter
DE102011010097A1 (en) * 2011-02-01 2012-08-02 Alex Küng helicopter frame

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