CN201139949Y - Remote control helicopter - Google Patents
Remote control helicopter Download PDFInfo
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- CN201139949Y CN201139949Y CNU2007200557665U CN200720055766U CN201139949Y CN 201139949 Y CN201139949 Y CN 201139949Y CN U2007200557665 U CNU2007200557665 U CN U2007200557665U CN 200720055766 U CN200720055766 U CN 200720055766U CN 201139949 Y CN201139949 Y CN 201139949Y
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- 230000000694 effects Effects 0.000 claims 1
- 239000012634 fragment Substances 0.000 claims 1
- 230000002787 reinforcement Effects 0.000 claims 1
- 230000003139 buffering effect Effects 0.000 abstract description 4
- 230000005540 biological transmission Effects 0.000 description 9
- 230000003014 reinforcing effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
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Abstract
Description
[技术领域] [technical field]
本实用新型涉及一种玩具,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 utility model relates to a toy, in particular to a remote control helicopter which uses two pairs of upper and lower rotors to rotate positively and negatively to produce lift force 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 feature of the biplane remote control helicopter is: two pairs of rotors on the same axis, one pair is a positive rotation rotor, and the other pair is a counter rotation rotor, thereby offsetting the counter rotation force generated when the two pairs of rotors rotate. When both pairs of rotors accelerate or decelerate simultaneously, the helicopter ascends or descends. When one pair of rotors speeds up and the other pair slows down, 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,直升机可自由的飞行,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,尤其是降落时旋转轴上的旋翼在降落瞬间冲力大,旋转轴在很大冲力作用下往往会撞穿主轴支撑点,使得旋转轴上的齿轮与电机齿轮脱离,影响直升机再次飞行。因此,有必要改进现有直升机的结构,以增强其实用性能。At present, most of the biplane remote control helicopters sold on the market are relatively large oil-powered coaxial biplane remote control helicopters, which cannot be sold in large quantities due to high risk, high cost, low production volume, and complicated process; electric power biplane remote control helicopters use wireless control. Helicopters can fly freely and are highly entertaining. However, due to the unstable rotation of the wings of electric power remote control helicopters, the helicopters are very unstable during flight and have large swings; at the same time, due to the fact that electric helicopters inevitably collide with hard objects in actual use , such as colliding with the ground when landing, or colliding with obstacles such as walls when flying, it is often damaged by collision, especially when the rotor on the rotating shaft has a large momentum at the moment of landing, the rotating shaft will often crash through under the action of a large momentum. The main shaft support point makes the gear on the rotating shaft disengage from the motor gear, affecting the helicopter to fly again. Therefore, it is necessary to improve the structure of the existing helicopter to enhance its practical performance.
[实用新型内容][utility model content]
本实用新型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 utility model overcomes the above-mentioned technical deficiencies, and provides a remote-controlled helicopter with stable flight and strong anti-collision performance.
为实现上述目的,本实用新型采用了下列技术方案:In order to achieve the above object, the utility model adopts the following technical solutions:
一种遥控直升机,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:所述下旋翼套装在管上,所述上旋翼活动套装在轴上端,轴上部套设有防护套,防护套下端活动套装在上述管外;A remote-controlled helicopter, including a casing, a base, an upper rotor and a lower rotor, a motor, a transmission gear set connected to the motor, and a controller. The motor and the transmission gear set are installed on the base, and the base is equipped with a rotatable Shaft and 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. It is characterized in that: the lower rotor is set on the tube, and the upper rotor is movably set on the upper end of the shaft. The lower end of the protective sleeve is movable outside the above-mentioned tube;
如上所述机座上设置有沉孔,在沉孔底部放置有一起缓冲作用的小钢珠,所述轴下端插装在沉孔内;As mentioned above, a counterbore is provided on the machine base, and a small steel ball with buffering effect is placed at the bottom of the counterbore, and the lower end of the shaft is inserted into the counterbore;
如上所述机座上设置有沉孔,在沉孔底部放置有一可与所述轴弹性接触的弹片,所述轴下端插装在沉孔内;As mentioned above, a counterbore is provided on the machine base, and a shrapnel elastically contacting the shaft is placed at the bottom of the counterbore, and the lower end of the shaft is inserted into the counterbore;
如上所述机座由上、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结合,该上座部中央设有一贯通的轴孔,所述沉孔位于下座部中央,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;As mentioned above, the machine base is composed of an upper seat part and a lower seat part separated from the upper and lower parts. The lower seat part is combined with the upper seat part through the surrounding support part. A through shaft hole is provided in the center of the upper seat part. The lower end of the tube passes through the above-mentioned shaft hole and is fixedly connected with the reverse rotation gear on the transmission gear set, and the shaft passes through the tube and is fixedly connected with the forward rotation gear on the transmission gear set;
如上所述轴为空心轴,所述上座部的轴孔处固定连接有空心管,所述管套装上述空心管内;As mentioned above, the shaft is a hollow shaft, and a hollow tube is fixedly connected to the shaft hole of the upper seat, and the tube is set inside the hollow tube;
如上所述沉孔内还套装有稳定轴的钢套,所述轴下端插装在钢套内;As mentioned above, the counterbore is also equipped with a steel sleeve for stabilizing the shaft, and the lower end of the shaft is inserted into the steel sleeve;
如上所述防护套上端为‘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;As mentioned above, the upper end of the protective cover is in the shape of a 'cross', and the angle between the 'cross' is provided with reinforcing ribs, and the upper end of the protective cover is protrudingly installed in the 'cross' groove at the center of the upper rotor;
如上所述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;As mentioned above, a screw is screwed on the wall of the protective sleeve, and a positioning groove is opened on the shaft, and the front end of the screw is clamped in the above positioning groove;
如上所述轴上部活动连接有平衡锤装置,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;As mentioned above, a counterweight device is movably connected to the upper part of the shaft. The counterweight device includes a balance frame movably connected to the protective sleeve and two counterweights fixedly connected to the balance frame. Flying ribs;
如上所述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。As mentioned above, the connecting parts of the counterweight and the balance frame are all screwed with screws, and the screws pass through the screw holes on the balance frame and are stuck in the slots on the shaft of the counterweight.
本实用新型的有益效果是:The beneficial effects of the utility model 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,能很容易的被平衡锤装置纠正,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 counterweight device for balancing are connected by connecting rods, which solves the stable relationship between the counterweight device and the upper rotor. When the upper rotor is unstable, it can be easily corrected by the counterweight device. The lever connection structure formed by the hole ball head connecting rod movably connecting the upper rotor and the counterweight 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采用螺钉紧固连接,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 counterweight device are fastened and connected by screws. The front end of the connecting screw is stuck in the corresponding groove, 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,其上端套设有采用螺钉卡接的防护套,其下端放置有一起缓冲作用的小钢珠。当遥控飞机降落时,卡接螺钉将轴紧固住,避免了轴的上串或下移;而小钢珠将轴向下冲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,从而大大提高了遥控直升机的飞行稳定性能及抗撞击性能;3. The upper end of the shaft that is fixedly connected with the upper rotor is provided with a protective cover that is clamped with screws, and the lower end is placed with a small steel ball that acts as a buffer. When the remote control plane lands, the clamping screw fastens the shaft, avoiding the shaft from going up or down; and the small steel balls disperse the downward impact force of the shaft to different directions, so as to prevent the shaft from colliding with the supporting point and causing the shaft to be damaged. The positive rotation gear is separated from the motor gear, which greatly 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。4. The upper and lower rotors are made of anti-fall tough plastic, which is light and durable.
[附图说明] [Description of drawings]
下面结合附图与本实用新型的实施方式作进一步详细的描述:Below in conjunction with accompanying drawing and embodiment of the present utility model, describe in further detail:
图1为本实用新型的爆炸图;Fig. 1 is the explosion diagram of the utility model;
图2为图1中A处放大图;Figure 2 is an enlarged view of A in Figure 1;
图3为本实用新型的立体图;Fig. 3 is the perspective view of the utility model;
图4为本实用新型上旋翼处各部件组装结构剖示图;Fig. 4 is a cross-sectional view of the assembly structure of the components at the upper rotor of the utility model;
图5为本实用新型第二组上旋翼处各部件组装结构剖示图;Fig. 5 is a sectional view of the assembly structure of the components at the second set of upper rotors of the utility model;
图6为本实用新型第三组上旋翼处各部件组装结构剖示图;Fig. 6 is a cross-sectional view of the assembly structure of the components at the third group of upper rotors of the utility model;
图7为本实用新型内部机构与旋翼组装示意图;Figure 7 is a schematic diagram of the internal mechanism and rotor assembly of the utility model;
图8为本实用新型内部机构与旋翼组装组装结构剖示图;Figure 8 is a cross-sectional view of the internal mechanism and rotor assembly structure of the utility model;
图9为图8中B处放大图。Fig. 9 is an enlarged view of B in Fig. 8 .
[具体实施方式] [Detailed ways]
如图所示,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,所述下旋翼14固定套装在管19上,所述上旋翼13活动套装在轴18上端,轴18上部套设有防护套4,防护套4下端活动套装在上述管19外,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。为了增强连接处的牢固性能,本实用新型中,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,以防止轴18的上串或下移;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 remote control helicopter includes an
为了避免轴18在受冲击力时直接与机座12硬性撞击,本实用新型中,机座12上设置有沉孔125,在沉孔125底部放置有一起缓冲作用的小钢珠126,所述轴18下端插装在沉孔125内,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。In order to prevent the
当本实用新型降落时,轴18沿轴向向下移动,其上部通过防护套4对管19的顶压来防止过度移动;轴18下部通过顶压在小钢珠126上,小钢珠126受力后作不定向转动,从而将轴18向下冲击力分散到不同方向,从而避免轴18撞坏支撑点。除了使用小钢珠126外,还可以在沉孔125底部放置有一可与所述轴18弹性接触的弹片,当轴18沿轴向向下移动时,弹片也可起到缓冲作用。When the utility model falls, the
本实用新型中,机座12下部固定连接有两个电机15,两电机15主轴上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,所述沉孔125位于下座部122中央,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。In the utility model, two
其中,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,提高本实用新型抗撞击能力。Wherein, the
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。The upper part of the
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
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 of the
Claims (10)
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| Application Number | Priority Date | Filing Date | Title |
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| CNU2007200557665U CN201139949Y (en) | 2007-08-14 | 2007-08-14 | Remote control helicopter |
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| CNU2007200557665U CN201139949Y (en) | 2007-08-14 | 2007-08-14 | Remote control helicopter |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011035525A1 (en) * | 2009-09-24 | 2011-03-31 | 上海九鹰电子科技有限公司 | Propeller connecting piece for electric model airplane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011035525A1 (en) * | 2009-09-24 | 2011-03-31 | 上海九鹰电子科技有限公司 | Propeller connecting piece for electric model airplane |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20081029 Termination date: 20090914 |