CN107310715B - Variable-pitch propeller and flying robot - Google Patents

Variable-pitch propeller and flying robot Download PDF

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Publication number
CN107310715B
CN107310715B CN201710541539.1A CN201710541539A CN107310715B CN 107310715 B CN107310715 B CN 107310715B CN 201710541539 A CN201710541539 A CN 201710541539A CN 107310715 B CN107310715 B CN 107310715B
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China
Prior art keywords
paddle
slider
seat
limiting
variable
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CN107310715A (en
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恽为民
王俊
庞作伟
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Partnerx Robot Changzhou Co ltd
Shanghai Partnerx Robotics Co ltd
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Partnerx Robot Changzhou Co ltd
Shanghai Partnerx Robotics Co ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/32Blade pitch-changing mechanisms mechanical
    • B64C11/36Blade pitch-changing mechanisms mechanical non-automatic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)

Abstract

The invention discloses a variable-pitch propeller and a flying robot, which belong to the technical field of aircrafts, wherein the propeller comprises a propeller seat, a paddle and a sliding block, and the propeller seat is provided with a sliding groove and an auxiliary groove communicated with the sliding groove; the paddle is rotationally connected with the side wall of the paddle seat; the sliding block is in sliding connection with the sliding groove, a guide column accommodated in the auxiliary groove is arranged on the side face of the sliding block, one end, far away from the sliding block, of the guide column is in sliding connection with the paddle, and the guide column is used for converting movement of the sliding block into rotation of the paddle relative to the paddle seat. The rotation of paddle is conveniently adjusted through the removal of slider, and then changes paddle pitch size to change unmanned aerial vehicle power system, increase and decrease unmanned aerial vehicle product promotes the ratio, and then change unmanned aerial vehicle's response speed in the flight, reach the purpose of adjustment unmanned aerial vehicle product mobility, satisfy the demand of different service environment.

Description

一种可变螺距的螺旋桨及飞行机器人A variable-pitch propeller and flying robot

技术领域technical field

本发明涉及飞行器技术领域,尤其涉及一种可变螺距的螺旋桨及应用该可变螺距的螺旋桨的飞行机器人。The invention relates to the technical field of aircraft, in particular to a variable-pitch propeller and a flying robot using the variable-pitch propeller.

背景技术Background technique

随着飞行器技术的日益发展,飞行器在航空测量、安全监控等领域得到广泛应用。螺旋桨是飞行器的重要组成部分,螺旋桨是指靠桨叶在空气或水中旋转,将发动机转动功率转化为推进力的装置。螺距是螺旋桨的一个重要参数,螺距的定义为:假定空气是绝对静止不动的,那么螺旋桨旋转一周,飞机所前进的距离就是一个螺距。所以,在发动机转速一定的前提下,螺距越大,则飞机的速度就越快。显然桨叶的迎角大,桨距就大,桨叶迎角与螺距成正比的关系,因此一些的螺旋桨飞机或直升机说变螺距其实改变的就是桨叶的迎角,而桨叶相对于其所在的安装座转动一定的角度,即可改变桨叶的迎角。大多数的多旋翼无人机,其螺旋桨为定螺距桨叶,待产品定型后,其推动比也随之固定。若用户根据不同的使用环境,需要调整螺旋桨的螺距,进而调整产品机动性的需求,现有产品很难实现。With the development of aircraft technology, aircraft has been widely used in aerial survey, safety monitoring and other fields. The propeller is an important part of an aircraft. The propeller refers to a device that converts the rotational power of the engine into propulsion by rotating the blades in the air or water. The pitch is an important parameter of the propeller. The definition of the pitch is: assuming that the air is absolutely still, then the propeller rotates once, and the distance the aircraft advances is a pitch. Therefore, under the premise of a certain engine speed, the larger the pitch, the faster the aircraft. Obviously, the larger the angle of attack of the blade, the larger the pitch, and the relationship between the angle of attack of the blade and the pitch is proportional, so some propeller planes or helicopters say that changing the pitch actually changes the angle of attack of the blade, and the angle of attack of the blade relative to its other The angle of attack of the blade can be changed by turning the mounting seat where it is located at a certain angle. Most multi-rotor drones have fixed-pitch propellers, and after the product is finalized, its propulsion ratio is also fixed. If the user needs to adjust the pitch of the propeller according to different use environments, and then adjust the mobility of the product, it is difficult to achieve it with existing products.

发明内容Contents of the invention

本发明的目的在于提供一种可变螺距的螺旋桨,以解决现有技术中存在的螺旋桨为定螺距桨叶、可适应范围窄的技术问题。The object of the present invention is to provide a variable-pitch propeller to solve the technical problem in the prior art that the propeller is a fixed-pitch blade and its adaptable range is narrow.

本发明的另一目的在于提供一种飞行机器人,以解决现有技术中存在的螺旋桨为定螺距桨叶、可适应范围窄的技术问题。Another object of the present invention is to provide a flying robot to solve the technical problem in the prior art that the propeller is a fixed-pitch blade and the adaptable range is narrow.

如上构思,本发明所采用的技术方案是:As above design, the technical solution adopted in the present invention is:

一种可变螺距的螺旋桨,包括:A variable pitch propeller comprising:

桨座,其上开设有滑槽和与所述滑槽连通的辅槽;A paddle seat with a chute and an auxiliary chute communicating with the chute;

桨叶,其与所述桨座的侧壁转动连接;a paddle, which is rotatably connected to the side wall of the paddle seat;

滑块,其与所述滑槽滑动连接,所述滑块的侧面上设置有容置于所述辅槽内的导向柱,所述导向柱远离所述滑块的一端与所述桨叶滑动连接,用于将所述滑块的移动转化为所述桨叶相对于所述桨座的转动。A slider, which is slidably connected with the chute, and a guide column accommodated in the auxiliary groove is provided on the side of the slider, and the end of the guide column away from the slider slides with the paddle connected to convert the movement of the slider into the rotation of the paddle relative to the paddle seat.

其中,所述桨叶上设置有连接孔,所述桨座上于所述连接孔的对应位置设置有螺纹沉孔,调节螺钉穿过所述连接孔与所述螺纹沉孔连接,所述连接孔与所述调节螺钉活动连接。Wherein, the paddle is provided with a connection hole, and the paddle seat is provided with a threaded counterbore at the corresponding position of the connection hole, and the adjusting screw passes through the connection hole to connect with the threaded counterbore, and the connection The hole is flexibly connected with the adjusting screw.

其中,所述调节螺钉包括依次连接的螺纹部、第一凸台部和第二凸台部,所述螺纹部与所述螺纹沉孔连接,所述第一凸台部与所述连接孔活动连接,所述第二凸台部位于所述桨叶远离所述桨座的一侧,用于对所述桨叶限位。Wherein, the adjusting screw includes a threaded part, a first boss part and a second boss part connected in sequence, the threaded part is connected with the threaded counterbore, and the first boss part is movable with the connecting hole connected, the second boss portion is located on the side of the paddle away from the paddle seat, and is used to limit the paddle.

其中,所述连接孔有两个,其中一个为圆形孔,另一个为圆弧形孔,所述圆弧形孔与所述圆形孔同圆心,所述桨叶能以所述圆形孔的中心为转轴于所述圆弧形孔限定的范围内转动。Wherein, there are two connecting holes, one of which is a circular hole, and the other is an arc-shaped hole, the arc-shaped hole is concentric with the circular hole, and the paddle can be The center of the hole is the rotating shaft which rotates within the range defined by the arc-shaped hole.

其中,所述桨叶上对应所述导向柱的位置开设有腰形沉槽,所述导向柱远离所述滑块的一端与所述腰形沉槽滑动连接,用于带动所述桨叶转动并对所述桨叶限位。Wherein, a waist-shaped sinker is provided on the paddle corresponding to the position of the guide post, and the end of the guide post away from the slider is slidably connected with the waist-shaped sinker to drive the paddle to rotate And limit the paddle.

其中,还包括:Among them, also include:

调节螺栓,其与所述滑块螺纹连接,通过旋转所述调节螺栓带动所述滑块沿所述滑槽直线滑动;An adjusting bolt is threadedly connected with the slider, and the slider is driven to slide linearly along the chute by rotating the adjusting bolt;

压板,其与所述桨座固定连接并与所述调节螺栓远离所述滑块的一端转动连接,用于对所述调节螺栓限位。A pressure plate is fixedly connected to the paddle seat and rotatably connected to an end of the adjusting bolt away from the slider, and is used for limiting the adjusting bolt.

其中,所述调节螺栓包括螺杆、与所述螺杆连接的限位部和设置在所述限位部远离所述螺杆的一侧的圆形凸台,所述螺杆与所述滑块螺纹连接,所述圆形凸台穿过所述压板上的限位通孔并与所述压板转动连接。Wherein, the adjusting bolt includes a screw rod, a limiting portion connected to the screw rod, and a circular boss arranged on a side of the limiting portion away from the screw rod, the screw rod is threadedly connected with the slider, The circular boss passes through the limiting through hole on the pressing plate and is rotatably connected with the pressing plate.

其中,所述限位部靠近所述压板的侧面上沿周向均匀间隔分布有若干个限位凸起,所述压板靠近所述限位部的侧面上于所述限位凸起的对应位置开设有限位凹槽。Wherein, on the side of the position-limiting part close to the pressure plate, several position-limiting protrusions are evenly spaced along the circumferential direction, and the side of the position-limiting part close to the position-limiting part is at the corresponding position of the position-limiting protrusions. Set up limited grooves.

其中,所述桨座上于所述滑槽的一端设置有容置所述限位部的定位槽,所述限位部与所述定位槽转动连接。Wherein, a positioning groove for accommodating the limiting portion is provided on one end of the sliding groove on the oar seat, and the limiting portion is rotatably connected with the positioning groove.

一种飞行机器人,包括如上任一项所述的可变螺距的螺旋桨。A flying robot, comprising the variable-pitch propeller described in any one of the above.

本发明的有益效果:Beneficial effects of the present invention:

本发明提出的可变螺距的螺旋桨,包括桨座、桨叶和滑块,桨座上开设有滑槽和与滑槽连通的辅槽;桨叶与桨座的侧壁转动连接;滑块与所述滑槽滑动连接,滑块的侧面上设置有容置于辅槽内的导向柱,导向柱远离滑块的一端与桨叶滑动连接,用于将滑块的移动转化为桨叶相对于桨座的转动。通过滑块的移动方便调节桨叶相对于桨座的转动,进而变换桨叶螺距大小,从而改变无人机动力系统,增减无人机产品推动比,进而改变无人机在飞行过程中的响应速度,达到调整无人机产品机动性的目的,满足不同使用环境的需求。The propeller with variable pitch proposed by the present invention comprises a paddle seat, paddle blades and a slider, the paddle seat is provided with a chute and an auxiliary groove communicated with the chute; the blade is rotatably connected with the side wall of the paddle seat; The chute is slidably connected, and the side of the slider is provided with a guide column accommodated in the auxiliary groove, and the end of the guide column away from the slider is slidably connected with the paddle, so as to convert the movement of the slider into relative to the paddle. Rotation of the propeller. Through the movement of the slider, it is convenient to adjust the rotation of the propeller relative to the propeller seat, and then change the pitch of the propeller, thereby changing the power system of the UAV, increasing or decreasing the propulsion ratio of the UAV product, and then changing the UAV during flight. Response speed achieves the purpose of adjusting the mobility of UAV products to meet the needs of different use environments.

本发明提出的飞行机器人,因采用上述可变螺距的螺旋桨,因此能够变换桨叶螺距大小,从而改变无人机动力系统,增减无人机产品推动比,进而改变无人机在飞行过程中的响应速度,达到调整无人机产品机动性的目的,满足不同使用环境的需求。The flying robot proposed by the present invention adopts the above-mentioned variable-pitch propeller, so it can change the pitch of the blade, thereby changing the power system of the UAV, increasing or decreasing the propulsion ratio of the UAV product, and then changing the speed of the UAV during the flight. The response speed can achieve the purpose of adjusting the mobility of UAV products and meet the needs of different use environments.

附图说明Description of drawings

图1是本发明提供的可变螺距的螺旋桨的分解结构示意图;Fig. 1 is the exploded structure schematic diagram of the propeller of variable pitch provided by the present invention;

图2是图1中的桨座的结构示意图;Fig. 2 is a schematic structural view of the paddle seat in Fig. 1;

图3是图1中的调节螺钉的结构示意图;Fig. 3 is a structural schematic diagram of the adjusting screw in Fig. 1;

图4是图1中的调节螺栓的结构示意图;Fig. 4 is a schematic structural view of the adjusting bolt in Fig. 1;

图5是图1中的压板的结构示意图;Fig. 5 is a schematic structural view of the pressing plate in Fig. 1;

图6是本发明提供的可变螺距的螺旋桨的主视图;Fig. 6 is the front view of the propeller of variable pitch provided by the present invention;

图7是图6的俯视图;Figure 7 is a top view of Figure 6;

图8是图6的A-A向剖视图;Fig. 8 is the A-A direction sectional view of Fig. 6;

图9是图6的侧视图;Fig. 9 is a side view of Fig. 6;

图10是图6的B-B向剖视图;Fig. 10 is a B-B direction sectional view of Fig. 6;

图11是与图10对应的图6的C-C向剖视图;Fig. 11 is a C-C cross-sectional view of Fig. 6 corresponding to Fig. 10;

图12是图6的另一状态的B-B向剖视图;Fig. 12 is a B-B cross-sectional view of another state of Fig. 6;

图13是与图12对应的图6的C-C向剖视图。Fig. 13 is a sectional view taken along line C-C of Fig. 6 corresponding to Fig. 12 .

图中:In the picture:

1、桨座;2、桨叶;3、滑块;4、调节螺钉;5、调节螺栓;6、压板;1. Propeller seat; 2. Propeller blade; 3. Slider; 4. Adjusting screw; 5. Adjusting bolt; 6. Pressing plate;

11、滑槽;12、辅槽;13、螺纹沉孔;14、定位槽;11. Chute; 12. Auxiliary groove; 13. Thread counterbore; 14. Positioning groove;

21、圆形孔;22、圆弧形孔;23、腰形沉槽;21. Circular hole; 22. Arc-shaped hole; 23. Waist sink;

31、导向柱;31. Guide column;

41、螺纹部;42、第一凸台部;43、第二凸台部;41. Threaded part; 42. First boss part; 43. Second boss part;

51、螺杆;52、限位部;53、圆形凸台;521、限位凸起;51, screw rod; 52, limit part; 53, circular boss; 521, limit protrusion;

61、限位通孔;62、限位凹槽。61, limiting through hole; 62, limiting groove.

具体实施方式Detailed ways

下面结合附图和实施方式进一步说明本发明的技术方案。可以理解的是,此处所描述的具体实施例仅仅用于解释本发明,而非对本发明的限定。另外还需要说明的是,为了便于描述,附图中仅示出了与本发明相关的部分而非全部。The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention. In addition, it should be noted that, for the convenience of description, only parts related to the present invention are shown in the drawings but not all of them.

参见图1至图13,一种可变螺距的螺旋桨,包括桨座1、桨叶2和滑块3。桨座1上开设有滑槽11和与滑槽11连通的辅槽12;桨叶2与桨座1的侧壁转动连接;滑块3与滑槽11滑动连接,滑块3的侧面上设置有容置于辅槽12内的导向柱31,导向柱31远离滑块3的一端与桨叶2滑动连接,用于将滑块3的移动转化为桨叶2相对于桨座1的转动。Referring to FIGS. 1 to 13 , a variable-pitch propeller includes a propeller seat 1 , a propeller blade 2 and a slider 3 . A chute 11 and an auxiliary groove 12 communicating with the chute 11 are provided on the paddle seat 1; the paddle 2 is rotationally connected with the side wall of the paddle seat 1; the slider 3 is slidingly connected with the chute 11, and the side of the slider 3 is provided with There is a guide column 31 accommodated in the auxiliary groove 12 , and the end of the guide column 31 away from the slider 3 is slidingly connected with the paddle 2 for converting the movement of the slider 3 into the rotation of the paddle 2 relative to the paddle seat 1 .

通过滑块3的移动方便调节桨叶2相对于桨座的转动,进而变换桨叶2螺距大小,从而改变无人机动力系统,增减无人机产品推动比,进而改变无人机在飞行过程中的响应速度,达到调整无人机产品机动性的目的,满足不同使用环境的需求。Through the movement of the slider 3, it is convenient to adjust the rotation of the blade 2 relative to the paddle seat, and then change the pitch of the blade 2, thereby changing the power system of the UAV, increasing or decreasing the driving ratio of the UAV product, and then changing the flight of the UAV. The response speed in the process achieves the purpose of adjusting the mobility of UAV products and meets the needs of different use environments.

在本实施例中,桨叶2有两个,分别位于桨座1相对的的两侧,因此,滑块3上的导向柱31也设置有两个,分别位于滑块3相对的两侧。当然桨叶2的数量可以根据实际需要设置,在此不作限制。In this embodiment, there are two paddles 2, which are respectively located on opposite sides of the paddle seat 1, therefore, there are also two guide posts 31 on the slider 3, which are respectively located on opposite sides of the slider 3. Of course, the number of paddles 2 can be set according to actual needs, and there is no limitation here.

桨叶2上设置有连接孔,桨座1上于连接孔的对应位置设置有螺纹沉孔13,调节螺钉4穿过连接孔与螺纹沉孔13连接,连接孔与调节螺钉4活动连接。在本实施例中,连接孔有两个,其中一个为圆形孔21,另一个为圆弧形孔22,圆弧形孔22与圆形孔21同圆心,桨叶2能以圆形孔21的中心为转轴于圆弧形孔22限定的范围内转动。The paddle 2 is provided with a connection hole, and the paddle seat 1 is provided with a threaded counterbore 13 at the corresponding position of the connection hole. In this embodiment, there are two connecting holes, one of which is a circular hole 21, and the other is an arc-shaped hole 22. The arc-shaped hole 22 is concentric with the circular hole 21, and the paddle 2 can The center of 21 is that the rotating shaft rotates in the range limited by the arc-shaped hole 22 .

调节螺钉4包括依次连接的螺纹部41、第一凸台部42和第二凸台部43,螺纹部41与螺纹沉孔13连接,第一凸台部42与连接孔活动连接,第二凸台部43位于桨叶2远离所述桨座1的一侧,用于对桨叶2限位。在本实施例中,第一凸台部42的直径大于螺纹部41的直径,第二凸台部43的直径大于第一凸台部42的直径。当然,第二凸台部43也可以不是圆柱状,只要保证桨叶2不会从第一凸台部42处脱出即可。The adjusting screw 4 includes a threaded part 41, a first boss part 42 and a second boss part 43 connected in sequence, the threaded part 41 is connected with the threaded counterbore 13, the first boss part 42 is movably connected with the connecting hole, and the second boss part 42 is connected with the connecting hole. The platform 43 is located on the side of the paddle 2 away from the paddle seat 1 , and is used for limiting the paddle 2 . In this embodiment, the diameter of the first boss portion 42 is larger than the diameter of the threaded portion 41 , and the diameter of the second boss portion 43 is larger than the diameter of the first boss portion 42 . Certainly, the second boss portion 43 may not be cylindrical, as long as it is ensured that the paddle 2 will not come out from the first boss portion 42 .

桨叶2上对应导向柱31的位置开设有腰形沉槽23,导向柱31远离滑块3的一端与腰形沉槽23滑动连接,用于带动桨叶2转动并对桨叶2限位。当然,沉槽也可以不是腰形,而是其他能够实现导向限位功能的形状,在此不作限制。因为导向柱31沿沉槽滑动并对桨叶2限位,因此沉槽不能是与圆形孔21同圆心的弧形孔,否则无法实现限位功能。A waist-shaped sinking groove 23 is provided on the position corresponding to the guide post 31 on the paddle 2, and the end of the guide post 31 far away from the slider 3 is slidably connected with the waist-shaped sinking groove 23, which is used to drive the paddle 2 to rotate and limit the paddle 2 . Of course, the sinker can also be not waist-shaped, but other shapes capable of realizing the function of guiding and limiting, which is not limited here. Because the guide column 31 slides along the sinker groove to limit the position of the paddle 2, the sinker groove cannot be an arc-shaped hole with the same center as the circular hole 21, otherwise the limit function cannot be realized.

还包括调节螺栓5和压板6,调节螺栓5与滑块3螺纹连接,通过旋转调节螺栓5带动滑块3沿滑槽11直线滑动;压板6与桨座1固定连接并与调节螺栓5远离滑块3的一端转动连接,用于对调节螺栓5限位。It also includes an adjusting bolt 5 and a pressure plate 6, the adjusting bolt 5 is threadedly connected with the slider 3, and the adjusting bolt 5 is rotated to drive the slider 3 to slide linearly along the chute 11; One end of the block 3 is rotatably connected to limit the adjustment bolt 5 .

调节螺栓5包括螺杆51、与螺杆51连接的限位部52和设置在限位部52远离螺杆51的一侧的圆形凸台53,螺杆51与滑块3螺纹连接,圆形凸台53穿过压板6上的限位通孔61并与压板6转动连接。限位部52靠近压板6的侧面上沿周向均匀间隔分布有若干个限位凸起521,压板6靠近限位部52的侧面上于限位凸起521的对应位置开设有限位凹槽62。桨座1上于滑槽11的一端设置有容置限位部52的定位槽14,限位部52与定位槽14转动连接。The adjusting bolt 5 includes a screw rod 51, a limiting portion 52 connected to the screw rod 51 and a circular boss 53 arranged on the side of the limiting portion 52 away from the screw rod 51, the screw rod 51 is threadedly connected with the slide block 3, and the circular boss 53 Pass through the limiting through hole 61 on the pressing plate 6 and be connected with the pressing plate 6 in rotation. On the side of the limiting portion 52 close to the pressure plate 6, there are several limiting protrusions 521 evenly distributed along the circumferential direction, and the side of the pressing plate 6 close to the limiting portion 52 is provided with a limiting groove 62 at the corresponding position of the limiting protrusions 521. . One end of the chute 11 on the paddle seat 1 is provided with a positioning groove 14 for accommodating a limiting portion 52 , and the limiting portion 52 is rotatably connected to the positioning groove 14 .

在装配时,将调节螺栓5旋入并穿过滑块3上的螺孔,然后将滑块3嵌入桨座1上的滑槽11内,同时将导向柱31容置于辅槽12内,并将调节螺栓5的限位部52嵌入定位槽14内,用压块压住调节螺栓5,使限位凹槽62与限位凸起521相卡合,用螺钉将压块紧固于桨座1上,从而限制调节螺栓5的自由度,使得调节螺栓5只保留沿其轴向旋转的自由度;将导向柱31远离滑块3的一端插入桨叶2上的腰形沉槽23中,用调节螺钉4连接桨叶2和桨座1,但是调节螺钉4不会将桨叶2锁死,因为第一凸台部42与连接孔活动连接,使得桨叶2能以圆形孔21的中心为转轴于圆弧形孔22限定的范围内转动。When assembling, screw the adjusting bolt 5 into and pass through the screw hole on the slider 3, then insert the slider 3 into the chute 11 on the paddle seat 1, and at the same time place the guide column 31 in the auxiliary groove 12, And insert the limit portion 52 of the adjusting bolt 5 into the positioning groove 14, press the adjusting bolt 5 with a pressure block, make the limit groove 62 engage with the limit protrusion 521, and fasten the pressure block to the paddle with screws seat 1, thereby restricting the degree of freedom of the adjustment bolt 5, so that the adjustment bolt 5 only retains the degree of freedom of rotation along its axial direction; insert the end of the guide post 31 away from the slider 3 into the waist-shaped sinking groove 23 on the blade 2 , use the adjusting screw 4 to connect the paddle 2 and the paddle seat 1, but the adjusting screw 4 will not lock the paddle 2, because the first boss part 42 is movably connected with the connection hole, so that the paddle 2 can be connected with the circular hole 21 The center is that the rotating shaft rotates within the range limited by the arc-shaped hole 22 .

调节螺距时,旋转调节螺栓5,滑块3沿调节螺栓5轴向于滑槽11内移动,进而带动导向柱31沿辅槽12移动,因导向柱31的一端与桨叶2的腰形沉槽23滑动连接,因此导向柱31挤压腰形沉槽23的内壁对桨叶2导向,使得桨叶2能以圆形孔21的中心为转轴转动,当停止旋转调节螺栓5时,导向柱31不再移动,导向柱31与腰形沉槽23紧抵,桨叶2沿圆形孔21为轴心转动方向的自由度被锁死,进而实现对桨叶2的限位,最终实现改变桨叶2的螺距。When adjusting the pitch, rotate the adjusting bolt 5, the slide block 3 moves in the chute 11 along the axis of the adjusting bolt 5, and then drives the guide post 31 to move along the auxiliary groove 12, because one end of the guide post 31 and the waist shape of the paddle 2 sink The slot 23 is slidingly connected, so the guide column 31 squeezes the inner wall of the waist-shaped sinking groove 23 to guide the paddle 2, so that the paddle 2 can rotate with the center of the circular hole 21 as the rotating shaft. When the rotation of the adjusting bolt 5 is stopped, the guide column 31 no longer moves, and the guide column 31 is in close contact with the waist-shaped sinker 23, and the degree of freedom of the paddle 2 along the circular hole 21 as the axis rotation direction is locked, thereby realizing the limitation of the paddle 2, and finally realizing the change The pitch of blade 2.

在旋转调节螺栓5的过程中,因压块上的限位凹槽62与调节螺栓5上的限位凸起521相卡合,相邻限位凹槽62之间的有固定角度,保证调节螺栓5在旋转过程中经N个固定角度后能够定位,进而控制滑块3沿调节螺栓5轴向运动的N个行程。During the process of rotating the adjusting bolt 5, because the limiting groove 62 on the pressure block is engaged with the limiting protrusion 521 on the adjusting bolt 5, there is a fixed angle between adjacent limiting grooves 62 to ensure adjustment. The bolt 5 can be positioned after going through N fixed angles during the rotation process, thereby controlling N strokes of the slider 3 moving axially along the adjusting bolt 5 .

图10至图13示出了桨叶2分别位于两种状态时的示意图。桨叶2由图11的状态旋转到图13的状态过程是:旋转调节螺栓5使得滑块3竖直向下运动,同时,导向柱31挤压腰形沉槽23侧壁,使得桨叶2以圆形孔21的中心为轴心作顺时针转动;当滑块3停止向下运动时,桨叶2沿圆形孔21的中心为轴心转动方向的自由度被锁死,实现改变桨叶2的螺距。Fig. 10 to Fig. 13 show the schematic diagrams when the paddle 2 is in two states respectively. The process of the paddle 2 rotating from the state of FIG. 11 to the state of FIG. 13 is: rotating the adjusting bolt 5 to make the slide block 3 move vertically downward, at the same time, the guide column 31 squeezes the side wall of the waist-shaped sinker 23, so that the paddle 2 Rotate clockwise with the center of the circular hole 21 as the axis; when the slider 3 stops moving downward, the degree of freedom of the paddle 2 along the center of the circular hole 21 as the axis is locked, realizing changing the paddle The pitch of leaf 2.

本发明实施例还提供一种飞行机器人,包括上述的可变螺距的螺旋桨,因能够变换桨叶2螺距大小,从而改变无人机动力系统,增减无人机产品推动比,进而改变无人机在飞行过程中的响应速度,达到调整无人机产品机动性的目的,满足不同使用环境的需求。The embodiment of the present invention also provides a flying robot, including the above-mentioned variable-pitch propeller, because it can change the size of the pitch of the blade 2, thereby changing the unmanned aerial vehicle power system, increasing or decreasing the driving ratio of the unmanned aerial vehicle product, and then changing the unmanned The response speed of the drone during the flight can achieve the purpose of adjusting the maneuverability of drone products and meet the needs of different use environments.

以上实施方式只是阐述了本发明的基本原理和特性,本发明不受上述实施方式限制,在不脱离本发明精神和范围的前提下,本发明还有各种变化和改变,这些变化和改变都落入要求保护的本发明范围内。本发明要求保护范围由所附的权利要求书及其等效物界定。The above embodiments only set forth the basic principles and characteristics of the present invention. The present invention is not limited by the above embodiments. On the premise of not departing from the spirit and scope of the present invention, the present invention also has various changes and changes. These changes and changes are all fall within the scope of the claimed invention. The protection scope of the present invention is defined by the appended claims and their equivalents.

Claims (6)

1.一种可变螺距的螺旋桨,其特征在于,包括:1. A variable-pitch propeller, characterized in that, comprising: 桨座(1),其上开设有滑槽(11)和与所述滑槽(11)连通的辅槽(12);A paddle seat (1), on which a chute (11) and an auxiliary chute (12) communicating with the chute (11) are opened; 桨叶(2),其与所述桨座(1)的侧壁转动连接;a paddle (2), which is rotatably connected to the side wall of the paddle seat (1); 滑块(3),其与所述滑槽(11)滑动连接,所述滑块(3)的侧面上设置有容置于所述辅槽(12)内的导向柱(31),所述导向柱(31)远离所述滑块(3)的一端与所述桨叶(2)滑动连接,用于将所述滑块(3)的移动转化为所述桨叶(2)相对于所述桨座(1)的转动;A slider (3), which is slidably connected with the chute (11), a guide column (31) accommodated in the auxiliary groove (12) is provided on the side of the slider (3), and the The end of the guide column (31) away from the slider (3) is slidably connected with the paddle (2), and is used to convert the movement of the slider (3) into the movement of the paddle (2) relative to the Describe the rotation of paddle seat (1); 所述桨叶(2)上设置有连接孔,所述桨座(1)上于所述连接孔的对应位置设置有螺纹沉孔(13),调节螺钉(4)穿过所述连接孔与所述螺纹沉孔(13)连接,所述连接孔与所述调节螺钉(4)活动连接;The paddle (2) is provided with a connecting hole, the paddle seat (1) is provided with a threaded counterbore (13) at the corresponding position of the connecting hole, and the adjusting screw (4) passes through the connecting hole and The threaded counterbore (13) is connected, and the connecting hole is movably connected with the adjusting screw (4); 所述连接孔有两个,其中一个为圆形孔(21),另一个为圆弧形孔(22),所述圆弧形孔(22)与所述圆形孔(21)同圆心,所述桨叶(2)能以所述圆形孔(21)的中心为转轴于所述圆弧形孔(22)限定的范围内转动;There are two connecting holes, one of which is a circular hole (21), and the other is an arc-shaped hole (22), and the arc-shaped hole (22) is concentric with the circular hole (21), The paddle (2) can rotate within the range defined by the arc-shaped hole (22) with the center of the circular hole (21) as the axis of rotation; 所述桨叶(2)上对应所述导向柱(31)的位置开设有腰形沉槽(23),所述导向柱(31)远离所述滑块(3)的一端与所述腰形沉槽(23)滑动连接,用于带动所述桨叶(2)转动并对所述桨叶(2)限位;A waist-shaped sinker (23) is provided on the paddle (2) corresponding to the position of the guide post (31), and the end of the guide post (31) away from the slider (3) is in contact with the waist-shaped sinker (23). The sinker (23) is slidingly connected to drive the paddle (2) to rotate and limit the paddle (2); 所述调节螺钉(4)包括依次连接的螺纹部(41)、第一凸台部(42)和第二凸台部(43),所述螺纹部(41)与所述螺纹沉孔(13)连接,所述第一凸台部(42)与所述连接孔活动连接,所述第二凸台部(43)位于所述桨叶(2)远离所述桨座(1)的一侧,用于对所述桨叶(2)限位。The adjusting screw (4) includes a threaded part (41), a first boss part (42) and a second boss part (43) connected in sequence, and the threaded part (41) and the threaded counterbore (13 ) connection, the first boss portion (42) is flexibly connected to the connection hole, and the second boss portion (43) is located on the side of the paddle (2) away from the paddle seat (1) , used to limit the paddle (2). 2.根据权利要求1所述的可变螺距的螺旋桨,其特征在于,还包括:2. The variable-pitch propeller according to claim 1, further comprising: 调节螺栓(5),其与所述滑块(3)螺纹连接,通过旋转所述调节螺栓(5)带动所述滑块(3)沿所述滑槽(11)直线滑动;An adjusting bolt (5), which is threadedly connected with the slider (3), drives the slider (3) to slide linearly along the chute (11) by rotating the adjusting bolt (5); 压板(6),其与所述桨座(1)固定连接并与所述调节螺栓(5)远离所述滑块(3)的一端转动连接,用于对所述调节螺栓(5)限位。The pressure plate (6), which is fixedly connected with the paddle seat (1) and rotated with the end of the adjusting bolt (5) away from the slider (3), is used to limit the position of the adjusting bolt (5) . 3.根据权利要求2所述的可变螺距的螺旋桨,其特征在于,所述调节螺栓(5)包括螺杆(51)、与所述螺杆(51)连接的限位部(52)和设置在所述限位部(52)远离所述螺杆(51)的一侧的圆形凸台(53),所述螺杆(51)与所述滑块(3)螺纹连接,所述圆形凸台(53)穿过所述压板(6)上的限位通孔(61)并与所述压板(6)转动连接。3. The variable-pitch propeller according to claim 2, characterized in that, the adjusting bolt (5) comprises a screw rod (51), a stopper (52) connected to the screw rod (51) and a Said limiting portion (52) is away from the circular boss (53) on the side of said screw (51), said screw (51) is threadedly connected with said slider (3), said circular boss (53) passes through the limiting through hole (61) on the pressing plate (6) and is rotatably connected with the pressing plate (6). 4.根据权利要求3所述的可变螺距的螺旋桨,其特征在于,所述限位部(52)靠近所述压板(6)的侧面上沿周向均匀间隔分布有若干个限位凸起(521),所述压板(6)靠近所述限位部(52)的侧面上于所述限位凸起(521)的对应位置开设有限位凹槽(62)。4. The variable-pitch propeller according to claim 3, characterized in that, on the side of the position-limiting part (52) close to the pressure plate (6), several position-limiting projections are evenly spaced along the circumferential direction (521), the side of the pressure plate (6) close to the limiting part (52) defines a limiting groove (62) at a position corresponding to the limiting protrusion (521). 5.根据权利要求4所述的可变螺距的螺旋桨,其特征在于,所述桨座(1)上于所述滑槽(11)的一端设置有容置所述限位部(52)的定位槽(14),所述限位部(52)与所述定位槽(14)转动连接。5. The variable-pitch propeller according to claim 4, characterized in that, one end of the chute (11) on the propeller seat (1) is provided with a seat for accommodating the limiting portion (52). The positioning slot (14), the limiting part (52) is rotatably connected with the positioning slot (14). 6.一种飞行机器人,其特征在于,包括如权利要求1-5任一项所述的可变螺距的螺旋桨。6. A flying robot, characterized in that it comprises the variable-pitch propeller according to any one of claims 1-5.
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Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107972862B (en) * 2017-11-21 2020-11-17 歌尔科技有限公司 Load control method and device based on unmanned aerial vehicle and unmanned aerial vehicle
CN108033013A (en) * 2017-12-14 2018-05-15 邵文远 A kind of VTOL fixed-wing unmanned plane
CN109969389A (en) * 2017-12-28 2019-07-05 昆山优尼电能运动科技有限公司 A blade connection structure
CN109677602B (en) * 2018-12-26 2020-08-07 张耀天 Unmanned aerial vehicle wing
CN112067238A (en) * 2020-10-14 2020-12-11 安徽卓尔航空科技有限公司 Wind tunnel experiment pitch adjusting structure

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB464991A (en) * 1935-11-01 1937-04-29 Grettir Algarsson Improvements in and relating to variable pitch propellers
DE707983C (en) * 1937-06-05 1941-07-09 Ver Deutsche Metallwerke Ag Adjustment gear for changing the blade pitch of two or more winged adjusting screws
US2283774A (en) * 1941-08-13 1942-05-19 Milton D Thompson Feathering-blade propeller
GB768595A (en) * 1954-03-30 1957-02-20 Feroy Arne Improvements in or relating to variable pitch propeller
GB1603282A (en) * 1978-04-01 1981-11-25 Bamford & Co Ltd F Variable pitch propeller
CN1062876A (en) * 1990-12-27 1992-07-22 国家工业宇航学会 Gyrocraft rotor hub body
US6364610B1 (en) * 1999-08-05 2002-04-02 Nasyc Holding S.A. Manually adjustable variable-pitch boat propeller
JP2007050869A (en) * 2005-08-17 2007-03-01 Hooku Ai Rando:Kk Variable-pitch propeller
CN204341396U (en) * 2014-11-26 2015-05-20 重庆翼动科技有限公司 A kind of rotor structure of SUAV (small unmanned aerial vehicle)
CN205256669U (en) * 2015-12-24 2016-05-25 上海埃威航空电子有限公司 Many rotor unmanned aerial vehicle of variable pitch and power device thereof
CN105947194A (en) * 2016-06-17 2016-09-21 王伟 Pitch-regulated mechanism of propeller and aircraft provided with mechanism
CN106081067A (en) * 2016-07-04 2016-11-09 王伟 A kind of variable-pitch propeller and the aircraft assembling this device
CN106081101A (en) * 2015-12-30 2016-11-09 王伟 The pitch-changing mechanism of a kind of propeller and the aircraft assembling this device
CN207078312U (en) * 2017-07-05 2018-03-09 上海未来伙伴机器人有限公司 A kind of propeller of variable pitch and flying robot

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090026310A1 (en) * 2007-07-23 2009-01-29 Linn Romeo S Variable pitch anti torque coaxial counter rotation bi-prop rotor
FR2942615B1 (en) * 2009-02-27 2011-04-01 Snecma DEVICE WITH CONTRAROTATIVE PROPELLERS HAVING A MEANS FOR CHANGING THE STEPS OF THE PROPELLERS

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB464991A (en) * 1935-11-01 1937-04-29 Grettir Algarsson Improvements in and relating to variable pitch propellers
DE707983C (en) * 1937-06-05 1941-07-09 Ver Deutsche Metallwerke Ag Adjustment gear for changing the blade pitch of two or more winged adjusting screws
US2283774A (en) * 1941-08-13 1942-05-19 Milton D Thompson Feathering-blade propeller
GB768595A (en) * 1954-03-30 1957-02-20 Feroy Arne Improvements in or relating to variable pitch propeller
GB1603282A (en) * 1978-04-01 1981-11-25 Bamford & Co Ltd F Variable pitch propeller
CN1062876A (en) * 1990-12-27 1992-07-22 国家工业宇航学会 Gyrocraft rotor hub body
US6364610B1 (en) * 1999-08-05 2002-04-02 Nasyc Holding S.A. Manually adjustable variable-pitch boat propeller
JP2007050869A (en) * 2005-08-17 2007-03-01 Hooku Ai Rando:Kk Variable-pitch propeller
CN204341396U (en) * 2014-11-26 2015-05-20 重庆翼动科技有限公司 A kind of rotor structure of SUAV (small unmanned aerial vehicle)
CN205256669U (en) * 2015-12-24 2016-05-25 上海埃威航空电子有限公司 Many rotor unmanned aerial vehicle of variable pitch and power device thereof
CN106081101A (en) * 2015-12-30 2016-11-09 王伟 The pitch-changing mechanism of a kind of propeller and the aircraft assembling this device
CN105947194A (en) * 2016-06-17 2016-09-21 王伟 Pitch-regulated mechanism of propeller and aircraft provided with mechanism
CN106081067A (en) * 2016-07-04 2016-11-09 王伟 A kind of variable-pitch propeller and the aircraft assembling this device
CN207078312U (en) * 2017-07-05 2018-03-09 上海未来伙伴机器人有限公司 A kind of propeller of variable pitch and flying robot

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