CN110588971A - A bird-like flying flapping wing robot that can rotate its wings autonomously - Google Patents
A bird-like flying flapping wing robot that can rotate its wings autonomously Download PDFInfo
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- CN110588971A CN110588971A CN201910938199.5A CN201910938199A CN110588971A CN 110588971 A CN110588971 A CN 110588971A CN 201910938199 A CN201910938199 A CN 201910938199A CN 110588971 A CN110588971 A CN 110588971A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C33/00—Ornithopters
- B64C33/02—Wings; Actuating mechanisms therefor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
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Abstract
本发明提供了一种可自主扭转机翼的仿鸟类飞行扑翼机器人,包括:机架、驱动机构、扑动机构、自主扭转机构、机翼和尾翼;驱动机构、扑动机构及自主扭转机构均安装在机架上,扑动机构分别与驱动机构和自主扭转机构相连,机翼分别与扑动机构和自主扭转机构相连,尾翼与自主扭转机构相连;驱动机构驱动扑动机构上下扑动,且带动自主扭转机构运动,使机翼可自主上下扑动且前后扭转,尾翼在机翼前后扭转的同时上下转动,在结构简单、仿生程度高、飞行效率高,且不额外增加舵机的前提下,实现机翼自主扭转,有效提高飞行升力和推力。
The invention provides a bird-like flying flapping wing robot capable of autonomously twisting the wings, comprising: a frame, a driving mechanism, a flapping mechanism, an autonomous twisting mechanism, wings and an empennage; a driving mechanism, a flapping mechanism and an autonomous twisting mechanism. The mechanisms are all installed on the frame, the flapping mechanism is connected with the driving mechanism and the autonomous torsion mechanism respectively, the wings are respectively connected with the flapping mechanism and the autonomous torsion mechanism, and the empennage is connected with the autonomous torsion mechanism; the driving mechanism drives the flapping mechanism to flutter up and down , and drives the autonomous torsion mechanism to move, so that the wings can flutter up and down autonomously and twist back and forth, and the empennage turns up and down while the wings twist back and forth, which has a simple structure, high degree of bionics, high flight efficiency, and no additional steering gear Under the premise, the independent rotation of the wings can be realized, which can effectively improve the flight lift and thrust.
Description
技术领域technical field
本发明属于仿生机器人领域,尤其涉及一种可自主扭转机翼的仿鸟类飞行扑翼机器人。The invention belongs to the field of bionic robots, and in particular relates to a bird-like flying flapping wing robot capable of autonomously twisting wings.
背景技术Background technique
自然界中的昆虫和鸟类全部采用扑翼的方式进行飞行,仿生扑翼飞行器是模仿昆虫以及鸟类翅膀扑动而设计的一种新型机器人,具有体积小、重量轻、能耗低、噪音低、机动性能优越、隐蔽性强等优势,通过翅膀的扑动和柔性变形产生的向上的升力和向前的推力,实现扑翼机器人在空中的灵活飞行,具有极强的仿生性。经过对昆虫及部分鸟类的研究发现,它们上下扑动的两个过程对飞行有着不同的意义,其下扑过程主要提供飞行的升力,而上扑过程主要产生前进的推力,若要获得较大的升力和推力,昆虫和部分鸟类在飞行过程中翅膀就需要因应上扑和下扑而及时进行扭转变形,但是,目前常见的仿鸟扑翼飞行器很多都不能实现翅膀的扭转,或者能实现扭转但需要额外的电机辅助或者结构非常复杂,难以微型化,以及存在仿生程度不高等问题。Insects and birds in nature all use flapping wings to fly. The bionic flapping wing aircraft is a new type of robot designed to imitate the flapping wings of insects and birds. It has small size, light weight, low energy consumption, and low noise. , Superior maneuverability, strong concealment and other advantages, through the upward lift and forward thrust generated by the flapping and flexible deformation of the wings, the flexible flight of the flapping wing robot in the air is realized, and it has strong bionic properties. Through research on insects and some birds, it has been found that the two processes of their up and down flapping have different meanings to flight. With large lift and thrust, the wings of insects and some birds need to be twisted and deformed in time in response to the upswing and downswing during flight. However, many of the common bird-like flapping wing aircraft cannot realize the twisting of the wings, or can To achieve torsion but requires additional motor assistance or the structure is very complex, it is difficult to miniaturize, and there are problems such as a low degree of bionics.
发明内容Contents of the invention
本发明旨在至少解决现有技术或相关技术中存在的技术问题之一。The present invention aims to solve at least one of the technical problems existing in the prior art or related art.
为此,本发明提出一种可自主扭转机翼的仿鸟类飞行扑翼机器人。For this reason, the present invention proposes a kind of bird-like flying flapping wing robot that can twist wings autonomously.
有鉴于此,本发明提供了一种可自主扭转机翼的仿鸟类飞行扑翼机器人,包括:机架、驱动机构、扑动机构、自主扭转机构、机翼和尾翼;所述驱动机构、扑动机构及自主扭转机构均安装在机架上,所述扑动机构分别与所述驱动机构和自主扭转机构相连,所述机翼分别与所述扑动机构和自主扭转机构相连,所述尾翼与自主扭转机构相连;所述驱动机构驱动扑动机构上下扑动,且带动自主扭转机构运动,使所述机翼可自主上下扑动且前后扭转,所述尾翼在机翼前后扭转的同时上下转动。In view of this, the present invention provides a bird-like flying flapping wing robot capable of autonomously twisting wings, including: a frame, a drive mechanism, a flapping mechanism, an autonomous twisting mechanism, a wing and an empennage; the drive mechanism, Both the flapping mechanism and the autonomous twisting mechanism are installed on the frame, the flapping mechanism is connected with the driving mechanism and the autonomous twisting mechanism respectively, the wings are respectively connected with the flapping mechanism and the autonomous twisting mechanism, the The empennage is connected with the autonomous torsion mechanism; the driving mechanism drives the flapping mechanism to flutter up and down, and drives the autonomous torsion mechanism to move, so that the wing can flutter up and down autonomously and twist back and forth. Turn up and down.
优选地,所述驱动机构包括:电机、电机齿轮、双联齿轮、双联齿轮轴、曲柄齿轮、曲柄齿轮轴及曲柄梁;所述电机设置在机架上,所述双联齿轮通过所述双联齿轮轴设置在机架上,双联齿轮包括第一齿轮和第二齿轮,所述曲柄齿轮通过所述曲柄齿轮轴设置在机架上,所述曲柄梁设置在曲柄齿轮上;所述电机齿轮设置在电机的输出轴上,并与所述第一齿轮啮合,所述曲柄齿轮与第二齿轮啮合。Preferably, the drive mechanism includes: a motor, a motor gear, a double gear, a double gear shaft, a crank gear, a crank gear shaft and a crank beam; the motor is arranged on the frame, and the double gear passes through the The double gear shaft is arranged on the frame, the double gear includes a first gear and a second gear, the crank gear is arranged on the frame through the crank gear shaft, and the crank beam is arranged on the crank gear; The motor gear is arranged on the output shaft of the motor and meshes with the first gear, and the crank gear meshes with the second gear.
优选地,所述电机为空心杯电机,并设置在所述机架的电机槽中,机架后侧设置有第一限位垫片,所述第一限位垫片穿过电机与机架固定连接,所述机架的前端面在垂直于双联齿轮轴的竖直方向上设置有纵向滑槽;所述双联齿轮设置有中心孔,双联齿轮轴穿过双联齿轮的中心孔将双联齿轮设置在机架上,所述双联齿轮轴两端设置有第二限位垫片;曲柄齿轮设置有中心孔,曲柄齿轮轴穿过曲柄齿轮中心孔将曲柄齿轮设置在机架上,曲柄齿轮轴两端设置第三有限位垫片,曲柄齿轮中心孔旁侧还设置有副孔,曲柄梁穿过副孔与曲柄齿轮连接。Preferably, the motor is a hollow cup motor, and is arranged in the motor slot of the frame, and a first spacer is arranged on the rear side of the frame, and the first spacer passes through the motor and the frame Fixedly connected, the front end of the frame is provided with a longitudinal chute in the vertical direction perpendicular to the double gear shaft; the double gear is provided with a central hole, and the double gear shaft passes through the central hole of the double gear Set the dual gear on the frame, and the two ends of the dual gear shaft are provided with second spacers; the crank gear is provided with a central hole, and the crank gear shaft passes through the central hole of the crank gear to arrange the crank gear on the frame Above, the third limit gasket is arranged at both ends of the crank gear shaft, and an auxiliary hole is arranged beside the crank gear central hole, and the crank beam passes through the auxiliary hole and is connected with the crank gear.
优选地,所述扑动机构包括:连杆、联动杆、左翼根部、右翼根部、左旋转滑道、右旋转滑道、左翼支架、右翼支架;所述连杆上下两端均设置有开孔,曲柄梁穿过连杆下端开孔和曲柄齿轮的副孔,将连杆和曲柄齿轮连接,曲柄梁与曲柄齿轮固定连接,连杆与曲柄梁旋转连接,所述连杆下端开孔轴向两端外侧设置有第四限位垫片,所述左旋转滑道和右旋转滑道均与机架旋转连接,且内部均设置有滑槽,所述左翼根部的一端和右翼根部的一端均设置有通孔,所述联动杆穿过连杆上端开孔、左翼根部的通孔、右翼根部的通孔以及机架的纵向滑槽与自主扭转机构连接,联动杆可在机架的纵向滑槽内上下滑动,左翼根部的另一端和右翼根部的另一端分别穿过所述左旋转滑道内部滑槽和右旋转滑道内部滑槽,且分别与左翼支架的一端和右翼支架的一端同中心轴连接,所述联动杆带动左翼根部和右翼根部分别在左旋转滑道和右旋转滑道内滑动,使所述左翼支架和右翼支架分别在左翼根部和右翼根部的带动下上下运动。Preferably, the flapping mechanism includes: a connecting rod, a linkage rod, a root of the left wing, a root of the right wing, a left-rotating slide, a right-rotating slide, a left-wing bracket, and a right-wing bracket; the upper and lower ends of the connecting rod are provided with openings , the crank beam passes through the hole at the lower end of the connecting rod and the auxiliary hole of the crank gear, and connects the connecting rod and the crank gear. A fourth spacer is provided on the outside of the two ends, and the left and right rotation slides are connected to the frame in rotation, and the inside is provided with a chute, and one end of the root of the left wing and one end of the root of the right wing are both A through hole is provided, and the linkage rod passes through the opening at the upper end of the connecting rod, the through hole at the root of the left wing, the through hole at the root of the right wing, and the longitudinal chute of the frame to connect with the independent torsion mechanism, and the linkage rod can slide in the longitudinal direction of the frame. Sliding up and down in the slot, the other end of the root of the left wing and the other end of the root of the right wing pass through the internal chute of the left rotation slideway and the internal chute of the right rotation slideway respectively, and are respectively connected with one end of the left wing support and one end of the right wing support. The central axis is connected, and the linkage rod drives the left wing root and the right wing root to slide in the left and right rotation slides respectively, so that the left wing support and the right wing support move up and down driven by the left wing root and the right wing root respectively.
优选地,所述自主扭转机构包括:滑动块、传动连杆、第一滑道、第二滑道和尾杆,所述滑动块位于所述机架两侧壁之间,滑动块的一端被所述联动杆穿过并与其相连,在联动杆的带动下可在机架两侧壁之间上下滑动,滑动块的另一端与所述传动连杆的一端相连,所述第一滑道和第二滑道与机架两侧壁均连接,并与机架两侧壁间均存有间隙,第一滑道和第二滑道的两端均设置有开口,且内部均设置有滑槽,所述传动连杆的另一端通过第一滑道开口,穿过第一滑道的滑槽与所述尾杆一端相连,传动连杆在滑动块的带动下前后摆动且在第一滑道滑槽内滑动,第一滑道随传动连杆前后摆动,所述尾杆另一端通过第二滑道的开口,穿过第二滑道的滑槽与尾翼相连,尾杆在传动连杆的带动下前后摆动且在第二滑道的滑槽内滑动,第二滑道随尾杆前后摆动。Preferably, the autonomous twisting mechanism includes: a sliding block, a transmission link, a first slideway, a second slideway and a tail rod, the sliding block is located between the two side walls of the frame, and one end of the sliding block is The linkage rod passes through and is connected with it, driven by the linkage rod, it can slide up and down between the two side walls of the frame, the other end of the sliding block is connected with one end of the transmission linkage, and the first slideway and The second slideway is connected to both side walls of the frame, and there is a gap between the two sides of the frame, and both ends of the first slideway and the second slideway are provided with openings, and the insides are provided with chute , the other end of the transmission connecting rod passes through the opening of the first slideway, and is connected to one end of the tail rod through the chute of the first slideway. Sliding in the chute, the first chute swings back and forth with the transmission connecting rod, the other end of the tail rod passes through the opening of the second chute, and the chute passing through the second chute is connected with the tail wing, and the tail rod is on the side of the transmission connecting rod Driven to swing back and forth and slide in the chute of the second slideway, the second slideway swings back and forth with the tail rod.
优选地,所述自主扭转机构还包括:第一销钉、第二销钉、第三销钉和第四销钉;所述滑动块与传动连杆通过第一销钉连接,所述传动连杆与尾杆通过第二销钉连接,所述第一滑道与机架通过第三销钉连接,所述第二滑道与机架通过第四销钉连接。Preferably, the autonomous torsion mechanism further includes: a first pin, a second pin, a third pin and a fourth pin; the sliding block is connected to the transmission link through the first pin, and the transmission link and the tail rod are connected through The second pin is connected, the first slideway is connected with the frame through the third pin, and the second slideway is connected with the frame through the fourth pin.
优选地,所述滑动块为一端设置有开口矩形槽的方体结构,开口矩形槽的两侧壁上设置有相对称的第一对孔,所述传动连杆两侧壁靠近滑动块一端设置有相对称的第二对孔,传动连杆两侧壁远离滑动块的一端设置有相对称的第三对孔,所述传动连杆近滑动块一端插入开口矩形槽,所述第一销钉穿过第一对孔和第二对孔将滑动块和传动连杆旋转连接,所述尾杆的一端设置有通孔,所述第二销钉穿过第三对孔和通孔将传动连杆和尾杆旋转连接;所述第一滑道左侧壁和右侧壁设置有相对称的孔,所述第二滑道左侧壁和右侧壁设置有相对称的孔,所述第三销钉包括第三左销钉和第三右销钉,所述第四销钉包括第四左销钉和第四右销钉,所述第三左销钉一端与机架左侧壁固定连接,另一端插入位于第一滑道左侧壁上的孔中,且不接触传动连杆,所述第三右销钉一端与机架右侧壁固定连接,另一端插入位于第一滑道右侧壁上的孔中,且不接触传动连杆,所述第四左销钉一端与机架左侧壁固定连接,另一端插入位于第二滑道左侧壁上的孔中,且不接触尾杆,所述第四右销钉一端与机架右侧壁固定连接,另一端插入位于第二滑道右侧壁上的孔中,且不接触尾杆。Preferably, the sliding block is a square structure with an open rectangular slot at one end, a first pair of symmetrical holes are provided on the two side walls of the open rectangular slot, and the two side walls of the transmission link are set close to one end of the sliding block. There is a second pair of symmetrical holes, and a third pair of symmetrical holes is provided on the two side walls of the transmission connecting rod away from the sliding block. The end of the transmission connecting rod near the sliding block is inserted into the open rectangular slot, and the first pin penetrates Through the first pair of holes and the second pair of holes, the sliding block and the transmission connecting rod are rotatably connected, and one end of the tail rod is provided with a through hole, and the second pin passes through the third pair of holes and the through hole to connect the transmission connecting rod and the through hole. The tail rod is connected by rotation; the left side wall and the right side wall of the first slideway are provided with symmetrical holes, the left sidewall and the right sidewall of the second slideway are provided with symmetrical holes, and the third pin It includes a third left pin and a third right pin, the fourth pin includes a fourth left pin and a fourth right pin, one end of the third left pin is fixedly connected to the left side wall of the rack, and the other end is inserted into the first slide in the hole on the left side wall of the first slideway without contacting the transmission link, one end of the third right pin is fixedly connected to the right side wall of the frame, and the other end is inserted into the hole on the right side wall of the first slideway without contacting the transmission link. Contacting the transmission link, one end of the fourth left pin is fixedly connected to the left side wall of the frame, and the other end is inserted into the hole on the left side wall of the second slideway without contacting the tail rod. One end of the fourth right pin It is fixedly connected with the right side wall of the rack, and the other end is inserted into the hole on the right side wall of the second slideway without touching the tail rod.
优选地,所述机翼包括左机翼和右机翼,所述左机翼前端与左翼支架相连接,右机翼前端与右翼支架相连接,左机翼后端和右机翼后端均与尾杆连接。Preferably, the wings include a left wing and a right wing, the front end of the left wing is connected to the left wing support, the front end of the right wing is connected to the right wing support, and the rear end of the left wing and the rear end of the right wing are both Connect with tail rod.
优选地,所述尾翼上设置有开孔,所述尾杆一端插入尾翼开孔与其连接,尾翼上方一面与尾杆上切面保持平行。Preferably, the empennage is provided with an opening, one end of the tail rod is inserted into the opening of the empennage and connected thereto, and the upper side of the empennage is kept parallel to the upper section of the tail rod.
优选地,所述机架采用碳纤维薄板材料,所述连杆、左翼支架、右翼支架均采用碳纤维材料,所述机翼采用天然橡胶薄膜材料,所述尾翼采用塑料泡沫材料。Preferably, the frame is made of carbon fiber sheet material, the connecting rod, left wing bracket, and right wing bracket are all made of carbon fiber material, the wing is made of natural rubber film material, and the empennage is made of plastic foam material.
与现有技术相比,本发明的有益效果是:Compared with prior art, the beneficial effect of the present invention is:
1.本发明能实现机器人机翼扑动过程中翼的俯仰角自主扭转,在下扑和上扑过程中调整飞行攻角的变化,使得扑动过程中所受的空气阻力减小,并于扑动过程中增加在前进方向上的推力,提高了前飞速度。1. The present invention can realize the autonomous twisting of the pitch angle of the wing during the flapping process of the robot wing, and adjust the change of the flight angle of attack during the flapping and flapping process, so that the air resistance suffered during the flapping process is reduced, and the flapping process is more efficient. During the maneuvering process, the thrust in the forward direction is increased, and the forward flight speed is increased.
2.本发明实现了尾杆的周期性转动,从而使尾杆带动尾翼上下扑动,进一步增大飞行机器人在前飞方向上的推力,从而使得飞行机器人的飞行速度和空中机动性得以提升,同时尾翼也具有增大升力的效果。2. The present invention realizes the periodic rotation of the tail rod, so that the tail rod drives the tail wing to flutter up and down, further increasing the thrust of the flying robot in the forward flight direction, thereby improving the flying speed and air mobility of the flying robot, Simultaneously the empennage also has the effect of increasing lift.
本发明的附加方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本发明的实践了解到。Additional aspects and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention.
附图说明Description of drawings
图1示出了根据本发明的一个实施例的可自主扭转机翼的仿鸟类飞行扑翼机器人的结构示意图;Fig. 1 shows a schematic structural view of a bird-like flying flapping wing robot capable of autonomously twisting wings according to an embodiment of the present invention;
图2示出了根据本发明的又一个实施例的可自主扭转机翼的仿鸟类飞行扑翼机器人的结构示意图;Fig. 2 shows a structural schematic diagram of a bird-like flying flapping wing robot capable of autonomously twisting wings according to yet another embodiment of the present invention;
图3示出了根据本发明的再一个实施例的可自主扭转机翼的仿鸟类飞行扑翼机器人的结构示意图;Fig. 3 shows a structural schematic diagram of a bird-like flying flapping wing robot capable of autonomously twisting wings according to yet another embodiment of the present invention;
图4示出了根据本发明的再一个实施例的可自主扭转机翼的仿鸟类飞行扑翼机器人的结构示意图;Fig. 4 shows a structural schematic diagram of a bird-like flying flapping wing robot capable of autonomously twisting wings according to yet another embodiment of the present invention;
图5示出了根据本发明的再一个实施例的可自主扭转机翼的仿鸟类飞行扑翼机器人的结构示意图;Fig. 5 shows a structural schematic diagram of a bird-like flying flapping wing robot capable of autonomously twisting wings according to yet another embodiment of the present invention;
图6示出了根据本发明的再一个实施例的可自主扭转机翼的仿鸟类飞行扑翼机器人的结构示意图;Fig. 6 shows a schematic structural view of a bird-like flying flapping wing robot capable of autonomously twisting wings according to yet another embodiment of the present invention;
其中:1机架1;2驱动机构;201电机;202电机齿轮;203双联齿轮;2031第一齿轮;2032第二齿轮;204双联齿轮轴;205曲柄齿轮;206曲柄齿轮轴;207曲柄梁;3扑动机构;301连杆;302联动杆;3031左翼根部;3032右翼根部;3041左旋转滑道;3042右旋转滑道;3051左翼支架;3052右翼支架;4自主扭转机构;401滑动块;4011第一销钉;402传动连杆;4021第二销钉;403第一滑道;4031第三销钉;404尾杆;405第二滑道;4051第四销钉;5机翼;501左机翼;502右机翼;6尾翼。Wherein: 1 frame 1; 2 driving mechanism; 201 motor; 202 motor gear; 203 duplex gear; 2031 first gear; 2032 second gear; 204 duplex gear shaft; 205 crank gear; 206 crank gear shaft; 207 crank Beam; 3 flapping mechanism; 301 connecting rod; 302 linkage rod; 3031 root of left wing; 3032 root of right wing; 3041 left rotation slide; 3042 right rotation slide; Block; 4011 first pin; 402 transmission link; 4021 second pin; 403 first slideway; 4031 third pin; 404 tail rod; 405 second slideway; 4051 fourth pin; 5 wings; 501 left machine Wing; 502 right wing; 6 empennage.
具体实施方式Detailed ways
为了能够更清楚地理解本发明的上述目的、特征和优点,下面结合附图和具体实施方式对本发明进行进一步的详细描述。需要说明的是,在不冲突的情况下,本申请的实施例及实施例中的特征可以相互组合。In order to understand the above-mentioned purpose, features and advantages of the present invention more clearly, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted that, in the case of no conflict, the embodiments of the present application and the features in the embodiments can be combined with each other.
在下面的描述中阐述了很多具体细节以便于充分理解本发明,但是,本发明还可以采用其他不同于在此描述的其他方式来实施,因此,本发明的保护范围并不受下面公开的具体实施例的限制。In the following description, many specific details are set forth in order to fully understand the present invention. However, the present invention can also be implemented in other ways different from those described here. Therefore, the protection scope of the present invention is not limited by the specific details disclosed below. EXAMPLE LIMITATIONS.
下面参照图1至图6描述根据本发明一些实施例所述可自主扭转机翼的仿鸟类飞行扑翼机器人。The following describes the bird-like flying flapping wing robot that can automatically twist the wings according to some embodiments of the present invention with reference to FIGS. 1 to 6 .
在本发明的实施例中,如图1所示,本发明提供了一种机架1、驱动机构2、扑动机构3、自主扭转机构4、机翼5和尾翼6;驱动机构2、扑动机构3及自主扭转机构4均安装在机架1上,扑动机构3分别与驱动机构2和自主扭转机构4相连,机翼5分别与扑动机构3和自主扭转机构4相连,尾翼6与自主扭转机构4相连;驱动机构2驱动扑动机构3上下扑动,且带动自主扭转机构4运动,使机翼5可自主上下扑动且前后扭转,尾翼6在机翼5前后扭转的同时上下转动。In an embodiment of the present invention, as shown in Figure 1, the present invention provides a frame 1, a driving mechanism 2, a flapping mechanism 3, an autonomous twisting mechanism 4, a wing 5 and an empennage 6; Both the moving mechanism 3 and the autonomous torsion mechanism 4 are installed on the frame 1, the flapping mechanism 3 is connected with the driving mechanism 2 and the autonomous torsion mechanism 4 respectively, the wing 5 is connected with the flapping mechanism 3 and the autonomous torsion mechanism 4 respectively, and the empennage 6 Connected with the autonomous torsion mechanism 4; the driving mechanism 2 drives the flapping mechanism 3 to flutter up and down, and drives the autonomous torsion mechanism 4 to move, so that the wing 5 can flutter up and down autonomously and twist back and forth. Turn up and down.
在该实施例中,驱动机构2、扑动机构3以及自主扭转机构4均安装在机架1上,扑动机构3分别与驱动机构2和自主扭转机构4相连,机翼5分别与扑动机构3和自主扭转机构4相连,尾翼6与自主扭转机构4相连,驱动机构2驱动扑动机构3,控制机翼5上下扑动,自主扭转机构4在扑动机构3的带动下,伴随着机翼5的上下扑动,同时实现机翼5翼面的前后扭转,而尾翼6则在自主扭转机构4的带动下,在机翼5翼面前后扭转的同时,上下转动,增加向前飞行的推力,本发明提供的可自主扭转机翼的仿鸟类飞行扑翼机器人,在结构简单、仿生程度高、飞行效率高,且不额外增加舵机的前提下,实现机翼5自主扭转,有效提高飞行升力和推力。In this embodiment, the driving mechanism 2, the flapping mechanism 3 and the autonomous twisting mechanism 4 are all installed on the frame 1, the flapping mechanism 3 is connected with the driving mechanism 2 and the autonomous twisting mechanism 4 respectively, and the wings 5 are connected with the flapping mechanism respectively. Mechanism 3 is connected to autonomous torsion mechanism 4, empennage 6 is connected to autonomous torsion mechanism 4, drive mechanism 2 drives flutter mechanism 3, controls wing 5 to flutter up and down, autonomous torsion mechanism 4 is driven by flutter mechanism 3, accompanied by The fluttering of wing 5 up and down realizes the front and back twisting of wing 5 aerofoil simultaneously, and empennage 6 is then under the drive of autonomous torsion mechanism 4, while wing 5 wing front twists back and forth, rotates up and down, increases forward flight The thrust of the bird-like flapping wing robot that can independently twist the wings provided by the present invention can realize the autonomous twisting of the wings 5 under the premise of simple structure, high degree of bionics, high flight efficiency, and no additional steering gear. Effectively improve flight lift and thrust.
在本发明的一个实施例中,优选地,如图2至图4所示,驱动机构2包括:电机201、电机齿轮202、双联齿轮203、双联齿轮轴204、曲柄齿轮205、曲柄齿轮轴206及曲柄梁207;电机201设置在机架1上,双联齿轮203通过双联齿轮轴204设置在机架1上,双联齿轮203包括第一齿轮2031和第二齿轮2032,曲柄齿轮205通过曲柄齿轮轴206设置在机架1上,曲柄梁207设置在曲柄齿轮205上;电机齿轮202设置在电机201的输出轴上,并与第一齿轮2031啮合,曲柄齿轮205与第二齿轮2032啮合。In one embodiment of the present invention, preferably, as shown in FIGS. Axle 206 and crank beam 207; Motor 201 is arranged on the frame 1, and duplex gear 203 is arranged on the frame 1 by duplex gear shaft 204, and duplex gear 203 comprises first gear 2031 and second gear 2032, crank gear 205 is arranged on the frame 1 through the crank gear shaft 206, and the crank beam 207 is arranged on the crank gear 205; the motor gear 202 is arranged on the output shaft of the motor 201, and meshes with the first gear 2031, and the crank gear 205 and the second gear 2032 meshed.
在该实施例中,电机201提供驱动动力,电机齿轮202受到到电机201的驱动进行转动,带动双联齿轮203转动,双联齿轮203的转动带动曲柄齿轮205的转动,曲柄齿轮205的运动带动曲柄梁207转动。In this embodiment, the motor 201 provides driving power, the motor gear 202 is driven by the motor 201 to rotate, and drives the dual gear 203 to rotate, the rotation of the dual gear 203 drives the rotation of the crank gear 205, and the motion of the crank gear 205 drives The crank beam 207 rotates.
在本发明的一个实施例中,优选地,如图2至图4所示,电机201为空心杯电机,并设置在机架1的电机槽中,机架1后侧设置有第一限位垫片,第一限位垫片穿过电机201与机架1固定连接,机架1的前端面在垂直于双联齿轮轴204的竖直方向上设置有纵向滑槽;双联齿轮203设置有中心孔,双联齿轮轴204穿过双联齿轮203的中心孔将双联齿轮203设置在机架1上,双联齿轮轴204两端设置第二有限位垫片;曲柄齿轮205设置有中心孔,曲柄齿轮轴206穿过曲柄齿轮205中心孔将曲柄齿轮205设置在机架1上,曲柄齿轮轴206两端设置有第三限位垫片,曲柄齿轮205中心孔旁侧还设置有副孔,曲柄梁207穿过副孔与曲柄齿轮205连接。In one embodiment of the present invention, preferably, as shown in Figures 2 to 4, the motor 201 is a hollow cup motor, and is arranged in the motor slot of the frame 1, and the rear side of the frame 1 is provided with a first stop Gasket, the first limit gasket passes through the motor 201 and is fixedly connected with the frame 1, and the front end face of the frame 1 is provided with a longitudinal chute in the vertical direction perpendicular to the double gear shaft 204; the double gear 203 is provided with There is a central hole, the double gear shaft 204 passes through the central hole of the double gear 203 and the double gear 203 is arranged on the frame 1, and the second limit gasket is arranged at the two ends of the double gear shaft 204; the crank gear 205 is provided with Central hole, the crank gear shaft 206 passes through the central hole of the crank gear 205 and the crank gear 205 is arranged on the frame 1. A third spacer is provided at the two ends of the crank gear shaft 206, and the crank gear 205 central hole is also provided with a Auxiliary hole, the crank beam 207 passes through the auxiliary hole and is connected with the crank gear 205 .
在该实施例中,机架1后侧设置有第一限位垫片,用于辅助限制电机201的轴向位移,双联齿轮轴204将双联齿轮203设置在机架1上,双联齿轮轴204两端安装有第二限位垫片,用于限制双轮齿轮的轴向位移,曲柄齿轮轴206将曲柄齿轮205设置在机架1上,曲柄齿轮轴206两端设置有第三限位垫片,用于限制曲柄齿轮205的轴向位移。In this embodiment, the rear side of the frame 1 is provided with a first spacer, which is used to assist in limiting the axial displacement of the motor 201. The double gear shaft 204 sets the double gear 203 on the frame 1. The two ends of the gear shaft 204 are equipped with a second spacer, which is used to limit the axial displacement of the double wheel gear. The crank gear shaft 206 arranges the crank gear 205 on the frame 1, and the crank gear shaft 206 two ends are provided with a third spacer. The limit washer is used to limit the axial displacement of the crank gear 205 .
在本发明的一个实施例中,优选地,如图2至图4所示,扑动机构3包括:连杆301、联动杆302、左翼根部3031、右翼根部3032、左旋转滑道3041、右旋转滑道3042、左翼支架3051、右翼支架3052;连杆301上下两端均设置有开孔,曲柄梁207穿过连杆301下端开孔和曲柄齿轮205的副孔,将连杆301和曲柄齿轮205连接,曲柄梁207与曲柄齿轮205固定连接,连杆301与曲柄梁207旋转连接,连杆301下端开孔轴向两端外侧设置有第四限位垫片,左旋转滑道3041和右旋转滑道3042均与机架1旋转连接,且内部均设置有滑槽,左翼根部3031的一端和右翼根部3032的一端均设置有通孔,联动杆302穿过连杆301上端开孔、左翼根部3031的通孔、右翼根部3032的通孔以及机架1的纵向滑槽与自主扭转机构4连接,联动杆302可在机架1的纵向滑槽内上下滑动,左翼根部3031的另一端和右翼根部3032的另一端分别穿过左旋转滑道3041内部滑槽和右旋转滑道3042内部滑槽,且分别与左翼支架3051的一端和右翼支架3052的一端同中心轴连接,联动杆302带动左翼根部3031和右翼根部3032分别在左旋转滑道3041和右旋转滑道3042内滑动,使左翼支架3051和右翼支架3052分别在左翼根部3031和右翼根部3032的带动下上下运动,连杆301下端开孔轴向两端外侧设置有第四限位垫片,用于限制所述连杆301在机身前后方向上的位移。In one embodiment of the present invention, preferably, as shown in FIGS. Swivel slideway 3042, left wing support 3051, right wing support 3052; Connecting rod 301 upper and lower ends are all provided with openings, and crank beam 207 passes through connecting rod 301 lower end opening and the secondary hole of crank gear 205, connects connecting rod 301 and crank The gear 205 is connected, the crank beam 207 is fixedly connected with the crank gear 205, the connecting rod 301 is rotationally connected with the crank beam 207, the opening at the lower end of the connecting rod 301 is provided with a fourth spacer outside the axial ends of the two ends, and the left rotation slideway 3041 and The right rotation slideways 3042 are all connected with the frame 1 in rotation, and are provided with chute inside, one end of the left wing root 3031 and one end of the right wing root 3032 are all provided with through holes, and the linkage rod 302 passes through the opening at the upper end of the connecting rod 301, The through hole of the left wing root 3031, the through hole of the right wing root 3032 and the longitudinal chute of the frame 1 are connected with the independent torsion mechanism 4, the linkage rod 302 can slide up and down in the longitudinal chute of the frame 1, and the other end of the left wing root 3031 and the other end of the right wing root 3032 pass through the inner chute of the left rotation slideway 3041 and the inner chute of the right rotation slideway 3042 respectively, and are respectively connected with one end of the left wing bracket 3051 and one end of the right wing bracket 3052 with the central axis, and the linkage rod 302 Drive the left wing root 3031 and the right wing root 3032 to slide in the left rotation slideway 3041 and the right rotation slideway 3042 respectively, so that the left wing support 3051 and the right wing support 3052 move up and down under the drive of the left wing root 3031 and the right wing root 3032 respectively, and the connecting rod 301 A fourth spacer is provided outside the two axial ends of the opening at the lower end to limit the displacement of the connecting rod 301 in the front-rear direction of the fuselage.
在该实施例中,联动杆302穿过连杆301上端开孔、左翼根部3031一端设置的通孔、右翼根部3032一端设置的通孔、以及机架1的纵向滑槽与自主扭转机构4连接,当连杆301随着曲柄梁207的转动而运动时,连杆301拉动联动杆302在纵向滑槽内上下滑动,带动左翼根部3031和右翼根部3032运动,左翼根部3031和右翼根部3032在运动的过程中,分别在左旋转滑道3041、右旋转滑道3042内滑动,并带动左旋转滑道3041和右旋转滑道3042转动,左翼支架3051和右翼支架3052也随着左翼根部3031和右翼根部3032的运动而同步运动,从而带动机翼5的扑动。In this embodiment, the linkage rod 302 passes through the opening at the upper end of the connecting rod 301, the through hole provided at one end of the left wing root 3031, the through hole provided at one end of the right wing root 3032, and the longitudinal chute of the frame 1 to connect with the autonomous torsion mechanism 4 , when the connecting rod 301 moves with the rotation of the crank beam 207, the connecting rod 301 pulls the linkage rod 302 to slide up and down in the longitudinal chute, driving the left wing root 3031 and the right wing root 3032 to move, and the left wing root 3031 and the right wing root 3032 are moving During the process, they slide in the left-handed slideway 3041 and the right-handed slideway 3042 respectively, and drive the left-handed slideway 3041 and the right-handed slideway 3042 to rotate. The movement of the root 3032 moves synchronously, thereby driving the flapping of the wing 5 .
在本发明的一个实施例中,优选地,如图2至图4所示,自主扭转机构4包括:滑动块401、传动连杆402、第一滑道403、第二滑道405和尾杆404,滑动块401位于所述机架1两侧壁之间,滑动块401的一端被联动杆302穿过并与其相连,在联动杆302的带动下可在机架1两侧壁之间上下滑动,滑动块401的另一端与传动连杆402的一端相连,第一滑道403和第二滑道405与机架1两侧壁均连接,并与机架1两侧壁间均存有间隙,第一滑道403和第二滑道405的两端均设置有开口,且内部均设置有滑槽,传动连杆402的另一端通过第一滑道403开口,穿过第一滑道403的滑槽与所述尾杆404一端相连,传动连杆402在滑动块401的带动下前后摆动且在第一滑道403滑槽内滑动,第一滑道403随传动连杆402前后摆动,尾杆404另一端通过第二滑道405的开口,穿过第二滑道405的滑槽与尾翼6相连,尾杆404在传动连杆402的带动下前后摆动且在第二滑道405的滑槽内滑动,第二滑道405随尾杆404前后摆动。In one embodiment of the present invention, preferably, as shown in Figures 2 to 4, the autonomous twisting mechanism 4 includes: a sliding block 401, a transmission link 402, a first slide 403, a second slide 405 and a tail rod 404, the sliding block 401 is located between the two side walls of the frame 1, and one end of the sliding block 401 is passed through by the linkage rod 302 and connected with it, and can be moved up and down between the two side walls of the frame 1 under the drive of the linkage rod 302 Sliding, the other end of the sliding block 401 is connected with one end of the transmission link 402, the first slideway 403 and the second slideway 405 are connected with the two side walls of the frame 1, and there is a space between the two side walls of the frame 1 gap, both ends of the first slideway 403 and the second slideway 405 are provided with openings, and are provided with slide grooves inside, the other end of the transmission link 402 passes through the opening of the first slideway 403 and passes through the first slideway The chute of 403 is connected with one end of the tail rod 404, the transmission link 402 swings back and forth under the drive of the sliding block 401 and slides in the chute of the first slideway 403, and the first slideway 403 swings back and forth with the transmission link 402 , the other end of the tail rod 404 passes through the opening of the second slideway 405, and passes through the chute of the second slideway 405 to be connected with the empennage 6. sliding in the chute, the second slideway 405 swings back and forth with the tail rod 404.
在该实施例中,联动杆302穿过机架1的纵向滑槽与滑动块401相连,联动杆302在纵向滑槽内的上下运动带动滑动块401在机架1两侧壁之间上下滑动,同时带动传动连杆402与其相连的一端上下运动,由于传动连杆402穿过第一滑道403内部滑槽,因此传动连杆402在第一滑道403的滑槽内滑动的同时,并带动第一滑道403前后摆动,由于传动连杆402在第一滑道403内部滑动,传动连杆402与尾杆404相连的另一端在向上、向下运动的运动轨迹呈“C”型,尾杆404在传动连杆402的带动下,尾杆404与传动连杆402相连的一端会随着传动连杆402向上、向下运动,传动连杆402的运动拉动尾杆404运动,由于尾杆404穿过第二滑道405内部滑槽,所以尾杆404在第二滑道405的滑槽内滑动的同时,并带动第二滑道405前后摆动,尾杆404远离第二滑道405的一端会随着尾杆404向上、向下运动,运动轨迹呈“C”型。传动连杆402在滑动块401的带动下前后摆动,当滑动块401向下运动时,传动连杆402与滑动块401连接的一端向下运动,传动连杆402穿过第一滑道403与尾杆404连接的另一端则向上运动,尾杆404在传动连杆402的带动下,尾杆404与传动连杆402连接的一端向上运动,尾杆404穿过第二滑道405与尾翼6连接的另一端则向下运动,当滑动块401向上运动时,传动连杆402与滑动块401连接的一端向上运动,传动连杆402穿过第一滑道403与尾杆404连接的另一端则向下运动,尾杆404在传动连杆402的带动下,尾杆404与传动连杆402连接的一端向下运动,尾杆404穿过第二滑道405与尾翼6连接的另一端则向上运动。In this embodiment, the linkage rod 302 passes through the longitudinal chute of the frame 1 and is connected to the sliding block 401, and the up and down movement of the linkage rod 302 in the longitudinal chute drives the sliding block 401 to slide up and down between the two side walls of the frame 1 At the same time, it drives the end of the transmission link 402 to move up and down. Since the transmission link 402 passes through the inner chute of the first slideway 403, the transmission link 402 slides in the chute of the first slideway 403, and Drive the first slideway 403 to swing back and forth, because the transmission link 402 slides inside the first slideway 403, the other end of the transmission link 402 connected to the tail rod 404 moves upwards and downwards in a "C" shape, Tail rod 404 is driven by transmission connecting rod 402, and the end that tail rod 404 is connected with transmission connecting rod 402 can move upwards and downwards with transmission connecting rod 402, and the movement of transmission connecting rod 402 pulls tail rod 404 to move, because tail The rod 404 passes through the inner chute of the second slideway 405, so when the tail rod 404 slides in the chute of the second slideway 405, it drives the second slideway 405 to swing back and forth, and the tail rod 404 is far away from the second slideway 405 One end of the tail rod 404 moves upwards and downwards, and the movement track is "C" shaped. The transmission connecting rod 402 swings back and forth under the drive of the sliding block 401. When the sliding block 401 moves downward, the end of the transmission connecting rod 402 connected with the sliding block 401 moves downward, and the transmission connecting rod 402 passes through the first slideway 403 and The other end that tail rod 404 is connected then moves upwards, and tail rod 404 is driven by transmission connecting rod 402, and one end that tail rod 404 is connected with transmission connecting rod 402 moves upwards, and tail rod 404 passes through second slideway 405 and empennage 6 The other end of the connection then moves downwards. When the sliding block 401 moves upwards, the end of the transmission connecting rod 402 connected to the sliding block 401 moves upwards, and the transmission connecting rod 402 passes through the other end connected to the first slideway 403 and the tail rod 404. Then move downwards, tail rod 404 is under the drive of transmission connecting rod 402, and an end that tail rod 404 is connected with transmission connecting rod 402 moves downward, and tail rod 404 passes the other end that the second slideway 405 is connected with empennage 6 then upward movement.
在本发明的一个实施例中,优选地,自主扭转机构4还包括:第一销钉4011、第二销钉4021、第三销钉4031和第四销钉4051;滑动块401与传动连杆402通过第一销钉4011连接,传动连杆402与尾杆404通过第二销钉4021连接,第一滑道403与机架1通过第三销钉4031连接,第二滑道405与机架1通过第四销钉4051连接。In one embodiment of the present invention, preferably, the autonomous twisting mechanism 4 further includes: a first pin 4011, a second pin 4021, a third pin 4031 and a fourth pin 4051; the sliding block 401 and the transmission link 402 pass through the first The pin 4011 is connected, the transmission link 402 is connected with the tail rod 404 through the second pin 4021, the first slideway 403 is connected with the frame 1 through the third pin 4031, and the second slideway 405 is connected with the frame 1 through the fourth pin 4051 .
在本发明的一个实施例中,优选地,如图2至图6所示,滑动块401为一端设置有开口矩形槽的方体结构,开口矩形槽的两侧壁上设置有相对称的第一对孔,传动连杆402两侧壁靠近滑动块401一端设置有相对称的第二对孔,传动连杆402两侧壁远离滑动块401的一端设置有相对称的第三对孔,传动连杆402近滑动块401一端插入开口矩形槽,第一销钉4011穿过第一对孔和第二对孔将滑动块401和传动连杆402旋转连接,尾杆404的一端设置有通孔,第二销钉4021穿过第三对孔和通孔将传动连杆402和尾杆404旋转连接;第一滑道403左侧壁和右侧壁设置有相对称的孔,第二滑道405左侧壁和右侧壁设置有相对称的孔,第三销钉4031包括第三左销钉和第三右销钉,第四销钉4051包括第四左销钉和第四右销钉,第三左销钉一端与机架1左侧壁固定连接,另一端插入位于第一滑道403左侧壁上的孔中,且不接触传动连杆402,第三右销钉一端与机架1右侧壁固定连接,另一端插入位于第一滑道403右侧壁上的孔中,且不接触传动连杆402,第四左销钉一端与机架1左侧壁固定连接,另一端插入位于第二滑道405左侧壁上的孔中,且不接触尾杆404,第四右销钉一端与机架1右侧壁固定连接,另一端插入位于第二滑道405右侧壁上的孔中,且不接触尾杆404。In one embodiment of the present invention, preferably, as shown in FIG. 2 to FIG. 6 , the sliding block 401 is a square structure with an open rectangular slot at one end, and symmetrical first A pair of holes, the two side walls of the transmission connecting rod 402 close to the end of the sliding block 401 are provided with a second pair of symmetrical holes, and the end of the two side walls of the transmission connecting rod 402 away from the sliding block 401 is provided with a third pair of symmetrical holes. One end of the connecting rod 402 close to the sliding block 401 is inserted into the open rectangular slot, the first pin 4011 passes through the first pair of holes and the second pair of holes to rotate the sliding block 401 and the transmission connecting rod 402, and one end of the tail rod 404 is provided with a through hole. The second pin 4021 passes through the third pair of holes and the through hole to rotate the transmission link 402 and the tail rod 404; The side wall and the right side wall are provided with symmetrical holes, the third pin 4031 includes the third left pin and the third right pin, the fourth pin 4051 includes the fourth left pin and the fourth right pin, one end of the third left pin is connected to the machine The left side wall of frame 1 is fixedly connected, the other end is inserted into the hole on the left side wall of the first slideway 403, and does not contact the transmission link 402, one end of the third right pin is fixedly connected with the right side wall of frame 1, and the other end Insert it into the hole on the right side wall of the first slideway 403 without contacting the transmission link 402. One end of the fourth left pin is fixedly connected to the left sidewall of the frame 1, and the other end is inserted into the left sidewall of the second slideway 405. In the hole on the top, and do not touch the tail rod 404, one end of the fourth right pin is fixedly connected with the right side wall of the frame 1, and the other end is inserted into the hole on the right side wall of the second slideway 405, and does not contact the tail rod 404 .
在该实施例中,机架1、滑动块401、传动连杆402、第一滑道403以及第二滑道405之间的连接关系均通过销钉和孔配合,第三左销钉一端与机架1左侧壁固定连接,另一端插入位于第一滑道403左侧壁上的孔中,且不接触传动连杆402,第三右销钉一端与机架1右侧壁固定连接,另一端插入位于第一滑道403右侧壁上的孔中,且不接触传动连杆402,使第一滑道403与机架1侧壁连接,且不影响传动连杆402的运动,而第四左销钉一端与机架1左侧壁固定连接,另一端插入位于第二滑道405左侧壁上的孔中,且不接触尾杆404,第四右销钉一端与机架1右侧壁固定连接,另一端插入位于第二滑道405右侧壁上的孔中,且不接触尾杆404,则是将第二滑道405与机架1侧壁连接,且不影响尾杆404的运动。In this embodiment, the connection relationship between the frame 1, the sliding block 401, the transmission link 402, the first slideway 403, and the second slideway 405 is matched by a pin and a hole, and one end of the third left pin is connected to the frame. 1. The left side wall is fixedly connected, and the other end is inserted into the hole on the left side wall of the first slideway 403, and does not touch the transmission link 402. One end of the third right pin is fixedly connected with the right side wall of the frame 1, and the other end is inserted into Located in the hole on the right side wall of the first slideway 403, and does not contact the transmission link 402, the first slideway 403 is connected to the side wall of the frame 1 without affecting the movement of the transmission link 402, while the fourth left One end of the pin is fixedly connected to the left side wall of the frame 1, and the other end is inserted into the hole on the left side wall of the second slideway 405 without touching the tail rod 404, and one end of the fourth right pin is fixedly connected to the right side wall of the frame 1 , and the other end is inserted into the hole on the right side wall of the second slideway 405 without touching the tail rod 404, so that the second slideway 405 is connected to the side wall of the frame 1 without affecting the movement of the tail rod 404.
在本发明的一个实施例中,优选地,如图1至6所示,机翼5包括左机翼501和右机翼502,左机翼501前端与左翼支架3051相连接,右机翼502前端与右翼支架3052相连接,左机翼501后端和右机翼502后端均与尾杆404连接。In one embodiment of the present invention, preferably, as shown in FIGS. The front end is connected with the right wing bracket 3052 , and the rear ends of the left wing 501 and the right wing 502 are connected with the tail boom 404 .
在该实施例中,左机翼501前端和右机翼502前端分别与左翼支架3051和右翼支架3052相连接,左机翼501后端和右机翼502后端均与尾杆404连接,当联动杆302往上滑动时,左机翼501和右机翼502前端受到左翼支架3051和右翼支架3052的拉动向下降低,而左机翼501和右机翼502后端受到尾杆404的拉动向上抬升,从而使机翼5在下扑过程中产生前部向下方、后部向上方的扭转,进而赋予机翼5翼面前低后高的运动姿态。当联动杆302往下滑动时,左机翼501和右机翼502前端受到左翼支架3051和右翼支架3052的拉动向上抬升,而左机翼501和右机翼502后端受到尾杆404的拉动向下降低,从而使机翼5在上扑过程中产生前部向上方、后部向下方的扭转,进而赋予机翼5翼面前高后低的运动姿态。In this embodiment, the front end of the left wing 501 and the front end of the right wing 502 are respectively connected with the left wing bracket 3051 and the right wing bracket 3052, and the rear end of the left wing 501 and the rear end of the right wing 502 are connected with the tail boom 404. When the linkage lever 302 slides upwards, the front ends of the left wing 501 and the right wing 502 are pulled downward by the left wing bracket 3051 and the right wing bracket 3052, and the rear ends of the left wing 501 and the right wing 502 are pulled by the tail rod 404 Lifting up, so that the front part of the wing 5 is twisted downwards and the rear part is upwards during the downward flapping process, thereby giving the wing 5 a motion posture with the front low and the rear high. When the linkage lever 302 slides down, the front ends of the left wing 501 and the right wing 502 are pulled upward by the left wing bracket 3051 and the right wing bracket 3052, and the rear ends of the left wing 501 and the right wing 502 are pulled by the tail rod 404 Lowering downwards, so that the wing 5 produces the twist of the front part upwards and the rear part downwards during the upward pounce, and then gives the wing 5 a motion posture with a high front and a low rear.
在本发明的一个实施例中,优选地,如图1和图2所示,尾翼6上设置有开孔,尾杆404一端插入尾翼6开孔与其连接,尾翼6上方一面与尾杆404上切面保持平行。In one embodiment of the present invention, preferably, as shown in Figure 1 and Figure 2, an opening is provided on the empennage 6, and one end of the tail rod 404 is inserted into the opening of the empennage 6 to connect with it, and the upper side of the empennage 6 is connected to the tail rod 404. The cut planes remain parallel.
在该实施例中,尾杆404一端插入尾翼6开孔,尾杆404带动尾翼6上下转动。In this embodiment, one end of the tail rod 404 is inserted into the opening of the tail 6 , and the tail rod 404 drives the tail 6 to rotate up and down.
在本发明的一个实施例中,优选地,机架1采用碳纤维薄板材料,连杆301、左翼支架、右翼支架均采用碳纤维材料,机翼5采用天然橡胶薄膜材料,尾翼6采用塑料泡沫材料。In one embodiment of the present invention, preferably, the frame 1 is made of carbon fiber sheet material, the connecting rod 301, the left wing bracket, and the right wing bracket are all made of carbon fiber material, the wing 5 is made of natural rubber film material, and the empennage 6 is made of plastic foam material.
在该实施例中,各部件的材料的使用为具体实施例,实际操作中并不仅限于此。In this embodiment, the material used for each component is a specific embodiment, and is not limited thereto in actual operation.
本发明工作时,驱动机构2带动扑动机构3运动,同时带动自主扭转机构4运动,联动杆302随着曲柄齿轮205的转动而在机架1中部的滑道内上下滑动,带动左翼根部3031、右翼根部3032在左旋转滑道3041、右旋转滑道3042内滑动,联动杆302同时带动滑动块401上下滑动,当联动杆302往下滑动时,左翼根部3031、右翼根部3032外端抬升、里端降低,从而带动左翼支架3051、右翼支架3052抬升,使得机翼5左右两端逐渐运动得高过中间,从而带动机翼5前部向上扑动,同时,联动杆302带动滑动块401下降,从而带动传动连杆402前低后高,而抬高的传动连杆402后端又带动尾杆404前高后低,机翼5后部与尾杆404后端相连,尾杆404后端带动翼面后部降低,机翼5呈现前高后低的运动姿态,尾杆404末端与尾翼6相连,带动尾翼6后部向下方转动,当联动杆302往上滑动时,左翼根部3031、右翼根部3032外端降低、里端抬升,从而带动左翼支架3051、右翼支架3052降低,使得机翼5左右两端逐渐运动得低于中间,从而带动机翼5前部向下扑动,同时,联动杆302带动滑动块401上升,从而带动传动连杆402前高后低,而降低的传动连杆402后端又带动尾杆404前低后高,机翼5后部与尾杆404后端相连,尾杆404后端带动机翼5后部抬升,机翼5呈现前低后高的运动姿态,尾杆404末端与尾翼6相连,带动尾翼6后部向上方转动。When the present invention works, the drive mechanism 2 drives the flutter mechanism 3 to move, and simultaneously drives the independent torsion mechanism 4 to move, and the linkage rod 302 slides up and down in the slideway in the middle of the frame 1 along with the rotation of the crank gear 205, driving the left wing root 3031, The right wing root 3032 slides in the left rotation slideway 3041 and the right rotation slideway 3042, and the linkage rod 302 drives the sliding block 401 to slide up and down at the same time. The end is lowered, thereby driving the left wing support 3051 and the right wing support 3052 to lift, so that the left and right ends of the wing 5 gradually move higher than the middle, thereby driving the front part of the wing 5 to flutter upwards. At the same time, the linkage rod 302 drives the sliding block 401 to descend. Thereby driving the transmission link 402 to be low at the front and high at the rear, and the raised transmission link 402 rear end drives the tail rod 404 to be high at the front and low at the rear. The rear portion of the wing surface is lowered, and the wing 5 presents a motion posture of high front and low rear. The end of the tail rod 404 is connected with the empennage 6, which drives the rear portion of the empennage 6 to rotate downward. The outer end of the root 3032 is lowered and the inner end is raised, thereby driving the left wing bracket 3051 and the right wing bracket 3052 to lower, so that the left and right ends of the wing 5 gradually move lower than the middle, thereby driving the front of the wing 5 to flutter downward. At the same time, the linkage The rod 302 drives the sliding block 401 to rise, thereby driving the transmission connecting rod 402 to be high at the front and low at the rear, and the rear end of the lowered transmission connecting rod 402 drives the tail rod 404 to be low at the front and high at the rear, and the rear part of the wing 5 is connected to the rear end of the tail rod 404 , the tail rod 404 rear end drives the rear portion of the wing 5 to lift, and the wing 5 presents a motion posture of low front and high rear, and the end of the tail rod 404 is connected with the empennage 6 to drive the rear portion of the empennage 6 to rotate upwards.
当联动杆302下滑拉动机翼5前部上扑时,由于机翼5后部被尾杆404往下拉,机翼5总体呈现向下的扭转姿态,尾翼6往下方转动;同理,当联动杆302上滑拉动机翼5前部下扑时,机翼5后部被尾杆404往上抬,机翼5呈现向上的扭转姿态,尾翼6往上方转动。When the linkage rod 302 slides down and pulls the front part of the wing 5 to jump up, because the rear part of the wing 5 is pulled down by the tail rod 404, the wing 5 generally presents a downward twisting posture, and the tail 6 rotates downward; When the bar 302 slides up and pulls the front part of the wing 5 to flutter down, the rear part of the wing 5 is lifted up by the tail rod 404, the wing 5 presents an upward twisting posture, and the empennage 6 turns upwards.
本发明的仿鸟类飞行扑翼机器人将一个曲柄滑块机构和滑动式杠杆组结合,曲柄滑块机构用于产生仿鸟类扑翼机器人机翼5的上下扑动动作,滑动式杠杆组用于产生仿鸟类扑翼飞行机器人机翼5的前后扭转动作,使得该仿鸟类飞行扑翼机器人在下扑过程中机翼5产生前低后高的姿态,在上扑过程中机翼5产生前高后低的姿态。The bird-like flying flapping wing robot of the present invention combines a crank slider mechanism and a sliding type lever group, and the crank slider mechanism is used to generate the up and down flapping action of the wing 5 of the bird-like flapping wing robot, and the sliding type lever group is used In order to produce the forward and backward twisting action of the bird-like flapping wing flying robot wing 5, the wing 5 of the bird-like flying flapping wing robot produces a low-front and rear-high posture during the downward flapping process, and the wing 5 produces a low-back posture during the upward flapping process. High front and low back posture.
本发明的仿鸟类飞行扑翼机器人在工作过程中机翼5上下扑动可产生向上升力,由于滑动式杠杆组的作用,使得尾杆404后端在机翼5下扑时上翘,在机翼5上扑时下翘,从而带动机翼5进行扭转;由于尾翼6与尾杆404末端相连,尾翼6会随着尾杆404末端的上下翘动而出现顺、逆时针的转动。In the bird-like flying flapping wing robot of the present invention, the wing 5 flutters up and down in the working process to generate upward lift force. Due to the effect of the sliding lever group, the rear end of the tail rod 404 is upturned when the wing 5 flutters down. When the wing 5 flutters up, it turns downwards, thereby driving the wing 5 to twist; because the tail 6 is connected to the end of the tail rod 404, the tail 6 will rotate clockwise or counterclockwise as the end of the tail rod 404 moves up and down.
本发明能实现机器人机翼5扑动过程中机翼5的俯仰角自主扭转,在下扑和上扑过程中调整飞行攻角的变化,使得扑动过程中所受的空气阻力减小,并于扑动过程中增加前进方向上的推力,可提高前飞速度,能达到节省能量消耗的效果;本发明实现了尾杆404的滑动式顺、逆时针转动,从而使尾杆404带动尾翼6进行顺、逆时针方向转动,进一步增大仿鸟类飞行扑翼机器人在前飞方向上的推力,提高了前飞速度以及机动性,同时,在尾翼6进行顺、逆时针方向转动时,带动仿鸟类飞行扑翼机器人机身出现上升、下降趋势,由于尾杆404后端中心上止点与尾杆404前端中心点的连线与水平面间的夹角,大于所述尾杆404后端中心下止点与尾杆404前端中心点的连线与水平面间的夹角,所以累加的结果就是机身会出现抬升的现象,从而仿鸟类飞行扑翼机器人在飞行过程中机身相对地面的仰角会进一步增大,即会增加向上的升力,可增大机器人的飞行高度以及缩短到达指定高度的所需时间,同时缩减了能量的消耗。The present invention can realize the autonomous twisting of the pitch angle of the wing 5 during the flapping process of the robot wing 5, and adjust the change of the flight angle of attack during the flapping and flapping processes, so that the air resistance suffered during the flapping process is reduced, and the Increase the thrust in the forward direction during the flapping process, which can increase the speed of the forward flight, and can achieve the effect of saving energy consumption; the present invention realizes the sliding clockwise and anticlockwise rotation of the tail rod 404, so that the tail rod 404 drives the empennage 6 to carry out Rotating clockwise or counterclockwise further increases the thrust of the bird-like flying flapping wing robot in the direction of forward flight, improving the speed and maneuverability of forward flight. At the same time, when the tail 6 rotates clockwise or counterclockwise, it drives There is an upward and downward trend in the fuselage of the bird flying flapping wing robot, because the angle between the line between the top dead center of the rear end center of the tail rod 404 and the center point of the front end of the tail rod 404 and the horizontal plane is greater than the center of the rear end of the tail rod 404 The angle between the line connecting the bottom dead center and the center point of the front end of the tail rod 404 and the horizontal plane, so the result of the accumulation is that the fuselage will rise, so that the flapping wing robot is like a bird flying. The elevation angle will be further increased, that is, the upward lift force will be increased, which can increase the flying height of the robot and shorten the time required to reach the specified height, while reducing energy consumption.
在本发明的描述中,术语“多个”则指两个或两个以上,除非另有明确的限定,术语“上”、“下”、“左”、“右”、等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制;术语“连接”、“安装”、“固定”等均应做广义理解,例如,“连接”可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是直接相连,也可以通过中间媒介间接相连。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明中的具体含义。In the description of the present invention, the term "plurality" refers to two or more than two, and unless otherwise clearly defined, the terms "upper", "lower", "left", "right", etc. indicate directions or The positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, Therefore, it cannot be understood as a limitation to the present invention; the terms "connection", "installation", "fixation" and the like should be understood in a broad sense, for example, "connection" can be a fixed connection, a detachable connection, or an integral connection; It can be directly connected or indirectly connected through an intermediary. Those of ordinary skill in the art can understand the specific meanings of the above terms in the present invention according to specific situations.
在本发明的描述中,术语“一个实施例”、“一些实施例”、“具体实施例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或特点包含于本发明的至少一个实施例或示例中。在本发明中,对上述术语的示意性表述不一定指的是相同的实施例或实例。而且,描述的具体特征、结构、材料或特点可以在任何的一个或多个实施例或示例中。In the description of the present invention, descriptions of the terms "one embodiment", "some embodiments", "specific embodiments" and the like mean that a specific feature, structure, material or characteristic described in connection with the embodiment or example is included in the present invention In at least one embodiment or example of . In the present invention, the schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials or characteristics described may be in any one or more embodiments or examples.
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