技术领域technical field
本发明涉及一种汽车，特别是涉及一种飞行汽车。The invention relates to a car, in particular to a flying car.
背景技术Background technique
随着科技急速的发展以及人类生活需求的增长，汽车已经成为人们日常出行的主要交通工具，上班高峰时期交通堵塞已经成为各个城市的普遍问题。飞行汽车因此诞生，可以成为一种理想的交通工具，为交通运输的轨道增加了一个维度，即地面上堵塞时，可转换为飞行模式，在方便出行的同时又缓解了交通拥堵的状况。目前已有的飞行汽车多数为折叠翼飞行汽车，其机翼外置于机体两侧，因此整个飞行汽车的几何尺寸较大且占用空间较大，行驶停靠均不如普通汽车灵活方便。With the rapid development of science and technology and the growth of human life needs, cars have become the main means of transportation for people's daily travel, and traffic jams during rush hours have become a common problem in various cities. The birth of flying cars can become an ideal means of transportation, adding a dimension to the transportation track, that is, when the ground is congested, it can be converted to flight mode, which is convenient for travel and relieves traffic congestion. At present, most of the existing flying cars are folding-wing flying cars, and their wings are placed on both sides of the body. Therefore, the entire flying car has a large geometric size and takes up a lot of space. It is not as flexible and convenient to drive and dock as ordinary cars.
发明内容Contents of the invention
本发明所要解决的技术问题是提供一种飞行汽车，其具有普通汽车特征优势并能实现飞行目的，几何尺寸较小且占用空间较小，行驶停靠如普通汽车灵活方便。The technical problem to be solved by the present invention is to provide a flying car, which has the characteristics and advantages of ordinary cars and can realize the purpose of flying.
本发明是通过下述技术方案来解决上述技术问题的：一种飞行汽车，其特征在于，其包括车体、前翼机构、伸展翼机构、下尾翼机构以及上尾翼机构，前翼机构设置在车体的前端下方，伸展翼机构设置在车体中部下方，下尾翼机构设置在车体的后端下方，上尾翼机构设置在车体后端上方；其中前翼机构包括前翼、第一交叉连杆、第一连杆、第一塞杆、第一缸筒、第一固定架、第一铰接端口和第一滑槽道，第一铰接端口和第一滑槽道都位于前翼上表面，前翼通过第一交叉连杆与第一固定架相连，第一固定架安装在车体上，第一连杆的两端与第一固定架相连，第一缸筒的一端通过第一塞杆与第一连杆的中间连接，第一缸筒的另一端与第一固定架固定；伸展翼机构包括一级伸展翼、二级伸展翼，一级伸展翼和二级伸展翼连接；下尾翼机构包括下尾翼、第二交叉连杆、第二连杆、第二塞杆、第二缸筒、第二固定架、第二铰接端口、第二滑槽道，第二铰接端口和第二滑槽道都位于下尾翼上表面，下尾翼通过第二交叉连杆与第二固定架相连，第二固定架安装在车体上，第二连杆的两端与第二固定架相连，第二缸筒的一端通过第二塞杆与第二连杆的中间连接，第二缸筒的另一端与第二固定架固定；上尾翼机构包括上尾翼、扰流板、安定架，上尾翼和扰流板都与安定架相连。The present invention solves the above-mentioned technical problems through the following technical solutions: a flying car, which is characterized in that it includes a car body, a front wing mechanism, an extended wing mechanism, a lower tail mechanism and an upper tail mechanism, and the front wing mechanism is arranged on Below the front end of the car body, the extending wing mechanism is arranged under the middle part of the car body, the lower empennage mechanism is arranged under the rear end of the car body, and the upper empennage mechanism is arranged above the rear end of the car body; wherein the front wing mechanism includes a front wing, a first cross The connecting rod, the first connecting rod, the first plug rod, the first cylinder, the first fixed frame, the first hinged port and the first slideway, the first hinged port and the first slideway are located on the upper surface of the front wing , the front wing is connected with the first fixed frame through the first cross link, the first fixed frame is installed on the vehicle body, the two ends of the first connecting rod are connected with the first fixed frame, and one end of the first cylinder is passed through the first plug The rod is connected to the middle of the first connecting rod, and the other end of the first cylinder is fixed to the first fixed frame; the extension wing mechanism includes a first-level extension wing and a second-level extension wing, and the first-level extension wing and the second-level extension wing are connected; The empennage mechanism comprises a lower empennage, a second cross link, a second connecting rod, a second plug rod, a second cylinder, a second fixed frame, a second hinged port, a second chute, a second hinged port and a second The chute paths are located on the upper surface of the lower empennage, the lower empennage is connected with the second fixed frame through the second cross link, the second fixed frame is installed on the vehicle body, the two ends of the second connecting rod are connected with the second fixed frame, the second One end of the second cylinder is connected to the middle of the second connecting rod through the second plug rod, and the other end of the second cylinder is fixed to the second fixed frame; the upper empennage mechanism includes an upper empennage, a spoiler, a stabilizer, an upper empennage and The spoilers are connected to the stabilizer.
优选地，所述车体底部内部有足够的空间放置机翼。Preferably, there is enough space inside the bottom of the vehicle body to place wings.
优选地，所述车体收起机翼时形状为子弹型。Preferably, the vehicle body is bullet-shaped when the wings are retracted.
优选地，所述伸展翼机构的形状为梯形。Preferably, the shape of the spreading wing mechanism is trapezoidal.
优选地，所述车体表面呈流线型。Preferably, the surface of the vehicle body is streamlined.
优选地，所述前翼机构、伸展翼机构以及下尾翼机构用于提供升力；上尾翼机构用于控制飞行汽车的姿态。Preferably, the front wing mechanism, the extended wing mechanism and the lower tail mechanism are used to provide lift; the upper tail mechanism is used to control the attitude of the flying car.
优选地，所述前翼机构在地面行驶时收缩在车体内部，在飞行时从车体下方伸出。Preferably, the front wing mechanism is retracted inside the vehicle body when driving on the ground, and protrudes from under the vehicle body when flying.
优选地，所述伸展翼机构在地面行驶时两级嵌套收缩在车体内部，在飞行时从车体两侧伸出。Preferably, the expandable wing mechanism is nested and shrunk inside the vehicle body in two stages when driving on the ground, and protrudes from both sides of the vehicle body when flying.
优选地，所述下尾翼机构在地面行驶时收缩在车体内部，在飞行时从车体下方伸出。Preferably, the lower empennage mechanism is retracted inside the vehicle body when driving on the ground, and protrudes from below the vehicle body when flying.
优选地，所述上尾翼机构在地面行驶时扰流板向上翘起以提供负升力，启动飞行时扰流板向下转动以提供升力。Preferably, when the upper empennage mechanism is running on the ground, the spoiler tilts up to provide negative lift, and when the flight is started, the spoiler turns downward to provide lift.
本发明的积极进步效果在于：本发明既能在地面上行驶，也能在空中飞行。本发明的各部分机翼可以完全隐藏于车体之中，这使得本发明在地面行驶时完全具有普通汽车的特点以及行驶方式，体积大小与普通汽车占据空间大小相当，且行驶、停靠灵活方便、操作方式与普通汽车相同。本发明的各部分机翼完全伸展打开后，依靠翼型表面产生的升力可以实现小型飞机的基本功能从而实现飞行目的。由于本发明的子弹型车体设计与可伸缩翼设计的结合，使得本发明可以在较小空间体积下可以完成地面行驶和空中飞行任务。本发明可以缓解严重负荷交通问题，且将车辆驾驶与飞行驾驶相结合，将飞行驾驶变得简易化、大众化、普及化。The positive progressive effect of the present invention is that: the present invention can not only travel on the ground, but also fly in the air. Each part of the wing of the present invention can be completely hidden in the car body, which makes the present invention fully have the characteristics and driving mode of an ordinary car when driving on the ground, the volume is equivalent to the space occupied by an ordinary car, and the driving and parking are flexible and convenient , The operation method is the same as that of ordinary cars. After each part of the wing of the invention is fully stretched and opened, the basic functions of the small aircraft can be realized by relying on the lift generated by the surface of the airfoil so as to realize the purpose of flight. Due to the combination of the bullet-shaped vehicle body design and the retractable wing design of the present invention, the present invention can complete ground driving and air flight tasks in a small space volume. The invention can alleviate the serious load traffic problem, and combines vehicle driving and flight driving to simplify, popularize and popularize flight driving.
附图说明Description of drawings
图1为本发明地面行驶时的结构示意图。Fig. 1 is a schematic diagram of the structure of the present invention when driving on the ground.
图2为本发明空中飞行时的结构示意图。Fig. 2 is a schematic diagram of the structure of the present invention when flying in the air.
图3为本发明空中飞行时的侧视图。Fig. 3 is a side view of the present invention when flying in the air.
图4为本发明前翼机构结构示意图。Fig. 4 is a structural schematic diagram of the front wing mechanism of the present invention.
图5为本发明下尾翼机构结构示意图。Fig. 5 is a structural schematic diagram of the lower empennage mechanism of the present invention.
图6为本发明空中飞行时的俯视图。Fig. 6 is a top view of the present invention when flying in the air.
图7为本发明中飞行时的前视图。Fig. 7 is a front view during flight of the present invention.
具体实施方式detailed description
下面结合附图给出本发明较佳实施例，以详细说明本发明的技术方案。The preferred embodiments of the present invention are given below in conjunction with the accompanying drawings to describe the technical solution of the present invention in detail.
如图1至图7所示，本发明飞行汽车包括车体1、前翼机构2、伸展翼机构3、下尾翼机构4以及上尾翼机构5，前翼机构2设置在车体1的前端下方，伸展翼机构3设置在车体1中部下方，下尾翼机构4设置在车体1的后端下方，上尾翼机构5设置在车体1后端上方；其中前翼机构2包括前翼21、第一交叉连杆22、第一连杆23、第一塞杆24、第一缸筒25、第一固定架26、第一铰接端口21a和第一滑槽道21b，第一铰接端口21a和第一滑槽道21b都位于前翼21上表面，前翼21通过第一交叉连杆22与第一固定架26相连，第一固定架26安装在车体1上，第一连杆23的两端与第一固定架26相连，第一缸筒25的一端通过第一塞杆24与第一连杆23的中间连接，第一缸筒25的另一端与第一固定架26固定；伸展翼机构3包括一级伸展翼31、二级伸展翼32，一级伸展翼31和二级伸展翼32连接；下尾翼机构4包括下尾翼41、第二交叉连杆42、第二连杆43、第二塞杆44、第二缸筒45、第二固定架46、第二铰接端口41a、第二滑槽道41b，第二铰接端口41a和第二滑槽道41b都位于下尾翼41上表面，下尾翼41通过第二交叉连杆42与第二固定架46相连，第二固定架46安装在车体1上，第二连杆43的两端与第二固定架46相连，第二缸筒45的一端通过第二塞杆44与第二连杆43的中间连接，第二缸筒45的另一端与第二固定架46固定；上尾翼机构5包括上尾翼51、扰流板52、安定架53，上尾翼51和扰流板52都与安定架53相连。As shown in Figures 1 to 7, the flying car of the present invention includes a car body 1, a front wing mechanism 2, an extended wing mechanism 3, a lower tail mechanism 4 and an upper tail mechanism 5, and the front wing mechanism 2 is arranged below the front end of the car body 1 , the stretching wing mechanism 3 is arranged below the middle part of the car body 1, the lower empennage mechanism 4 is arranged under the rear end of the car body 1, and the upper empennage mechanism 5 is arranged above the rear end of the car body 1; wherein the front wing mechanism 2 includes a front wing 21, The first cross link 22, the first connecting rod 23, the first plug rod 24, the first cylinder 25, the first fixed frame 26, the first hinged port 21a and the first slideway 21b, the first hinged port 21a and The first chute way 21b is all located on the upper surface of the front wing 21, the front wing 21 is connected with the first fixed mount 26 through the first cross link 22, the first fixed mount 26 is installed on the vehicle body 1, the first connecting rod 23 Two ends are connected with the first fixed mount 26, and one end of the first cylinder 25 is connected with the middle of the first plug rod 24 and the first connecting rod 23, and the other end of the first cylinder 25 is fixed with the first fixed mount 26; Wing mechanism 3 comprises one-level extension wing 31, two-stage expansion wing 32, and one-level expansion wing 31 and second-level expansion wing 32 are connected; Lower empennage mechanism 4 comprises lower empennage 41, second cross link 42, second link 43 , the second plug rod 44, the second cylinder barrel 45, the second fixed frame 46, the second hinged port 41a, the second chute 41b, the second articulated port 41a and the second chute 41b are all located on the lower empennage 41 On the surface, the lower empennage 41 is connected with the second fixed frame 46 through the second cross link 42, the second fixed frame 46 is installed on the vehicle body 1, the two ends of the second connecting rod 43 are connected with the second fixed frame 46, the second One end of the cylinder barrel 45 is connected in the middle of the second plug rod 44 and the second connecting rod 43, and the other end of the second cylinder barrel 45 is fixed with the second fixed frame 46; the upper empennage mechanism 5 includes an upper empennage 51, a spoiler 52 , stabilizer 53, upper empennage 51 and spoiler 52 are all linked to each other with stabilizer 53.
车体底部内部有足够的空间可以放置机翼，这样节约空间。There is enough space inside the bottom of the car body to place the wings, which saves space.
车体收起机翼时的形状为子弹型，这样节约空间。The shape of the body when the wings are folded is bullet-shaped, which saves space.
伸展翼机构的形状为梯形，这样结构更加稳定。The shape of the spreading wing mechanism is trapezoidal, so the structure is more stable.
本飞行汽车的工作原理如下：车体表面呈流线型，用于减小空气阻力；前翼机构、伸展翼机构以及下尾翼机构用于提供升力；上尾翼机构用于控制飞行汽车的姿态。其中前翼机构、伸展翼机构、下尾翼机构和上尾翼机构分别设置在车体的前端下方、车体中部下方、后端下方和后端安定架上。前翼机构在地面行驶时收缩在车体内部，在飞行时从车体下方伸出。所述伸展翼机构在地面行驶时两级嵌套收缩在车体内部，在飞行时从车体两侧伸出。所述下尾翼机构在地面行驶时收缩在车体内部，在飞行时从车体下方伸出。所述上尾翼机构在地面行驶时扰流板向上翘起以提供负升力，启动飞行时扰流板向下转动以提供升力。在飞行时扰流板可根据需求调整转动角度。一级伸展翼通过丝杠机构驱动从车体内部移动至车体外侧，二级伸展翼通过伺服机构驱动从一级伸展翼内部移动伸展。第一连杆、第一塞杆和第一缸筒用于调节前翼与第一固定架之间的距离。扰流板可进行一定角度的转动。上尾翼机构在地面行驶时扰流板向上翘起，以提供负升力，启动飞行时扰流板向下转动，以提供升力，在飞行时扰流板可根据需求调整转动角度。The working principle of the flying car is as follows: the surface of the car body is streamlined to reduce air resistance; the front wing mechanism, the extended wing mechanism and the lower tail mechanism are used to provide lift; the upper tail mechanism is used to control the attitude of the flying car. Wherein the front wing mechanism, the stretching wing mechanism, the lower empennage mechanism and the upper empennage mechanism are respectively arranged under the front end, the middle part of the car body, the rear end and the rear stabilizer. The front wing mechanism is retracted inside the hull when driving on the ground, and protrudes from under the hull when flying. The two-stage nesting shrinks inside the car body when running on the ground, and protrudes from both sides of the car body when flying. The lower empennage mechanism shrinks inside the car body when driving on the ground, and protrudes from the bottom of the car body when flying. When the upper empennage mechanism is running on the ground, the spoiler is tilted up to provide negative lift, and when the flight is started, the spoiler turns downward to provide lift. When flying, the spoiler can adjust the rotation angle according to the demand. The first-stage stretching wing is driven from the inside of the car body to the outside of the car body by a screw mechanism, and the second-stage stretching wing is driven by a servo mechanism to move and extend from the inside of the first-stage stretching wing. The first connecting rod, the first plug rod and the first cylinder are used to adjust the distance between the front wing and the first fixed frame. The spoiler can be rotated at a certain angle. When the upper empennage mechanism is driving on the ground, the spoiler tilts up to provide negative lift. When the flight is started, the spoiler turns downward to provide lift. During flight, the spoiler can adjust the rotation angle according to the demand.
综上所述，本发明可以同时实现地面行驶和空中飞行，地面行驶时与普通汽车占据空间大小相当，且行驶停靠灵活方便。飞行时能实现普通小型飞机的飞行目的。To sum up, the present invention can realize ground driving and air flight at the same time. When driving on the ground, it occupies the same space as an ordinary car, and the driving and parking are flexible and convenient. The flight purpose of common small aircraft can be realized during flight.
以上所述的具体实施例，对本发明的解决的技术问题、技术方案和有益效果进行了进一步详细说明，所应理解的是，以上所述仅为本发明的具体实施例而已，并不用于限制本发明，凡在本发明的精神和原则之内，所做的任何修改、等同替换、改进等，均应包含在本发明的保护范围之内。The specific embodiments described above have further described the technical problems, technical solutions and beneficial effects of the present invention in detail. It should be understood that the above descriptions are only specific embodiments of the present invention and are not intended to limit In the present invention, any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included within the protection scope of the present invention.
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610433670.1ACN105946484B (en) | 2016-06-18 | 2016-06-18 | flying car |
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610433670.1ACN105946484B (en) | 2016-06-18 | 2016-06-18 | flying car |
| Publication Number | Publication Date |
|---|---|
| CN105946484Atrue CN105946484A (en) | 2016-09-21 |
| CN105946484B CN105946484B (en) | 2018-05-01 |
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610433670.1AExpired - Fee RelatedCN105946484B (en) | 2016-06-18 | 2016-06-18 | flying car |
| Country | Link |
|---|---|
| CN (1) | CN105946484B (en) |
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| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| CF01 | Termination of patent right due to non-payment of annual fee | Granted publication date:20180501 Termination date:20210618 | |
| CF01 | Termination of patent right due to non-payment of annual fee |