[go: up one dir, main page]

CN115091905B - An electric flying car - Google Patents

An electric flying car Download PDF

Info

Publication number
CN115091905B
CN115091905B CN202210864688.2A CN202210864688A CN115091905B CN 115091905 B CN115091905 B CN 115091905B CN 202210864688 A CN202210864688 A CN 202210864688A CN 115091905 B CN115091905 B CN 115091905B
Authority
CN
China
Prior art keywords
wing
automobile
flying
vehicle
tail
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202210864688.2A
Other languages
Chinese (zh)
Other versions
CN115091905A (en
Inventor
李立军
门馨伟
吴泽华
杨恺熠
樊欣雨
刘骁
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beihang University
Original Assignee
Beihang University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Beihang University filed Critical Beihang University
Priority to CN202210864688.2A priority Critical patent/CN115091905B/en
Publication of CN115091905A publication Critical patent/CN115091905A/en
Application granted granted Critical
Publication of CN115091905B publication Critical patent/CN115091905B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60FVEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

The flying car can run on the ground and fly in the air, and becomes a novel vehicle capable of solving the problem of urban traffic jam and flexibly transporting people or goods. However, the existing flying automobile has high oil consumption or electricity consumption, high risk of medium-high altitude flying and large occupied space of Liu Hangshi wings. Therefore, the invention provides an electric flying automobile, which belongs to the technical field of vehicles and aviation, and comprises an automobile body, a battery system, a left automobile wing, a right automobile wing, an automobile wing upper connecting piece, a left propeller, a right propeller, a tail wing mounting bracket, a tail wing, a motor connecting arm, a folding wing rotating motor and the like, wherein the electric flying automobile has two modes of land running and ultra-low altitude flying: when flying, the wings extend, and the automobile is in the ground effect area; the wing is put into the body when the road is on the ground. The invention has the advantages of convenient folding of the wing, small occupied space of Liu Hangshi, energy conservation, high safety and the like, and has very wide application prospect.

Description

一种电动飞行汽车An electric flying car

技术领域Technical Field

本发明涉及一种基于可折叠翼的电动飞行器,尤其涉及一种电动飞行汽车,属于航空、汽车技术领域。The invention relates to an electric aircraft based on foldable wings, in particular to an electric flying car, and belongs to the field of aviation and automobile technology.

背景技术Background technique

随着科技的进步,交通工具多栖化已成为发展趋势。飞行汽车,既可以在地面上行驶,又可以在空中飞行,成为能够解决城市交通拥堵问题,灵活运输人或者货物的新型交通工具,国内外的多家企业和院所都在开展飞行汽车的研发与工程应用工作。飞行汽车按起降方式不同,可分为垂直起降和滑跑起降两种。垂直起降的飞行汽车,大都与多旋翼无人机类似,起飞和降落灵活,飞控操纵简单,但是飞行速度慢,巡航飞行能耗高,而且多旋翼在汽车陆行时不容易安放,影响地面行驶功能,使其难以具有与普通汽车一样的地面行驶稳定性和操控性。滑跑起降飞行汽车需要一段长度的道路滑跑才能完成起飞,巡航飞行能耗低,但车翼折叠之后占用空间大。此外,目前飞行汽车基本都为中高空飞行汽车,在数百米或千米高度飞行,一旦出现故障就可能导致灾难性后果,所以对使用者的驾驶技能和心理素质要求很高,再加上人们普遍存在对高空飞行的担忧,导致飞行汽车推广应用困难。而且,飞行汽车的飞行高度越高,油耗或者电耗越大,经济性越差。With the advancement of science and technology, multi-habitat transportation has become a development trend. Flying cars can travel on the ground and fly in the air. They have become a new type of transportation that can solve the problem of urban traffic congestion and flexibly transport people or goods. Many companies and institutions at home and abroad are carrying out research and development and engineering application of flying cars. Flying cars can be divided into two types according to different take-off and landing methods: vertical take-off and landing and taxiing take-off and landing. Most vertical take-off and landing flying cars are similar to multi-rotor drones. They are flexible in take-off and landing, and the flight control is simple to operate. However, they have slow flight speeds and high energy consumption during cruising. In addition, multi-rotors are not easy to place when the car is on land, which affects the ground driving function and makes it difficult for it to have the same ground driving stability and controllability as ordinary cars. Taxiing take-off and landing flying cars need a certain length of road taxiing to complete take-off. The cruising flight has low energy consumption, but the car wings take up a lot of space after folding. In addition, most flying cars are medium- and high-altitude flying cars, flying at hundreds of meters or kilometers. Once a malfunction occurs, it may lead to catastrophic consequences, so it requires high driving skills and psychological quality of the user. In addition, people generally have concerns about high-altitude flying, which makes it difficult to promote and apply flying cars. Moreover, the higher the flying altitude of the flying car, the greater the fuel or electricity consumption, and the worse the economy.

地效作用是一种奇妙的空气动力学现象,即当运动的物体距离地面(或水面)很近时,物体上下表面的压力差增加,物体的升力会陡然增大,从而可以实现贴地或贴海飞行。将地效作用与汽车结合起来,同时使用新能源,发明一种电动地效飞行汽车,既可以在地面道路上行驶,又可以实现十米以下的超低空飞行,安全性高,经济性好,使用灵活方便,具有非常广阔的应用前景。Ground effect is a wonderful aerodynamic phenomenon, that is, when a moving object is very close to the ground (or water surface), the pressure difference between the upper and lower surfaces of the object increases, and the lift of the object will increase sharply, so that it can fly close to the ground or the sea. By combining ground effect with cars and using new energy, an electric ground effect flying car was invented, which can not only drive on the ground road, but also achieve ultra-low altitude flight below ten meters. It has high safety, good economy, flexible and convenient use, and has a very broad application prospect.

发明内容Summary of the invention

1、发明目的:1. Purpose of the invention:

本发明的目的在于提供一种电动飞行汽车,既可以陆行,又可以基于地效作用进行超低空飞行,车翼可以折叠,以解决现有飞行汽车的高空飞行危险性高,能耗大,经济性差,机翼占用空间大等问题。The purpose of the present invention is to provide an electric flying car that can travel on land and fly at ultra-low altitude based on ground effect. The wings of the car can be folded to solve the problems of existing flying cars such as high risk of high-altitude flight, high energy consumption, poor economy, and large space occupied by the wings.

2、技术方案:2. Technical solution:

本发明一种电动飞行汽车,其特征在于,包括以下部分:车身、前车窗、电池系统、前轮、底盘系统、左车翼、左车翼前段、左车翼后段、车翼上部连接件、车尾、左螺旋桨、尾翼安装支架、尾翼、右螺旋桨、后轮、右车翼、车顶、车翼撑杆连接件、右翼撑杆、铰接件、前摆臂、横向转轴、下摆臂、后摆臂、电机连接臂、折叠翼旋转电机、左翼撑杆、右车翼前段、右车翼后段;它们之间的关系是:车身为飞行汽车的主体承载结构,电池系统位于车身的底部中间位置;左车翼和右车翼对称布置于车身的两侧,以驾驶员的视角来区分左右;左车翼由左车翼前段、左车翼后段、车翼上部连接件和车翼下部锁定机构组成;右车翼由右车翼前段、右车翼后段、车翼上部连接件和车翼下部锁定机构组成;尾翼通过尾翼安装支架安装于车身的车尾上;左螺旋桨和右螺旋桨安装于车尾;车翼撑杆连接件、右翼撑杆、铰接件、前摆臂、横向转轴、下摆臂、后摆臂、电机连接臂、折叠翼旋转电机、左翼撑杆位于车身的内部,与车翼一起构成了飞行汽车的折叠翼系统;The present invention discloses an electric flying car, characterized in that it comprises the following parts: a car body, a front car window, a battery system, a front wheel, a chassis system, a left car wing, a front section of the left car wing, a rear section of the left car wing, a car wing upper connecting piece, a car tail, a left propeller, a tail wing mounting bracket, a tail wing, a right propeller, a rear wheel, a right car wing, a car roof, a car wing support rod connecting piece, a right wing support rod, a hinge, a front swing arm, a lateral rotating shaft, a lower swing arm, a rear swing arm, a motor connecting arm, a folding wing rotating motor, a left wing support rod, a front section of the right car wing, and a rear section of the right car wing; the relationship between them is that the car body is the main bearing structure of the flying car, the battery system is located in the middle of the bottom of the car body; the left car wing and The right wing is symmetrically arranged on both sides of the vehicle body, and the left and right are distinguished from the driver's perspective; the left wing is composed of the left wing front section, the left wing rear section, the wing upper connecting piece and the wing lower locking mechanism; the right wing is composed of the right wing front section, the right wing rear section, the wing upper connecting piece and the wing lower locking mechanism; the tail wing is installed on the rear of the vehicle body through the tail wing mounting bracket; the left propeller and the right propeller are installed at the rear of the vehicle; the wing strut connecting piece, the right wing strut, the hinge, the front swing arm, the lateral shaft, the lower swing arm, the rear swing arm, the motor connecting arm, the folding wing rotating motor, and the left wing strut are located inside the vehicle body, and together with the wing constitute the folding wing system of the flying car;

本发明一种电动飞行汽车具有陆地行驶和超低空地效飞行两种模式,具有自动起飞和降落功能:飞行时,汽车处于地效应作用区域内,左车翼和右车翼处于伸展状态,为飞行提供升力,通过左螺旋桨和右螺旋桨的转动来推动飞行汽车在空中前进;陆地行驶时,车顶的后部和车身的后部两侧收缩,左车翼和右车翼先分别沿车翼长度方向的中线围绕各自的车翼上部连接件折叠,然后再由左翼撑杆和右翼撑杆带动左右车翼折叠后放进车身内部,同时尾翼的迎角变为负值,减少汽车的空气升力,增大下压力,提高行驶稳定性;The electric flying car of the present invention has two modes of land driving and ultra-low altitude ground effect flight, and has automatic take-off and landing functions: when flying, the car is in the ground effect action area, the left car wing and the right car wing are in an extended state, providing lift for flight, and the flying car is pushed forward in the air by the rotation of the left propeller and the right propeller; when driving on land, the rear part of the car roof and the rear sides of the car body are retracted, the left car wing and the right car wing are first folded around their respective upper car wing connecting pieces along the center line of the car wing length direction, and then the left and right car wings are driven by the left wing support rod and the right wing support rod to fold and put into the car body, and at the same time, the attack angle of the tail wing becomes a negative value, thereby reducing the air lift of the car, increasing the downforce, and improving the driving stability;

所述车身,为承载式车身,白车身部分采用铝合金材料,分区域压铸成型后使用冲铆连接装配,关键承载区域再使用内部胶粘纤维增强复合材料层的方式增强,以获得轻质高强的车身结构;车身底部覆盖有一块底护板,由工程塑料制成,底护板的外表面用于防护地面的碎石等的冲击,底护板的内表面设置有安全气囊夹层,当飞行汽车失控坠落地面时,车身底部的安全气囊从夹层中弹出,用于缓冲地面的冲击力,保护成员的安全;The body is a load-bearing body, the body-in-white part is made of aluminum alloy material, and is assembled by punching and riveting after being die-cast in different regions. The key load-bearing area is reinforced by an internal adhesive fiber reinforced composite material layer to obtain a lightweight and high-strength body structure; the bottom of the body is covered with a bottom guard plate made of engineering plastics, the outer surface of the bottom guard plate is used to protect against the impact of gravel on the ground, etc., and the inner surface of the bottom guard plate is provided with an airbag interlayer. When the flying car loses control and falls to the ground, the airbag at the bottom of the body pops out from the interlayer to cushion the impact of the ground and protect the safety of the members;

所述前车窗,采用聚甲基丙烯酸树脂有机玻璃制成,中后部区域具有滑动开启的功能,用于乘员上下车;The front window is made of polymethacrylic resin organic glass, and the middle and rear area has a sliding opening function for passengers to get on and off the vehicle;

所述电池系统,包括电池模组、电池箱、散热系统、传感器、继电器、线束和电池管理系统;电池箱的上盖和下箱体为承载结构,与车身、底盘系统一体化,以减少飞行汽车的零部件;车翼通过车翼撑杆连接件安装在电池箱的上盖;The battery system includes a battery module, a battery box, a cooling system, a sensor, a relay, a wiring harness and a battery management system; the upper cover and the lower box of the battery box are load-bearing structures, which are integrated with the vehicle body and chassis system to reduce the number of parts of the flying car; the wing is installed on the upper cover of the battery box through the wing support rod connector;

所述前轮和后轮,由轮毂电机驱动,轮毂电机的动力由电池系统提供,当汽车在陆地上行驶时,提供行驶驱动力,当汽车离开地面进入巡航飞行状态时,前轮和后轮收起,并由车轮罩覆盖,避免飞行过程中在车轮附近产生空气湍流和激振,防止车身两侧的空气流场紊乱;The front wheels and rear wheels are driven by wheel hub motors, which are powered by a battery system. When the vehicle is traveling on land, the wheel hub motors provide driving force. When the vehicle leaves the ground and enters a cruising flight state, the front wheels and rear wheels are retracted and covered by wheel covers to avoid air turbulence and vibration near the wheels during flight and to prevent turbulence in the air flow field on both sides of the vehicle body.

所述左车翼,主要作用为汽车飞行提高升力和保证飞行稳定,为组合式结构,由左车翼前段和左车翼后段通过车翼上部连接件连接;左车翼前段和左车翼后段采用碳纤维或玄武岩纤维增强复合材料制成;飞行状态时展开,通过车翼下部锁定机构将左车翼前段和左车翼后段固定在一起,巡航飞行时迎角为4度,以获得良好的能耗经济性;陆行状态时,车翼下部锁定机构打开,车翼进行折叠;The left wing is mainly used to increase the lift and ensure the flight stability of the vehicle. It is a combined structure, and is composed of a left wing front section and a left wing rear section connected by an upper wing connecting piece. The left wing front section and the left wing rear section are made of carbon fiber or basalt fiber reinforced composite materials. When in flight, the left wing front section and the left wing rear section are fixed together by a locking mechanism at the lower part of the wing. The angle of attack is 4 degrees during cruising flight to obtain good energy consumption economy. When in land mode, the locking mechanism at the lower part of the wing is opened, and the wing is folded.

所述左螺旋桨和右螺旋桨,为汽车的飞行提供推进力,采用碳纤维增强复合材料制成,以减轻重量和提高疲劳寿命;The left propeller and the right propeller provide propulsion for the flight of the car and are made of carbon fiber reinforced composite materials to reduce weight and increase fatigue life;

所述尾翼,采用碳纤维增强复合材料制成,以减轻重量和提高疲劳寿命;通过尾翼安装支架安装在车身的尾部,尾翼安装支架的上部为“V”型托举结构,下部为内“X”型筋肋配外“凹”型框架结构,以稳固支撑尾翼;尾翼具有自动旋转功能,飞行状态迎角为正值,获得足够升力,提高飞行的经济性;尾翼陆行状态迎角为负值,获得足够的下压力,提高陆行稳定性;The tail wing is made of carbon fiber reinforced composite material to reduce weight and increase fatigue life; it is installed on the tail of the vehicle body through a tail wing mounting bracket, the upper part of the tail wing mounting bracket is a "V"-shaped lifting structure, and the lower part is an inner "X"-shaped rib with an outer "concave"-shaped frame structure to firmly support the tail wing; the tail wing has an automatic rotation function, and the angle of attack in the flight state is a positive value to obtain sufficient lift and improve the economy of flight; the angle of attack of the tail wing in the land state is a negative value to obtain sufficient downforce and improve the land stability;

所述车顶,采用纤维增强复合材料制成,后部具有折叠功能,为车翼的折叠提高空间;The roof is made of fiber-reinforced composite material, and has a folding function at the rear to increase space for folding the wings;

所述右翼撑杆的一端通过车翼撑杆连接件与右车翼前段相连,另一端与铰接件相连;折叠翼旋转电机转动,驱动电机连接臂转动,带动下摆臂,使前摆臂围绕横向转轴转动,进而带动右翼撑杆和左翼撑杆运动,实现左车翼和右车翼折叠或展开。One end of the right wing strut is connected to the front section of the right wing through a wing strut connecting piece, and the other end is connected to a hinge; the folding wing rotating motor rotates, driving the motor connecting arm to rotate, driving the lower swing arm, causing the front swing arm to rotate around the transverse rotating axis, thereby driving the right wing strut and the left wing strut to move, thereby realizing the folding or unfolding of the left and right wings.

3、本发明一种电动飞行汽车,相比现有技术具有以下进步和有益效果:3. The electric flying car of the present invention has the following improvements and beneficial effects compared with the prior art:

(1)两侧车翼采用两级折叠设计,可以折叠后放入车身内,节省道路占用和停车空间,而且可以提高地面道路行驶的稳定性;(1) The two side wings adopt a two-stage folding design, which can be folded and put into the body of the vehicle, saving road occupation and parking space, and improving the stability of ground road driving;

(2)利用地效作用实现贴近地面或海面的超低空飞行,飞行高度低,安全性更好,使用者不会产生高空坠落恐惧,经济性好,节省了飞机汽车爬升百米乃至千米所消耗的能量;(2) Using ground effect to achieve ultra-low altitude flight close to the ground or sea surface, the flight altitude is low, the safety is better, the user will not have the fear of falling from high altitude, the economy is good, and the energy consumed by airplanes and cars to climb hundreds or even thousands of meters is saved;

(3)车身采用铝合金压铸成型,车翼、尾翼等结构采用复合材料,大大降低了整车的重量,油耗或电耗降低,续航里程增加。(3) The vehicle body is made of aluminum alloy die-casting, and the wings, tail wing and other structures are made of composite materials, which greatly reduces the weight of the vehicle, reduces fuel consumption or power consumption, and increases the cruising range.

总之,本发明是一种节能和安全的电动飞行汽车,可以超低空快速飞行,也可以在地面道路上高速行驶,是一种新型的交通工具,具有广阔的应用前景。In summary, the present invention is an energy-saving and safe electric flying car that can fly quickly at ultra-low altitudes and can also travel at high speeds on ground roads. It is a new type of transportation and has broad application prospects.

附图说明BRIEF DESCRIPTION OF THE DRAWINGS

图1是本发明的飞行状态的三维轴测透视图;FIG1 is a three-dimensional isometric perspective view of the present invention in flight;

图2是本发明的飞行状态的三维框线图;FIG2 is a three-dimensional block diagram of the flight state of the present invention;

图3是本发明的车翼展开状态结构图;FIG3 is a structural diagram of a vehicle wing in an unfolded state of the present invention;

图4是本发明的地面行驶状态的三维框线图;FIG4 is a three-dimensional frame diagram of the ground driving state of the present invention;

图中符号说明如下:The symbols in the figure are explained as follows:

1-车身、2-前车窗、3-电池系统、4-前轮、5-底盘系统、6-左车翼、7-左车翼前段、8-左车翼后段、9-车翼上部连接件、10-车尾、11-左螺旋桨、12-尾翼安装支架、13-尾翼、14-右螺旋桨、15-后轮、16-右车翼、17-车顶、18-车翼撑杆连接件、19-右翼撑杆、20-铰接件、21-前摆臂、22-横向转轴、23-下摆臂、24-后摆臂、25-电机连接臂、26-折叠翼旋转电机、27-左翼撑杆、28-右车翼前段、29-右车翼后段。1-body, 2-front window, 3-battery system, 4-front wheel, 5-chassis system, 6-left wing, 7-front section of left wing, 8-rear section of left wing, 9-upper wing connector, 10-rear, 11-left propeller, 12-tail mounting bracket, 13-tail, 14-right propeller, 15-rear wheel, 16-right wing, 17-roof, 18-wing support rod connector, 19-right wing support rod, 20-hinge, 21-front swing arm, 22-lateral rotation axis, 23-lower swing arm, 24-rear swing arm, 25-motor connecting arm, 26-folding wing rotation motor, 27-left wing support rod, 28-front section of right wing, 29-rear section of right wing.

具体实施方式Detailed ways

下面结合附图对本发明实施例作进一步详细说明:The embodiments of the present invention are further described in detail below with reference to the accompanying drawings:

如附图所示,本发明一种电动飞行汽车,包括以下部分:车身1、前车窗2、电池系统3、前轮4、底盘系统5、左车翼6、左车翼前段7、左车翼后段8、车翼上部连接件9、车尾10、左螺旋桨11、尾翼安装支架12、尾翼13、右螺旋桨14、后轮15、右车翼16、车顶17、车翼撑杆连接件18、右翼撑杆19、铰接件20、前摆臂21、横向转轴22、下摆臂23、后摆臂24、电机连接臂25、折叠翼旋转电机26、左翼撑杆27、右车翼前段28、右车翼后段29;它们之间的关系是:车身1为飞行汽车的主体承载结构,电池系统3位于车身1的底部中间位置;左车翼6和右车翼16对称布置于车身1的两侧,以驾驶员的视角来区分左右;左车翼6由左车翼前段7、左车翼后段8、车翼上部连接件9和车翼下部锁定机构组成;右车翼16由右车翼前段28、右车翼后段29、车翼上部连接件9和车翼下部锁定机构组成;尾翼13通过尾翼安装支架12安装于车身1的车尾10上;左螺旋桨11和右螺旋桨14安装于车尾10;车翼撑杆连接件18、右翼撑杆19、铰接件20、前摆臂21、横向转轴22、下摆臂23、后摆臂24、电机连接臂25、折叠翼旋转电机26、左翼撑杆27位于车身1的内部,与车翼一起构成了飞行汽车的折叠翼系统;As shown in the accompanying drawings, an electric flying car of the present invention comprises the following parts: a car body 1, a front window 2, a battery system 3, a front wheel 4, a chassis system 5, a left wing 6, a left wing front section 7, a left wing rear section 8, a wing upper connecting piece 9, a car tail 10, a left propeller 11, a tail wing mounting bracket 12, a tail wing 13, a right propeller 14, a rear wheel 15, a right wing 16, a car roof 17, a car wing support rod connecting piece 18, a right wing support rod 19, a hinge 20, a front swing arm 21, a lateral rotation shaft 22, a lower swing arm 23, a rear swing arm 24, a motor connecting arm 25, a folding wing rotating motor 26, a left wing support rod 27, a right wing front section 28, and a right wing rear section 29; the relationship between them is that the car body 1 is the main bearing structure of the flying car, the battery system 3 is located in the middle of the bottom of the car body 1; the left wing The wing 6 and the right wing 16 are symmetrically arranged on both sides of the vehicle body 1, and the left and right are distinguished from the driver's perspective; the left wing 6 is composed of a left wing front section 7, a left wing rear section 8, an upper wing connection member 9 and a lower wing locking mechanism; the right wing 16 is composed of a right wing front section 28, a right wing rear section 29, an upper wing connection member 9 and a lower wing locking mechanism; the tail 13 is installed on the rear 10 of the vehicle body 1 through a tail wing mounting bracket 12; the left propeller 11 and the right propeller 14 are installed on the rear 10; the wing strut connecting member 18, the right wing strut 19, the hinge 20, the front swing arm 21, the lateral rotation shaft 22, the lower swing arm 23, the rear swing arm 24, the motor connecting arm 25, the folding wing rotating motor 26, and the left wing strut 27 are located inside the vehicle body 1, and together with the wing constitute the folding wing system of the flying car;

所述车身1,为承载式车身,白车身部分采用铝合金材料,分区域压铸成型后使用冲铆连接装配,关键承载区域再使用内部胶粘纤维增强复合材料层的方式增强,以获得轻质高强的车身结构;车身底部覆盖有一块底护板,由工程塑料制成,底护板的外表面用于防护地面的碎石等的冲击,底护板的内表面设置有安全气囊夹层,当飞行汽车失控坠落地面时,车身底部的安全气囊从夹层中弹出,用于缓冲地面的冲击力,保护成员的安全;The body 1 is a load-bearing body. The body-in-white part is made of aluminum alloy material. After being die-cast in different regions, it is connected and assembled by punching and riveting. The key load-bearing area is reinforced by using an internal adhesive fiber reinforced composite material layer to obtain a lightweight and high-strength body structure. The bottom of the body is covered with a bottom guard plate made of engineering plastic. The outer surface of the bottom guard plate is used to protect against the impact of gravel on the ground, and the inner surface of the bottom guard plate is provided with an airbag interlayer. When the flying car loses control and falls to the ground, the airbag at the bottom of the body pops out from the interlayer to cushion the impact of the ground and protect the safety of the members.

所述前车窗2,采用聚甲基丙烯酸树脂有机玻璃制成,中后部区域具有滑动开启的功能,用于乘员上下车;The front window 2 is made of polymethacrylate resin organic glass, and the middle and rear area has a sliding opening function for passengers to get on and off the vehicle;

所述电池系统3,包括电池模组、电池箱、散热系统、传感器、继电器、线束和电池管理系统;电池箱的上盖和下箱体为承载结构,与车身1、底盘系统5一体化,以减少飞行汽车的零部件;车翼通过车翼撑杆连接件18安装在电池箱的上盖;The battery system 3 includes a battery module, a battery box, a cooling system, a sensor, a relay, a wiring harness and a battery management system; the upper cover and the lower box of the battery box are load-bearing structures, which are integrated with the vehicle body 1 and the chassis system 5 to reduce the number of parts of the flying car; the wing is installed on the upper cover of the battery box through the wing support rod connector 18;

所述前轮4和后轮15,由轮毂电机驱动,轮毂电机的动力由电池系统3提供,当汽车在陆地上行驶时,提供行驶驱动力,当汽车离开地面进入巡航飞行状态时,前轮和后轮收起,并由车轮罩覆盖,避免飞行过程中在车轮附近产生空气湍流和激振,防止车身两侧的空气流场紊乱;The front wheels 4 and the rear wheels 15 are driven by wheel hub motors, and the power of the wheel hub motors is provided by the battery system 3. When the car is driving on land, the wheel hub motors provide driving force. When the car leaves the ground and enters a cruising flight state, the front wheels and the rear wheels are retracted and covered by wheel covers to avoid air turbulence and vibration near the wheels during flight, and to prevent air flow disturbance on both sides of the car body;

所述左车翼6,主要作用为汽车飞行提高升力和保证飞行稳定,为组合式结构,由左车翼前段7和左车翼后段8通过车翼上部连接件9连接;左车翼前段7和左车翼后段8采用碳纤维或玄武岩纤维增强复合材料制成;飞行状态时展开,通过车翼下部锁定机构将左车翼前段7和左车翼后段8固定在一起,巡航飞行时迎角为4度,以获得良好的能耗经济性;陆行状态时,车翼下部锁定机构打开,车翼进行折叠;The left wing 6 is mainly used to increase the lift and ensure the flight stability of the vehicle. It is a combined structure, which is connected by the left wing front section 7 and the left wing rear section 8 through the wing upper connecting piece 9; the left wing front section 7 and the left wing rear section 8 are made of carbon fiber or basalt fiber reinforced composite materials; when in flight, the left wing front section 7 and the left wing rear section 8 are fixed together by the wing lower locking mechanism, and the angle of attack is 4 degrees during cruising flight to obtain good energy consumption economy; when in land state, the wing lower locking mechanism is opened and the wing is folded;

所述左螺旋桨11和右螺旋桨14,为汽车的飞行提供推进力,采用碳纤维增强复合材料制成,以减轻重量和提高疲劳寿命;The left propeller 11 and the right propeller 14 provide propulsion for the flight of the vehicle and are made of carbon fiber reinforced composite materials to reduce weight and increase fatigue life;

所述尾翼13,采用碳纤维增强复合材料制成,以减轻重量和提高疲劳寿命;通过尾翼安装支架12安装在车身1的尾部,尾翼安装支架12的上部为“V”型托举结构,下部为内“X”型筋肋配外“凹”型框架结构,以稳固支撑尾翼13;尾翼13具有自动旋转功能,飞行状态迎角为正值,获得足够升力,提高飞行的经济性;尾翼13陆行状态迎角为负值,获得足够的下压力,提高陆行稳定性;The tail 13 is made of carbon fiber reinforced composite material to reduce weight and increase fatigue life; it is installed on the tail of the vehicle body 1 through the tail mounting bracket 12, the upper part of the tail mounting bracket 12 is a "V"-shaped lifting structure, and the lower part is an inner "X"-shaped rib with an outer "concave" frame structure to firmly support the tail 13; the tail 13 has an automatic rotation function, and the angle of attack in the flight state is a positive value, so as to obtain sufficient lift and improve the economic efficiency of the flight; the angle of attack of the tail 13 in the land state is a negative value, so as to obtain sufficient downforce and improve the land stability;

所述车顶17,采用纤维增强复合材料制成,后部具有折叠功能,为车翼的折叠提高空间;The roof 17 is made of fiber-reinforced composite material, and the rear portion has a folding function to increase space for folding the wings;

所述右翼撑杆19的一端通过车翼撑杆连接件18与右车翼前段28相连,另一端与铰接件20相连;折叠翼旋转电机26转动,驱动电机连接臂25转动,带动下摆臂23,使前摆臂21围绕横向转轴22转动,进而带动右翼撑杆19和左翼撑杆27运动,实现左车翼6和右车翼16折叠或展开;One end of the right wing support rod 19 is connected to the right wing front section 28 through the wing support rod connecting member 18, and the other end is connected to the hinge 20; the folding wing rotating motor 26 rotates, driving the motor connecting arm 25 to rotate, driving the lower swing arm 23, and making the front swing arm 21 rotate around the transverse rotation axis 22, thereby driving the right wing support rod 19 and the left wing support rod 27 to move, so as to realize the folding or unfolding of the left wing 6 and the right wing 16;

如附图所示,本发明一种电动飞行汽车具有陆地行驶和超低空地效飞行两种模式,具有自动起飞和降落功能:飞行时,汽车处于地效应作用区域内,左车翼6和右车翼16处于伸展状态,为飞行提供升力,通过左螺旋桨11和右螺旋桨14的转动来推动飞行汽车在空中前进;陆地行驶时,车顶17的后部和车身1的后部两侧收缩,左车翼6和右车翼16先分别沿车翼长度方向的中线围绕各自的车翼上部连接件折叠,然后再由左翼撑杆27和右翼撑杆19带动左右车翼折叠后放进车身内部,同时尾翼13的迎角变为负值,减少汽车的空气升力,增大下压力,提高行驶稳定性。As shown in the accompanying drawings, an electric flying car of the present invention has two modes: land driving and ultra-low altitude ground effect flight, and has automatic take-off and landing functions: when flying, the car is in the ground effect area, the left wing 6 and the right wing 16 are in an extended state, providing lift for flight, and the flying car is pushed forward in the air by the rotation of the left propeller 11 and the right propeller 14; when driving on land, the rear part of the roof 17 and the two sides of the rear part of the body 1 are retracted, and the left wing 6 and the right wing 16 are first folded around their respective upper wing connecting parts along the center line of the wing length direction, and then the left and right wings are driven by the left wing strut 27 and the right wing strut 19 to fold and put into the body, and at the same time, the angle of attack of the tail wing 13 becomes a negative value, reducing the air lift of the car, increasing the downforce, and improving the driving stability.

本发明按照设想实施特例进行了说明,但不局限于上述实例,凡是符合本发明的思路,采用相似结构及材料替换的方法所获得的技术方案,都属于本发明的保护范围之内。The present invention is described according to the envisioned implementation examples, but is not limited to the above examples. Any technical solution obtained by using similar structures and material replacement methods that conform to the ideas of the present invention belongs to the protection scope of the present invention.

Claims (2)

1. An electric flying automobile comprises an automobile body, a front automobile window, a battery system, a front wheel, a chassis system, a left automobile wing, an automobile tail, a left propeller, an empennage mounting bracket, an empennage, a right propeller, a rear wheel, a right automobile wing, a roof, a automobile wing stay bar connecting piece, a right wing stay bar, a hinge piece, a front swing arm, a transverse rotating shaft, a lower swing arm, a rear swing arm, a motor connecting arm, a folding wing rotating motor and a left wing stay bar; the method is characterized in that: the vehicle body is a main body bearing structure of the flying vehicle, and the battery system is positioned at the middle position of the bottom of the vehicle body; the left wing and the right wing are symmetrically arranged on two sides of the vehicle body, so that the left wing and the right wing are distinguished from each other in view of a driver; the left wing consists of a left wing front section, a left wing rear section, a wing upper connecting piece and a wing lower locking mechanism; the right wing consists of a right wing front section, a right wing rear section, a wing upper connecting piece and a wing lower locking mechanism; the tail wing is arranged on the tail of the car body through a tail wing mounting bracket; the left propeller and the right propeller are arranged at the tail of the vehicle; the wing strut connecting piece, the right wing strut, the hinge piece, the front swing arm, the transverse rotating shaft, the lower swing arm, the rear swing arm, the motor connecting arm, the folding wing rotating motor and the left wing strut are positioned in the vehicle body, and form a folding wing system of the aerocar together with the wing;
The electric flying automobile has two modes of land running and ultra-low altitude ground effect flying, and has the functions of automatic take-off and landing: when flying, the automobile is in a ground effect action area, the left wing and the right wing are in an extending state, lift force is provided for flying, and the flying automobile is pushed to advance in the air through rotation of the left propeller and the right propeller; when the vehicle runs on land, the rear part of the vehicle roof and the two sides of the rear part of the vehicle body shrink, the left wing and the right wing are folded around the upper connecting pieces of the respective wings along the central lines of the length directions of the wings, then the left wing stay bar and the right wing stay bar drive the left wing and the right wing to be folded and then put into the vehicle body, and meanwhile, the attack angle of the tail wing becomes negative, so that the air lift force of the vehicle is reduced, the downward pressure is increased, and the running stability is improved;
the body is a bearing type body, the body-in-white part is made of aluminum alloy materials, after being subjected to split-region die casting, the body-in-white part is assembled by punching and riveting, and the key bearing region is reinforced by using an internal adhesive fiber reinforced composite material layer so as to obtain a light high-strength body structure; the bottom of the automobile body is covered with a bottom guard plate made of engineering plastics, the outer surface of the bottom guard plate is used for protecting the impact of broken stone on the ground, the inner surface of the bottom guard plate is provided with an air bag interlayer, and when the flying automobile falls off the ground in a runaway manner, the air bag at the bottom of the automobile body pops out of the interlayer and is used for buffering the impact force of the ground so as to protect the safety of members;
the front window is made of polymethyl methacrylate resin organic glass, and the middle and rear areas have a sliding opening function and are used for passengers to get on or off the vehicle;
The battery system comprises a battery module, a battery box, a heat dissipation system, a sensor, a relay, a wire harness and a battery management system; the upper cover and the lower box body of the battery box are of bearing structures and are integrated with the vehicle body and the chassis system so as to reduce parts of the flying vehicle; the vehicle wing is arranged on the upper cover of the battery box through a vehicle wing stay bar connecting piece;
The front wheel and the rear wheel are driven by the hub motor, the power of the hub motor is provided by the battery system, when the automobile runs on land, the running driving force is provided, when the automobile leaves the ground and enters a cruising flight state, the front wheel and the rear wheel are retracted and covered by the wheel covers, air turbulence and excitation are prevented from being generated near the wheels in the flight process, and air flow field disorders on two sides of the automobile body are prevented;
The left wing mainly plays roles in improving lift force and ensuring stable flying of an automobile, is of a combined structure, and is connected by a front section of the left wing and a rear section of the left wing through a connecting piece at the upper part of the wing; the front section of the left wing and the rear section of the left wing are made of carbon fiber or basalt fiber reinforced composite materials; the automobile is unfolded in a flight state, the front section of the left automobile wing and the rear section of the left automobile wing are fixed together through the locking mechanism at the lower part of the automobile wing, and the attack angle is 4 degrees during cruising flight, so that good energy consumption economy is obtained; when the vehicle runs on the ground, the locking mechanism at the lower part of the vehicle wing is opened, and the vehicle wing is folded;
the left propeller and the right propeller provide propulsion for the flight of the automobile and are made of carbon fiber reinforced composite materials so as to reduce the weight and improve the fatigue life;
The tail wing is made of carbon fiber reinforced composite materials so as to reduce weight and improve fatigue life; the tail wing mounting bracket is arranged at the tail part of the vehicle body, the upper part of the tail wing mounting bracket is of a V-shaped lifting structure, and the lower part of the tail wing mounting bracket is of an inner X-shaped rib matched with an outer concave frame structure so as to firmly support the tail wing; the tail wing has an automatic rotation function, the attack angle of the flight state is a positive value, enough lift force is obtained, and the economy of flight is improved; the attack angle of the tail wing in the land state is a negative value, so that enough downward pressure is obtained, and the stability of the land is improved;
The vehicle roof is made of fiber reinforced composite materials, and the rear part of the vehicle roof has a folding function, so that the space for folding the vehicle wings is increased.
2. An electric flying vehicle according to claim 1, wherein: one end of the right wing stay bar is connected with the front section of the right wing through a wing stay bar connecting piece, and the other end of the right wing stay bar is connected with the hinge piece; the folding wing rotating motor rotates, the driving motor connecting arm rotates to drive the lower swing arm, the front swing arm rotates around the transverse rotating shaft, and then the right wing supporting rod and the left wing supporting rod are driven to move, so that the folding or unfolding of the left wing and the right wing is realized.
CN202210864688.2A 2022-07-21 2022-07-21 An electric flying car Active CN115091905B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210864688.2A CN115091905B (en) 2022-07-21 2022-07-21 An electric flying car

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210864688.2A CN115091905B (en) 2022-07-21 2022-07-21 An electric flying car

Publications (2)

Publication Number Publication Date
CN115091905A CN115091905A (en) 2022-09-23
CN115091905B true CN115091905B (en) 2024-05-31

Family

ID=83298375

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210864688.2A Active CN115091905B (en) 2022-07-21 2022-07-21 An electric flying car

Country Status (1)

Country Link
CN (1) CN115091905B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118850384A (en) * 2024-09-25 2024-10-29 南通海洛达智能科技有限公司 An automatic attitude adjustment device for unmanned aerial vehicle landing

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1390743A (en) * 2002-04-30 2003-01-15 广州天象地效飞行器股份有限公司 Effectively power-boosting ground effect aircraft
CN1887609A (en) * 2006-07-18 2007-01-03 吴冠豪 Carplane
CN102616096A (en) * 2012-04-24 2012-08-01 赵辉 Solar flying automobile with folding wings
CN102649391A (en) * 2012-05-03 2012-08-29 张瑞钧 Ground-effect type extreme low-altitude dual-purpose aerocar or dual-purpose aircraft
CN103522858A (en) * 2013-10-16 2014-01-22 北京航空航天大学 a flying car
CN103770589A (en) * 2014-02-28 2014-05-07 武汉蓝天翔航空科技有限公司 Flying car
CN104477384A (en) * 2014-12-15 2015-04-01 佛山市神风航空科技有限公司 Flat wing panel ornithopter
CN107757273A (en) * 2017-09-27 2018-03-06 北京航空航天大学 A kind of hovercar
CN107984992A (en) * 2017-11-28 2018-05-04 北京航空航天大学 It is a kind of can VTOL land and air double-used vehicle
CN108146169A (en) * 2017-11-28 2018-06-12 北京航空航天大学 The land and air double-used vehicle of folding after a kind of wing
CN111923672A (en) * 2020-08-21 2020-11-13 重庆航天职业技术学院 Flying automobile
CN213007448U (en) * 2020-08-21 2021-04-20 重庆航天职业技术学院 Aerocar capable of adjusting ground grabbing force and lifting force
CN113370730A (en) * 2021-07-20 2021-09-10 广东汇天航空航天科技有限公司 Flying car

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030094536A1 (en) * 2001-10-25 2003-05-22 Labiche Mitchell G. Flyable automobile
SK6347Y1 (en) * 2011-08-30 2013-01-02 Aeromobil Sro Method of transformation of hybrid vehicles for land and air and hybrid vehicle
BG111231A (en) * 2012-06-07 2013-12-31 КРЪСТЕВ ИванKrustev Ivan Road aircraft

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1390743A (en) * 2002-04-30 2003-01-15 广州天象地效飞行器股份有限公司 Effectively power-boosting ground effect aircraft
CN1887609A (en) * 2006-07-18 2007-01-03 吴冠豪 Carplane
CN102616096A (en) * 2012-04-24 2012-08-01 赵辉 Solar flying automobile with folding wings
CN102649391A (en) * 2012-05-03 2012-08-29 张瑞钧 Ground-effect type extreme low-altitude dual-purpose aerocar or dual-purpose aircraft
CN103522858A (en) * 2013-10-16 2014-01-22 北京航空航天大学 a flying car
CN103770589A (en) * 2014-02-28 2014-05-07 武汉蓝天翔航空科技有限公司 Flying car
CN104477384A (en) * 2014-12-15 2015-04-01 佛山市神风航空科技有限公司 Flat wing panel ornithopter
CN107757273A (en) * 2017-09-27 2018-03-06 北京航空航天大学 A kind of hovercar
CN107984992A (en) * 2017-11-28 2018-05-04 北京航空航天大学 It is a kind of can VTOL land and air double-used vehicle
CN108146169A (en) * 2017-11-28 2018-06-12 北京航空航天大学 The land and air double-used vehicle of folding after a kind of wing
CN111923672A (en) * 2020-08-21 2020-11-13 重庆航天职业技术学院 Flying automobile
CN213007448U (en) * 2020-08-21 2021-04-20 重庆航天职业技术学院 Aerocar capable of adjusting ground grabbing force and lifting force
CN113370730A (en) * 2021-07-20 2021-09-10 广东汇天航空航天科技有限公司 Flying car

Also Published As

Publication number Publication date
CN115091905A (en) 2022-09-23

Similar Documents

Publication Publication Date Title
US9815345B2 (en) Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself
US8511603B2 (en) Roadable aircraft with collapsible wings and ductless fan
CN108116668B (en) All-electric multi-rotor manned aircraft for land and air
WO2015090071A1 (en) Land and water flying automobile
WO2012010021A1 (en) Air-ground double-purpose aircraft
CN102616096A (en) Solar flying automobile with folding wings
CN103522858A (en) a flying car
CN108177491A (en) One kind can vertical take-off and landing flying car
CN115091905B (en) An electric flying car
CN105730168A (en) Three-duct vertical take-off and landing flying car
CN115320298B (en) Ground effect flying car
CN119428029A (en) Helicopter flying car
CN109305234A (en) Van truck drag reduction device
CN2467345Y (en) Flying vehicle
CN105922830B (en) Flight electric car
CN205255921U (en) Flight electric automobile
CN205523488U (en) Three duct VTOL hovercar
CN205255922U (en) Electricelectric moves carplane
RU122981U1 (en) COMPACT AIRCRAFT
CN109130744B (en) Four-seat aerocar
CN111469618A (en) Air and land dual-use flying car and method of use
CN115366592A (en) Special safe intelligent land, water and air solar energy helicopter
CN205326726U (en) Flight electric motor car
CN106218333A (en) Pure electronic hovercar
CN106671712B (en) Flying electric vehicle

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant