[go: up one dir, main page]

CN114852331A - A manned flying car with morphological intelligence - Google Patents

A manned flying car with morphological intelligence Download PDF

Info

Publication number
CN114852331A
CN114852331A CN202210678769.3A CN202210678769A CN114852331A CN 114852331 A CN114852331 A CN 114852331A CN 202210678769 A CN202210678769 A CN 202210678769A CN 114852331 A CN114852331 A CN 114852331A
Authority
CN
China
Prior art keywords
flying
fan
driving
morphological
propeller
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.)
Pending
Application number
CN202210678769.3A
Other languages
Chinese (zh)
Inventor
张新钰
黄康尧
朱启豪
刘华平
罗建曦
李骏
申灏文
韩燕�
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.)
Tsinghua University
Original Assignee
Tsinghua 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 Tsinghua University filed Critical Tsinghua University
Priority to CN202210678769.3A priority Critical patent/CN114852331A/en
Publication of CN114852331A publication Critical patent/CN114852331A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C37/00Convertible aircraft
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The invention relates to the technical field of hovercars, in particular to a manned hovercar with intelligent form, wherein the hovercar adopts a flight driving fusion frame design with an integrated topological structure, a main flight structure adopts a multi-rotor type layout and a four-shaft eight-propeller aircraft structure, and a ground driving structure adopts an Ackerman steering and Macpherson suspension damping type chassis structure; judging based on signals acquired by a laser displacement sensor deployed on the flying automobile, and starting flying operation of the flying automobile when the ground runs and is congested; and after the flight operation is finished, the aerocar performs landing operation, and after the landing operation is finished, the aerocar starts ground driving operation.

Description

一种具备形态智能的载人飞行汽车A manned flying car with morphological intelligence

技术领域technical field

本发明涉及飞行汽车技术领域,特别涉及一种具备形态智能的载人飞行汽车。The invention relates to the technical field of flying cars, in particular to a manned flying car with morphological intelligence.

背景技术Background technique

飞行汽车与普通汽车最明显的区别是它具有空中飞行功能。近年来随着城市空中交通概念的兴起,用于解决城市交通拥堵问题、仅具有空中飞行功能的电动垂直起降飞行器亦称为飞行汽车,飞行汽车概念的内涵拓展为具有陆空两栖功能或用于城市空中交通的运载工具。The most obvious difference between a flying car and an ordinary car is that it has the function of flying in the air. In recent years, with the rise of the concept of urban air transportation, the electric vertical take-off and landing aircraft that only has the function of flying in the air is also called flying car, which is used to solve the problem of urban traffic congestion. vehicles for urban air traffic.

目前已有技术方案有:The existing technical solutions include:

由于现代科技的发展,飞行汽车主要可以分为折叠翼式飞行汽车,多旋翼式飞行汽车,自旋翼式飞行汽车三大类。Due to the development of modern science and technology, flying cars can be mainly divided into three categories: folding-wing flying cars, multi-rotor flying cars, and spin-wing flying cars.

1、垂直起降的飞行汽车采用可折叠机翼设计。在公路行驶时,机翼可以折叠在车身两侧,螺旋桨折叠在整流罩内,可以像普通的民用汽车一样在公路上行驶。在飞行模式时,机翼和螺旋桨展开。车轮收缩在车体内部整流罩内,减小飞行时车轮的阻力。飞行模式采用倾转旋翼飞机的原理。起飞时,双发动机与水平线承一定夹角,使其可以垂直起降,到达一定高度后双发逐渐转至水平,提供持续动力。此外具有垂直起降功能,安全系数更高,对路面起飞场地的要求低。但是采用倾转旋翼结构导致它的造价较高,能耗比大大增加,使用成本高,适众面小。1. The vertical take-off and landing flying car adopts a foldable wing design. When driving on the road, the wings can be folded on the sides of the body, and the propellers can be folded in the fairing, which can be driven on the road like an ordinary civilian car. When in flight mode, the wings and propellers are deployed. The wheels are retracted inside the fairing inside the car body, reducing the drag of the wheels during flight. The flight mode adopts the principle of tilt-rotor aircraft. When taking off, the twin engines bear a certain angle with the horizontal line, so that it can take off and land vertically. After reaching a certain height, the twin engines gradually turn to the level to provide continuous power. In addition, it has the function of vertical take-off and landing, which has a higher safety factor and lower requirements for the take-off site on the road. However, the use of the tilt-rotor structure leads to its high cost, greatly increased energy consumption ratio, high use cost and small adaptability.

2、多旋翼式飞行汽车应用外置对称螺旋桨原理,在提供足够升力的同时抵消扭矩力,具有垂直起降的能力,不再局限于起飞和降落场地。其可以通过事先规划的航线进行无人驾驶飞行,对乘员的操作能力限制低,误操机率低,安全性高。但是相比于其他飞行汽车它的使用的成本高、速度慢、耗能大、航程小、维护成本高。仅适合小范围内交通,短距离路程使用2. The multi-rotor flying car applies the principle of an external symmetrical propeller, which can offset the torque force while providing sufficient lift, and has the ability to take off and land vertically, which is no longer limited to take-off and landing sites. It can conduct unmanned flight through pre-planned routes, with low restrictions on the operating ability of the occupants, low probability of misoperation, and high safety. However, compared with other flying cars, its use cost is high, the speed is slow, the energy consumption is large, the range is small, and the maintenance cost is high. Only suitable for small-scale traffic, short-distance travel

3、自旋翼飞车设计,同时融合了汽车和摩托车的功能,将旋翼折叠后可以在公路上正常行驶。展开旋翼后,通过集体尾部的螺旋桨提供推力,使自旋翼旋转产生升力,需170m的滑跑起飞。它飞行速度快,对场地的需求低,它满足了人们日常对汽车和飞行的需求,有一定的实用性。但是不具有悬停能力,垂直起降功能。3. The design of the spin-wing flying car integrates the functions of cars and motorcycles at the same time. After the rotor is folded, it can drive normally on the road. After the rotor is deployed, thrust is provided by the propeller at the tail of the collective, so that the rotor rotates to generate lift, which requires a 170m run to take off. It flies fast and has low demand for venues. It meets people's daily needs for cars and flying, and has certain practicability. But it does not have hovering ability, vertical take-off and landing function.

此外,现有的飞行汽车,由于其设计与技术的局限性,不仅造价较高,能耗比大大增加,使用成本高,适众面小,大重量还不能满足复杂场景着陆的要求,更是在执行特定任务时,没有办法通过山地类乡间复杂地形,因而在涉及军事领域无法得到有效的应用。In addition, due to the limitations of its design and technology, the existing flying cars not only have high construction costs, greatly increase the energy consumption ratio, high use costs, small size and weight, but also cannot meet the requirements of landing in complex scenarios. When performing specific tasks, there is no way to pass through the mountainous and rural complex terrain, so it cannot be effectively applied in the military field.

发明内容SUMMARY OF THE INVENTION

现有的飞行汽车,由于其设计与技术的局限性,不仅造价较高,能耗比大大增加,使用成本高,适众面小,大重量,还不能满足复杂场景着陆的要求,更是在执行特定任务时,没有办法通过山地类乡间复杂地形,因而在涉及军事领域无法得到有效的应用。Due to the limitations of its design and technology, the existing flying cars not only have high construction costs, greatly increase the energy consumption ratio, high use costs, small size and heavy weight, but also cannot meet the requirements of landing in complex scenarios. When performing specific tasks, there is no way to pass through the complex terrain of mountainous and rural areas, so it cannot be effectively applied in the military field.

本发明的目的在于克服上述现有技术的缺陷,提出了一种具备形态智能的载人飞行汽车。所述飞行汽车采用一体化拓扑结构的飞行驾驶融合车架设计,主体飞行结构采用多旋翼式布局与四轴八螺旋桨的飞行器结构,地面驾驶结构采用阿克曼转向与麦弗逊悬挂减震形式的底盘结构;基于部署在飞行汽车上的激光位移传感器采集的信号进行判断,当地面行驶遇到拥堵时,飞行汽车启动飞行操作;当飞行操作结束后,飞行汽车实行降落操作,当降落操作结束后,飞行汽车启动地面驾驶操作。The purpose of the present invention is to overcome the above-mentioned defects of the prior art, and to propose a manned flying vehicle with morphological intelligence. The flying car adopts the integrated topological structure of the flight-driving fusion frame design, the main flight structure adopts a multi-rotor layout and a four-axis eight-propeller aircraft structure, and the ground driving structure adopts Ackerman steering and McPherson suspension shock absorption. The chassis structure of the flying car is based on the signal collected by the laser displacement sensor deployed on the flying car. When the ground travel encounters congestion, the flying car starts the flight operation; when the flight operation ends, the flying car performs the landing operation, and when the landing operation ends After that, the flying car starts the ground driving operation.

作为上述载人飞行汽车的一种改进,所述螺旋桨周围采用扇形可拓展防护涵道设计,包括通过滑轨连接的扇形可拓展防护涵道内圈和扇形可拓展防护涵道外圈,扇形可拓展防护涵道内圈位于扇形可拓展防护涵道外圈的内侧。As an improvement of the above manned flying vehicle, a fan-shaped expandable protective duct design is adopted around the propeller, including a fan-shaped expandable protective duct inner ring and a fan-shaped expandable protective duct outer ring connected by sliding rails, and the fan-shaped expandable protective duct is designed. The inner ring of the duct is located inside the outer ring of the fan-shaped expandable protective duct.

作为上述载人飞行汽车的一种改进,当所述飞行汽车启动飞行操作并上升至设定高度时,扇形可拓展防护涵道内圈旋转出扇形可拓展防护涵道外圈,用于保护螺旋桨不受他物的影响并提升螺旋桨的气动性能;As an improvement of the above manned flying car, when the flying car starts the flight operation and rises to the set height, the inner ring of the fan-shaped expandable protective duct rotates out of the outer ring of the fan-shaped expandable protective duct to protect the propeller from influence of other objects and improve the aerodynamic performance of the propeller;

当所述飞行汽车启动降落操作并下降至设定高度时,扇形可拓展防护涵道内圈旋转进入扇形可拓展防护涵道外圈,螺旋桨执行固定位置停桨操作,以缩短飞行汽车的横向尺寸,利于在单车道内行驶。When the flying car starts the landing operation and descends to the set height, the inner ring of the fan-shaped expandable protective duct rotates into the outer ring of the fan-shaped expandable protective duct, and the propeller performs a fixed position stop operation to shorten the lateral size of the flying car, which is beneficial to Drive in a single lane.

作为上述载人飞行汽车的一种改进,所述飞行驾驶融合车架使用碳纤维管作为框架,碳纤维管之间通过航空铝合金连接,底盘功能组件与覆盖件直接布置于车架上。As an improvement of the above-mentioned manned flying vehicle, the flying-driving fusion frame uses carbon fiber tubes as the frame, and the carbon fiber tubes are connected by aviation aluminum alloy, and the functional components of the chassis and the cover are directly arranged on the frame.

作为上述载人飞行汽车的一种改进,所述飞行驾驶融合车架包括副车架本体,所述副车架本体由麦弗逊悬挂减震形式的底盘上的碳纤维管与航空铝合金以销钉定位与螺栓抱死的方式连接。As an improvement of the above-mentioned manned flying vehicle, the flying-driving fusion frame includes a sub-frame body, and the sub-frame body is composed of carbon fiber tubes and aviation aluminum alloys on the chassis in the form of McPherson suspension and shock absorption with pins The positioning is connected with the way of bolt locking.

作为上述载人飞行汽车的一种改进,所述飞行驾驶融合车架包括车架本体,在所述车架本体的前下部采用三角加强筋碳纤维管连接链接点。As an improvement of the above-mentioned manned flying vehicle, the flying-driving fusion frame includes a frame body, and a triangular reinforcing rib carbon fiber tube is used to connect the link points at the front lower part of the frame body.

作为上述载人飞行汽车的一种改进所述八螺旋桨不设在同一个平面,前部螺旋桨位于车身前玻璃下位置,后部螺旋桨位于车身上位置。As an improvement of the above manned flying vehicle, the eight propellers are not arranged on the same plane, the front propeller is located under the front glass of the vehicle body, and the rear propeller is located on the vehicle body.

作为上述载人飞行汽车的一种改进,所述飞行汽车的电机动力源布局采用非正方形的平行异面中心对称结构。As an improvement of the above-mentioned manned flying car, the motor power source layout of the flying car adopts a non-square parallel and out-of-plane center-symmetric structure.

作为上述载人飞行汽车的一种改进,所述飞行汽车包括车顶窗、左右两侧的上车窗和下车窗,上述车窗均采用透明材料,例如优选但不限于透明材质亚克力板。As an improvement of the above-mentioned manned flying car, the flying car includes a roof window, an upper window and a lower window on the left and right sides, and the above windows are all made of transparent materials, such as preferably but not limited to transparent acrylic sheets.

与现有技术相比,本发明的优势在于:Compared with the prior art, the advantages of the present invention are:

1、本发明的飞行汽车针对复杂地形,包括但不限于城市路面和特殊路面情况,提供垂直起降四轴八桨的拓补融合设计,可以克服现有飞行汽车的难于陆空切换的问题;扇形可拓展防护涵道及固定位置停桨解决了横向尺寸过长导致无法正常上路的问题;1. The flying car of the present invention provides a topological fusion design of four axes and eight propellers for vertical take-off and landing for complex terrain, including but not limited to urban road surfaces and special road conditions, which can overcome the problem of difficult land-air switching of existing flying cars; The fan-shaped expandable protective duct and the fixed position of the paddle solve the problem that the horizontal dimension is too long and the road cannot be normally driven;

2、本发明飞行汽车的垂直起降功能以及在地面驾驶过程中能正常通过复杂路面,方便地面驾驶时驾驶员对周围环境的观察与安全驾驶,地面驾驶能够确保在正常铺装路面的单车道内行驶,不妨碍其他车辆的行驶;2. The vertical take-off and landing function of the flying car of the present invention and the fact that it can normally pass through complex roads during ground driving facilitates the driver's observation of the surrounding environment and safe driving during ground driving, and the ground driving can ensure that the vehicle is in a single lane with normal paved roads. drive without interfering with the movement of other vehicles;

3、本发明的飞行汽车造价低,自重轻,解决了传统飞行汽车设计的减重问题。3. The flying car of the present invention has low cost and light weight, and solves the weight reduction problem of traditional flying car design.

附图说明Description of drawings

图1是本发明的具备形态智能的载人飞行汽车主视图;1 is a front view of a manned flying vehicle with morphological intelligence according to the present invention;

图2是本发明的载人飞行汽车内部结构示意图。FIG. 2 is a schematic diagram of the internal structure of the manned flying vehicle of the present invention.

附图标记reference number

1、扇形可拓展防护涵道内圈 2、扇形可拓展防护涵道外圈1. Sector-shaped expandable protective duct inner ring 2. Sector-shaped expandable protective duct outer ring

3、电池箱 4、螺旋桨3. Battery box 4. Propeller

5、车门 6、驾驶座椅5. Doors 6. Driver's Seat

7、转向 8、底盘7. Steering 8. Chassis

9、左侧后上车窗 10、车门上方窗9. Left rear upper window 10. Upper door window

11、车顶窗 12、左侧前上车窗11. Roof window 12. Left front upper window

13、右前旋翼 14、左前旋翼13. Right front rotor 14. Left front rotor

15、右后旋翼 16、左后旋翼15. Right rear rotor 16. Left rear rotor

17、左侧下车窗 18、碳纤维管17. Left lower window 18. Carbon fiber tube

19、航空铝合金连接件 20、螺栓19. Aviation aluminum alloy connectors 20. Bolts

21、三角加强筋碳纤维管21. Triangular reinforced carbon fiber tube

具体实施方式Detailed ways

本发明以多旋翼常规布局为主,采用四轴八桨飞行器结构作为主体飞行结构,地面行驶以阿克曼转向与麦弗逊悬挂减震形式的底盘类型的拓补融合结构。为方便地面驾驶时驾驶员对周围环境的观察与安全驾驶,飞行的电机动力源布局采用非正方形的平行异面中心对称结构。螺旋桨周围采用扇形可拓展防护涵道的设计;地面行驶时采用固定位置停桨的方法缩短横向尺寸。The present invention is mainly based on the conventional layout of multi-rotors, adopts the structure of a four-axis eight-propeller aircraft as the main flight structure, and adopts a topological fusion structure of the chassis type in the form of Ackerman steering and McPherson suspension shock absorption for ground driving. In order to facilitate the driver's observation of the surrounding environment and safe driving when driving on the ground, the layout of the motor power source for the flight adopts a non-square parallel and out-of-plane center-symmetric structure. The fan-shaped expandable protective duct design is adopted around the propeller; the horizontal dimension is shortened by stopping the propeller at a fixed position when driving on the ground.

下面结合附图和实施例对本发明的技术方案进行详细的说明。The technical solutions of the present invention will be described in detail below with reference to the accompanying drawings and embodiments.

实施例Example

如图1所示,本发明的实施例提出了一种具备形态智能的载人飞行汽车。本发明主要是阐述形态智能的扇形可拓展防护涵道、定桨与拓扑融合车架结构,以智能形态解决了2种技术问题。As shown in FIG. 1 , an embodiment of the present invention proposes a manned flying vehicle with morphological intelligence. The invention mainly describes the fan-shaped expandable protective duct, fixed paddle and topology fusion frame structure with intelligent form, and solves two technical problems with intelligent form.

1、形态智能-扇形可拓展防护涵道1. Form intelligence - fan-shaped expandable protective duct

飞车应用了智能检测传感器,可以减少人为手动操控,增加自动化控制程度,从而提高操控方面的便利性。本发明基于激光位移传感器,根据前螺旋桨靠近、远离地面的动作特征判断距离地面的距离,以实现对螺旋桨进行扇形可拓展防护涵道相应的智能控制。当地面驾驶的飞行汽车遇到拥堵,实行飞行模式后,上升2米时,扇形可拓展防护涵道将从内道旋转出与之形成闭环,保护螺旋桨的同时提高气动性能。当飞行汽车飞行操作结束后,实行降落操作,当距离地面2米距离时,扇形可拓展防护涵道将旋转进入内道,以避免与道路上的其他车辆发生摩擦。The flying car uses intelligent detection sensors, which can reduce manual manual control and increase the degree of automatic control, thereby improving the convenience of control. Based on the laser displacement sensor, the invention judges the distance from the ground according to the action characteristics of the front propeller approaching and moving away from the ground, so as to realize the corresponding intelligent control of the fan-shaped expandable protective duct on the propeller. When the ground-driven flying car encounters congestion, after the flight mode is implemented, when it rises 2 meters, the fan-shaped expandable protective duct will rotate out of the inner channel to form a closed loop, which protects the propeller and improves the aerodynamic performance. After the flight operation of the flying car is completed, the landing operation is carried out. When the distance is 2 meters from the ground, the fan-shaped expandable protective duct will rotate into the inner lane to avoid friction with other vehicles on the road.

螺旋桨4周围采用扇形可拓展防护涵道设计;扇形可拓展防护涵道内圈1与扇形可拓展防护涵道外圈2通过滑轨进行连接,扇形可拓展防护涵道内圈1位于所述扇形可拓展防护涵道外圈2的内侧。The fan-shaped expandable protective duct design is adopted around the propeller 4; the fan-shaped expandable protective duct inner ring 1 and the fan-shaped expandable protective duct outer ring 2 are connected by sliding rails, and the fan-shaped expandable protective duct inner ring 1 is located in the fan-shaped expandable protective duct. The inner side of the ducted outer ring 2.

防护涵道的形态智能:The form intelligence of protective ducts:

当地面驾驶时扇形可拓展防护涵道内圈1旋转进入扇形可拓展防护涵道外圈2内,为提高地面通过性,实现缩短横向尺寸,能够确保地面行驶时在正常铺装路面的单车道内行驶,不妨碍其他车辆的行驶,旋转收纳后不仅降低运输难度,显著降低运输成本,还减小开模的尺寸,减低加工难度;当空中驾驶时,扇形可拓展防护涵道内圈1旋转出扇形可拓展防护涵道外圈2后,保护螺旋桨不受他物的影响外还能使螺旋桨产生更大的升力,提高气动性能。When driving on the ground, the inner ring 1 of the fan-shaped expandable protective duct rotates into the outer ring 2 of the fan-shaped expandable protective duct. In order to improve the ground passability and shorten the lateral dimension, it can ensure that the road can be driven in a single lane with normal pavement when driving on the ground. It does not hinder the driving of other vehicles. After being rotated and stored, it not only reduces the difficulty of transportation, but also significantly reduces the transportation cost, but also reduces the size of the mold opening and reduces the difficulty of processing; when driving in the air, the fan-shaped expandable protective duct inner ring 1 rotates out of the fan-shaped shape to expand After protecting the ducted outer ring 2, the propeller can be protected from the influence of other objects, and the propeller can also generate more lift and improve the aerodynamic performance.

2、形态智能-固定位置停桨2. Form intelligence - stop paddle at a fixed position

当地面行驶时,扇形可拓展防护涵道内圈1旋转进入扇形可拓展防护涵道外圈2内后,螺旋桨4将执行固定位置停桨的操作,为的是提高地面通过性,实现缩短横向尺寸,能够确保地面行驶时在正常铺装路面的单车道内行驶。When driving on the ground, after the inner ring 1 of the fan-shaped expandable protective duct rotates into the outer ring 2 of the fan-shaped expandable protective duct, the propeller 4 will perform the operation of stopping the propeller at a fixed position, in order to improve the ground passability and shorten the horizontal dimension. It can ensure that the road is driven in a single lane with normal pavement when driving on the ground.

3、形态智能-拓扑融合车架结构3. Form intelligence-topology fusion frame structure

图2是本发明的载人飞行汽车内部结构示意图。FIG. 2 is a schematic diagram of the internal structure of the manned flying vehicle of the present invention.

由于大型飞行器对结构强度与刚度要求较高,且对重量极其敏感,而传统车底盘为保证行驶舒适性与可靠性往往选用重量较高的设计。拓扑融合车架结构,使用主体碳纤维管与航空铝合金连接、局部铝合金或合金钢焊接的方案,原底盘功能组件与覆盖件等直接布置于车架上。前旋翼上置会遮挡驾驶者陆地驾驶与空中操控的视线,故下置;后旋翼下置会对陆地驾驶时影响驾驶者后视镜的观察视野,故上置。因此前旋翼位于下方后旋翼位于上方的设计产生。随着国家对节能减排要求的提高,如何应用先进的结构设计技术对车架进行结构设计,来实现车架的减重轻量化,从而满足国家日趋严厉的法规要求及提升升力,成为未来汽车厂生存的关键因素。Because large aircraft have high requirements on structural strength and rigidity, and are extremely sensitive to weight, traditional vehicle chassis often choose a design with higher weight to ensure driving comfort and reliability. Topological fusion of frame structure, using the main carbon fiber tube and aviation aluminum alloy connection, local aluminum alloy or alloy steel welding scheme, the original chassis functional components and cover parts are directly arranged on the frame. The upper position of the front rotor will block the driver's sight of land driving and air control, so it is placed at the bottom; the lower position of the rear rotor will affect the observation field of the driver's rearview mirror when driving on land, so it is placed at the top. Hence the design with the front rotor below and the rear rotor above. With the improvement of the country's requirements for energy saving and emission reduction, how to apply advanced structural design technology to the structural design of the frame to achieve weight reduction and light weight of the frame, so as to meet the increasingly stringent national regulations and improve lift, and become a future car key factor for plant survival.

为更好实现轻量化设计中的减重任务,本发明总体设计舍弃了传统汽车底盘与飞行框架,设计了新的飞行驾驶融合车架结构。新融合车架采用了一体化的拓扑结构,本发明以多旋翼常规布局为主,四轴八桨飞行器结构作为主体飞行结构,地面行驶以阿克曼转向7与麦弗逊悬挂减震形式的底盘8为主,使用主体碳纤维管与航空铝合金连接、局部铝合金或合金钢焊接的方案,车架使用碳纤维管作为框架,通过航空铝合金进行连接。原底盘功能组件与覆盖件等直接布置于车架上。此外,为方便地面驾驶时驾驶员对周围环境的观察与安全驾驶,飞行的电机动力源布局采用非正方形的平行异面中心对称结构。In order to better realize the weight reduction task in the lightweight design, the overall design of the present invention abandons the traditional automobile chassis and flight frame, and designs a new flight-driving integrated frame structure. The new fusion frame adopts an integrated topology structure. The present invention is based on the conventional multi-rotor layout, the four-axis eight-propeller aircraft structure is used as the main flight structure, and the ground driving is in the form of Ackerman steering 7 and McPherson suspension shock absorption. Chassis 8 is mainly used, using the main carbon fiber tube to connect with aviation aluminum alloy, and local aluminum alloy or alloy steel welding scheme. The frame uses carbon fiber tube as the frame, which is connected by aviation aluminum alloy. The original chassis functional components and cover parts are directly arranged on the frame. In addition, in order to facilitate the driver's observation of the surrounding environment and safe driving when driving on the ground, the layout of the flying motor power source adopts a non-square parallel and out-of-plane center-symmetric structure.

一种拓补融合车架结构,包括副车架本体,所述车架结构由麦弗逊悬挂减震形式的底盘8上的17根(可根据实际需要增减)碳纤维管18与航空铝合金19以销钉定位与螺栓20抱死的方式连接。还包括本体上的部分链接点连接形成稳定三角加强筋碳纤维管21结构,所述交叉加强筋结构设于车架本体前下部。所述车架本体的电机由电机支架支撑,与碳纤维管螺栓连接。所述车架考虑到地面驾驶与飞行时的视野安全,对四轴八桨的飞行汽车螺旋桨不设在同一个平面,而是前部螺旋桨下至与后部螺旋桨上至的设计。前部螺旋桨位考虑到驾驶者视野受限的原因,位于车身前玻璃下位置。后部则考虑到车身与后方来车碰撞的问题,位于车身上部位。A topological fusion frame structure, including a sub-frame body, the frame structure is composed of 17 carbon fiber tubes 18 (which can be increased or decreased according to actual needs) on a chassis 8 in the form of McPherson suspension and shock absorption, and aviation aluminum alloys. 19 is connected in such a way that the pin is positioned and the bolt 20 is locked. It also includes some link points on the body to form a stable triangular reinforcing rib carbon fiber tube 21 structure, and the cross reinforcing rib structure is arranged on the front lower part of the frame body. The motor of the frame body is supported by the motor bracket and connected with the carbon fiber tube bolts. The frame takes into account the safety of vision during ground driving and flight, and the propellers of the four-axis and eight-propeller flying car are not set on the same plane, but the front propeller is designed to go down and the rear propeller to go up. The front propeller position is located under the front glass of the body due to the limited visibility of the driver. The rear part is located on the upper part of the body in consideration of the collision between the body and the car coming from behind.

由于飞行汽车考虑飞行需求,车顶采用透明材质亚克力板车顶窗11;由于飞行需求车身侧面的车窗不限于上部分的左侧后上车窗9,左侧前上车窗12,在下部也做了透明材质亚克力板左侧下车窗的17和右侧下车窗(由于视角的原因,在图中未标注)设计,使驾驶体验更佳及安全性更高。Since the flying car considers the flight requirements, the roof adopts a transparent material acrylic panel roof window 11; due to the flight requirements, the side windows of the vehicle body are not limited to the left rear upper window 9 on the upper part, and the left front upper window 12, which is in the lower part. 17 of the left lower window and the right lower window (due to the angle of view, not marked in the picture) are also designed to make the driving experience better and safer.

本发明以多旋翼常规布局为主,采用四轴八桨飞行器结构作为主体飞行结构,地面行驶以阿克曼转向与麦弗逊悬挂减震形式的底盘类型的拓补融合结构。飞行的电机动力源布局采用非正方形的平行异面中心对称结构,螺旋桨周围采用扇形可拓展防护涵道及定桨的设计。The present invention is mainly based on the conventional layout of multi-rotors, adopts the structure of a four-axis eight-propeller aircraft as the main flight structure, and adopts a topological fusion structure of the chassis type in the form of Ackerman steering and McPherson suspension shock absorption for ground driving. The motor power source layout of the flight adopts a non-square parallel and out-of-plane center-symmetric structure, and a fan-shaped expandable protective duct and fixed propeller are used around the propeller.

针对扇形可拓展防护涵道,可以用外螺旋桨罩沿螺旋桨心折叠至内螺旋桨罩上部或者下部也可实现,但稳定性差。For the fan-shaped expandable protective duct, the outer propeller cover can be folded along the propeller core to the upper or lower part of the inner propeller cover, but the stability is poor.

定桨与车架部分,暂无替代方案。There is no alternative for the fixed paddle and frame part.

本发明的关键点:Key points of the present invention:

一种结合了扇形可拓展防护涵道与拓补融合车架、拥有固定停桨位的飞行汽车。为了飞行汽车地面形式和空中驾驶时可正常在单道行驶及道路上空行驶,为了减轻飞行汽车重量,为了驾驶员的安全舒适驾驶视野和感受的关键点与欲保护点为:A flying car that combines a fan-shaped expandable protective duct with a topological fusion frame and has a fixed paddle position. To reduce the weight of the flying car, the key points and the points to be protected for the driver's safety and comfortable driving vision and feeling are:

1、形态智能-扇形可拓展防护涵道:1. Form intelligence - fan-shaped expandable protective duct:

螺旋桨4周围采用扇形可拓展防护涵道设计;当地面驾驶时扇形可拓展防护涵道内圈1旋转进入扇形可拓展防护涵道外圈2内,为提高地面通过性,实现缩短横向尺寸,能够确保地面行驶时在正常铺装路面的单车道内行驶,不妨碍其他车辆的行驶,旋转收纳后不仅降低运输难度,显著降低运输成本,还减小开模的尺寸,减低加工难度;当空中驾驶时,扇形可拓展防护涵道内圈1旋转出扇形可拓展防护涵道外圈2后,保护螺旋桨不受他物的影响外还能使螺旋桨产生更大的升力,提高气动性能。The fan-shaped expandable protective duct design is adopted around the propeller 4; when driving on the ground, the fan-shaped expandable protective duct inner ring 1 rotates into the fan-shaped expandable protective duct outer ring 2, in order to improve the ground passability, shorten the lateral size, and ensure the ground When driving, it can drive in a single lane with normal pavement without hindering the driving of other vehicles. After being rotated and stored, it not only reduces the difficulty of transportation, but also significantly reduces the transportation cost, but also reduces the size of the mold opening and reduces the difficulty of processing; when driving in the air, the fan-shaped After the inner ring 1 of the expandable protective duct rotates out of a fan-shaped outer ring 2 of the expandable protective duct, it protects the propeller from being affected by other objects, and can also make the propeller generate more lift and improve aerodynamic performance.

2、形态智能-固定位置停桨:2. Form intelligence - stop the paddle at a fixed position:

当地面行驶时,扇形可拓展防护涵道内圈1旋转进入扇形可拓展防护涵道外圈2内后,螺旋桨4将执行固定位置停桨的操作,为的是提高地面通过性,实现缩短横向尺寸,能够确保地面行驶时在正常铺装路面的单车道内行驶。When driving on the ground, after the inner ring 1 of the fan-shaped expandable protective duct rotates into the outer ring 2 of the fan-shaped expandable protective duct, the propeller 4 will perform the operation of stopping the propeller at a fixed position, in order to improve the ground passability and shorten the horizontal dimension. It can ensure that the road is driven in a single lane with normal pavement when driving on the ground.

3、形态智能-拓扑融合车架结构:3. Form intelligence-topology fusion frame structure:

拓扑融合车架结构,由于大型飞行器对结构强度与刚度要求较高,且对重量极其敏感,而传统车底盘为保证行驶舒适性与可靠性往往选用重量较高的设计。为更好实现轻量化设计中的减重任务,本发明总体设计舍弃了传统汽车底盘与飞行框架,设计了新的飞行驾驶融合车架结构。新融合车架采用了一体化的拓扑结构,本发明以多旋翼常规布局为主,四轴八桨飞行器结构作为主体飞行结构,地面行驶以阿克曼转向7与麦弗逊悬挂减震形式的底盘8为主,使用主体碳纤维管与航空铝合金连接、局部铝合金或合金钢焊接的方案,原底盘功能组件与覆盖件等直接布置于车架上。此外,为方便地面驾驶时驾驶员对周围环境的观察与安全驾驶,飞行的电机动力源布局采用非正方形的平行异面中心对称结构。Topological fusion frame structure, because large aircrafts have high requirements on structural strength and stiffness, and are extremely sensitive to weight, while traditional vehicle chassis often choose a design with higher weight to ensure driving comfort and reliability. In order to better realize the weight reduction task in the lightweight design, the overall design of the present invention abandons the traditional automobile chassis and flight frame, and designs a new flight-driving integrated frame structure. The new fusion frame adopts an integrated topology structure. The present invention is based on the conventional multi-rotor layout, the four-axis eight-propeller aircraft structure is used as the main flight structure, and the ground driving is in the form of Ackerman steering 7 and McPherson suspension shock absorption. Chassis 8 is the main one. The main carbon fiber tube is connected with aviation aluminum alloy, and the local aluminum alloy or alloy steel is welded. The original chassis functional components and cover parts are directly arranged on the frame. In addition, in order to facilitate the driver's observation of the surrounding environment and safe driving when driving on the ground, the layout of the flying motor power source adopts a non-square parallel and out-of-plane center-symmetric structure.

最后所应说明的是,以上实施例仅用以说明本发明的技术方案而非限制。尽管参照实施例对本发明进行了详细说明,本领域的普通技术人员应当理解,对本发明的技术方案进行修改或者等同替换,都不脱离本发明技术方案的精神和范围,其均应涵盖在本发明的权利要求范围当中。Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and not to limit them. Although the present invention has been described in detail with reference to the embodiments, those of ordinary skill in the art should understand that any modification or equivalent replacement of the technical solutions of the present invention will not depart from the spirit and scope of the technical solutions of the present invention, and should be included in the present invention. within the scope of the claims.

Claims (9)

1.一种具备形态智能的载人飞行汽车,其特征在于,所述飞行汽车采用一体化拓扑结构的飞行驾驶融合车架设计,主体飞行结构采用多旋翼式布局与四轴八螺旋桨的飞行器结构,地面驾驶结构采用阿克曼转向与麦弗逊悬挂减震形式的底盘结构;基于部署在飞行汽车上的激光位移传感器采集的信号进行判断,当地面行驶遇到拥堵时,飞行汽车启动飞行操作;当飞行操作结束后,飞行汽车实行降落操作,当降落操作结束后,飞行汽车启动地面驾驶操作。1. a manned flying car with morphological intelligence, it is characterized in that, described flying car adopts the flying driving fusion frame design of integrated topology structure, and the main flight structure adopts the aircraft structure of multi-rotor type layout and four-axis eight-propeller , the ground driving structure adopts the chassis structure in the form of Ackerman steering and McPherson suspension shock absorption; based on the signals collected by the laser displacement sensor deployed on the flying car, the flying car will start the flight operation when the ground driving encounters congestion. ; When the flight operation ends, the flying car performs the landing operation, and when the landing operation ends, the flying car starts the ground driving operation. 2.根据权利要求1所述的具备形态智能的载人飞行汽车,其特征在于,所述螺旋桨周围采用扇形可拓展防护涵道设计,包括通过滑轨连接的扇形可拓展防护涵道内圈(1)和扇形可拓展防护涵道外圈(2),扇形可拓展防护涵道内圈(1)位于扇形可拓展防护涵道外圈(2)的内侧。2. The manned flying vehicle with morphological intelligence according to claim 1, wherein the fan-shaped expandable protective duct design is adopted around the propeller, including the fan-shaped expandable protective duct inner ring (1) connected by the slide rail. ) and a fan-shaped expandable protective duct outer ring (2), and the fan-shaped expandable protective duct inner ring (1) is located inside the fan-shaped expandable protective duct outer ring (2). 3.根据权利要求2所述的具备形态智能的载人飞行汽车,其特征在于,3. The manned flying vehicle with morphological intelligence according to claim 2, characterized in that, 当所述飞行汽车启动飞行操作并上升至设定高度时,扇形可拓展防护涵道内圈(1)旋转出扇形可拓展防护涵道外圈(2),用于保护螺旋桨(4)不受他物的影响并提升螺旋桨(4)的气动性能;When the flying car starts the flight operation and rises to the set height, the fan-shaped expandable protective duct inner ring (1) rotates out of the fan-shaped expandable protective duct outer ring (2) to protect the propeller (4) from other objects influence and improve the aerodynamic performance of the propeller (4); 当所述飞行汽车启动降落操作并下降至设定高度时,扇形可拓展防护涵道内圈(1)旋转进入扇形可拓展防护涵道外圈(2),螺旋桨(4)执行固定位置停桨操作,以缩短飞行汽车的横向尺寸,利于在单车道内行驶。When the flying car starts the landing operation and descends to the set height, the fan-shaped expandable protective duct inner ring (1) rotates into the fan-shaped expandable protective duct outer ring (2), and the propeller (4) performs a fixed position propeller stop operation, In order to shorten the lateral size of the flying car, it is conducive to driving in a single lane. 4.根据权利要求1所述的具备形态智能的载人飞行汽车,其特征在于,所述飞行驾驶融合车架使用碳纤维管作为框架,碳纤维管之间通过航空铝合金进行连接,底盘功能组件与覆盖件直接布置于车架上。4. The manned flying vehicle with morphological intelligence according to claim 1, wherein the air-driving fusion frame uses carbon fiber tubes as the frame, and the carbon fiber tubes are connected by an aviation aluminum alloy, and the chassis functional components are connected to the frame. The cover is arranged directly on the frame. 5.根据权利要求4所述的具备形态智能的载人飞行汽车,其特征在于,所述飞行驾驶融合车架包括副车架本体,所述副车架本体由麦弗逊悬挂减震形式的底盘(8)上的碳纤维管(18)与航空铝合金连接件(19)以销钉定位与螺栓(20)抱死的方式连接。5 . The manned flying vehicle with morphological intelligence according to claim 4 , wherein the flight-driving fusion frame comprises a sub-frame body, and the sub-frame body is suspended in the form of MacPherson shock absorption. 6 . The carbon fiber tube (18) on the chassis (8) is connected with the aviation aluminum alloy connecting piece (19) in the manner of pin positioning and locking of the bolt (20). 6.根据权利要求4所述的具备形态智能的载人飞行汽车,其特征在于,所述飞行驾驶融合车架包括车架本体,在所述车架本体的前下部采用三角加强筋碳纤维管(21)连接链接点。6. The manned flying vehicle with morphological intelligence according to claim 4, characterized in that, the flying-driving fusion frame comprises a frame body, and a triangular reinforcing rib carbon fiber tube ( 21) Connect the link points. 7.根据权利要求1所述的具备形态智能的载人飞行汽车,其特征在于,所述八螺旋桨不设在同一个平面,前部螺旋桨位于车身前玻璃下位置,后部螺旋桨位于车身上位置。7 . The manned flying vehicle with morphological intelligence according to claim 1 , wherein the eight propellers are not arranged on the same plane, the front propellers are located under the front glass of the vehicle body, and the rear propellers are located on the vehicle body. 8 . . 8.根据权利要求1所述的具备形态智能的载人飞行汽车,其特征在于,所述飞行汽车的电机动力源布局采用非正方形的平行异面中心对称结构。8 . The manned flying car with morphological intelligence according to claim 1 , wherein the motor power source layout of the flying car adopts a non-square parallel and out-of-plane center-symmetric structure. 9 . 9.根据权利要求1所述的具备形态智能的载人飞行汽车,其特征在于,所述飞行汽车包括车顶窗、左右两侧的上车窗和下车窗,上述车窗均采用透明材料。9 . The manned flying car with morphological intelligence according to claim 1 , wherein the flying car comprises a roof window, an upper window and a lower window on the left and right sides, and the above windows are all made of transparent materials. 10 . .
CN202210678769.3A 2022-06-15 2022-06-15 A manned flying car with morphological intelligence Pending CN114852331A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210678769.3A CN114852331A (en) 2022-06-15 2022-06-15 A manned flying car with morphological intelligence

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210678769.3A CN114852331A (en) 2022-06-15 2022-06-15 A manned flying car with morphological intelligence

Publications (1)

Publication Number Publication Date
CN114852331A true CN114852331A (en) 2022-08-05

Family

ID=82624099

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210678769.3A Pending CN114852331A (en) 2022-06-15 2022-06-15 A manned flying car with morphological intelligence

Country Status (1)

Country Link
CN (1) CN114852331A (en)

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050230524A1 (en) * 2003-10-24 2005-10-20 Toyota Jidosha Kabushiki Kaisha Vertical take-off and landing aircraft
CN102166930A (en) * 2011-03-29 2011-08-31 南京航空航天大学 Hovercar
CN106696620A (en) * 2017-01-20 2017-05-24 南昌航空大学 Novel single double ducted fan combined type hovercar
US20190061922A1 (en) * 2017-08-28 2019-02-28 Saudi Arabian Oil Company Thruster based locomotion for perched unmanned aerial vehicles
CN109677600A (en) * 2018-08-16 2019-04-26 深圳市格上格创新科技有限公司 A kind of shrinkable unmanned plane rotor protective device and unmanned plane
CN110488863A (en) * 2019-08-07 2019-11-22 清华大学 Air-ground amphibious unmanned platform
CN210149097U (en) * 2019-07-04 2020-03-17 长春工程学院 A land-air cross-domain emergency UAV
CN210881562U (en) * 2019-10-09 2020-06-30 酷黑科技(北京)有限公司 Foldable storage aerocar with storable duct
CN113442670A (en) * 2021-06-28 2021-09-28 中铁十二局集团有限公司 Novel tunnel engineering amphibious climbing detection robot
CN113682098A (en) * 2021-09-22 2021-11-23 天津工业大学 Air-ground hybrid mobile robot
CN114393965A (en) * 2022-02-25 2022-04-26 清华大学 A self-folding land-air amphibious multi-modal vehicle

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050230524A1 (en) * 2003-10-24 2005-10-20 Toyota Jidosha Kabushiki Kaisha Vertical take-off and landing aircraft
CN102166930A (en) * 2011-03-29 2011-08-31 南京航空航天大学 Hovercar
CN106696620A (en) * 2017-01-20 2017-05-24 南昌航空大学 Novel single double ducted fan combined type hovercar
US20190061922A1 (en) * 2017-08-28 2019-02-28 Saudi Arabian Oil Company Thruster based locomotion for perched unmanned aerial vehicles
CN109677600A (en) * 2018-08-16 2019-04-26 深圳市格上格创新科技有限公司 A kind of shrinkable unmanned plane rotor protective device and unmanned plane
CN210149097U (en) * 2019-07-04 2020-03-17 长春工程学院 A land-air cross-domain emergency UAV
CN110488863A (en) * 2019-08-07 2019-11-22 清华大学 Air-ground amphibious unmanned platform
CN210881562U (en) * 2019-10-09 2020-06-30 酷黑科技(北京)有限公司 Foldable storage aerocar with storable duct
CN113442670A (en) * 2021-06-28 2021-09-28 中铁十二局集团有限公司 Novel tunnel engineering amphibious climbing detection robot
CN113682098A (en) * 2021-09-22 2021-11-23 天津工业大学 Air-ground hybrid mobile robot
CN114393965A (en) * 2022-02-25 2022-04-26 清华大学 A self-folding land-air amphibious multi-modal vehicle

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
张新钰等: "基于深度学习的自动驾驶技术综述", 《清华大学学报(自然科学版)》 *
杨征宇,陈茹雯,陈伟: "《汽车车身结构数字化开发技术》", 30 November 2014, 国防工业出版社 *
陈新亚: "《视频图解汽车构造与原理》", 30 September 2020, 机械工业出版社 *

Similar Documents

Publication Publication Date Title
US9815345B2 (en) Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself
US7938358B2 (en) Roadable aircraft with folding wings and integrated bumpers and lighting
US8267347B2 (en) Winging car
US8371520B2 (en) Rapidly convertible hybrid aircraft and manufacturing method
US5836541A (en) Easily-convertible fixed-wing roadable aircraft
CN103770589B (en) Hovercar
CN103522858A (en) a flying car
CN105730168B (en) Three culvert vertical take-off and landing hovercars
CN105922830B (en) Flight electric car
CN119428029A (en) Helicopter flying car
CN114852331A (en) A manned flying car with morphological intelligence
CN2467345Y (en) Flying vehicle
CN115091905B (en) An electric flying car
CN111469618A (en) Air and land dual-use flying car and method of use
RU143819U1 (en) VEHICLE AND LAND VEHICLE VEHICLE
CN118578821A (en) 3-point wheeled power chassis-folding wings-double tail struts-4+1 propeller flying car layout
RU2576071C2 (en) Configuration of vehicle for motion in air and on ground and device to this end
CN113212751A (en) Air-ground dual-purpose aircraft
CN119190350A (en) A modular vehicle with multiple take-off modes
CN116834487A (en) Vertical take-off and landing suspension movable wing tilting flying electric automobile, take-off and landing method and lifting steering method
NZ622189B2 (en) Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20220805

RJ01 Rejection of invention patent application after publication