[go: up one dir, main page]

WO2018196041A1 - 一种飞行摩托 - Google Patents

一种飞行摩托 Download PDF

Info

Publication number
WO2018196041A1
WO2018196041A1 PCT/CN2017/083963 CN2017083963W WO2018196041A1 WO 2018196041 A1 WO2018196041 A1 WO 2018196041A1 CN 2017083963 W CN2017083963 W CN 2017083963W WO 2018196041 A1 WO2018196041 A1 WO 2018196041A1
Authority
WO
WIPO (PCT)
Prior art keywords
rotor
seat
frame
engine
gearbox
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.)
Ceased
Application number
PCT/CN2017/083963
Other languages
English (en)
French (fr)
Inventor
陶亮
申守建
李文明
陈登科
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.)
Sun Hawk(henan) Aviation Industry Co Ltd
Original Assignee
Sun Hawk(henan) Aviation Industry Co Ltd
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 Sun Hawk(henan) Aviation Industry Co Ltd filed Critical Sun Hawk(henan) Aviation Industry Co Ltd
Publication of WO2018196041A1 publication Critical patent/WO2018196041A1/zh
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft

Definitions

  • the invention relates to the technical field of motorcycles, in particular to a flying motorcycle.
  • the object of the present invention is to provide a flying motorcycle, which solves the problem of the control of the flying motorcycle and the problem of the voyage, and makes the flying motorcycle truly reach the practical level, which is a leap-forward development of the history of the human aircraft.
  • a flying motorcycle comprising a frame and an engine mounted in the middle of the rack; the top and the bottom of the rack are respectively provided with a seat and a landing gear, and the seat passes through the seat
  • the chair damper is fixedly connected to the frame; the back of the seat is equipped with a catapult rescue umbrella, and the two sides of the seat are respectively equipped with a pitch roll joystick and a throttle stick; the position of the foot under the seat a heading bar is provided;
  • a gear box is mounted on both ends of the frame, and a retainer bracket is mounted on the top of the gear box, and a top of the retainer bracket is fixedly connected with the rotor retainer;
  • the gear box is internally mounted a pair of helical bevel teeth, and a transverse input shaft inside the gearbox is coupled to one end of the drive shaft through a coupling; the other end of the drive shaft is coupled to a power take-off shaft of the engine via a coupling; the pair of spiral
  • the lower part of the seat is equipped with a servo electronic flight controller, and the electronic flight controller of the steering gear is electrically connected to the rudder, and the three-axis gyro is mounted on the electronic flight controller of the steering gear. instrument.
  • an engine damper is installed between the engine and the frame.
  • the number of pieces of the rotor blade is 2-6 pieces, and the rotor pieces are evenly mounted on the rotor head.
  • the utility model has the beneficial effects that: the flying motorcycle of the invention, the power unit is powered by an aero-engine, and the transmission shaft axial direction front and rear two gear boxes are simultaneously outputted through a reduction gear box (the power can also be passed).
  • the engine crankshaft is directly output to the gearbox by the transmission shaft.
  • the gearbox is composed of a pair of spiral bevel gears.
  • the function of the gearbox is to change the power output direction from the front-rear direction to the upward output, and also has the function of the reduction gear box.
  • the output shaft of the box is mounted with a variable pitch rotor.
  • the number of rotors may be more than two pieces according to design requirements, generally no more than six pieces, and the upward lifting force is provided by the rotation of the two sets of front and rear rotors to fly the flying motorcycle off the ground;
  • the flying motorcycle has solved the problem of control of the flying motorcycle and the problem of navigation time, so that the flying motorcycle can truly reach the practical level, which is a leap-forward development of the history of human aircraft.
  • Figure 1 is a schematic view of the overall structure of the present invention
  • Figure 2 is a plan view of the present invention
  • Figure 3 is a schematic structural view of a gear box of the present invention.
  • a flying motorcycle comprising a frame 1 and an engine 2 mounted in the middle of the frame 1.
  • the frame 1 is made of metal pipe welding, and may also be lighter.
  • the material is made of a composite material such as carbon fiber;
  • the top and bottom of the frame 1 are respectively provided with a seat 3 and a landing gear 4, and the seat 3 is fixedly connected to the frame 1 through the seat damper 5;
  • the back of the 3 is mounted with a catapult 6 and the two sides of the seat 3 are respectively mounted with a pitch roll lever 7 and a throttle lever 8; a position of the foot below the seat 3 is provided with a heading pedal 9;
  • a gearbox 10 is mounted on both ends of the frame 1, and a retainer bracket 11 is mounted on the top of the gearbox 10, and a top of the retainer bracket 11 is fixedly coupled to the rotor retainer 12;
  • the gearbox 10 is internally mounted There is a pair of spiral bevel teeth 13, and the transverse input shaft 14 inside the gearbox 10 is connected to one end of the
  • the disk 20, and the first inclined rotor 21 at the upper portion of the swash plate 20 is fixedly coupled to the rotor blade 19 via the first link 22; the second inclined rotor 23 at the lower portion of the swash plate 20 is fixed to the steering gear 25 via the second link 24.
  • a lower portion of the seat 3 is mounted with a steering electronic flight controller 26, and the steering electronic flight controller 26 is electrically connected to the steering gear 25, and a three-axis gyroscope is mounted on the steering electronic flight controller 26;
  • An engine damper 27 is mounted between the frame 1 and the rotor blade 19 is mounted in a number of 2-6 pieces, and the rotor blades 19 are evenly mounted on the rotor head 18 at equal intervals.
  • the flying motorcycle of the invention adopts the combination of the control principle of the helicopter rotor and the flight control of the drone gyroscope, and the specific practices are as follows:
  • the rotor blade 19 of 18 is determined by the spacing of the blades, and a swash plate 20 for controlling the pitch is disposed under each set of the rotor mounting shafts.
  • the first inclined rotor 21 at the upper portion of the swash plate 20 passes through the first link 22 and each piece.
  • the rotor blades 19 are connected. When the swash plate 20 slides up and down, the rotor blade 19 of the rotor head 18 is correspondingly enlarged or smaller.
  • the swash plate 20 is composed of a first inclined rotor 21 and a second inclined rotor 23,
  • the intermediate shaft is connected by a bearing, the first inclined rotor 21 rotates with the rotor head 18, and the second inclined rotor 23 is connected to three steering gears 25 distributed at an angle of 120 degrees.
  • the steering gear 25 is an actuator for controlling the flight attitude, and is controlled by electronic flight.
  • the electronic flight controller 26 is designed with a three-axis gyroscope and an accelerometer, and other arithmetic circuits for controlling the attitude balance of the flying motorcycle.
  • the electronic flight controller 26 receives the pilot's joystick command. And control the steering gear to perform the action.
  • the second tilting rotor 23 does not rotate with the rotor, but the tilting angle can be sent by the pilot to the electronic flight controller 26 via the joystick, and the electronic flight controller 26 controls the second tilting rotor 23 through the steering gear 25 to control the tilt angle of the rotor surface.
  • the second inclined rotor 23 can be low or high, and can be left low and right high, or deflected in any direction, which allows the rotor surface to tilt in any direction, which changes the angle of the rotor during each rotation cycle.
  • the line controller 26 can achieve the purpose of complete synchronous control of the two sets of rotors before and after, but the two sets of front and rear rotors can only control the flight before and after the flight, and can not carry out the heading control. To achieve the heading control, it is necessary to control the airfoil of the front and rear rotors simultaneously. The two sides are inclined in opposite directions. In order to quickly and conveniently grasp the flying skills of the flying motorcycle, the heading control design is controlled by the heading mast 9, so that the whole flying motorcycle is handled in a similar manner to the traditional helicopter, making learning and driving easier.
  • the invention uses the electronic flight controller 26 to participate in the control of the flight attitude.
  • the electronic flight controller 26 is internally equipped with a three-axis gyroscope, the stability of the flight motorcycle is controlled by a three-axis gyroscope, which makes driving very simple and does not require precise With the skill and skill, the driver only needs to give the altitude and heading instructions.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)

Abstract

一种飞行摩托，包括机架(1)和安装于机架(1)中部的发动机(2)；其特征在于：所述机架(1)顶部和底部分别设置有座椅(3)和起落架(4)，且座椅(3)通过座椅减震器(5)与机架(1)固定连接；所述座椅(3)的背面安装有弹射救生伞(6)，且座椅(3)的两侧分别安装有俯仰横滚操纵杆和油门操纵杆；所述座椅(3)下方脚踏的位置设置有航向脚蹬杆(9)；所述机架(1)的两端均安装有齿轮箱(10)，且齿轮箱(10)的顶部安装有护圈支架(11)，且护圈支架(11)的顶部与旋翼护圈(12)固定连接；所述齿轮箱(10)内部安装有一对螺旋伞齿，且齿轮箱(10)内部的横向输入轴通过联轴器与传动轴的一端连接。该飞行摩托，很好的解决了飞行摩托的控制问题以及航时问题。

Description

一种飞行摩托 技术领域
本发明涉及摩托车技术领域，具体为一种飞行摩托。
背景技术
飞行摩托是人类单人飞行器的终极梦想，遗憾的是迄今为止世界上还没有一款可以使用的飞行摩托，基本停留在概念型和设想中，多见于很多科幻电影里，在美国、澳大利亚、英国、俄罗斯等地也有人做过初步尝试，还有但都因为无法有效控制或动力电池航时太短而停留在研发层面，但由于飞行摩托的实用性，使人类不愿放弃对它的研发进程。
发明内容
本发明的目的在于提供一种飞行摩托，很好的解决了飞行摩托的控制问题以及航时问题，使飞行摩托真正达到实用级别，是人类飞行器历史得到跨越式发展。
为实现上述目的，本发明提供如下技术方案：一种飞行摩托，包括机架和安装于机架中部的发动机；所述机架顶部和底部分别设置有座椅和起落架，且座椅通过座椅减震器与机架固定连接；所述座椅的背面安装有弹射救生伞，且座椅的两侧分别安装有俯仰横滚操纵杆和油门操纵杆；所述座椅下方脚踏的位置设置有航向脚蹬杆；所述机架的两端均安装有齿轮箱，且齿轮箱的顶部安装有护圈支架，且护圈支架的顶部与旋翼护圈固定连接；所述齿轮箱内部安装有一对螺旋伞齿，且齿轮箱内部的横向输入轴通过联轴器与传动轴的一端连接；所述传动轴的另一端通过联轴器与发动机的动力输出轴连接；所述一对螺旋伞齿的中部贯穿有输出主轴，且输出主轴的顶端通过浆毂与设置在旋翼护圈内的旋翼头固定连接；所述旋翼头上安装有旋翼片；所述输出主轴上且位于旋翼头的下方安装有倾斜盘，且倾斜盘上部的第一倾斜转子通过第一连杆与旋翼片固定连接；所述倾斜盘下部的第二倾斜转子通过第二连杆 与舵机固定连接。
作为本发明的一种优选技术方案，所述座椅的下部安装有舵机电子飞行控制器，且舵机电子飞行控制器与舵机电性连接，且舵机电子飞行控制器上安装有三轴陀螺仪。
作为本发明的一种优选技术方案，所述发动机与机架之间安装有发动机减震器。
作为本发明的一种优选技术方案，所述旋翼片安装的片数为2-6片，且旋翼片等距均匀安装在旋翼头上。
有益效果
与现有技术相比，本发明的有益效果是：本发明飞行摩托，动力单元采用一台航空发动机提供动力，通过一个减速箱用传动轴向前后两组齿轮箱同时输出动(动力也可以通过发动机曲轴用传动轴直接输出至齿轮箱)，齿轮箱是由一对螺旋伞齿构成，其作用是将动力输出方向由前后方向改变为向上输出，同时也具备减速箱功能，在前后两个齿轮箱向上的输出轴上安装有可变浆距的旋翼，旋翼的数量根据设计要求可以是二片以上，一般不超过六片，通过前后两组旋翼旋转提供向上的升力使飞行摩托飞离地面；该飞行摩托，很好的解决了飞行摩托的控制问题以及航时问题，使飞行摩托真正达到实用级别，是人类飞行器历史得到跨越式发展。
附图说明
图1为本发明的整体结构示意图；
图2为本发明的俯视图；
图3为本发明的齿轮箱结构示意图；
图中：1-机架、2-发动机、3-座椅、4-起落架、5-座椅减震器、6-弹射救生伞、7-俯仰横滚操纵杆、8-油门操纵杆、9-航向脚蹬杆、10-齿轮箱、11-护圈支架、12-旋翼护圈、13-一对螺旋伞齿、14-横向输入轴、15-传动轴、 16-输出主轴、17-浆毂、18-旋翼头、19-旋翼片、20-倾斜盘、21-第一倾斜转子、22-第一连杆、23-第二倾斜转子、24-第二连杆、25-舵机、26-电子飞行控制器、27-发动机减震器。
具体实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。
请参阅图1-3本发明提供的一种实施例：一种飞行摩托，包括机架1和安装于机架1中部的发动机2，机架1由金属管材焊接制成，也可以由其他轻质材料如碳纤维等复合材料制造；所述机架1顶部和底部分别设置有座椅3和起落架4，且座椅3通过座椅减震器5与机架1固定连接；所述座椅3的背面安装有弹射救生伞6，且座椅3的两侧分别安装有俯仰横滚操纵杆7和油门操纵杆8；所述座椅3下方脚踏的位置设置有航向脚蹬杆9；所述机架1的两端均安装有齿轮箱10，且齿轮箱10的顶部安装有护圈支架11，且护圈支架11的顶部与旋翼护圈12固定连接；所述齿轮箱10内部安装有一对螺旋伞齿13，且齿轮箱10内部的横向输入轴14通过联轴器与传动轴15的一端连接；所述传动轴15的另一端通过联轴器与发动机2的动力输出轴连接；所述一对螺旋伞齿13的中部贯穿有输出主轴16，且输出主轴16的顶端通过浆毂17与设置在旋翼护圈12内的旋翼头18固定连接；所述旋翼头18上安装有旋翼片19；所述输出主轴16上且位于旋翼头18的下方安装有倾斜盘20，且倾斜盘20上部的第一倾斜转子21通过第一连杆22与旋翼片19固定连接；所述倾斜盘20下部的第二倾斜转子23通过第二连杆24与舵机25固定连接；所述座椅3的下部安装有舵机电子飞行控制器26，且舵机电子飞行控制器26与舵机25电性连接，且舵机电子飞行控制器26上安装有三轴陀螺仪；所述发动机2 与机架1之间安装有发动机减震器27；所述旋翼片19安装的片数为2-6片，且旋翼片19等距均匀安装在旋翼头18上。
本发明飞行摩托采用了直升机旋翼的控制原理与无人机陀螺仪飞行控制相结合的办法完成，具体做法如下：
两组旋翼头18水平旋转时，自然产生向上的升力，这是飞行摩托得以垂直起降和悬停的基本条件，但是如何保证两组旋翼头18升力的平衡成为关键，由于升力是由旋翼头18的旋翼片19片距决定的，在每组旋翼安装轴的下方设置有一个可以控制浆距的倾斜盘20，倾斜盘20上部的第一倾斜转子21通过有第一连杆22与每片旋翼片19相连，当倾斜盘20上下滑动时旋翼头18的旋翼片19片距会相应的变大或者变小，倾斜盘20是由第一倾斜转子21和第二倾斜转子23两部分组成，中间用轴承相连，第一倾斜转子21随旋翼头18旋转，第二倾斜转子23与三个呈120度角分布的舵机25相连，舵机25是控制飞行姿态的执行机构，由电子飞行控制器26，电子飞行控制器26内设计有三轴陀螺仪和加速度计，及其他运算电路，用来控制飞行摩托的姿态平衡，电子飞行控制器26接收飞行员操纵杆的指令并控制舵机进行动作。
当旋翼头18旋转产生的翼面向前倾斜，自然就在产生升力的同时，产生前行的推力，第一倾斜转子21紧贴第二倾斜转子23转动，其倾斜角度由第二倾斜转子23决定，第一倾斜转子21随旋翼转动，由于前低后高，第一连杆22和支点的作用迫使旋翼上升下降，最后按斜盘的角度旋转，达到旋翼面倾斜旋转的目的。第二倾斜转子23不随旋翼转动，但倾斜角度可以由飞行员通过操纵杆发送指令给电子飞行控制器26，电子飞行控制器26通过舵机25控制第二倾斜转子23而达到控制旋翼面倾斜角度的目的。第二倾斜转子23不光可以前低后高，还可以左低右高，或向任意方向偏转，这就使得旋翼面可以向任意方向倾斜，这个改变旋翼在每个旋转周期内角度的控制称周期距控制，用来控制行进方向和飞行摩托的姿态，由于该控制系统引入了电子飞 行控制器26，才能达到前后两组旋翼完全同步控制的目的，但是前后两组旋翼同步只能控制飞行摩托前后左右飞行，不能进行航向控制，实现航向控制就需要控制前后旋翼的翼面同时向两侧相反方向倾斜，为了能快速方便的掌握飞行摩托的飞行技巧，航向控制设计采用航向脚蹬杆9进行控制，这样整个飞行摩托的操控方式和传统直升机非常类似，使学习驾驶更加容易，另外本发明使用了电子飞行控制器26参与飞行姿态的控制，由于电子飞行控制器26内部安装有三轴陀螺仪，飞行摩托的稳定性由三轴陀螺仪控制，使得驾驶变的非常简单，无需精确的操作和娴熟的技巧，驾驶者只需要给出高度和航向指令即可。
需要说明的是，在本文中，诸如第一和第二等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来，而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。而且，术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含，从而使得包括一系列要素的过程、方法、物品或者设备不仅包括那些要素，而且还包括没有明确列出的其他要素，或者是还包括为这种过程、方法、物品或者设备所固有的要素。在没有更多限制的情况下。由语句“包括一个......限定的要素，并不排除在包括所述要素的过程、方法、物品或者设备中还存在另外的相同要素”。
尽管已经示出和描述了本发明的实施例，对于本领域的普通技术人员而言，可以理解在不脱离本发明的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型，本发明的范围由所附权利要求及其等同物限定。

Claims (4)

  1. 一种飞行摩托，包括机架(1)和安装于机架(1)中部的发动机(2)；其特征在于：所述机架(1)顶部和底部分别设置有座椅(3)和起落架(4)，且座椅(3)通过座椅减震器(5)与机架(1)固定连接；所述座椅(3)的背面安装有弹射救生伞(6)，且座椅(3)的两侧分别安装有俯仰横滚操纵杆(7)和油门操纵杆(8)；所述座椅(3)下方脚踏的位置设置有航向脚蹬杆(9)；所述机架(1)的两端均安装有齿轮箱(10)，且齿轮箱(10)的顶部安装有护圈支架(11)，且护圈支架(11)的顶部与旋翼护圈(12)固定连接；所述齿轮箱(10)内部安装有一对螺旋伞齿(13)，且齿轮箱(10)内部的横向输入轴(14)通过联轴器与传动轴(15)的一端连接；所述传动轴(15)的另一端通过联轴器与发动机(2)的动力输出轴连接；所述一对螺旋伞齿(13)的中部贯穿有输出主轴(16)，且输出主轴(16)的顶端通过浆毂(17)与设置在旋翼护圈(12)内的旋翼头(18)固定连接；所述旋翼头(18)上安装有旋翼片(19)；所述输出主轴(16)上且位于旋翼头(18)的下方安装有倾斜盘(20)，且倾斜盘(20)上部的第一倾斜转子(21)通过第一连杆(22)与旋翼片(19)固定连接；所述倾斜盘(20)下部的第二倾斜转子(23)通过第二连杆(24)与舵机(25)固定连接。
  2. 根据权利要求1所述的一种飞行摩托，其特征在于：所述座椅(3)的下部安装有舵机电子飞行控制器(26)，且舵机电子飞行控制器(26)与舵机(25)电性连接，且舵机电子飞行控制器(26)上安装有三轴陀螺仪。
  3. 根据权利要求1所述的一种飞行摩托，其特征在于：所述发动机(2)与机架(1)之间安装有发动机减震器(27)。
  4. 根据权利要求1所述的一种飞行摩托，其特征在于：所述旋翼片(19)安装的片数为2-6片，且旋翼片(19)等距均匀安装在旋翼头(18)上。
PCT/CN2017/083963 2017-04-26 2017-05-11 一种飞行摩托 Ceased WO2018196041A1 (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201710283348.XA CN106904055A (zh) 2017-04-26 2017-04-26 一种飞行摩托
CN201710283348.X 2017-04-26

Publications (1)

Publication Number Publication Date
WO2018196041A1 true WO2018196041A1 (zh) 2018-11-01

Family

ID=59211240

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/083963 Ceased WO2018196041A1 (zh) 2017-04-26 2017-05-11 一种飞行摩托

Country Status (2)

Country Link
CN (1) CN106904055A (zh)
WO (1) WO2018196041A1 (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12221210B2 (en) 2021-10-25 2025-02-11 Levanta Tech Inc. Wing-in-ground effect vehicles and uses thereof

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108639320A (zh) * 2018-06-05 2018-10-12 河南三和航空工业有限公司 一种双旋翼无人直升机
CN113752765A (zh) * 2021-09-17 2021-12-07 熊辉 一种水陆空摩托车

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060208133A1 (en) * 2005-03-18 2006-09-21 Ligo Kenneth A Personal aircraft vehicle
CN101885295A (zh) * 2010-07-19 2010-11-17 杨朝习 陆空两用飞行器
CN104773290A (zh) * 2015-03-19 2015-07-15 南京航空航天大学 双涵道共轴多旋翼飞行摩托
CN204688413U (zh) * 2015-05-01 2015-10-07 张绍臣 直升机倾斜盘左右不对称球头夹
CN205468356U (zh) * 2016-04-05 2016-08-17 江苏数字鹰科技发展有限公司 一种具有座舱稳定系统的多旋翼飞行汽车或飞行摩托
WO2016142555A1 (es) * 2015-03-12 2016-09-15 Martinez Gil Francisco Motocicleta voladora

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204623828U (zh) * 2015-03-19 2015-09-09 南京航空航天大学 双涵道共轴多旋翼飞行摩托
CN205221109U (zh) * 2015-08-21 2016-05-11 河南三和航空工业有限公司 多轴载人飞行器
CN206664180U (zh) * 2017-04-26 2017-11-24 河南三和航空工业有限公司 一种飞行摩托

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060208133A1 (en) * 2005-03-18 2006-09-21 Ligo Kenneth A Personal aircraft vehicle
CN101885295A (zh) * 2010-07-19 2010-11-17 杨朝习 陆空两用飞行器
WO2016142555A1 (es) * 2015-03-12 2016-09-15 Martinez Gil Francisco Motocicleta voladora
CN104773290A (zh) * 2015-03-19 2015-07-15 南京航空航天大学 双涵道共轴多旋翼飞行摩托
CN204688413U (zh) * 2015-05-01 2015-10-07 张绍臣 直升机倾斜盘左右不对称球头夹
CN205468356U (zh) * 2016-04-05 2016-08-17 江苏数字鹰科技发展有限公司 一种具有座舱稳定系统的多旋翼飞行汽车或飞行摩托

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12221210B2 (en) 2021-10-25 2025-02-11 Levanta Tech Inc. Wing-in-ground effect vehicles and uses thereof

Also Published As

Publication number Publication date
CN106904055A (zh) 2017-06-30

Similar Documents

Publication Publication Date Title
CN110316370B (zh) 一种分布式动力倾转机翼飞机的布局与控制方法
US10464671B2 (en) Personal flight vehicle
US8727266B2 (en) Flying machine comprising twin contra-rotating vertical axis propellers
US10414484B2 (en) Aircraft
CN102107733B (zh) 仿生飞行器
CN113753229B (zh) 一种可折叠式固定翼四旋翼复合无人机及其控制方法
US7178757B1 (en) Motorcycle rider autogyro
CN103979105B (zh) 一种垂直起降可变翼飞行器
CN101108654B (zh) 双涵道单人垂直起降飞行器
CN106428540B (zh) 一种组合涵道飞行器及其飞行控制系统和方法
CN102211663B (zh) 齿轮倾转式共轴机
JP2022530223A (ja) 垂直離着陸航空機、および関連する制御方法
CN102730192B (zh) 一种可垂直起降的飞行器
WO2018196041A1 (zh) 一种飞行摩托
US2108093A (en) Aircraft
GB2419122A (en) Vertical take-off and landing aircraft
CN104590535A (zh) 一种用于飞艇动力装置的推进装置
CN114560083A (zh) 一种仿蜂鸟式直升飞行器及其飞行方法
CN208484828U (zh) 一种能垂直起降的固定翼飞行器
RU146302U1 (ru) Скоростной комбинированный вертолет
CN102390531A (zh) 一种涵道、机翼组合型微型飞行器
RU2480378C1 (ru) Летательный аппарат
CN104627360A (zh) H型结构的直升机
CN109080824A (zh) 一种带倾转螺旋桨的固定翼飞行器
CN202481307U (zh) 四螺旋桨垂直起降飞机

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 17906825

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 17906825

Country of ref document: EP

Kind code of ref document: A1