WO2022134450A1 - 一种空中电磁飞车 - Google Patents

一种空中电磁飞车 Download PDF

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Publication number
WO2022134450A1
WO2022134450A1 PCT/CN2021/095466 CN2021095466W WO2022134450A1 WO 2022134450 A1 WO2022134450 A1 WO 2022134450A1 CN 2021095466 W CN2021095466 W CN 2021095466W WO 2022134450 A1 WO2022134450 A1 WO 2022134450A1
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vehicle body
vehicle
flying
compressed air
air pump
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PCT/CN2021/095466
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English (en)
French (fr)
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仝泽耀
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仝泽耀
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Priority to US17/635,007 priority Critical patent/US20230339520A1/en
Publication of WO2022134450A1 publication Critical patent/WO2022134450A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B3/00—Elevated railway systems with suspended vehicles
    • B61B3/02—Elevated railway systems with suspended vehicles with self-propelled vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L13/00—Electric propulsion for monorail vehicles, suspension vehicles or rack railways; Magnetic suspension or levitation for vehicles
    • B60L13/04—Magnetic suspension or levitation for vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B12/00—Component parts, details or accessories not provided for in groups B61B7/00 - B61B11/00
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B13/00—Other railway systems
    • B61B13/10—Tunnel systems
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02N—ELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR
    • H02N15/00—Holding or levitation devices using magnetic attraction or repulsion, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/26—Rail vehicles

Definitions

  • the invention relates to the technical field of rail transportation, in particular to an aerial electromagnetic flying car.
  • the technical problem to be solved by the present invention is to overcome the defect of the above-mentioned technology, and provide:
  • An aerial electromagnetic flying vehicle comprising a flying vehicle and a track system
  • the flying car includes a car body, a magnet, a solenoid, a compressed air pump, an air intake pipe, an air outlet and a braking device, the magnets are four and are respectively arranged at the end points of the flying car, and the solenoid has four corresponding sleeved on the magnet, the compressed air pump is arranged in the vehicle body; one end of the air intake pipe is connected with the compressed air pump, and the other end penetrates the vehicle body and communicates with the outside; the air outlet pipe One end is connected with the compressed air pump, and the other end penetrates the vehicle body and communicates with the outside; the braking device is arranged on the vehicle body;
  • the rail system includes a rail, a rubber rail, and a support plate; the rail is arranged above the vehicle body, and cooperates with the magnet; the rubber rail is arranged at the lower end of the rail, and is connected with the The braking devices cooperate with each other, and the support plate is arranged on the lower end of the rubber track.
  • the intake pipe has two branch pipes, which respectively penetrate the vehicle body from the front end and the top end of the vehicle body and are connected with the compressed air pump.
  • the braking device is rotatably connected with the vehicle body, and the braking device is retractable.
  • the end of the braking device is provided with a rubber pad
  • the rubber track is provided with a rubber groove
  • the rubber pad cooperates with the rubber groove
  • a distance sensor is provided at a position of the vehicle body close to the rail system, for judging the distance between the vehicle body and the rail system.
  • a gyroscope is provided at the center of gravity of the flying vehicle for judging the balance state of the flying vehicle.
  • the flying car and the track system are arranged in a circular tube-type tunnel to reduce the influence of wind.
  • the present invention has the advantages that: the electromagnetic flying vehicle is in a non-contact air flight state, and it is not subject to other external resistances except for the resistance of the air. Compared with vehicles such as cars, the external resistance is smaller, the energy utilization rate is higher, and the energy consumption is less. Electromagnetic flying cars that use compressed air as a power source are pollution-free vehicles.
  • the electromagnetic aerial vehicle can make full use of the urban space, and at the same time save energy and protect the environment, which is more in line with the development needs of modern people to protect the environment and global warming.
  • FIG. 1 is a schematic diagram of the overall structure of an aerial electromagnetic flying vehicle of the present invention.
  • FIG. 2 is a front view of an aerial electromagnetic flying vehicle of the present invention.
  • FIG. 3 is a top view of an aerial electromagnetic flying vehicle of the present invention.
  • iron does not refer to the material of iron alone, it refers to all substances similar to iron that can be attracted by magnets, including but not limited to iron, steel and current-carrying wires and coils Wait.
  • the "track” is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying the shape and features of the referred device, it is only used for the description of two consecutively separated objects , its cross-sectional area shape includes but is not limited to circle, square, triangle and bar.
  • the "support plate” is not just a flat plate, but refers to any system structure that can support the vehicle body to stay in the air.
  • first feature and second feature may include one or more of the features.
  • first and second are only used for descriptive purposes, and should not be construed as indicating or implying relative importance or implying the number of indicated technical features.
  • a feature defined as “first” or “second” may expressly or implicitly include one or more of that feature.
  • FIGS. 1 to 3 an aerial electromagnetic flying vehicle, including a flying vehicle 1 and a track system;
  • the flying car includes a car body 2, a magnet 3, a solenoid 4, a compressed air pump 5, an air intake pipe 6, an air outlet pipe 7 and a braking device 8.
  • the solenoid coil 4 has four corresponding sleeves on the magnet 3, and the compressed air pump 5 is arranged in the vehicle body 2;
  • One end of the air outlet pipe 7 is connected with the compressed air pump 5, and the other end penetrates the vehicle body 2 and communicates with the outside;
  • the braking device 8 is arranged on the vehicle body 2;
  • the rail system includes a rail 9, a rubber rail 10, and a support plate 11; the rail 9 is provided above the vehicle body 2, and cooperates with the magnet 3; Below, and in cooperation with the braking device 8 , the support plate 11 is arranged on the lower end of the rubber track 10 .
  • the intake pipe 6 has two branch pipes, which respectively penetrate the vehicle body from the front end and the top end of the vehicle body 2 and are connected to the compressed air pump 5 .
  • the braking device 8 is rotatably connected to the vehicle body 2 , and the braking device 8 is retractable.
  • the end of the brake device 8 is provided with a rubber pad 12, and the rubber track 10 is provided with a rubber groove 13, and the rubber pad 12 and the rubber groove 13 cooperate with each other.
  • a distance sensor is provided at the position of the vehicle body 2 close to the rail system, which is used to determine the distance between the vehicle body 2 and the rail system.
  • a gyroscope 14 is provided at the center of gravity of the vehicle body 2 for judging the balance state of the vehicle body in flight.
  • the flying car 1 and the track system are arranged in a circular pipe-type tunnel to reduce the influence of wind.
  • the present invention in order to make the electromagnetic aerial vehicle levitate and fly, four strong magnets 3 are respectively arranged in the vehicle body 2, and a energized solenoid 4 that can adjust the current is wrapped around the magnets.
  • the magnets 3 and The energized solenoid 4 interacts with the rails 9 in the track system to suspend the vehicle;
  • the power system is composed of a compressed air pump 5, an air intake pipe 6 and an air outlet pipe 7, and the compressed air pump 5 sucks air from the air intake pipe 6 and compresses it, Then it is pumped backward through the air outlet pipe 7 to obtain reverse thrust, which is used to propel the flying car 1 forward along the rail 9;
  • the braking device 8 is retractable and connected to the car body 2 in rotation.
  • the braking device 8 is in a retracted state .
  • the rubber pad 12 provided on the braking device 8 is in contact with the rubber groove 13 on the rubber track 10, and the friction generated between the two can make the flying car 1 stop quickly, and the rubber
  • the groove 13 also acts as a limit when the vehicle is stopped to prevent the flying car 1 from falling out of the track system.

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  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Regulating Braking Force (AREA)

Abstract

一种空中电磁飞车，包括飞车（1）以及轨道系统；飞车（1）包括车体（2）、磁体（3）、螺线圈（4）、压缩空气泵（5）、进气管（6）、出气管（7）以及刹车装置（8），磁体（3）有四个且分别设于飞车（1）的端点处，螺线圈（4）有四个对应套接在磁体（3）上，压缩空气泵（5）设于车体（1）内；进气管（6）的一端与压缩空气泵（5）相连，另一端贯穿车体（1）并与外部相通；出气管（7）的一端与压缩空气泵（5）相连，另一端贯穿车体（1）并与外部相通；刹车装置（8）设于车体（1）上；轨道系统包括铁轨（9）、橡胶轨道（10）、以及支撑板（11）；铁轨（9）设于车体（1）的上方，且与磁体（3）相互配合；橡胶轨道（10）设于铁轨（9）的下方，且与刹车装置（8）相互配合，支撑板（11）设于橡胶轨道（10）的下端。电磁空中飞车和汽车等交通工具相比，外界的阻力更小，能量利用率更高，耗费的能源更少，属于无污染的交通工具，可以充分利用的城市空间，同时节能环保，更符合现代人保护环境以及全球变暖的发展需求。

Description

一种空中电磁飞车 技术领域
本发明涉及轨道交通技术领域，具体是指一种空中电磁飞车。
背景技术
经过一百三十多年的发展，汽车行业的发展已经进入顶峰。现如今我国机动车的拥有量已经达到了3.6亿辆。庞大的机动车拥有量给城市带来了极大的交通压力。上班堵车，出行堵车成为了制约我们发展越来越严重的问题。传统的磁悬浮列车造价高昂，维护复杂使用成本高，为此，我们提出一种空中电磁飞车。
发明内容
本发明要解决的技术问题是克服上述技术的缺陷，提供：
一种空中电磁飞车，包括飞车以及轨道系统；
所述飞车包括车体、磁体、螺线圈、压缩空气泵、进气管、出气管以及刹车装置，所述磁体有四个且分别设于所述飞车的端点处，所述螺线圈有四个对应套接在所述磁体上，所述压缩空气泵设于所述车体内；所述进气管的一端与所述压缩空气泵相连，另一端贯穿所述车体并与外部相通；所述出气管的一端与所述压缩空气泵相连，另一端贯穿所述车体并与外部相通；所述刹车装置设于所述车体上；
所述轨道系统包括铁轨、橡胶轨道、以及支撑板；所述铁轨设于所述车体的上方，且与所述磁体相互配合；所述橡胶轨道设于所述铁轨的下端，且与所述刹车装置相互配合，所述支撑板设于所述橡胶轨道的下端。
作为改进，所述进气管有两条支管，分别从所述车体的前端和顶端贯穿所述车体并与所述压缩空气泵相连。
作为改进，所述刹车装置与所述车体转动连接，且所述刹车装置可伸缩。
作为改进，所述刹车装置的端部设有橡胶垫，所述橡胶轨道上设有橡胶凹槽，所述橡胶垫与所述橡胶凹槽相互配合。
作为改进，所述车体的靠近所述轨道系统的部位设有距离传感器，用于判断所述车体与所述轨道系统之间的间距。
作为改进，所述飞车重心位置设有陀螺仪，用于判断车体飞行的平衡状态。
作为改进，所述飞车以及轨道系统设于圆形管道型隧道内，用于降低风力的影响。
本发明与现有技术相比的优点在于：电磁空中飞车行驶属于无接触的空中飞行状态，除了空气的阻力之外，它再不受其他的外界阻力。和汽车等交通工具相比，外界的阻力更小，能量利用率更高，耗费的能源更少。利用压缩空气作为动力来源的电磁空中飞车属于无污染的交通工具。
电磁空中飞车可以充分利用的城市空间，同时节能环保，更符合现代人保护环境以及全球变暖的发展需求。
附图说明
图1是本发明一种空中电磁飞车的整体结构示意图。
图2是本发明一种空中电磁飞车的主视图。
图3是本发明一种空中电磁飞车的俯视图。
图中，1、飞车；2、车体；3、磁体；4、螺线圈；5、压缩空气泵；6、进气管；7、出气管；8、刹车装置；9、铁轨；10、橡胶轨道；11、支撑板；12、橡胶垫；13、橡胶凹槽；14、陀螺仪。
具体实施方式
下面详细描述本发明的实施例，实施例的示例在附图中示出，其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。在本发明的描述中，需要理解的是，术语“上”、“下”、“前”、“后”、“左”、“右”、“内”、“外”、“竖向”、“周向”等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述本发明和简化描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作，因此不能理解为对本发明的限制。
在本发明的描述中，“铁”并不是独指铁这种材质，它所指的是一切具有类似铁这样可以被磁铁所吸引的物质，其中包括但不限于铁，钢以及通电导线以及线圈等。
在本发明的描述中，“轨道”，仅是为了便于描述本发明和简化描述，而不是指示或暗示所指的装置的形状和特征，它仅是用于对连续分离的两个物体的描述，它的横截面积形状包括但不限于圆形，方形，三角形和条形等。
在本发明的描述中，“支撑板”并非只是平面板，而是指一切具有可以支撑车体在空中停留的系统构造。
在本发明的描述中，“第一特征”、“第二特征”可以包括一个或者更多个该特征。此外，术语“第一”、“第二”仅用于描述目的，而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此，限定有“第一”、“第二”的特征可以明示或者隐含地包括一个或者更多个该特征。
下面结合附图对一种空中电磁飞车做进一步的详细说明。
结合附图，图1～图3，一种空中电磁飞车，包括飞车1以及轨道系统；
结合附图，图1～图3，飞车包括车体2、磁体3、螺线圈4、压缩空气泵5、进气管6、出气管7以及刹车装置8，磁体3有四个且分别设于飞车1的端点处，螺线圈4有四个对应套接在磁体3上，压缩空气泵5设于车体2内；进气管6的一端与压缩空气泵5相连，另一端贯穿车体2并与外部相通；出气管7的一端与压缩空气泵5相连，另一端贯穿车体2并与外部相通；刹车装置8设于车体2上；
结合附图，图1～图3，轨道系统包括铁轨9、橡胶轨道10、以及支撑板11；铁轨9设于车体2的上方，且与磁体3相互配合；橡胶轨道10设于铁轨9的下方，且与刹车装置8相互配合，支撑板11设于橡胶轨道10的下端。
本实施例中，如图1～图3所示，进气管6有两条支管，分别从车体2的前端和顶端贯穿车体并与压缩空气泵5相连。
本实施例中，如图1～图3所示，刹车装置8与车体2转动连接，且刹车装置8可伸缩。
本实施例中，如图1～图3所示，刹车装置8的端部设有橡胶垫12，橡胶轨道10上设 有橡胶凹槽13，橡胶垫12与橡胶凹槽13相互配合。
本实施例中，如图1～图3所示，车体2的靠近轨道系统的部位设有距离传感器，用于判断车体2与轨道系统之间的间距。
本实施例中，如图1～图3所示，车体2的重心位置设有陀螺仪14，用于判断车体飞行的平衡状态。
本实施例中，如图1～图3所示，飞车1以及轨道系统设于圆形管道型隧道内，用于降低风力的影响。
本发明的工作原理：本发明中，为了使电磁空中飞车悬浮飞行，在车体2内分别设有四个强磁体3，并在磁体外包绕有可以调节电流的通电螺线圈4，磁体3和通电螺线圈4共同与轨道系统中的铁轨9相互作用，使车辆悬浮；动力系统由压缩空气泵5、进气管6以及出气管7组成，压缩空气泵5从进气管6中吸入空气并压缩，然后通过出气管7向后泵出，获得反推力，用于推进飞车1沿铁轨9前进；刹车装置8可伸缩并与车体2转动相连，在飞车1行进过程中，刹车装置8处于收回状态，当刹车的时候，刹车装置8展开，设于刹车装置8上的橡胶垫12与橡胶轨道10上的橡胶凹槽13抵接，两者之间产生的摩擦可使飞车1迅速停下，橡胶凹槽13也在车辆停止的状态起到限位的作用，防止飞车1从轨道系统中脱出。
以上对本发明及其实施方式进行了描述，这种描述没有限制性，附图中所示的也只是本发明的实施方式之一，实际的结构并不局限于此。总而言之如果本领域的普通技术人员受其启示，在不脱离本发明创造宗旨的情况下，不经创造性的设计出与该技术方案相似的结构方式及实施例，均应属于本发明的保护范围。

Claims (7)

  1. 一种空中电磁飞车，其特征在于：包括飞车(1)以及轨道系统；
    所述飞车包括车体(2)、磁体(3)、螺线圈(4)、压缩空气泵(5)、进气管(6)、出气管(7)以及刹车装置(8)，所述磁体(3)有四个且分别设于所述飞车(1)的端点处，所述螺线圈(4)有四个对应套接在所述磁体(3)上，所述压缩空气泵(5)设于所述车体(2)内；所述进气管(6)的一端与所述压缩空气泵(5)相连，另一端贯穿所述车体(2)并与外部相通；所述出气管(7)的一端与所述压缩空气泵(5)相连，另一端贯穿所述车体(2)并与外部相通；所述刹车装置(8)设于所述车体(2)上；
    所述轨道系统包括铁轨(9)、橡胶轨道(10)、以及支撑板(11)；所述铁轨(9)设于所述车体(2)的上方，且与所述磁体(3)螺线圈(4)相互配合；所述橡胶轨道(10)设于所述铁轨(9)的下方且并不一定相互连接，且与所述刹车装置(8)相互配合，所述支撑板(11)设于所述橡胶轨道(10)的下端。
  2. 所述进气管(6)有两条支管，分别从所述车体(2)的前端和顶端贯穿所述车体并与所述压缩空气泵(5)相连。
  3. 根据权利要求1所述的一种空中电磁飞车，其特征在于：所述刹车装置(8)与所述车体(2)转动连接，且所述刹车装置(8)可伸缩。
  4. 根据权利要求1所述的一种空中电磁飞车，其特征在于：所述刹车装置(8)的端部设有橡胶垫(12)，所述橡胶轨道(10)上设有橡胶凹槽(13)，所述橡胶垫(12)与所述橡胶凹槽(13)相互配合。
  5. 根据权利要求1所述的一种空中电磁飞车，其特征在于：所述车体(2)的靠近所述轨道系统的部位设有距离传感器，用于判断所述车体(2)与所述轨道系统之间的间距。
  6. 根据权利要求1所述的一种空中电磁飞车，其特征在于：所述车体(2)的重心位置设有陀螺仪(14)来判断所述车体(2)的平衡状态。
  7. 根据权利要求1所述的一种空中电磁飞车，其特征在于：所述飞车(1)以及轨道系统设于圆形管道型隧道内，用于降低风力的影响。
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