WO2013040847A1 - Through-flow air suspension platform - Google Patents

Through-flow air suspension platform Download PDF

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Publication number
WO2013040847A1
WO2013040847A1 PCT/CN2012/000852 CN2012000852W WO2013040847A1 WO 2013040847 A1 WO2013040847 A1 WO 2013040847A1 CN 2012000852 W CN2012000852 W CN 2012000852W WO 2013040847 A1 WO2013040847 A1 WO 2013040847A1
Authority
WO
WIPO (PCT)
Prior art keywords
cross
flow
fan
suspension platform
air suspension
Prior art date
Application number
PCT/CN2012/000852
Other languages
French (fr)
Chinese (zh)
Inventor
陈晓春
Original Assignee
Chen Xiaochun
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
Priority claimed from CN2011203548626U external-priority patent/CN202279234U/en
Priority claimed from CN201110281430.1A external-priority patent/CN102358423B/en
Application filed by Chen Xiaochun filed Critical Chen Xiaochun
Publication of WO2013040847A1 publication Critical patent/WO2013040847A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/16Combinations of two or more pumps ; Producing two or more separate gas flows
    • F04D25/166Combinations of two or more pumps ; Producing two or more separate gas flows using fans
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/04Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type

Definitions

  • the invention belongs to the field of flying devices, and in particular relates to a cross flow air suspension platform.
  • the above four methods are capable of achieving vertical takeoff and landing and air hovering, but they cannot be effectively applied to flying cars and urban traffic due to both principle and structural problems. Let's take a look at their shortcomings in this respect: A: Jet: The temperature of the jet is too high, the noise is very large and the energy consumption is huge. The above disadvantages can be seen from the British fighter jets.
  • Flapping Wing Many animals have the first to develop a perfect flight structure, and it carries the original dream of human flight, but for thousands of years people have not developed it to carry people to fly, but also because of structural constraints If you need to carry people, then the wings will be too large to fly freely in the city.
  • Hot air balloon and airship type aircraft Although it can achieve smooth take-off and landing, its volume is even more amazing. It is impossible to walk through small city streets, and it is difficult to adapt to urban life due to slow take-off and landing. Rapid and efficient requirements.
  • the present invention provides a cross-flow air suspension platform, which can solve the difficulties encountered by the foregoing four methods in urban flight traffic in a completely new way, and realizes the built-in thrust suspension device. And miniaturization and flattening, the most important thing is that it replaces the chassis driving system of the car and the huge propeller take-off and landing mechanism of the helicopter in a completely new way. It can be said that it is the hovering and taking off and landing of the future helicopter and flying vehicle foundation. Device.
  • the invention adopts a structure formed by a cross-flow fan and an engine, and the force is used for mutual use, and the principle of the force and the reaction force is utilized, and the counter-thrust obtained by the cross-flow fan to promote the one-way flow of the air is fully utilized, and the platform is realized in the air. Suspended flight device.
  • the impeller and the outer casing of the cross-flow fan form a structure in which the air moves in one direction, and the impeller of the cross-flow fan rotates at a high speed under the driving of the engine.
  • the impeller rotates at a high speed
  • the air is sucked by the impeller, and a thrust is given to the air, and the air is supplied to the impeller.
  • the force is applied, the air also gives the impeller a counter force to give the fan a lift.
  • the impeller and the engine shaft are arranged in parallel, and can also be installed at right angles through the transmission mechanism and the engine shaft.
  • the cross flow fan is also called a cross flow fan, and the impeller is multi-leaf type, long cylindrical shape, and has a forward multi-wing blade.
  • the airflow enters the cascade from the open end of the impeller, passes through the interior of the impeller, and is discharged into the volute from the other side of the cascade to form a working airflow.
  • the flow of the airflow in the impeller is complex, the velocity field of the airflow is unsteady, and there is a vortex in the impeller, centered near the volute tongue.
  • the existence of the vortex causes a circulating flow at the output end of the impeller. Outside the vortex, the flow line of the airflow in the impeller is arc-shaped. Therefore, the flow velocity at each point on the outer circumference of the impeller is inconsistent. The closer to the vortex core, the greater the velocity, and the closer to the volute, the smaller the velocity.
  • the airflow speed and pressure at the fan outlet are not uniform, so the flow coefficient and pressure coefficient of the fan are average.
  • the position of the vortex has a great influence on the performance of the cross-flow fan.
  • the center of the vortex is close to the inner circumference of the impeller and close to the volute tongue.
  • the performance of the fan is better.
  • the cross-flow fan is mainly composed of three parts: impeller, air duct and electric motor. It has the following characteristics:
  • the axial length is not limited, and the length of the impeller can be arbitrarily selected according to different use requirements;
  • the cross flow air suspension platform is characterized in that it comprises at least two cross flow fans, the cross flow fans are disposed in the same plane, and the cross flow fan comprises a cylindrical fan shell, a fan The opposite sides of the shell are respectively provided with an air inlet and an air outlet, and the air outlet is arranged downward, and the fan shaft of the cross flow fan is connected with the rotating shaft of the engine.
  • the cross-flow air suspension platform is characterized in that the air inlet and the air outlet of the fan casing are strip-shaped ports which are disposed along the longitudinal direction of the fan casing cylinder and have the same length as the cylinder.
  • the tubular air suspension platform is characterized in that the width of the air inlet is wider than the width of the air outlet.
  • the cross-flow air suspension platform is characterized in that the width of the air inlet is three times the width of the air outlet.
  • the cross-flow air suspension platform is characterized in that a fan-shaped fan impeller is arranged in the fan casing, and the fan impeller is composed of strip-shaped blades arranged along the length of the cylinder and having the same length as the cylinder The strip blade is disposed obliquely to the circumferential section of the cylinder.
  • the tubular air suspension platform is characterized in that the strip blades are disposed at an angle of 45° to the circumferential section of the cylinder.
  • the cross-flow air suspension platform is characterized in that: two rotating shafts are respectively arranged on the two sides of the engine, the rotating shafts are respectively connected with one driving shaft, and the main bevel gears are symmetrically arranged on the driving shafts, and each main cone Two cross-flow fans are respectively arranged on both sides of the gear, the fan shaft of the cross-flow fan is vertically arranged with the transmission shaft, the auxiliary bevel gear is arranged on the fan shaft, and the main bevel gear and the auxiliary bevel gear are vertically meshed with each other.
  • the tubular air suspension platform is characterized in that the cross flow fan is disposed between two mutually parallel side beams, and the engine is staggered outside the side beams.
  • the cross-flow air suspension platform is characterized in that it comprises an outer ring and a support plate, the support plate is arranged at the center of the outer ring, the engine is arranged on the support plate, and the fan shaft on one side of the cross flow fan is connected with the engine shaft.
  • the other side of the cross-flow fan is connected to the outer ring, and the engine and the cross-flow fan are symmetrically arranged in the outer ring.
  • the cross-flow air suspension platform is characterized in that a cross-flow fan disposed parallel to or perpendicular to the cross-flow air suspension platform and disposed downstream of the air outlet is disposed on the rear side of the cross-flow air suspension platform.
  • the left and right sides of the flow air suspension platform are respectively connected with a cross flow fan which is perpendicular to the cross flow air suspension platform and which is arranged forwardly from the air outlet.
  • the fan shaft of the cross flow fan is connected with the rotating shaft of the engine.
  • the cross-flow air suspension platform is characterized in that it comprises an outer frame, a cross-flow fan of a pair of shared engines is laterally disposed on the upper and lower sides of the outer frame, and a pair of shared engines are vertically disposed inside the outer frame Flow fan.
  • the cross-flow air suspension platform is characterized in that it comprises an inner frame, an outer frame is arranged around the inner frame, a cross-flow fan is arranged in the outer frame, and the cross-flow fan is clockwise or reverse In the hour hand arrangement, the fan shaft of the cross flow fan is connected to the rotating shaft of the engine.
  • the cross-flow air suspension platform is characterized in that a set of fixing plates are fixedly arranged in the inner frame.
  • the cross-flow air suspension platform is characterized in that: an outer frame is arranged, and a cross-flow fan is fixedly disposed on four circumferential corners of the outer frame, and the fan shaft of the cross-flow fan is connected to the gearbox, The engine is connected to the gearbox.
  • the tubular air suspension platform is characterized in that a steering gear is connected to the cross flow fan.
  • the tubular air suspension platform is characterized in that the gearbox and the engine are provided with a control port for connecting an external control system.
  • the function and effect of the invention 1. It can make the real flying car appear, and the life of most helicopters and a part of the car; 2. Realize the rapid traffic in the huge area and volume city in the future; 3. Reduce the urban road construction And the construction of peripheral highways to maximize the protection of the land to protect the natural environment; 4.
  • the flight device has an emergency fault in the air, because of its small structure and no external high-speed rotating device, it can use the parachute to land when the high altitude fails.
  • the entire aircraft can be protected by a honeycomb airbag, thereby maximizing the safety of the internal passengers, and avoiding the fact that the existing aircraft is in flight or not, and the vast majority of the survivors have no terrible situation, in special circumstances.
  • It can also be used for aerodynamic suspension stretchers in the battle of rugged mountains to transport combat wounded, and can also be applied to high-efficiency transport of small quantities of battlefield materials and supplies in the field.
  • FIG. 1 is a schematic structural view of a cross flow fan of a cross flow air suspension platform of the present invention
  • FIG. 2 is a schematic structural view of a first embodiment of a through-flow air suspension platform of the present invention
  • FIG. 3 is a schematic structural view of a second embodiment of a tubular air suspension platform of the present invention
  • FIG. 5 is a schematic structural view of a third embodiment of a through-flow air suspension platform
  • FIG. 5 is a schematic structural view of a set forward and brake power device of the tubular air suspension platform of the present invention
  • FIG. 6 is a schematic structural view of a fourth embodiment of the throughflow air suspension platform of the present invention
  • FIG. 7 is a schematic structural view of a fifth embodiment of the throughflow air suspension platform of the present invention
  • Figure 9 is a schematic structural view of a seventh embodiment of the through-flow air suspension platform of the present invention
  • Figure 10 is a schematic structural view of an eighth embodiment of the tubular air suspension platform of the present invention
  • 2 fan shell
  • 3 fan impeller
  • 4 consistent flow fan 5
  • 6 one support plate
  • 7 side beam
  • 8 main bevel gear
  • 9 one transmission shaft
  • 10-outer frame Inner frame
  • 12- fixed plate 13-transmission; 14-rudder; 15-control port.
  • the basic assembly of the tubular air suspension platform of the present invention is a cross flow fan 4 connected to an engine 1.
  • the cross flow fan 4 comprises a cylindrical fan casing 2, and two opposite sides of the fan casing 2 are respectively provided with strip-shaped air inlets and outlets of the same length as the cylinder along the length of the cylinder casing 2 At the tuyere, the width of the air inlet is wider than the air outlet, which is roughly three times the width of the air outlet, and the air outlet is facing downward.
  • the fan casing 2 is provided with a cylindrical fan impeller 3, and the fan impeller 3 is composed of strip-shaped blades provided along the length of the cylinder and having the same length as the cylinder, and the strip-shaped blades are inclined with respect to the circumferential section of the cylinder. It is approximately at an angle of 45° to the circumferential section of the cylinder.
  • the fan shaft of the cross flow fan 4 is connected to the shaft of the engine 1.
  • a rotating shaft is respectively arranged on both sides of the engine 1, and each of the rotating shafts is connected with a transmission shaft 9, and the main bevel gear is symmetrically arranged on the transmission shaft 9 respectively.
  • Two cross-flow fans 4 are respectively disposed on two sides of each main bevel gear 8.
  • the fan shaft of the cross-flow fan 4 is vertically disposed with the transmission shaft 9, and the auxiliary bevel gear, the main bevel gear 8 and the auxiliary bevel gear are disposed on the fan shaft. Vertically meshed with each other.
  • the number of bevel gears and cross-flow fan 4 can be set as needed. As shown in Fig.
  • each main drive shaft 9 is provided with four main bevel gears 8, each of which has two cross-flow fans respectively. 4 connections, a total of 8 cross-flow fans 4.
  • the engine 1 in the middle works to drive the drive shaft. 9 rotation, the drive shaft 9 drives the main bevel gear 8 to rotate, the main bevel gear 8 drives the auxiliary bevel gear to rotate, thereby driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, and discharging from the lower air outlet.
  • Give the air a thrust, and the air also gives the platform a counter-force to allow the platform to gain a lift and float in the air.
  • the engine suspension below the platform. This type of platform is generally suitable for use in flying cars and can be used to replace the chassis of an ordinary car to suspend the car in the air.
  • a second embodiment of the tubular air suspension platform of the present invention is provided.
  • the cross flow fan 4 of the platform is disposed between two mutually parallel side beams 7, and the engine 1 is staggered outside the side beam 7.
  • the fan shaft of each cross flow fan 4 is connected to the rotating shaft of one engine 1.
  • the number of cross-flow fan 4 and the corresponding engine 1 can be set as required.
  • four cross-flow fans 4 are arranged in the middle of the side beam 7, and four engines 1 are staggered on the outer side of the side beam 7.
  • the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counteracting force to make the platform Get a lift and float in the air.
  • This platform can be used in a flying car, instead of the chassis of an ordinary car, so that the car can be suspended in the air, or a stretcher plate can be placed on it for a pneumatic suspension stretcher.
  • the platform includes an outer ring 5 and a support plate 6.
  • the support plate 6 is disposed at the center of the outer ring 5, and the engine 1 is disposed at
  • the fan shaft on the side of the cross flow fan 4 is connected to the shaft of the engine 1, and the other side of the cross flow fan 4 is connected to the outer ring 5, and the engine 1 and the cross flow fan 4 are symmetrically arranged in the outer ring 5.
  • the number of the cross flow fan 4 and the engine 1 can be set as needed. In Fig.
  • the support plate 6 is square, and an engine 1 is disposed in the middle of the four sides of the square, and each of the engines 1 is connected to a cross flow fan 4 , A total of 4 cross-flow fans 4, the outer ring is divided into 4 equal parts.
  • the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air. This platform is suitable for use in new round aircraft.
  • the through-flow air suspension platform of the present invention can be provided with a power device for forward and brake, and the power device for forward and brake is also composed of a cross flow fan 4, which is connected at the rear side of the cross flow air suspension platform.
  • the cross-flow fan 4 disposed parallel to or perpendicular to the cross-flow air suspension platform and disposed at the left and right sides of the cross-flow air suspension platform is disposed perpendicular to the cross-flow air suspension platform.
  • the cross flow fan 4 provided with the tuyere forward, and the fan shaft of the cross flow fan 4 is connected to the rotating shaft of the engine 1.
  • the engine 1 drives the fan shaft of the cross-flow fan 4 on the rear side to rotate, sucking air from the front air inlet, discharging it from the rear air outlet, giving the air a thrust, and the air also gives the platform a counter force.
  • the engine works to drive the fan shaft of the cross-flow fan 4 on the left and right sides to rotate, and the air is sucked from the rear air inlet, and is discharged from the front air outlet to give the air a thrust, and the air also gives the platform a reverse Acting to reduce the speed of the platform forward until it stops.
  • This forward and brake power unit can be mounted on a variety of cross-flow air suspension platforms for propelling and braking the platform.
  • FIG. 6 is a fourth embodiment of the through-flow air suspension platform of the present invention.
  • the platform includes an outer frame 10 of a rectangular structure, and a cross-flow fan 4 of the shared engine 1 is laterally disposed on the upper and lower sides of the outer frame 10, A pair of cross-flow fans 4 sharing the engine 1 are longitudinally disposed inside the outer frame 10, and preferably four pairs of cross-flow fans 4 are longitudinally disposed inside the outer frame 10, and each pair of cross-flow fans 4 shares an engine 1.
  • the engine 1 is operated to drive the fan shaft of the cross flow fan 4 to rotate, and the air is taken from the air inlet above. Inhalation, discharged from the lower air outlet, gives the air a thrust, and the air also gives the platform a counter-force to allow the platform to gain a lift and float in the air.
  • FIG. 7 is a fifth embodiment of the through-flow air suspension platform of the present invention, the platform includes an inner frame 11 of a rectangular or square structure, and four outer frames 10 of a rectangular structure are disposed around the inner frame 11
  • a cross flow fan 4 is fixedly disposed in the outer frame 10, and the cross flow fan 4 is arranged in a clockwise or counterclockwise direction.
  • the fan shaft of each cross flow fan 4 is connected to the shaft of the engine 1.
  • the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air.
  • FIG. 8 is a sixth embodiment of the through-flow air suspension platform of the present invention.
  • the platform includes an inner frame 11 of a rectangular or square structure, and a set of fixing plates 12 are disposed in the inner frame 11, and the inner frame 11 is disposed outside.
  • a circular outer frame 10 having a rectangular structure and a square structure, a cross flow fan 4 is disposed in the outer frame 10 of the rectangular structure, and an engine 1 connected to the cross flow fan 4 is disposed in the outer frame 10 of the square structure, and The flow fan 4 is arranged in a clockwise or counterclockwise direction.
  • the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air.
  • FIG. 9 is a seventh embodiment of the through-flow air suspension platform of the present invention.
  • the platform includes an outer frame 10 of a rectangular structure, and the four corners of the outer frame 10 are respectively divided into rectangular frames, each of which is rectangular. frame A pair of cross flow fans 4 are disposed, and the fan shafts of each pair of cross flow fans 4 are disposed at the center of the outer frame 10.
  • a steering gear 14 is coupled to the fan casing 2 of the cross flow fan 4, and a gearbox 13 is connected to the fan shaft of the cross flow fan 4, the engine 1 is connected to the gearbox 13, and an external unit is provided on the gearbox 13 and the engine 1.
  • the control port 15 to which the control system is connected.
  • FIG. 10 is an eighth embodiment of the through-flow air suspension platform of the present invention.
  • one cross-flow fan 4 is reduced in each rectangular frame, and other structures are the same as the embodiment. 7 is the same.

Abstract

A through-flow air suspension platform comprises at least two through-flow blower fans (4). The through-flow blower fans (4) are arranged on the same plane. Each through-flow blower fan comprises a cylindrical blower fan shell (2). Two opposite sides of the blower fan shell (2) are respectively provided with an air inlet and an air outlet, the air outlet facing down. Blower fan shafts of the through-flow blower fans (4) are connected to a rotation shaft of an engine (1). The through-flow air suspension platform enables automobiles to fly, so that fast traffic is achieved in a city, road construction is reduced, a compact structure is implemented, and maximum protection of passenger safety is implemented.

Description

说明书 贯流式空气悬浮平台 技术领域  Instruction Manual Tubular Air Suspension Platform Technical Field
本发明属于飞行装置领域, 具体是一种贯流式空气悬浮平台。  The invention belongs to the field of flying devices, and in particular relates to a cross flow air suspension platform.
背景技术 Background technique
目前能够在空气中实现垂直起降和悬停的方式只有四种: A:喷气式、 B:螺 旋桨、 C:扑翼机、 D:热气球和飞艇类飞行器。 以上四类方法均能够实现垂直起 降和空中悬停, 但是由于原理和结构上的问题均无法有效运用于飞行汽车和城 市交通。 下面我们来看下他们在这方面的不足: A:喷气式: 喷射物温度过高、 噪音十分巨大同时能耗巨大,从英制鹞式战斗机可见其上述缺点; B:螺旋桨式: 螺旋桨是垂直起降落和悬停运用和发展的最好的最为成功的一种方式,但是其 在城市运用中的缺点也是明显的巨大的, 其螺旋桨效率提高的需要,造成旋转部 直径非常巨大,并且螺旋桨高速运转细微的刮擦都有可能造成巨大的灾难, 巨大 的螺旋桨是无法通过城市狭小的街道上空的, 当然巨大的噪音也是人们无法忍 受的, 并且在空中有紧急情况时候也不能象汽车一样进行紧急刹车; C:扑翼:是 很多动物最先拥有发展完美的飞行结构,并且它承载了人类对飞行最初梦想, 但 是千百年来人们并没有把它发展到可以载人飞行,同时也因为结构限制如果需 要载人,那么翅膀也会很庞大无法在城市中自由飞行; 热气球和飞艇类飞行器: 虽然能够实现平稳起飞和降落,但是它的体积更加是惊人的巨大,它不可能穿行 在细小的城市街道上空, 还有起飞和降落速度缓慢很难适应城市生活的迅速和 高效的要求。  There are currently only four ways to achieve vertical takeoff and landing and hovering in the air: A: Jet, B: Screw, C: Flapping, D: Hot Air Balloon and Airship. The above four methods are capable of achieving vertical takeoff and landing and air hovering, but they cannot be effectively applied to flying cars and urban traffic due to both principle and structural problems. Let's take a look at their shortcomings in this respect: A: Jet: The temperature of the jet is too high, the noise is very large and the energy consumption is huge. The above disadvantages can be seen from the British fighter jets. B: Propeller type: The propeller is vertical The best and most successful way of landing and hovering and development, but its shortcomings in urban applications are also significant. The need for increased propeller efficiency results in a very large rotating diameter and high propeller speed. Subtle scratches can cause huge disasters. The huge propellers cannot pass through the narrow streets of the city. Of course, the huge noise is unbearable, and it is impossible to perform emergency braking like a car when there is an emergency in the air. C: Flapping Wing: Many animals have the first to develop a perfect flight structure, and it carries the original dream of human flight, but for thousands of years people have not developed it to carry people to fly, but also because of structural constraints If you need to carry people, then the wings will be too large to fly freely in the city. Hot air balloon and airship type aircraft: Although it can achieve smooth take-off and landing, its volume is even more amazing. It is impossible to walk through small city streets, and it is difficult to adapt to urban life due to slow take-off and landing. Rapid and efficient requirements.
发明内容 为了解决上述技术问题, 本发明提供了一种贯流式空气悬浮平台, 能以一 种全新的方式解决前面四种方法在城市飞行交通中遇到的困难, 它实现了推力 悬浮装置的内置、 并且小型化和扁平化, 最主要的是它以一种全新的方法替代 了汽车的底盘行驶系统和直升机的巨大螺旋桨起降机构, 可以说它是未来直升 机和飞行汽车基础的悬停和起降装置。 Summary of the invention In order to solve the above technical problems, the present invention provides a cross-flow air suspension platform, which can solve the difficulties encountered by the foregoing four methods in urban flight traffic in a completely new way, and realizes the built-in thrust suspension device. And miniaturization and flattening, the most important thing is that it replaces the chassis driving system of the car and the huge propeller take-off and landing mechanism of the helicopter in a completely new way. It can be said that it is the hovering and taking off and landing of the future helicopter and flying vehicle foundation. Device.
本发明运用贯流风机和发动机形成的结构,利用力的作用是相互的,运用作 用力和反作用力的原理,充分利用贯流风机推动空气单向流动时得到的反推力, 实现平台在空气中悬浮的飞行装置。  The invention adopts a structure formed by a cross-flow fan and an engine, and the force is used for mutual use, and the principle of the force and the reaction force is utilized, and the counter-thrust obtained by the cross-flow fan to promote the one-way flow of the air is fully utilized, and the platform is realized in the air. Suspended flight device.
贯流风机的叶轮和外壳形成一个空气单向运动的的结构,贯流风机的叶轮 在发动机的驱动下高速旋转,叶轮高速旋转时靠叶轮吸入空气,并给空气一个推 力,在叶轮给空气一个力的时候,空气也给叶轮一个反作作用力而使风机得到一 个升力, 叶轮和发动机轴平行设置, 也可以通过传动机构和发动机轴直角安装。 贯流风机又叫横流风机, 叶轮为多叶式、 长圆筒形, 具有前向多翼形叶片。 叶 轮旋转时, 气流从叶轮敞开处进入叶栅, 穿过叶轮内部, 从另一面叶栅处排入 蜗壳, 形成工作气流。 气流在叶轮内的流动情况很复杂, 气流速度场是非稳定 的, 在叶轮内还存在一个旋涡, 中心位于蜗舌附近。 旋涡的存在, 使叶轮输出 端产生循环流, 在旋涡外, 叶轮内的气流流线呈圆弧形。 因此, 在叶轮外圆周 上各点的流速是不一致的, 越靠近涡心, 速度愈大, 越靠近涡壳, 则速度愈小。 在风机出风口处气流速度和压力不是均匀的, 因而风机的流量系数及压力系数 是平均值。 旋涡的位置对横流风机的性能影响较大, 旋涡中心接近叶轮内圆周 且靠近蜗舌, 风机性能较好; 旋涡中心离涡舌较远, 则循环流的区域增大, 风 机效率降低, 流量不稳定程度增加。 贯流风机主要由叶轮、 风道和电动机三部分组成, 具有以下特点: The impeller and the outer casing of the cross-flow fan form a structure in which the air moves in one direction, and the impeller of the cross-flow fan rotates at a high speed under the driving of the engine. When the impeller rotates at a high speed, the air is sucked by the impeller, and a thrust is given to the air, and the air is supplied to the impeller. When the force is applied, the air also gives the impeller a counter force to give the fan a lift. The impeller and the engine shaft are arranged in parallel, and can also be installed at right angles through the transmission mechanism and the engine shaft. The cross flow fan is also called a cross flow fan, and the impeller is multi-leaf type, long cylindrical shape, and has a forward multi-wing blade. When the impeller rotates, the airflow enters the cascade from the open end of the impeller, passes through the interior of the impeller, and is discharged into the volute from the other side of the cascade to form a working airflow. The flow of the airflow in the impeller is complex, the velocity field of the airflow is unsteady, and there is a vortex in the impeller, centered near the volute tongue. The existence of the vortex causes a circulating flow at the output end of the impeller. Outside the vortex, the flow line of the airflow in the impeller is arc-shaped. Therefore, the flow velocity at each point on the outer circumference of the impeller is inconsistent. The closer to the vortex core, the greater the velocity, and the closer to the volute, the smaller the velocity. The airflow speed and pressure at the fan outlet are not uniform, so the flow coefficient and pressure coefficient of the fan are average. The position of the vortex has a great influence on the performance of the cross-flow fan. The center of the vortex is close to the inner circumference of the impeller and close to the volute tongue. The performance of the fan is better. When the center of the vortex is far away from the vortex tongue, the area of the circulating flow increases, the efficiency of the fan decreases, and the flow rate does not. The degree of stability increases. The cross-flow fan is mainly composed of three parts: impeller, air duct and electric motor. It has the following characteristics:
1) 轴向长度不受限制, 可以根据不同的使用需要任意选择叶轮的长度; 1) The axial length is not limited, and the length of the impeller can be arbitrarily selected according to different use requirements;
2) 气流贯穿叶轮流动,受叶片两次力的作用,因此气流能到达很远的距离;2) The airflow flows through the impeller and is subjected to the force of the blade twice, so the airflow can reach a very long distance;
3) 无紊流, 出风均匀。 3) No turbulence, even air.
本发明是通过以下技术方案来实现的:  The present invention is achieved by the following technical solutions:
所述的贯流式空气悬浮平台, 其特征在于其包括至少 2个贯流风机, 所述 贯流风机设置在同一个平面内, 所述贯流风机包括圆筒形的风机壳, 风机壳上 的两个对侧分别设置有进风口和出风口, 出风口朝下设置, 贯流风机的风机轴 与发动机的转轴连接。  The cross flow air suspension platform is characterized in that it comprises at least two cross flow fans, the cross flow fans are disposed in the same plane, and the cross flow fan comprises a cylindrical fan shell, a fan The opposite sides of the shell are respectively provided with an air inlet and an air outlet, and the air outlet is arranged downward, and the fan shaft of the cross flow fan is connected with the rotating shaft of the engine.
所述的贯流式空气悬浮平台, 其特征在于所述风机壳的进风口和出风口是 沿着风机壳圆筒长度方向设置的, 与圆筒长度相同的条形口。  The cross-flow air suspension platform is characterized in that the air inlet and the air outlet of the fan casing are strip-shaped ports which are disposed along the longitudinal direction of the fan casing cylinder and have the same length as the cylinder.
所述的贯流式空气悬浮平台, 其特征在于所述进风口的宽度比出风口的宽 度宽。  The tubular air suspension platform is characterized in that the width of the air inlet is wider than the width of the air outlet.
所述的贯流式空气悬浮平台, 其特征在于所述进风口的宽度是出风口宽度 的三倍。  The cross-flow air suspension platform is characterized in that the width of the air inlet is three times the width of the air outlet.
所述的贯流式空气悬浮平台, 其特征在于所述风机壳中设置有圆筒形的风 机叶轮, 风机叶轮由沿着圆筒长度方向设置的, 与圆筒长度相同的条形叶片组 成, 所述条形叶片与圆筒的圆周切面倾斜设置。  The cross-flow air suspension platform is characterized in that a fan-shaped fan impeller is arranged in the fan casing, and the fan impeller is composed of strip-shaped blades arranged along the length of the cylinder and having the same length as the cylinder The strip blade is disposed obliquely to the circumferential section of the cylinder.
所述的贯流式空气悬浮平台, 其特征在于所述的条形叶片与圆筒的圆周切 面之间呈 45° 角设置。  The tubular air suspension platform is characterized in that the strip blades are disposed at an angle of 45° to the circumferential section of the cylinder.
所述的贯流式空气悬浮平台, 其特征在于所述的发动机两侧分别设置转轴, 所述转轴各连接一根传动轴, 所述传动轴上分别对称设置主锥齿轮, 每个主锥 齿轮的两侧分别设置两个贯流风机, 贯流风机的风机轴与传动轴垂直设置, 风 机轴上设置副锥齿轮, 主锥齿轮与副锥齿轮相互垂直啮合设置。 The cross-flow air suspension platform is characterized in that: two rotating shafts are respectively arranged on the two sides of the engine, the rotating shafts are respectively connected with one driving shaft, and the main bevel gears are symmetrically arranged on the driving shafts, and each main cone Two cross-flow fans are respectively arranged on both sides of the gear, the fan shaft of the cross-flow fan is vertically arranged with the transmission shaft, the auxiliary bevel gear is arranged on the fan shaft, and the main bevel gear and the auxiliary bevel gear are vertically meshed with each other.
所述的贯流式空气悬浮平台, 其特征在于所述贯流风机设置在两根相互平 行的边梁中间, 发动机交错设置在边梁外侧。  The tubular air suspension platform is characterized in that the cross flow fan is disposed between two mutually parallel side beams, and the engine is staggered outside the side beams.
所述的贯流式空气悬浮平台, 其特征在于包括一个外圈和一个支撑板, 支 撑板设置在外圈的圆心处, 发动机设置在支撑板上, 贯流风机一侧的风机轴与 发动机转轴连接, 贯流风机另一侧与所述外圈连接, 发动机与贯流风机在外圈 内对称设置。  The cross-flow air suspension platform is characterized in that it comprises an outer ring and a support plate, the support plate is arranged at the center of the outer ring, the engine is arranged on the support plate, and the fan shaft on one side of the cross flow fan is connected with the engine shaft. The other side of the cross-flow fan is connected to the outer ring, and the engine and the cross-flow fan are symmetrically arranged in the outer ring.
所述的贯流式空气悬浮平台, 其特征在于在贯流式空气悬浮平台的后侧连 接设置有与贯流式空气悬浮平台平行或垂直的, 出风口向后设置的贯流风机, 在贯流式空气悬浮平台的左右两侧各连接设置有与贯流式空气悬浮平台垂直 的, 出风口向前设置的贯流风机, 上述贯流风机的风机轴与发动机的转轴连接。  The cross-flow air suspension platform is characterized in that a cross-flow fan disposed parallel to or perpendicular to the cross-flow air suspension platform and disposed downstream of the air outlet is disposed on the rear side of the cross-flow air suspension platform. The left and right sides of the flow air suspension platform are respectively connected with a cross flow fan which is perpendicular to the cross flow air suspension platform and which is arranged forwardly from the air outlet. The fan shaft of the cross flow fan is connected with the rotating shaft of the engine.
所述的贯流式空气悬浮平台, 其特征在于包括外边框, 所述的外边框上下 外侧横向设置一对共用发动机的贯流风机, 所述的外边框内侧纵向设置一对以 上共用发动机的贯流风机。  The cross-flow air suspension platform is characterized in that it comprises an outer frame, a cross-flow fan of a pair of shared engines is laterally disposed on the upper and lower sides of the outer frame, and a pair of shared engines are vertically disposed inside the outer frame Flow fan.
所述的贯流式空气悬浮平台, 其特征在于包括内边框, 所述的内边框四周 设置外边框, 所述的外边框中设有贯流风机, 所述的贯流风机按照顺时针或逆 时针排列, 所述的贯流风机的风机轴与发动机的转轴连接。  The cross-flow air suspension platform is characterized in that it comprises an inner frame, an outer frame is arranged around the inner frame, a cross-flow fan is arranged in the outer frame, and the cross-flow fan is clockwise or reverse In the hour hand arrangement, the fan shaft of the cross flow fan is connected to the rotating shaft of the engine.
所述的贯流式空气悬浮平台, 其特征在于内边框中固定设置一组固定板。 所述的贯流式空气悬浮平台, 其特征在于包括外边框, 所述的外边框四个 周角上分别固定设置贯流风机, 所述的贯流风机的风机轴上连接变速箱, 所述 的变速箱上连接发动机。 所述的贯流式空气悬浮平台, 其特征在于所述的贯流风机上连接有舵机。 所述的贯流式空气悬浮平台, 其特征在于所述的变速箱与发动机上设有供 外部控制系统连接的控制口。 The cross-flow air suspension platform is characterized in that a set of fixing plates are fixedly arranged in the inner frame. The cross-flow air suspension platform is characterized in that: an outer frame is arranged, and a cross-flow fan is fixedly disposed on four circumferential corners of the outer frame, and the fan shaft of the cross-flow fan is connected to the gearbox, The engine is connected to the gearbox. The tubular air suspension platform is characterized in that a steering gear is connected to the cross flow fan. The tubular air suspension platform is characterized in that the gearbox and the engine are provided with a control port for connecting an external control system.
本发明的作用和效果 : 1.它可以使真正的飞行汽车出现, 并且革了大部分直 升机和一部分汽车的命; 2.实现未来巨大面积和体积城市中的快捷交通; 3.减 少城市道路建设和外围高速公路建设最大限度节约土地保护自然环境; 4.本飞 行装置在空中出现紧急故障时,因为其结构小巧额而且无外在高速旋转装置,那 么在高空出故障时候可以使用降落伞降落,在极低空出现故障可以运用蜂窝式 气囊保护整个飞行器, 从而最大限度保护内部乘客的安全,也避免了现有飞行器 在飞行中要么不出事,出事绝大多数无幸存者的可怕局面, 在特殊情况下还可运 用于在崎岖山地作战时的气动悬浮担架用于运送战斗伤员, 也可以适用于战地 小批量战地物资和给养的高效率输送。  The function and effect of the invention: 1. It can make the real flying car appear, and the life of most helicopters and a part of the car; 2. Realize the rapid traffic in the huge area and volume city in the future; 3. Reduce the urban road construction And the construction of peripheral highways to maximize the protection of the land to protect the natural environment; 4. When the flight device has an emergency fault in the air, because of its small structure and no external high-speed rotating device, it can use the parachute to land when the high altitude fails. In the event of a very low altitude, the entire aircraft can be protected by a honeycomb airbag, thereby maximizing the safety of the internal passengers, and avoiding the fact that the existing aircraft is in flight or not, and the vast majority of the survivors have no terrible situation, in special circumstances. It can also be used for aerodynamic suspension stretchers in the battle of rugged mountains to transport combat wounded, and can also be applied to high-efficiency transport of small quantities of battlefield materials and supplies in the field.
附图说明 DRAWINGS
图 1是本发明的贯流式空气悬浮平台的贯流风机结构示意图;  1 is a schematic structural view of a cross flow fan of a cross flow air suspension platform of the present invention;
图 2是本发明的贯流式空气悬浮平台的第一种实施例的结构示意图; 图 3是本发明的贯流式空气悬浮平台的第二种实施例的结构示意图; 图 4是本发明的贯流式空气悬浮平台的第三种实施例的结构示意图; 图 5 是本发明的贯流式空气悬浮平台的设置前进和刹车动力装置的结构示 意图;  2 is a schematic structural view of a first embodiment of a through-flow air suspension platform of the present invention; FIG. 3 is a schematic structural view of a second embodiment of a tubular air suspension platform of the present invention; FIG. 5 is a schematic structural view of a third embodiment of a through-flow air suspension platform; FIG. 5 is a schematic structural view of a set forward and brake power device of the tubular air suspension platform of the present invention;
图 6是本发明的贯流式空气悬浮平台的第四种实施例的结构示意图; 图 7是本发明的贯流式空气悬浮平台的第五种实施例的结构示意图; 图 8是本发明的贯流式空气悬浮平台的第六种实施例的结构示意图; 图 9是本发明的贯流式空气悬浮平台的第七种实施例的结构示意图; 图 10是本发明的贯流式空气悬浮平台的第八种实施例的结构示意图; 图中: 1一发动机; 2—风机壳; 3—风机叶轮; 4一贯流风机; 5—外圈; 6 一支撑板; 7—边梁; 8—主锥齿轮; 9一传动轴; 10-外边框; 11-内边框; 12- 固定板; 13-变速箱; 14-舵机; 15-控制口。 6 is a schematic structural view of a fourth embodiment of the throughflow air suspension platform of the present invention; FIG. 7 is a schematic structural view of a fifth embodiment of the throughflow air suspension platform of the present invention; A schematic structural view of a sixth embodiment of a throughflow air suspension platform; Figure 9 is a schematic structural view of a seventh embodiment of the through-flow air suspension platform of the present invention; Figure 10 is a schematic structural view of an eighth embodiment of the tubular air suspension platform of the present invention; 2—fan shell; 3—fan impeller; 4 consistent flow fan; 5—outer ring; 6 one support plate; 7—side beam; 8—main bevel gear; 9 one transmission shaft; 10-outer frame; Inner frame; 12- fixed plate; 13-transmission; 14-rudder; 15-control port.
具体实施方式 detailed description
下面结合附图对本发明进行详细说明。  The invention will be described in detail below with reference to the accompanying drawings.
如图 1所示是本发明的贯流式空气悬浮平台的基本组件,即一个贯流风机 4 与一个发动机 1连接。贯流风机 4包括圆筒形的风机壳 2, 风机壳 2上的两个对 侧分别沿着风机壳 2 圆筒长度方向设置有与圆筒长度相同的条形的进风口和出 风口, 进风口的宽度比出风口宽, 大致是出风口宽度的三倍, 出风口朝下设置。 风机壳 2中设置有圆筒形的风机叶轮 3,风机叶轮 3由沿着圆筒长度方向设置的 与圆筒长度相同的条形叶片组成, 条形叶片与圆筒的圆周切面倾斜设置, 大致 与圆筒的圆周切面之间呈 45° 角。贯流风机 4的风机轴与发动机 1的转轴连接。  As shown in Fig. 1, the basic assembly of the tubular air suspension platform of the present invention is a cross flow fan 4 connected to an engine 1. The cross flow fan 4 comprises a cylindrical fan casing 2, and two opposite sides of the fan casing 2 are respectively provided with strip-shaped air inlets and outlets of the same length as the cylinder along the length of the cylinder casing 2 At the tuyere, the width of the air inlet is wider than the air outlet, which is roughly three times the width of the air outlet, and the air outlet is facing downward. The fan casing 2 is provided with a cylindrical fan impeller 3, and the fan impeller 3 is composed of strip-shaped blades provided along the length of the cylinder and having the same length as the cylinder, and the strip-shaped blades are inclined with respect to the circumferential section of the cylinder. It is approximately at an angle of 45° to the circumferential section of the cylinder. The fan shaft of the cross flow fan 4 is connected to the shaft of the engine 1.
实施例 1  Example 1
如图 2所示是本发明的贯流式空气悬浮平台的第一种实施例, 在发动机 1 两侧分别设置转轴, 转轴各连接一根传动轴 9, 传动轴 9上分别对称设置主锥齿 轮 8, 每个主锥齿轮 8的两侧分别设置两个贯流风机 4, 贯流风机 4的风机轴与 传动轴 9垂直设置, 风机轴上设置副锥齿轮, 主锥齿轮 8与副锥齿轮相互垂直 啮合设置。 锥齿轮和贯流风机 4的数量可以根据需要进行设置, 如图 2所示, 每根传动轴 9上各设置有 4个主锥齿轮 8,每个主锥齿轮 8分别与 2个贯流风机 4连接, 一共有 8个贯流风机 4。 工作时, 靠中间的发动机 1工作, 带动传动轴 9旋转, 传动轴 9带动主锥齿轮 8旋转, 主锥齿轮 8带动副锥齿轮旋转, 从而带 动贯流风机 4 的风机轴旋转, 将空气从上面的进风口吸入, 从下面的出风口排 出, 给空气一个推力,空气也给平台一个反作作用力而使平台得到一个升力而悬 浮在空中。 为了使平台更平稳, 最好将发动机悬挂设置在平台下方。 这种平台 一般适合应用于飞行汽车, 可以用于代替普通汽车的底盘, 使汽车悬浮在空中。 2 is a first embodiment of the through-flow air suspension platform of the present invention. A rotating shaft is respectively arranged on both sides of the engine 1, and each of the rotating shafts is connected with a transmission shaft 9, and the main bevel gear is symmetrically arranged on the transmission shaft 9 respectively. 8. Two cross-flow fans 4 are respectively disposed on two sides of each main bevel gear 8. The fan shaft of the cross-flow fan 4 is vertically disposed with the transmission shaft 9, and the auxiliary bevel gear, the main bevel gear 8 and the auxiliary bevel gear are disposed on the fan shaft. Vertically meshed with each other. The number of bevel gears and cross-flow fan 4 can be set as needed. As shown in Fig. 2, each main drive shaft 9 is provided with four main bevel gears 8, each of which has two cross-flow fans respectively. 4 connections, a total of 8 cross-flow fans 4. When working, the engine 1 in the middle works to drive the drive shaft. 9 rotation, the drive shaft 9 drives the main bevel gear 8 to rotate, the main bevel gear 8 drives the auxiliary bevel gear to rotate, thereby driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, and discharging from the lower air outlet. Give the air a thrust, and the air also gives the platform a counter-force to allow the platform to gain a lift and float in the air. To make the platform smoother, it is best to place the engine suspension below the platform. This type of platform is generally suitable for use in flying cars and can be used to replace the chassis of an ordinary car to suspend the car in the air.
实施例 2  Example 2
如图 3所示是本发明的贯流式空气悬浮平台的第二种实施例, 该平台的贯 流风机 4设置在两根相互平行的边梁 7中间, 发动机 1交错设置在边梁 7外侧, 每个贯流风机 4的风机轴与一个发动机 1的转轴连接。 贯流风机 4和相应的发 动机 1的数量可以根据需要进行设置, 如图 3所示, 边梁 7中间设置有 4个贯 流风机 4, 边梁 7外侧交错设置有 4个发动机 1。 工作时, 发动机 1工作, 带动 贯流风机 4的风机轴旋转, 将空气从上面的进风口吸入, 从下面的出风口排出, 给空气一个推力,空气也给平台一个反作作用力而使平台得到一个升力而悬浮 在空中。 这种平台用途多样, 可以用于飞行汽车, 代替普通汽车的底盘, 使汽 车悬浮在空中, 也可在上面设置担架板, 用于气动悬浮担架。  As shown in FIG. 3, a second embodiment of the tubular air suspension platform of the present invention is provided. The cross flow fan 4 of the platform is disposed between two mutually parallel side beams 7, and the engine 1 is staggered outside the side beam 7. The fan shaft of each cross flow fan 4 is connected to the rotating shaft of one engine 1. The number of cross-flow fan 4 and the corresponding engine 1 can be set as required. As shown in Fig. 3, four cross-flow fans 4 are arranged in the middle of the side beam 7, and four engines 1 are staggered on the outer side of the side beam 7. During operation, the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counteracting force to make the platform Get a lift and float in the air. This platform can be used in a flying car, instead of the chassis of an ordinary car, so that the car can be suspended in the air, or a stretcher plate can be placed on it for a pneumatic suspension stretcher.
实施例 3  Example 3
如图 4所示是本发明的贯流式空气悬浮平台的第三种实施例, 该平台包括 一个外圈 5和一个支撑板 6, 支撑板 6设置在外圈 5的圆心处, 发动机 1设置在 支撑板 6上, 贯流风机 4一侧的风机轴与发动机 1转轴连接, 贯流风机 4另一 侧与外圈 5连接, 发动机 1与贯流风机 4在外圈 5内对称设置。 贯流风机 4和 发动机 1的数量可以根据需要进行设置, 在图 4中, 支撑板 6是正方形的, 正 方形的四条边的中间各设置有一个发动机 1,每个发动机 1连接一个贯流风机 4, 一共是 4个贯流风机 4, 将外圈分成 4等分。 工作时, 发动机 1工作, 带动贯流 风机 4 的风机轴旋转, 将空气从上面的进风口吸入, 从下面的出风口排出, 给 空气一个推力,空气也给平台一个反作作用力而使平台得到一个升力而悬浮在 空中。 这种平台适合用于新型的圆形飞行器。 4 is a third embodiment of the through-flow air suspension platform of the present invention. The platform includes an outer ring 5 and a support plate 6. The support plate 6 is disposed at the center of the outer ring 5, and the engine 1 is disposed at On the support plate 6, the fan shaft on the side of the cross flow fan 4 is connected to the shaft of the engine 1, and the other side of the cross flow fan 4 is connected to the outer ring 5, and the engine 1 and the cross flow fan 4 are symmetrically arranged in the outer ring 5. The number of the cross flow fan 4 and the engine 1 can be set as needed. In Fig. 4, the support plate 6 is square, and an engine 1 is disposed in the middle of the four sides of the square, and each of the engines 1 is connected to a cross flow fan 4 , A total of 4 cross-flow fans 4, the outer ring is divided into 4 equal parts. During operation, the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air. This platform is suitable for use in new round aircraft.
如图 5所示, 本发明的贯流式空气悬浮平台可以设置前进和刹车的动力装 置, 前进和刹车的动力装置也是由贯流风机 4组成, 在贯流式空气悬浮平台的 后侧连接设置有与贯流式空气悬浮平台平行或垂直的, 出风口向后设置的贯流 风机 4,在贯流式空气悬浮平台的左右两侧各连接设置有与贯流式空气悬浮平台 垂直的, 出风口向前设置的贯流风机 4, 上述贯流风机 4的风机轴与发动机 1的 转轴连接。 工作时, 发动机 1工作带动后侧的贯流风机 4的风机轴旋转, 将空 气从前面的进风口吸入, 从后面的出风口排出, 给空气一个推力,空气也给平台 一个反作作用力而使平台前进, 刹车时, 发动机工作带动左右两侧的贯流风机 4 的风机轴旋转, 将空气从后面的进风口吸入, 从前面的出风口排出, 给空气一 个推力,空气也给平台一个反作作用力而使平台前进速度减小直至停止。 这种前 进和刹车的动力装置可以安装在各种贯流式空气悬浮平台上, 用于使平台前进 和刹车。  As shown in FIG. 5, the through-flow air suspension platform of the present invention can be provided with a power device for forward and brake, and the power device for forward and brake is also composed of a cross flow fan 4, which is connected at the rear side of the cross flow air suspension platform. The cross-flow fan 4 disposed parallel to or perpendicular to the cross-flow air suspension platform and disposed at the left and right sides of the cross-flow air suspension platform is disposed perpendicular to the cross-flow air suspension platform. The cross flow fan 4 provided with the tuyere forward, and the fan shaft of the cross flow fan 4 is connected to the rotating shaft of the engine 1. During operation, the engine 1 drives the fan shaft of the cross-flow fan 4 on the rear side to rotate, sucking air from the front air inlet, discharging it from the rear air outlet, giving the air a thrust, and the air also gives the platform a counter force. When the platform is advanced, the engine works to drive the fan shaft of the cross-flow fan 4 on the left and right sides to rotate, and the air is sucked from the rear air inlet, and is discharged from the front air outlet to give the air a thrust, and the air also gives the platform a reverse Acting to reduce the speed of the platform forward until it stops. This forward and brake power unit can be mounted on a variety of cross-flow air suspension platforms for propelling and braking the platform.
实施例 4  Example 4
如图 6所示是本发明的贯流式空气悬浮平台的第四种实施例, 该平台包括 矩形结构的外边框 10,外边框 10上下外侧横向设置一对共用发动机 1的贯流风 机 4, 外边框 10内侧纵向设置一对以上共用发动机 1的贯流风机 4, 优选为在 外边框 10内侧纵向设置 4对贯流风机 4, 每对贯流风机 4共用一发动机 1。 工 作时, 发动机 1工作, 带动贯流风机 4的风机轴旋转, 将空气从上面的进风口 吸入, 从下面的出风口排出, 给空气一个推力,空气也给平台一个反作作用力而 使平台得到一个升力而悬浮在空中。 FIG. 6 is a fourth embodiment of the through-flow air suspension platform of the present invention. The platform includes an outer frame 10 of a rectangular structure, and a cross-flow fan 4 of the shared engine 1 is laterally disposed on the upper and lower sides of the outer frame 10, A pair of cross-flow fans 4 sharing the engine 1 are longitudinally disposed inside the outer frame 10, and preferably four pairs of cross-flow fans 4 are longitudinally disposed inside the outer frame 10, and each pair of cross-flow fans 4 shares an engine 1. During operation, the engine 1 is operated to drive the fan shaft of the cross flow fan 4 to rotate, and the air is taken from the air inlet above. Inhalation, discharged from the lower air outlet, gives the air a thrust, and the air also gives the platform a counter-force to allow the platform to gain a lift and float in the air.
实施例 5  Example 5
如图 7所示是本发明的贯流式空气悬浮平台的第五种实施例, 该平台包括 矩形或正方形结构的内边框 11, 内边框 11四周设置矩形结构的 4个外边框 10, 每个外边框 10中固定设置贯流风机 4, 并且贯流风机 4按顺时针或逆时针方向 排列。 每个贯流风机 4的风机轴与发动机 1的转轴连接。 工作时, 发动机 1工 作, 带动贯流风机 4 的风机轴旋转, 将空气从上面的进风口吸入, 从下面的出 风口排出, 给空气一个推力,空气也给平台一个反作作用力而使平台得到一个升 力而悬浮在空中。  FIG. 7 is a fifth embodiment of the through-flow air suspension platform of the present invention, the platform includes an inner frame 11 of a rectangular or square structure, and four outer frames 10 of a rectangular structure are disposed around the inner frame 11 A cross flow fan 4 is fixedly disposed in the outer frame 10, and the cross flow fan 4 is arranged in a clockwise or counterclockwise direction. The fan shaft of each cross flow fan 4 is connected to the shaft of the engine 1. During operation, the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air.
实施例 6  Example 6
如图 8所示是本发明的贯流式空气悬浮平台的第六种实施例, 该平台包括 矩形或正方形结构的内边框 11, 内边框 11内设置一组固定板 12, 内边框 11外 设置一圈矩形结构和正方形结构间隔的外边框 10,在矩形结构的外边框 10中设 有贯流风机 4, 在正方形结构的外边框 10中设有与贯流风机 4连接的发动机 1, 并且贯流风机 4按顺时针或逆时针方向排列。 工作时, 发动机 1工作, 带动贯 流风机 4 的风机轴旋转, 将空气从上面的进风口吸入, 从下面的出风口排出, 给空气一个推力,空气也给平台一个反作作用力而使平台得到一个升力而悬浮 在空中。  FIG. 8 is a sixth embodiment of the through-flow air suspension platform of the present invention. The platform includes an inner frame 11 of a rectangular or square structure, and a set of fixing plates 12 are disposed in the inner frame 11, and the inner frame 11 is disposed outside. a circular outer frame 10 having a rectangular structure and a square structure, a cross flow fan 4 is disposed in the outer frame 10 of the rectangular structure, and an engine 1 connected to the cross flow fan 4 is disposed in the outer frame 10 of the square structure, and The flow fan 4 is arranged in a clockwise or counterclockwise direction. During operation, the engine 1 works, driving the fan shaft of the cross flow fan 4 to rotate, sucking air from the upper air inlet, discharging from the lower air outlet, giving the air a thrust, and the air also giving the platform a counter force to make the platform Get a lift and float in the air.
实施例 7  Example 7
如图 9所示是本发明的贯流式空气悬浮平台的第七种实施例, 该平台包括 矩形结构的外边框 10, 外边框 10的四个周角上分别分隔成矩形框, 每个矩形框 中设置一对贯流风机 4, 每对贯流风机 4的风机轴均向外边框 10中心设置。 贯 流风机 4的风机壳 2上联动有舵机 14, 贯流风机 4的风机轴上连接变速箱 13, 变速箱 13上连接发动机 1,并且在变速箱 13与发动机 1上设有供外部控制系统 连接的控制口 15。 FIG. 9 is a seventh embodiment of the through-flow air suspension platform of the present invention. The platform includes an outer frame 10 of a rectangular structure, and the four corners of the outer frame 10 are respectively divided into rectangular frames, each of which is rectangular. frame A pair of cross flow fans 4 are disposed, and the fan shafts of each pair of cross flow fans 4 are disposed at the center of the outer frame 10. A steering gear 14 is coupled to the fan casing 2 of the cross flow fan 4, and a gearbox 13 is connected to the fan shaft of the cross flow fan 4, the engine 1 is connected to the gearbox 13, and an external unit is provided on the gearbox 13 and the engine 1. The control port 15 to which the control system is connected.
实施例 8  Example 8
如图 10所示是本发明的贯流式空气悬浮平台的第八种实施例, 在实施例 7 的基础上, 每个矩形框中减小 1个贯流风机 4, 其它结构均与实施例 7相同。  FIG. 10 is an eighth embodiment of the through-flow air suspension platform of the present invention. On the basis of the seventh embodiment, one cross-flow fan 4 is reduced in each rectangular frame, and other structures are the same as the embodiment. 7 is the same.
以上所述仅为本发明的较佳实施例, 并不用以限制本发明, 凡在本发明的 精神和原则之内所作的任何修改、 等同替换和改进等, 均包含在本发明的保护 范围之内。  The above is only the preferred embodiment of the present invention, and is not intended to limit the present invention. Any modifications, equivalents, and improvements made within the spirit and scope of the present invention are included in the scope of the present invention. Inside.

Claims

权利要求书 Claim
1.贯流式空气悬浮平台, 其特征在于其包括至少 2 个贯流风机 (4), 所述 贯流风机 (4) 设置在同一个平面内, 所述贯流风机 (4) 包括圆筒形的风机壳 1. A cross-flow air suspension platform, characterized in that it comprises at least two cross flow fans (4), said cross flow fans (4) being arranged in the same plane, said cross flow fan (4) comprising a cylinder Shaped fan casing
(2), 风机壳(2)上的两个对侧分别设置有进风口和出风口, 出风口朝下设置, 贯流风机 (4) 的风机轴与发动机 (1 ) 的转轴连接。 (2) The two opposite sides of the fan casing (2) are respectively provided with an air inlet and an air outlet, and the air outlet is disposed downward, and the fan shaft of the cross flow fan (4) is connected with the rotating shaft of the engine (1).
2.如权利要求 1所述的贯流式空气悬浮平台, 其特征在于所述风机壳 (2) 的进风口和出风口是沿着风机壳(2) 圆筒长度方向设置的, 与圆筒长度相同的 条形口。  2. The through-flow air suspension platform according to claim 1, wherein the air inlet and the air outlet of the fan casing (2) are disposed along a length of the cylinder of the fan casing (2), and A strip of the same length of the cylinder.
3.如权利要求 2 所述的贯流式空气悬浮平台, 其特征在于所述进风口的宽 度比出风口的宽度宽。  The tubular air suspension platform according to claim 2, wherein the air inlet has a width wider than a width of the air outlet.
4.如权利要求 3所述的贯流式空气悬浮平台, 其特征在于所述进风口的宽 度是出风口宽度的三倍。  4. The throughflow air suspension platform of claim 3 wherein said air inlet has a width that is three times the width of the air outlet.
5.如权利要求 1所述的贯流式空气悬浮平台, 其特征在于所述风机壳 (2) 中设置有圆筒形的风机叶轮 (3), 风机叶轮 (3) 由沿着圆筒长度方向设置的, 与圆筒长度相同的条形叶片组成, 所述条形叶片与圆筒的圆周切面倾斜设置。  The through-flow air suspension platform according to claim 1, characterized in that the fan casing (2) is provided with a cylindrical fan impeller (3), and the fan impeller (3) is arranged along the cylinder It is composed of strip-shaped blades of the same length as the length of the cylinder, and the strip-shaped blades are inclined with respect to the circumferential section of the cylinder.
6.如权利要求 5所述的贯流式空气悬浮平台, 其特征在于所述的条形叶片 与圆筒的圆周切面之间呈 45° 角设置。  6. A cross-flow air suspension platform according to claim 5 wherein said strip-shaped vanes are disposed at an angle of 45 to the circumferential section of the cylinder.
7.如权利要求 1所述的贯流式空气悬浮平台,其特征在于所述的发动机(1 ) 两侧分别设置转轴, 所述转轴各连接一根传动轴 (9), 所述传动轴 (9) 上分别 对称设置主锥齿轮(8), 每个主锥齿轮(8)的两侧分别设置两个贯流风机(4), 贯流风机 (4) 的风机轴与传动轴 (9) 垂直设置, 风机轴上设置副锥齿轮, 主 锥齿轮 (8) 与副锥齿轮相互垂直啮合设置。 The cross-flow air suspension platform according to claim 1, wherein the engine (1) is provided with a rotating shaft on each side thereof, and each of the rotating shafts is connected with a transmission shaft (9), and the transmission shaft ( 9) The main bevel gears (8) are symmetrically arranged on the upper side, and two cross-flow fans (4) are arranged on each side of each main bevel gear (8), and the fan shaft and the transmission shaft of the cross-flow fan (4) (9) Vertically, the auxiliary bevel gear is arranged on the fan shaft, and the main bevel gear (8) and the secondary bevel gear are perpendicularly meshed with each other.
8.如权利要求 1所述的贯流式空气悬浮平台,其特征在于所述贯流风机(4) 设置在两根相互平行的边梁(7) 中间, 发动机(1 )交错设置在边梁(7)外侧。 The cross-flow air suspension platform according to claim 1, characterized in that the cross flow fan (4) is disposed between two parallel side beams (7), and the engine (1) is staggered at the side beam (7) Outside.
9.如权利要求 1所述的贯流式空气悬浮平台,其特征在于包括一个外圈(5) 和一个支撑板 (6), 支撑板 (6) 设置在外圈 (5) 的圆心处, 发动机 (1 ) 设置 在支撑板 (6) 上, 贯流风机 (4)一侧的风机轴与发动机 (1 ) 转轴连接, 贯流 风机 (4) 另一侧与所述外圈 (5) 连接, 发动机 (1 ) 与贯流风机 (4) 在外圈 9. The through-flow air suspension platform according to claim 1, comprising an outer ring (5) and a support plate (6), the support plate (6) being disposed at a center of the outer ring (5), the engine (1) is disposed on the support plate (6), the fan shaft on one side of the cross flow fan (4) is connected to the rotating shaft of the engine (1), and the other side of the cross flow fan (4) is connected to the outer ring (5). Engine (1) and cross flow fan (4) in outer ring
(5) 内对称设置。 (5) Internally symmetric setting.
10.如权利要求 1所述的贯流式空气悬浮平台, 其特征在于在贯流式空气悬 浮平台的后侧连接设置有与贯流式空气悬浮平台平行或垂直的, 出风口向后设 置的贯流风机 (4), 在贯流式空气悬浮平台的左右两侧各连接设置有与贯流式 空气悬浮平台垂直的, 出风口向前设置的贯流风机 (4), 上述贯流风机 (4) 的 风机轴与发动机的转轴连接。  10 . The through-flow air suspension platform according to claim 1 , wherein a rear side connection of the tubular air suspension platform is disposed parallel or perpendicular to the cross flow air suspension platform, and the air outlet is disposed rearward. The cross flow fan (4) is connected with a cross flow fan (4) disposed on the left and right sides of the cross flow air suspension platform and perpendicular to the cross flow air suspension platform, and the air outlet is arranged forwardly, and the cross flow fan ( 4) The fan shaft is connected to the shaft of the engine.
11.如权利要求 1所述的贯流式空气悬浮平台,其特征在于包括外边框 ( 10), 所述的外边框 (10) 上下外侧横向设置一对共用发动机 (1 ) 的贯流风机 (4), 所述的外边框 (10) 内侧纵向设置一对以上共用发动机 (1 ) 的贯流风机 (4)。  The cross-flow air suspension platform according to claim 1, further comprising an outer frame (10), wherein the outer frame (10) is laterally disposed with a pair of cross-flow fans sharing the engine (1) 4), a pair of cross-flow fans (4) of the shared engine (1) are longitudinally disposed inside the outer frame (10).
12.如权利要求 1所述的贯流式空气悬浮平台,其特征在于包括内边框 ( 11 ), 所述的内边框(11 ) 四周设置外边框(10), 所述的外边框(10) 中设有贯流风 机(4), 所述的贯流风机 (4) 按照顺时针或逆时针排列, 所述的贯流风机(4) 的风机轴与发动机 (1 ) 的转轴连接。  The cross-flow air suspension platform according to claim 1, comprising an inner frame (11), an outer frame (10) disposed around the inner frame (11), and the outer frame (10) There is a cross flow fan (4), the cross flow fan (4) is arranged clockwise or counterclockwise, and the fan shaft of the cross flow fan (4) is connected to the rotating shaft of the engine (1).
13.如权利要求 12所述的贯流式空气悬浮平台, 其特征在于内边框 (11 ) 中固定设置一组固定板 (12)。  13. A through-flow air suspension platform according to claim 12, characterized in that a set of fixing plates (12) are fixedly arranged in the inner frame (11).
14.如权利要求 1所述的贯流式空气悬浮平台,其特征在于包括外边框 ( 10), 所述的外边框 (10) 四个周角上分别固定设置贯流风机 (4), 所述的贯流风机 (4) 的风机轴上连接变速箱 (13), 所述的变速箱 (13) 上连接发动机 (1)。 14. The throughflow air suspension platform of claim 1 including an outer frame (10), a cross-flow fan (4) is fixedly disposed on the four outer corners of the outer frame (10), and the gearbox (13) of the cross-flow fan (4) is connected to the gearbox (13), and the gearbox (13) ) Connect the engine (1).
15.如权利要求 14所述的贯流式空气悬浮平台, 其特征在于所述的贯流风 机 (4) 上连接有舵机 (14)。  15. A through-flow air suspension platform according to claim 14, characterized in that a steering gear (14) is connected to the cross-flow fan (4).
16.如权利要求 14所述的贯流式空气悬浮平台, 其特征在于所述的变速箱 ( 13) 与发动机 (1 ) 上设有供外部控制系统连接的控制口 (15)。  16. A through-flow air suspension platform according to claim 14, wherein said gearbox (13) and said engine (1) are provided with a control port (15) for connection to an external control system.
PCT/CN2012/000852 2011-09-21 2012-06-19 Through-flow air suspension platform WO2013040847A1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
CN2011203548626U CN202279234U (en) 2011-09-21 2011-09-21 Tubular air suspension platform
CN201110281430.1 2011-09-21
CN201110281430.1A CN102358423B (en) 2011-09-21 2011-09-21 Through-flow air suspension platform
CN201120354862.6 2011-09-21

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WO2013040847A1 true WO2013040847A1 (en) 2013-03-28

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* Cited by examiner, † Cited by third party
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US3212735A (en) * 1956-12-07 1965-10-19 Laing Nikolaus Thrust means for powering aircraft
US3082976A (en) * 1960-07-02 1963-03-26 Dornier Werke Gmbh Aircraft with ground effect landing gear
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CN202279234U (en) * 2011-09-21 2012-06-20 陈晓春 Tubular air suspension platform

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