US20150307112A1 - Suspension Transport System - Google Patents

Suspension Transport System Download PDF

Info

Publication number
US20150307112A1
US20150307112A1 US14/342,378 US201214342378A US2015307112A1 US 20150307112 A1 US20150307112 A1 US 20150307112A1 US 201214342378 A US201214342378 A US 201214342378A US 2015307112 A1 US2015307112 A1 US 2015307112A1
Authority
US
United States
Prior art keywords
tracks
disposed
wheels
transport system
wheel
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.)
Abandoned
Application number
US14/342,378
Other languages
English (en)
Inventor
Marvin Liu
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of US20150307112A1 publication Critical patent/US20150307112A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B15/00—Combinations of railway systems
    • 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
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B5/00—Elevated railway systems without suspended vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61C—LOCOMOTIVES; MOTOR RAILCARS
    • B61C11/00—Locomotives or motor railcars characterised by the type of means applying the tractive effort; Arrangement or disposition of running gear other than normal driving wheel
    • B61C11/06—Locomotives or motor railcars characterised by the type of means applying the tractive effort; Arrangement or disposition of running gear other than normal driving wheel tractive effort applied or supplied by aerodynamic force or fluid reaction, e.g. air-screws and jet or rocket propulsion
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61C—LOCOMOTIVES; MOTOR RAILCARS
    • B61C15/00—Maintaining or augmenting the starting or braking power by auxiliary devices and measures; Preventing wheel slippage; Controlling distribution of tractive effort between driving wheels
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T30/00—Transportation of goods or passengers via railways, e.g. energy recovery or reducing air resistance

Definitions

  • the present invention relates to a transport system, and more particularly, to a suspension transport system.
  • Automobile In our lives, common transport tool includes automobiles, trains, airplanes, ships, electric motor car, motorcycle, bicycles, etc.
  • Automobile has several types. According to the practical use, it includes passenger automobiles specialized for persons such as cars and coaches; cargo automobiles specialized or mainly for carrying goods such as vans, special truck, tipper trucks, tractor, etc.; other automobiles specialized for construction engineering, municipal public utilities, agriculture, race, etc. According to the adaptability to roads, it includes ordinary automobiles and SUVs.
  • power machine it includes piston-internal combustion engine automobiles, electric automobiles and gas turbine automobiles. Aircrafts also has many types.
  • civil aviation aircraft such as civil passenger aircraft, cargo aircraft, passenger and cargo aircraft and helicopter, as well as national aviation aircraft for army, police, customs and others.
  • type of aircraft engine it includes propeller-driven aircraft and jet aircraft.
  • flight speed it includes subsonic aircraft and supersonic aircraft.
  • Small household aircraft is also an important part of the aircraft, but limitations has been applied on it due to the complexity and difficulty by the air traffic management on the number of small household aircraft, which also brings high cost. Therefore, small household aircraft can not be widely used as a common transport tool.
  • an object of the present invention is to provide a suspension transport system which not only can travel on land, but also can travel rapidly on the tracks, and has low cost and may be used as a common transport tool.
  • a suspension transport system characterized in that: it includes operation tracks, a carrier device, flight wings, a connection device, driving devices, braking devices and a control device; said flight wings are of more than one wing-shaped structures which can generate a lift under the aerodynamic effect; said connection device includes a vertical shaft and a wheel axle connected to said vertical shaft, and disposed on each of the extended ends of the wheel axle are wheels that operate on the operation tracks; the flight wings are connected to and above the carrier device by means of connection device; disposed above the operation tracks is an operation space that restricts the wheel suspension height, and a feedback device is disposed between the operation tracks and the operation space; the driving devices at least include wheel driving devices that drive the wheels to operate; the braking devices include wheel braking devices and flight wing braking devices; the driving devices, the braking devices, and the feedback device are connected to the control device, which collects feedback device information, and transmits instructions to driving devices and braking devices.
  • an aircraft engine Disposed on the flight wings is an aircraft engine that drives said flight wings to operate.
  • the flight wings are a set of wing-shaped structure with the left and right sides extending symmetrically.
  • the flight wings are of a streamline-shaped structure which has a front portion of circular arc which extends backward.
  • the flight wings are of more than two which includes front and rear portions to be connected onto the connection device; or of more than two which includes upper and lower portions to be connected onto the connection device.
  • the operation tracks include several track supports spaced along the track operation direction, on which four tracks are spaced in parallel, wherein the vertical shaft operate between the two inside tracks, and the wheels operate between two outside tracks; the carrier device is located below the four tracks, and disposed on the vertical shaft which is below the four tracks is a limit rod; a feedback device is disposed between the limit rod and the tracks; the distance between the limit rod and the wheel axle is the operation space that restricts the wheel suspension height; rolling devices are connected on two ends of the limit rod, and on the vertical shaft between the limit rod and the wheel axle, respectively.
  • the operation tracks include several track supports spaced along the track operation direction, on which two tracks are spaced in parallel, wherein one limit track is disposed above each of the two tracks, and a feedback device is disposed at the bottom edge of the limit tracks; the vertical shaft operates between the two tracks, the flight wings are located above the two tracks, the carrier device is located below the two tracks, between the tracks and limit tracks is an operation space that restricts the wheel suspension height, and the wheels are located in the operation space.
  • each of the tracks and limit tracks above it are oppositely provided with a pair of protrusions extending along the track operation direction, wherein between the two protrusions is an operation space that restricts the wheel suspension height, and corresponding to the two protrusions, recesses are disposed around the circumference of the wheels which are located in the operation space restricted by the two protrusions; a feedback device is disposed on the bottom protrusion of the limit tracks.
  • the operation tracks are two tracks which are spaced to be laid on the ground, above each of which one limit track is connected and parallel with the track, wherein between the tracks and limit track is an operation space that restricts the wheel suspension height, and the wheels are located in the operation space; a feedback device is provided at the bottom edge of the limit track; the vertical shaft is divided into two portions, wherein the upper end of the upper portion of the vertical shaft is connected to the flight wings, and its lower end is connected to the carrier device; the upper end of the lower portion of the vertical shaft is connected to the carrier device, and its lower end is connected to the wheel axle.
  • each of the tracks and the limit tracks above it are oppositely provided with a pair of protrusions extending along the track operation direction, wherein between the two protrusions is an operation space that restricts the wheel suspension height, and corresponding to the two protrusions, recesses are disposed around the circumference of the wheels which are located in the operation space restricted by the two protrusions; a feedback device is disposed on the bottom protrusion of the limit tracks.
  • the track supports include two stubs correspondingly supporting each of the tracks respectively, wherein one connection beam is connected between the two stubs and a tow rope is disposed outside of the track supports.
  • extrusion-type speed reduction devices which include air pumps disposed inside the two tracks, wherein the periphery of the air pump is provided with a semicircular telescopic structure, and an extrusion plate is disposed on the inside surface of the telescopic structure.
  • a sliding contact power feeding device including transmission wires disposed along the tracks, and also including a contact electricity-taking appliance disposed outside the wheels, wherein the contact electricity-taking appliance contacts the transmission wires and is electrically connected to the wheel motor located inside of the wheels.
  • an impact cushion device Disposed at the front and rear portions of the connection device or at the front portion and rear portion of the carrier device is an impact cushion device which is a bar-shaped structure, and its outer end is provided with one rectangular impact plate, whose bottom is provided with a rolling device mounted on the operation tracks.
  • the present invention has the following advantages: 1. the present invention connects flight wings with a carrier device and operates on tracks, so that when reaching a certain travel speed, the wings generate a lift, making the load on tracks enter into a critical take-off state, and the pressure applied on tracks by the load during operation is very small, wherein the role of tracks played in the entire device is mainly the operation direction, significantly reducing the requirements for track construction, and reducing construction cost, which is obviously better than the existing track transport, and its operation track construction cost is significantly lower than ordinary road construction cost. 2.
  • the present invention connects flight wings with a carrier device, making the load on tracks enter into the critical take-off state, so that the load-to-track pressure during operation is very small, and at this time, when using wheel motor to drive, the carrier device may be moved rapidly without requiring a quite large driving torque, which can produce a significant effect on energy conservation compared with the existing transport tool. 3.
  • the present invention connects flight wings with a carrier device, making the load on tracks enter into the critical take-off state, significantly reducing operation resistance, which can make the speed of the carrier device on tracks close to the aircraft, and the household aircraft-like transport tool truly achieve family use. 4.
  • the operation tracks of the present invention may be disposed in the air, and the tracks may be used as a power feeding structure at the same time, which solves the current project condition that the current track transport requires to set up additional power feeding structure. 5.
  • the present invention is suspended to operate at low altitude by means of the tracks, while provided with an anti-impact impact cushion device at the front and rear without aircraft crashing risks, and without direct impact risk of cars and trains, which therefore significantly improves the safety and controllability of the use of the transport system.
  • the present invention may be used in a variety of air-land amphibious transport tools, adding a new type for the existing transport tool, which not only can meet people's fast-paced life requirement, but can greatly improve the transport efficiency of personalized transport tools at the same time; it has a great meaning, and has good application prospect for improving the existing transport tool condition and developing a new type of transport tool, while meeting people's consumption requirement.
  • FIG. 1 is a schematic view of Embodiment 1 of the transport system of air track operation of the present invention.
  • FIG. 2 is a partial schematic view of Embodiment 1 of the transport system of air track operation of the present invention.
  • FIG. 3 is a schematic view of Embodiment 2 of the transport system of air track operation of the present invention.
  • FIG. 4 is a schematic view of Embodiment 3 of the transport system of air track operation of the present invention.
  • FIG. 5 is a schematic view of the transport system of ground operation track of Embodiment 4 of the present invention.
  • FIG. 6 is a schematic view of installation of the impact cushion device of the present invention.
  • FIG. 7 is a top schematic view of installation of the impact cushion device of the present invention.
  • FIG. 8 is a schematic view of the impact cushion device of the present invention.
  • FIG. 9 is a schematic view of extrusion state of extrusion-type speed-reducing device of the present invention.
  • FIG. 10 is a schematic view of open state of extrusion-type speed-reducing device of the present invention.
  • FIG. 11 is a schematic view of track supports of the present invention.
  • FIG. 12 is a schematic view of track supports supporting double-deck tracks of the present invention.
  • FIG. 13 is a schematic view of power supplying device of air operation track of the present invention.
  • FIG. 14 is a partial schematic view of power supplying device of air operation track of the present invention.
  • FIG. 15 is a schematic view of one of flight wing structures of the present invention.
  • FIG. 16 is a schematic view of the present invention that the flight wings are disposed above a carrier device in a front and rear form.
  • FIG. 17 is a top schematic view of FIG. 16 .
  • FIG. 18 is a schematic view of the present invention that the flight wings are disposed above a carrier device in an upper and lower form.
  • FIG. 19 is a top schematic view of FIG. 18 .
  • the present invention includes a carrier device 1 , flight wings 2 , operation tracks 3 , a connection device 4 , driving devices 5 , braking devices 6 , and a control device 7 .
  • the carrier device 1 refers to a device capable of carrying persons or goods, which may be a car or car-like traveling device having wheels capable of operating independently on the land, and can also be a parcel-shaped, box-shaped, or other shaped object capable of operating independently on the land; the shape, structure, weight, function and others of the carrier device 1 may be the feature that present vehicle or device already has, or can also be designed according to operation requirements of the present invention.
  • the flight wings 2 refers to a wing-shaped device capable of generating a lift under the aerodynamic effect, which may be a structure designed according to the principle of aerodynamics, and the flight wings 2 itself may be provided with propellers 8 .
  • the operation tracks 3 may be the tracks on the ground, and may also be the tracks elevated in the air; however, whichever track it is, an operation space that restricts wheel or vertical shaft suspension height is provided.
  • connection device 4 refers to a device which connects the carrier device 1 below the flight wings 2 , and has wheels 41 capable of traveling along the operation tracks 3 , wherein the shape of wheels 41 can vary from the structure of the operation tracks 3 .
  • the driving devices 5 may be a wheel motor 51 of driving wheels 41 , and may also be an aircraft engine 52 which drives the propellers 8 on flight wings 2 or is directly propelled to operate by a turbine.
  • the braking devices 6 may be conventional wheel braking devices 61 which are connected to wheels 41 , and can also be wing braking devices 62 connected on the flight wings 2 , wherein the wing braking devices 62 may be conventional flight spoiler-like devices, which can increase or decrease air flow resistance by changing the up and down turning angles.
  • the braking devices 6 can also be extrusion-type speed reducing devices which extend oppositely on the operation tracks 3 and can perform extrusion braking on the connection device 4 .
  • the control device 7 may be mounted on the connection device 4 , flight wings 2 , or carrier device 1 , and can also be disposed in a remote control room, but receiving ends are only provided on the connection device 4 , flight wings 2 , or carrier device 1 .
  • the wheel motor 51 , aircraft engine 52 , wheel braking devices 61 , and wing braking devices 62 are electrically connected to the control device 7 by cables or by communication signals, and a feedback device (such as sensor, ect.) is disposed between the control device 7 and them to control the travel speed of wheels 41 and the lift of the flight wings 2 by the control device 7 , so that the suspension height of wheels 41 at high speed is restricted in the operation space disposed on the operation tracks 3 .
  • the operation tracks 3 include several track supports 31 spaced along the track operation direction, on which two pairs of tracks 32 are spaced in parallel, and the connection device 4 includes vertical shaft 42 operating between two inside tracks 32 , wherein the upper end of the vertical shaft 42 is connected to flight wings 2 , and the lower end of the vertical shaft 42 is connected to a carrier device 1 .
  • At least one wheel axles 43 is disposed on the vertical 42 between flight wings 2 and operation tracks 3 , wherein two ends of wheel axles 43 are respectively connected to a wheel 41 driven by the wheel motor 51 , and the wheels 41 operate on two outside tracks 32 ;
  • one limit rod 44 is disposed on the vertical shaft 42 between the carrier device 1 and the operation tracks 32 , wherein a touch feedback device is disposed between the limit rod 44 and the tracks 32 to transmit feedback information to a control device 7 , so that the control device 7 controls flight wings 2 to drive the wheels 41 to operate in the operation space restricted in suspension height.
  • rolling devices 45 may be provided at the place where the above three contact, such as wheels, rolling pulleys, or rolling bearings, and so on.
  • the difference between the embodiment and Embodiment 1 is: two spaced tracks 32 is disposed on track support 31 in parallel, above which is respectively provided with one limit track 33 , wherein between the limit tracks 33 and the tracks 32 is an operation space that restricts the suspension height of wheels 41 , and a touch feedback device is disposed at the bottom edge of the limit track 33 to transmit feedback information to a control device 7 , so that the control device 7 controls flight wings 2 to drive wheels 41 to operate in the operation space restricted in suspension height, and at this time it may no longer dispose a limit rod 44 .
  • the difference between the embodiment and Embodiment 2 is: on each of the track 32 and the limit tracks 33 above it is oppositely provided with a pair of protrusions 34 extending along the operation direction of tracks 32 , wherein between the two protrusions 34 is an operation space that restricts the suspension height of wheels 41 , and corresponding to the two protrusions 34 , recesses are disposed around the circumference of wheels 41 which are located in the operation space restricted by the two protrusions 34 .
  • a feedback device is disposed on the bottom protrusion 34 of the limit tracks 33 to transmit feedback information to a control device 7 , so that the control device 7 controls flight wings 2 to drive wheels 41 to operate in the operation space restricted in suspension height.
  • the connection device 4 includes vertical shaft 42 which is divided into two portions, wherein the upper end of the upper portion of the vertical shaft is connected to the flight wings 2 , the lower end of the upper portion of the vertical shaft is connected to the top of carrier device 1 , and the upper end of the lower portion of the vertical shaft is connected to the bottom of the carrier device 1 , and the lower end of the lower portion of the vertical shaft is connected to the wheel axle 43 , whose extended ends are provided with wheels 41 and on which is also provided a wheel motor 51 .
  • the operation tracks 3 include two tracks 32 laid on the ground, above which limit tracks 33 are connected and parallel with the tracks 32 , correspondingly.
  • the distance between the tracks 32 and the limit tracks 33 is the operation space that restricts the suspension height of wheels 41 , and a touch feedback device is disposed at the bottom edge of the limit tracks 33 to transmit feedback information to a control device 7 , so that the control device 7 controls the flight wings 2 to make wheels 41 operate in the operation space restricted in suspension height; when operating, wheels 41 are located on the operation tracks 3 between the tracks 32 and the limit tracks 33 , and the carrier device 1 and the flight wings 2 operate above the operation tracks 3 .
  • the operation tracks 3 play a supporting role for the carrier device 1 and flight wings 2 when starting, and play a limiting role for the operation routes and areas during operation.
  • Embodiment 4 The difference between the embodiment and Embodiment 4 is: on each of the tracks 32 and the limit tracks 33 above it, a pair of protrusions 34 extending along the operation direction of the tracks 32 are oppositely provided, wherein the distance between two protrusions 34 is the operation space that restricts the suspension height of wheels 41 , and corresponding to the two protrusions 34 , recesses are disposed around the circumference of wheels 41 , which are located in the operation space restricted by two protrusions 34 .
  • a feedback device is disposed on the bottom protrusion 34 of the limit tracks 33 to transmit feedback information to a control device 7 , so that the control device 7 controls flight wings 2 to make the wheels operate in the operation space restricted in suspension height.
  • an impact cushion device 9 is provided on the vertical shaft 42 above the wheel axle 43 for avoiding the impact of at the front and rear ends; in the above Embodiment 4 and Embodiment 5, both of the front end and rear end of the carrier device 1 are provided with an impact cushion device 9 ; the impact cushion device 9 may be a bar-shaped hydraulic or pneumatic cushion device, and can also be other buffers in the prior art. As shown in FIG. 6 , FIG. 7 , and FIG. 8 , description will now be made by taking the impact cushion device 9 disposed on the vertical shaft 42 as the example.
  • the outer end of the impact cushion device 9 may be provided with one rectangular impact plate 91 , and in order to reduce impact force and friction force, a rolling device may be provided at the bottom of the impact plate 91 , which is mounted on the operation tracks 3 and may use wheels, rolling pulleys, or rolling bearings to reduce the impact force and friction force between each other during operation.
  • an extrusion-type speed reducing device 10 may be disposed at the terminal and operation range of each pair of tracks 32 .
  • the extrusion-type speed reducing device 10 includes air pump 101 disposed inside the two tracks 32 , wherein the periphery of air pump 101 is provided with a semicircular telescopic structure 102 , the inside surface of which is provided with an extrusion plate 103 , and when extruded, air pump 101 makes the telescopic structure 102 expand inwardly and thus extrude the vertical shaft 42 of the connection device 4 , thereby it is decelerated.
  • track supports 31 include two stubs 35 correspondingly supporting each of track 32 , wherein the two stubs 35 are connected by one connection beam 36 , and a tow rope 37 is provided outside the track supports 31 .
  • a power feeding device 11 may be disposed on the tracks 32 set up in the air by the track supports 31 at the same time.
  • the power feeding device 11 is a sliding contact power feeding device, including transmission wires 111 disposed along the tracks 32 , and also including a contact electricity-taking appliance 112 disposed outside the wheels 41 , wherein the contact electricity-taking appliance 112 contacts the transmission wires 111 and is connected with the wheel motor 51 located inside the wheels 41 by wires across the wheel axle center.
  • the contact electricity-taking appliance 112 slides along the transmission wires 111 with contact, obtaining the power supply required by the wheel motor 51 .
  • one of bilateral tracks is the power feeding output line, and the other is the power feeding return line, i.e., live line and zero line.
  • the flight wings 2 may use other structures of aircraft wings or similar wings capable of generating a lift under the aerodynamic effect.
  • the flight wings 2 may be a symmetrical wing-shaped structure with two extending sides (as shown in FIG. 1 ).
  • the flight wings 2 may also be a non left-and-right extending structure, but a streamline-shaped structure which has a front portion of circular arc and tapers backward (as shown in FIG. 15 ).
  • This structure has a plurality of flight wings 2 , which are distributed from the front portion to the rear portion above the carrier device 1 (as shown in FIG. 16 and FIG. 17 ); this structure has a plurality of flight wings 2 , which are distributed from upper portion and lower portion above the carrier device 1 (as shown in FIG. 18 and FIG. 19 ); the flight wings 2 of this structure preferably has a width less than twice the width of the operation tracks.
  • the present invention includes a carrier device, flight wings, and operation tracks, wherein the flight wings are above the operation tracks, the carrier device is below the operation tracks, and a connection device is connected between the flight wings and the carrier device, which is removable with the carrier device.
  • Propellers and aircraft engine are mounted on the flight wings, wheels and a wheel motor are mounted on the operation tracks, or the wheels and the wheel motor are mounted only above the operation tracks.
  • the operation tracks play a supporting role for the carrier device and flight wings when starting, and play a limiting role for the operation routes and areas during operation.
  • the carrier device travels from the ground to a start platform, the flight wings is mounted, and the wheel motor and/or aircraft engine is/are started, the carrier device supported by the operation tracks is driven and accelerated along tracks, and then the flight wings generate a lift and the carrier device moves rapidly in the take-off state.
  • the carrier device travels away from the operation tracks and enters into the decelerating export zone, sliding slowly into the stop platform.
  • the present invention includes a carrier device, flight wings, and operation tracks, wherein the carrier device is above the operation tracks, the flight wings are above the carrier device, and a connection device is connected between the flight wings and the carrier device.
  • the operation tracks play a supporting role for the carrier device and flight wings when starting, and play a limiting role for the operation routes and areas during operation.
  • An aircraft engine is provided on the flight wings, and the wheels are mounted between the tracks of the operation tracks and the limit tracks.
  • the carrier device travels from the ground to the start platform, the flight wings is mounted, and drive devices are started, the carrier device supported by the operation tracks is driven and accelerated along tracks, and then the flight wings generate a lift and the carrier device moves rapidly in the take-off state.
  • the carrier device travels away from the operation tracks and enters into the decelerating export zone, sliding slowly into the stop platform.
  • Experimental materials light wood materials, aluminum alloy tubes, propellers, engine, and remote control.
  • Preparation of experimental device as shown in FIG. 2 , engrave the left and right sections of a wing using light wood materials respectively, make the joint for the vertical shaft of the connection device using the aluminum alloy tubes, mount a set of aircraft engine and propeller on each of the left and right sides of the wing, and then produce and mount ailerons and spoilers at the rear part above the wing using light wood materials, which can turn up and communicate with a remote control receiver.
  • Experimental materials aluminum alloy tubes, bearings, DC motors, wheels, and model remote control.
  • Preparation of experimental device as shown in FIG. 2 and FIG. 8 , make a vertical shaft and a wheel axle using aluminum alloy tubes, and mount a control device and a front and rear impact buffer in the middle section of the vertical shaft, mount a connection joint for carrying goods at the lower end of the vertical shaft, and then mount a set of DC wheel motors and wheels on each of the two sides of the wheel axle.
  • Production of experimental device as shown in FIG. 11 , set up an operation track with a height of 1 m by 20 ⁇ 20 mm stainless steel square tubes, and tow it by tow ropes, which includes track supports, tracks, and tow ropes.
  • Preparation of experimental device as shown in FIG. 12 , set up an operation track with a height of 1 m by 20 ⁇ 20 mm stainless steel square tubes, and tow it by tow ropes, which includes track supports, tracks, track operation ports and tow ropes.
  • Preparation of experimental device as shown in FIG. 5 , set up an operation track with a spacing of 10 cm between tracks and limit tracks by 20 ⁇ 20 mm stainless steel square tubes, including limit tracks and tracks.
  • Preparation of experimental device choose an aviation model with a wingspan of 1.5 m and its remote control device, separate wings from the fuselage, and mount a connection device made by aluminum alloy tubes and bearings at the top of the fuselage, wherein the wings are mounted at the upper end of the connection device.
  • Preparation of experimental device choose an aviation model with a wingspan of 1.5 m, separate wings from the fuselage, remove the driving structure on wings, and mount a connection device made by aluminum alloy tubes and bearings at the top of the fuselage, wherein wings is mounted at the upper end of the connection device, and a wheel rotating-driving device made by aluminum alloy tubes, a DC motor with a maximum revolution speed of 15000 rev/min, and wheels with a diameter of 10 cm are mounted on the connection device at the lower end of wings.
  • Experimental materials aluminum alloy sheets, aluminum alloy tubes, round steel tubes, rectangular steel tubes, square steel tubes, bearings, DC motor, wheels, remote control, iron plate, and car battery.
  • Preparation of experimental device take a round steel tube with a diameter of 19 mm to be welded on the 25 mm surface of 25 ⁇ 50 mm rectangular steel tubes, form a structure of round tubes on rectangular tubes, then by taking one rectangular steel tube as a support every 6 m, set up a straight single layer double-track operation track with a height of 1.5 m and a length of 3 km, and mount eight extrusion-type speed reducing devices at the last 800 m, and then make flight wings with a wingspan length of 2.5 m by aluminum alloy sheets and aluminum alloy tubes, make a carrier device by iron plates, make a connection device between wings and the carrier device by round steel tubes with a diameter of 22 mm and bearings, and make a wheel rotating-driving device by DC motor and wheels which is connected with a 24V battery placed in the carrier device, wherein the DC motor is a permanent magnet brushless DC motor, having the rated voltage of 24V, the power of 5.5 KW, and the maximum revolution speed of 10000 rev/min, and the radius of wheel
  • connection device is mounted between wings and the carrier device on the operation tracks, then the carrier device is mounted at the lower end, flight wings are mounted at the upper end, and a wheel rotating-driving device is mounted above the tracks, wherein the wheel is of a concave shaped structure which may be ridden on the operation tracks to operate.
  • Preparation of experimental device take two 25 ⁇ 50 mm rectangular steel tubes with a length of 6 m as a track, and a 50 ⁇ 50 mm square steel tube with a height of 1 m at its two ends as a support, set up a straight single-layer operation track with a length of 6 m, wherein the spacing between the left and right tracks is 5 cm.
  • the central portion of the track that is, use pressure jacks on two sides at 3 m long to extrude the telescopic structure to close to an engagement state.
  • Experimental materials aluminum alloy sheets, aluminum alloy tubes, round steel tubes, rectangular steel tubes, square steel tubes, bearings, DC motor, wheels, remote control, iron plate, car battery, and hydraulic buffer.
  • Preparation of experimental device prepare two carrier devices. Take two hydraulic buffers, whose two ends are respectively mounted on the wide surfaces of two 25 ⁇ 50 mm rectangular steel tubes, i.e., connection plate and avoid-impacting plate, making an impact cushion device; one end of the wide surfaces of one rectangular steel tube of the impact cushion device is connected with the rear portion of wing-loaded connection device, making a rear impact cushion device, and one end of wide surfaces of the other rectangular steel tube of impact cushion device is connected with the front portion of wing-loaded connection device, making a front impact cushion device.
  • the carrier device with the front impact cushion device is placed in the initial position, and the carrier device with the rear impact cushion device is placed at 1.1 km.
  • Load is added to 200 kg in the carrier device.
  • Velocimeters are respectively mounted at 1 km and 2.1 km to detect the travel speed when the carrier device reaches 1 km and 2.1 km.
  • a motor remote shutdown device is mounted at 1 km. The experiment first remotely starts the motor of the rear carrier device, then it can be seen that wheels start, and the carrier device moves forward along the operation tracks, rapidly accelerates, and the moving speed detected when accelerating to 1 km is 187-205 km/h, and at the same time the motor is remotely closed.
  • the front carrier device is impacted by the impact plate, pushing the front carrier device to move forward, and at the same time the rear carrier device decelerates.
  • the moving speed detected when reaching 2.1 km is 76-89 km/h, and at this time, the structures of the two carrier device are as a whole without damage.
  • the carrier devices gradually decelerates and stops by the extrusion-type speed reducing device. It indicates that the impact cushion device can significantly reduce impact damages between the carrier devices on tracks, ensuring a quick and stable operation of the carrier devices. Remove the connection of the carrier devices with flight wings, and the test ends.
  • Production of experimental device choose an aviation model with a wingspan of 1.5 m, separate wings from the fuselage, and mount a connection device made by stainless steel tubes at the top of the fuselage, mount wings at the upper end of the connection device, and mount a wheel rotating-driving device made by stainless steel tube, DC motor and wheels at the lower end of the fuselage. Operation tracks are laid on the ground, including tracks and limit tracks laid on the ground, wherein wheels are located between the tracks and limit tracks.
US14/342,378 2011-09-06 2012-09-05 Suspension Transport System Abandoned US20150307112A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CN201120332427.3 2011-09-06
CN2011203324273U CN202345677U (zh) 2011-09-06 2011-09-06 一种用于交通运输的快速运载结构
PCT/CN2012/001243 WO2013033974A1 (zh) 2011-09-06 2012-09-05 一种悬浮式运载系统

Publications (1)

Publication Number Publication Date
US20150307112A1 true US20150307112A1 (en) 2015-10-29

Family

ID=46534701

Family Applications (1)

Application Number Title Priority Date Filing Date
US14/342,378 Abandoned US20150307112A1 (en) 2011-09-06 2012-09-05 Suspension Transport System

Country Status (3)

Country Link
US (1) US20150307112A1 (zh)
CN (2) CN202345677U (zh)
WO (1) WO2013033974A1 (zh)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10286925B2 (en) * 2016-09-09 2019-05-14 Michael Steward Evans Intelligent POD management and transport
US10656052B2 (en) * 2017-08-29 2020-05-19 Uatc, Llc Testing environment for autonomous vehicles
CN112050842A (zh) * 2020-09-28 2020-12-08 苟辅秀 基于无人机及网络的环境监测装置
CN112529406A (zh) * 2020-12-10 2021-03-19 长安大学 公路大件运输安全评估方法、系统、存储介质及终端设备
US11220278B2 (en) * 2018-03-17 2022-01-11 Marvin Liu High speed transportation in running tube as running rail
US11551494B2 (en) 2019-12-23 2023-01-10 Uatc, Llc Predictive mobile test device control for autonomous vehicle testing

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102975722A (zh) * 2011-09-06 2013-03-20 北京康华源科技发展有限公司 一种用于交通运输的快速运载结构及其用途
CN202345677U (zh) * 2011-09-06 2012-07-25 北京康华源科技发展有限公司 一种用于交通运输的快速运载结构
CN106184749B (zh) * 2016-09-21 2018-07-17 苏州机甲龙机械科技有限公司 一种轨道式飞机及其槽道运行系统
CN107972682A (zh) * 2016-10-21 2018-05-01 冯文水 一种悬浮高铁
CN108237087A (zh) * 2017-12-30 2018-07-03 广东技术师范学院 一种货物分流系统及方法
CN109435970A (zh) * 2018-02-02 2019-03-08 王明忠 独立的高架太阳能发电网系统、高铁电动飞机公路新专线
CN110182230B (zh) * 2019-07-01 2024-01-30 中铁二院工程集团有限责任公司 悬挂式轨道梁及气动系统

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB154168A (en) * 1919-11-21 1921-06-24 Henri Coanda Improvements in aerial transporters
DE2327024C3 (de) * 1973-05-26 1980-05-08 Vereinigte Flugtechnische Werkefokker Gmbh, 2800 Bremen Bodeneffektfahrzeug
JPS55156543A (en) * 1979-05-24 1980-12-05 Rheon Automatic Machinery Co Apparatus for changing advancing direction of dough strip
CN2239916Y (zh) * 1995-12-19 1996-11-13 杨斌 有轨飞车
CN1304847A (zh) * 2000-06-30 2001-07-25 王洵 空气悬浮轨道式高速飞车
CN1715111A (zh) * 2003-10-08 2006-01-04 尚德敏 一种高速铁路
CN2683423Y (zh) * 2003-12-24 2005-03-09 张可池 可伸展翅翼的悬浮汽车运行装置
CN101234640A (zh) * 2008-03-05 2008-08-06 叶高峰 一种新型轨道交通方法、系统及轨道系统
CN202345677U (zh) * 2011-09-06 2012-07-25 北京康华源科技发展有限公司 一种用于交通运输的快速运载结构
CN102975722A (zh) * 2011-09-06 2013-03-20 北京康华源科技发展有限公司 一种用于交通运输的快速运载结构及其用途

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10286925B2 (en) * 2016-09-09 2019-05-14 Michael Steward Evans Intelligent POD management and transport
US10656052B2 (en) * 2017-08-29 2020-05-19 Uatc, Llc Testing environment for autonomous vehicles
US11220278B2 (en) * 2018-03-17 2022-01-11 Marvin Liu High speed transportation in running tube as running rail
US11551494B2 (en) 2019-12-23 2023-01-10 Uatc, Llc Predictive mobile test device control for autonomous vehicle testing
CN112050842A (zh) * 2020-09-28 2020-12-08 苟辅秀 基于无人机及网络的环境监测装置
CN112529406A (zh) * 2020-12-10 2021-03-19 长安大学 公路大件运输安全评估方法、系统、存储介质及终端设备

Also Published As

Publication number Publication date
CN202345677U (zh) 2012-07-25
WO2013033974A1 (zh) 2013-03-14
CN104144837B (zh) 2016-08-17
CN104144837A (zh) 2014-11-12

Similar Documents

Publication Publication Date Title
US20150307112A1 (en) Suspension Transport System
CN103692873B (zh) 一种水陆飞行汽车
US9085305B2 (en) Hybrid personal transit system
CN101961974A (zh) 水陆空多域机动载运车辆
US8015925B2 (en) Air bus transportation system
CN1112292C (zh) 路面轨道两用飞车
CN102164812A (zh) 配有内部空气流推进系统的陆地车辆
CN211195749U (zh) 一种倾转无轴涵道旋翼飞行汽车
CN202528786U (zh) 地效式超低空两用飞行汽车
CN102975722A (zh) 一种用于交通运输的快速运载结构及其用途
JP5004224B2 (ja) 短距離離着陸航空機
CN104149565A (zh) 一种陆空两用多功能小车
CN106864469A (zh) 一种悬浮式运输装置及其用途
CN114655325A (zh) 一种行进设备
CN104527408A (zh) 一种能跨越障碍物的汽车
CN101112898A (zh) 超轻轨翼悬浮电力飞车
JPS63242765A (ja) 飛行車両装置
CN113911143B (zh) 一种气动悬浮列车
RU2522189C2 (ru) Экраноплан-поезд
CN202053881U (zh) 增程式空气动力汽车
CN201385664Y (zh) 空中轨道车
CN205498931U (zh) 一种高速封闭环列车
CN104265576A (zh) 飞机、船艇、火车动车组、汽车等运输机器的节能方法及其装置
CN202557241U (zh) 水陆空多功能交通工具
CN216141817U (zh) 一种新型轨道交通系统

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- INCOMPLETE APPLICATION (PRE-EXAMINATION)