CN1215955C - High-speed transportation system - Google Patents
High-speed transportation system Download PDFInfo
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- CN1215955C CN1215955C CN 02123942 CN02123942A CN1215955C CN 1215955 C CN1215955 C CN 1215955C CN 02123942 CN02123942 CN 02123942 CN 02123942 A CN02123942 A CN 02123942A CN 1215955 C CN1215955 C CN 1215955C
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- aircraft
- wheel
- fuselage
- metope
- track
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Abstract
The present invention relates to a high-speed transportation system for transporting persons and goods at a high speed. An aircraft with wheels goes forward on a track of a wall surface through functions of rolling of horizontal drive wheels and electric screw propellers arranged on wings of the aircraft. When the speed reaches a certain value, lift force is generated by the wings on the aircraft, and the aircraft flies in the air at a high speed. Wheels in the horizontal direction and the horizontal drive wheels on the aircraft are always tightly combined with the wall surface of the track of the wall surface in a motion process of the aircraft. The dynamic force of the aircraft is provided by a motor, and the energy is electric energy. The electrical energy is conveyed through an electricity transmission bare wire arranged above the track of the wall surface, an electric connecting bow installed on the aircraft tightly contacts the electricity transmission bare wire, and the electrical energy is guided to the motor in the aircraft. Thus, the forward dynamic force of the aircraft is generated.
Description
Technical field: this transrapid system is in Communication and Transportation Engineering, is used for the novel high speed transport systems of rapid transit personnel and goods, belongs to a kind of transport facility.
Background technology: both at home and abroad, existing transrapid system is a lot, as the aircraft transport systems, and the express highway transport systems, high-speed railway transport system, and state-of-the art magnetic suspension train transport systems etc.All there are some problems in these transport systemss: it is big, to aerial contamination greatly, easily kidnapped by the terrorist that the aircraft dispatch system exists traffic cost height, energy consumption; Express highway transport systems investment is big, travelling speed is low, easily meet with a traffic accident; The high-speed railway transport system investment is big, the maintenance management work capacity is big; The investment of state-of-the art magnetic suspension train transport systems is relatively bigger, whether the people impaired than the health in the high-intensity magnetic field, still is worth research.
Summary of the invention: design goal of the present invention is a shortcoming of attempting to overcome above-mentioned existing transrapid system, adopts newly-designed metope track and course of new aircraft, thereby a kind of novel high speed transport systems is provided.
Structure of the present invention is provided by following examples and accompanying drawing thereof.
Description of drawings: Fig. 1 is the scheme drawing of the transrapid system of proposition according to the present invention.
Fig. 2 is the partial enlarged drawing of Fig. 1.
The specific embodiment: describe structure of the present invention and service condition in detail below in conjunction with Fig. 1, Fig. 2.
This transrapid system is made up of left-right symmetric [] type metope track (1) aircraft (2).Wing (4), tailplane (5) and elevating rudder (22) are installed on the fuselage (3) of aircraft (2).The every side in both sides of fuselage (3) be equipped with vertical bearing wheel (6) two or more vertical safety wheel (7) two or more.Fuselage (3) front part sides, every side are installed down the horizontal direction of adjustable direction and are taken turns (8) one.Fuselage (3) both sides, it is one or more that every side is installed horizontal drive wheel (9).Fuselage (3) both sides, every side are installed 1 and are connect electricity bow (10), connect electricity bow (10) and will send closely butt of electric bare wire (11) with install on metope track (1) top.Wing (4) left-right symmetric be mounted with electric screw slurry (12) two or more.
Vertical bearing wheel (6) will be installed in same vertical surface with vertical safety wheel (7), and this vertical surface requires in the inboard of the metope (25) of metope track (1), and vertical bearing wheel (6) can not be run into metope (25) with vertical safety wheel (7) like this.Each vertical bearing wheel (6) is installed, also require the wheel bottom radially outer (13) to be in same horizontal surface, that is to say, each vertical bearing wheel (6) will with lower horizontal plane (14) closed contact of metope track (1), the width requirement of lower horizontal plane (14) is wide to move to vertical bearing wheel (6) is always gone up at lower horizontal plane (14).
The wheel of horizontal direction wheel (8) and horizontal drive wheel (9) is outer (15) radially, require to be installed in same vertical surface.That is to say that horizontal direction wheel (8) and horizontal drive are taken turns after (9) install, its wheel radially outer (15) will with metope (25) closed contact of metope track (1).
Vertical bearing wheel (6) is installed on the bottom of fuselage (3), and the lower, transverse outer (16) of installation requirement horizontal direction wheel (8) and horizontal drive wheel (9) will be higher than vertical bearing wheel (6) bottom radially outer (13).The top of the vertical safety wheel of installation requirement (7) is outer (17) radially, be higher than the upper lateral outer (18) of horizontal direction wheel (8) and horizontal drive wheel (9); Simultaneously, outer (17) top radially outer (19) that will be higher than vertical bearing wheel (6) radially, the top that also requires vertical safety wheel (7).The bottom of the vertical safety wheel of installation requirement is outer (20) bottom radially outer (13) that will be higher than vertical bearing wheel (6) radially.
The overhead height of [] shape metope track (1) will be lower than the height of the lower edge face of the wing (3) of aircraft (2) and empennage (5).The electric screw slurry (12) that is loaded on wing (3) both sides will be installed in the both sides of metope track (1), can not collide with metope track lateral surface.Metope track (1) can be symmetrical [] shape, also can be
Shape.Metope track (1) can be layed in ground level, also can frame on many pillars (21), form overhead metope track.
Transrapid system of the present invention is work like this: when aircraft (2) starts, be installed on and connect electricity bow (10) on the fuselage (3) of aircraft (2), obtain electric current from the electric bare wire (11) that send that is installed on the metope track (1), electric current is through aircraft (2) internal computer control system (23), flow to the electrical motor that each drives horizontal drive wheel (9) and electric screw slurry (12), behind each motor starting, horizontal drive wheel (9) rotates, propeller (12) rotation.Under the effect of horizontal drive wheel (9) and propeller (12), aircraft (2) advances along the metope track.After aircraft (2) speed reached certain value, under the raising force effect of the wing (4) of aircraft (2), aircraft (2) rose to the sky, and the vertical bearing wheel (6) on the aircraft (2) breaks away from the lower horizontal plane (14) of metope tracks (1).At this moment, the horizontal direction on the aircraft (2) wheel (8) and horizontal drive take turns (9) still with metope (25) closed contact of wall track (1).
Under the manipulation of computerized control system (23), elevating rudder (22) the automatic compensation horizontal direction of aircraft (2), both made the vertical bearing of aircraft (2) take turns the lower horizontal plane (14) that (6) do not contact metope track (1), and made vertical safety wheel (7) not contact the upper horizontal plane (24) of metope track (1) again.
The accident if aircraft (2) in-to-in computerized control system (23) meets accident, elevating rudder (22) Control Failure of aircraft (2), the vertical safety wheel of aircraft (2) may touch the upper horizontal plane (24) of metope track, and perhaps the vertical bearing of aircraft (2) wheel (6) may touch the firm lower horizontal plane of metope track (14).Even like this, aircraft (2) the metope track (1) that also can not fly out causes fatal crass's accident.
Contemporary space shuttle is owing to the requirement of inner air and outer air pressure reduction, and fuselage will be done very firmly, and this has just increased the aircraft deadweight.The explosive motor of aircraft, jet turbine propelling screw engine or turbojet are heavier, and to carry amount of fuel very big in addition, cause contemporary space shuttle take-off weight very big.For example, the Boeing-767 that carrying is 224-200ER type aircraft, take-off weight reaches 179.172 tons.Aircraft of the present invention (2) is low-latitude flying, walks in metope track (1) again, does not have the possibility of head-on collision, and fuselage (3) deadweight is very light.Institute's distribution motivation is not heavy in addition, does not need to be with fuel oil, so whole aircraft (2) very light in weight yet.
Transrapid system of the present invention has the following advantages:
1, construction investment is little.
2, travelling speed height.
3, safe.
4, maintenance management work capacity is little.
5, aircraft (2) very light in weight.
6, use electric energy, energy consumption is low, not foul air.
7, traffic cost is low.
Claims (10)
1, in the Communication and Transportation Engineering, be used for a kind of transrapid system of rapid transit personnel and goods, this transport systems is made up of metope track (1) and aircraft (2), it is characterized in that:
A, metope track (1) are made of symmetrical [] shape, and metope track (1) top is equipped with send electric bare wire (11),
Wing (4), tailplane (5) and elevating rudder (22) are installed on the fuselage (3) of b, aircraft (2); Fuselage (3) both sides are equipped with vertical bearing wheel (6), vertical safety wheel (7); Fuselage (3) front part sides is equipped with horizontal direction wheel (8); Fuselage (3) both sides are equipped with horizontal drive wheel (9) and connect electricity bow (10); Wing (4) is mounted with electric screw slurry (12).
2, system according to claim 1 is characterized in that metope track (1) can be [] shape, also can be
Shape; The overhead height of metope track (1) will be lower than the height of the lower edge face of wing (3) on the aircraft (2) and empennage (5); The electric screw slurry (12) that two lateral surfaces of metope track (1) will articulate with wing (3) both sides of aircraft (2) is at regular intervals, can not collide; Metope track (1) can be layed in ground, also can frame on many pillars (21), form overhead metope track.
3, according to claim 1,2 described systems, it is characterized in that fuselage (3) front part sides of aircraft (2), it is one or more that every side is installed down (8) one on horizontal direction wheel, the horizontal drive wheel (9) of adjustable direction; Fuselage (3) both sides of aircraft (2), every side install vertical bearing wheel (6) two or more, vertical safety wheel (7) two or more; Fuselage (3) both sides of aircraft (2), every side are installed one and are connect electricity bow (10), connect electricity bow (10) and will send closely butt of electric bare wire (11) with install on metope track (1) top.
4, according to claim 1,2 described systems, the fuselage (3) that it is characterized in that aircraft (2) is gone up vertical bearing wheel (6) and vertical safety wheel (7) of installing, requirement is installed in same vertical surface, this vertical surface requires in the inboard of the metope (25) of metope track (1), and vertical bearing wheel (6) can not be run into metope (25) with vertical safety wheel (7) like this.
5, according to claim 1,2 described systems, it is characterized in that each vertical bearing wheel (6) that aircraft (2) is upward installed, requirement wheel bottom radially outer (13) will be in same horizontal surface, like this lower horizontal plane (14) closed contact of each vertical bearing wheel (6) and metope track (1).
6,, it is characterized in that wide always the going up at lower horizontal plane (14) to the vertical bearing wheel (6) that makes aircraft (2) of width requirement of the lower horizontal plane (14) of metope track (1) moved according to claim 1,2 described systems.
7, according to claim 1,2 described systems, it is characterized in that wheel that horizontal direction wheel (8) that aircraft (2) go up to be installed and horizontal drive take turns (9) radially outer (15), requirement is installed in same vertical surface, and require horizontal direction wheel (8) and horizontal drive to take turns after (9) install, its wheel radially outer (15) will with metope (25) closed contact of metope track (1).
8, according to claim 1,2 described systems, the bottom that it is characterized in that the vertical bearing wheel (6) that install fuselage (3) bottom of aircraft (2) radially outer (13) requires to be lower than the lower, transverse outer (16) that horizontal direction wheel (8) and horizontal drive are taken turns (9).
9, according to claim 1,2 described systems, the top that it is characterized in that the vertical safety wheel (7) that the fuselage (3) of aircraft (2) go up to be installed is outer (17) radially, be higher than the upper lateral outer (18) that horizontal direction wheel (8) and horizontal drive are taken turns (9).
10, according to claim 1,2 described systems, the top that it is characterized in that the vertical safety wheel (7) on the fuselage (3) of aircraft (2) is outer (17) radially, and the top that be higher than vertical bearing wheel (6) is outer (19) radially; The bottom of the vertical safety wheel (7) on aircraft (2) fuselage (3) is outer (20) radially, and the bottom that be higher than vertical bearing wheel (6) is outer (13) radially.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02123942 CN1215955C (en) | 2002-07-09 | 2002-07-09 | High-speed transportation system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02123942 CN1215955C (en) | 2002-07-09 | 2002-07-09 | High-speed transportation system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1386673A CN1386673A (en) | 2002-12-25 |
| CN1215955C true CN1215955C (en) | 2005-08-24 |
Family
ID=4745268
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02123942 Expired - Fee Related CN1215955C (en) | 2002-07-09 | 2002-07-09 | High-speed transportation system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1215955C (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111301441B (en) * | 2019-12-31 | 2021-05-07 | 张帅 | Three-dimensional layered space buoyancy traffic system above urban highway |
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2002
- 2002-07-09 CN CN 02123942 patent/CN1215955C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN1386673A (en) | 2002-12-25 |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20050824 Termination date: 20090810 |