CN106335638A

CN106335638A - Track aircraft

Info

Publication number: CN106335638A
Application number: CN201610840880.2A
Authority: CN
Inventors: 徐林波
Original assignee: Individual
Current assignee: Individual
Priority date: 2016-09-22
Filing date: 2016-09-22
Publication date: 2017-01-18

Abstract

A track aircraft is characterized in that the track aircraft mainly comprises a flyable object and one or one group of constraining guide rails; the flyable object is limited to operate in the constraining range and the track of the guide rail, and the guide rail serves as a take-off and landing runway of the flyable object; and a site is arranged on the side of the guide rail, so that personnel and materials can enter in and come out of the flyable object.

Description

There is orbit aerocraft

Technical field

A kind of means of transport, particularly airline instrument.

Background technology

Currently known airline instrument, mainly various can the fixed wing airplane of free flight in the air and going straight up to Machine.They are common to be disadvantageous in that: 1, complex structure, involve great expense, cost of transportation high, 2, have an air crash risk, 3, transport Amount is limited, 4, need to set up air traffic control system and the ground service service system of bulky complex, 5, for fixed wing airplane in addition it is also necessary to repair Build and take up an area huge, airport that cost is high, 6, for helicopter, flight speed is slow and carries less, and 7, for fixing circuit On, along for the mass transit of Cheng Jinhang, vehicle, especially high speed vehicle, than conventional flight fortune Defeated instrument has a clear superiority.

Content of the invention

For the problems referred to above, the invention provides one kind has orbit aerocraft, it is characterized in that: this have orbit aerocraft mainly by Can flyer (as aircraft) and one or one group constraint guide rail composition；Described can be limited in the pact of described guide rail by flyer Bundle scope and track on run, and using described guide rail as described can flyer takeoff and landing runway；In described guide rail Side arranges each website, for personnel and goods and materials turnover above-mentioned can flyer.

Above-mentioned by guide rail constrain can flyer power set, can be by the propeller of motor-driven, or its Its various known aircraft engine and power set.

By above-mentioned can flyer top with wheel hanging (or by its bottom set up) on guide rail, and the pact in guide rail Complete its rolling start in the range of bundle, leave the right or normal track and fly and slide landing.

Above-mentioned can flyer flying height, can be adjusted by changing its flight speed and lift and be controlled； And the regulation of its flight speed and lift, in addition to can passing through the various known regulation control modes of aircraft, can also use Track brake is adjusted control.

Above-mentioned can flyer left and right sides position constraint, with can magnetic force between flyer and track or both sides Directive wheel (in figure is not drawn into) is controlled by.

Above-mentioned the global shape of flyer can be similar to one section of aircraft fixed-wing, but its highly with width than traditional Aircraft fixed-wing is much larger, and the inside clear height of at least its upper section is greater than the height of ordinary people；Its shape of cross section and building Make the fixed-wing that structure is also similar to aircraft.

Above-mentioned the left and right two ends (or middle) of flyer can be hung with wheel and constrained on guide rail, and along guide rail Run；Its normal operating condition is the state of flight that leaves the right or normal track, and completes landing on guide rail.

Above-mentioned can be on flyer, the level height of front two rows wheel is adjustable.When above-mentioned can flyer need along Guide rail goes up a slope or during descending, in order that it remains horizontality, can using adjust front and back wheel level height so as to lead The method that the rail gradient is consistent is solved.

Above-mentioned can flyer be hollow cavity structure, and a part for its hollow cavity is isolated as cabin.

Can by several propellers be arranged on above-mentioned can the front of flyer, rear, on top or lower section body, to drive Move its operation.

Available column by this have orbit aerocraft across be erected at different kinds of roads (include various urban road, backroad, Highway, railway etc.) overhead, neither land occupation, and it is current not affect surface car.

Solar panel or solar film battery (in figure is not drawn into) can be erected at by column on the way and aircraft In the frame structure of the compositions such as guide rail, while generating in order to realize large solar, provide masking for surface road, in order to avoid The pavement damage causing is soaked in the traffic problems causing except ice and snow on road surfaces and rain drop erosion, and can provide huge rainwater-collecting Area.

This have an orbit aerocraft have the beneficial effect that 1, structure is simple, low cost of manufacture, 2, there is no falling risk and easily In operation management with automatically control, 3, freight volume is big, cost of transportation is low, 4, no landing risk, flight resistance be little, speed is fast, 5, Various road surface overhead can be erected at, thus not independent land occupation, and can effectively solving urban road congestion problem, 6, not On the premise of land occupation, the extensive laying problem of effectively solving solar panel or solar film battery, 7, can be Road provides masking, to exempt the traffic problems that ice and snow on road surfaces causes and the pavement damage that rain drop erosion immersion causes, 8, can carry For huge rainwater-collecting area etc..

Brief description

Fig. 1 is the stereoscopic principal structure chart of one of the embodiment of the present invention.

1. times constraint guide rails of in figure, on 1a. constrain guide rail, 2. can flyer, 3. propeller, 4. wheel, 5. aircraft Interior passenger.

Specific embodiment

In Fig. 1, this have orbit aerocraft mainly by can flyer (as aircraft) 2 and two lower constraint tracks 1 and two Constraint guide rail 1a composition on bar；Described flyer 2 can be limited in and run on the restriction range of described guide rail and track, and will Described guide rail 1 as can flyer 2 takeoff and landing runway；In described guide rail side setting website (in figure is not drawn into), For personnel and goods and materials turnover above-mentioned can flyer.

The top wheel 4 of flyer 2 can hang (or by its bottom set up) by above-mentioned on lower constraint guide rail 1, and Lower constraint guide rail 1 and on constrain guide rail 1a constraint under complete its rolling start, leave the right or normal track flight and slide landing.

Above-mentioned can flyer 2 flying height, can be adjusted by changing its flight speed and lift and be controlled； And the regulation of its flight speed and lift, in addition to can passing through the various known regulation control modes of conventional aircraft, also may be used To be adjusted control with track brake (in figure is not drawn into).

Above-mentioned can flyer 2 left and right sides position constraint, with can magnetic force or two between flyer 2 and guide rail Side directive wheel (in figure is not drawn into) is controlled by.

Above-mentioned the global shape of flyer 2 can be similar to one section of aircraft fixed-wing, but its highly with width than tradition Aircraft fixed-wing much larger, the inside clear height of at least its upper section is greater than the height of ordinary people；Its shape of cross section and Construction structure is also similar to the fixed-wing of aircraft.

Above-mentioned the left and right two ends (or middle) of flyer 2 can be hung with wheel and constrained on guide rail, and along leading Rail runs；Its normal operating condition is the state of flight that leaves the right or normal track, and completes landing on lower constraint guide rail 1.

Above-mentioned can flyer 2 be hollow cavity structure, and a part for its hollow cavity is isolated as cabin.

Can by several propellers 3 be arranged on above-mentioned can on front (or rear, the top, lower section) body of flyer 2, with Drive its operation.

Available column (in figure is not drawn into) has orbit aerocraft (to include various city road across being erected at different kinds of roads by this Road, backroad, highway, railway etc.) overhead, neither land occupation, and it is current not affect surface car.

Solar panel or solar film battery can be erected at and to be made up of column on the way and aircraft guide rail etc. In frame structure, while generating in order to realize large solar, provide masking for surface road, made with exempting ice and snow on road surfaces The pavement damage causing is soaked in the traffic problems becoming and rain drop erosion, and can provide huge rainwater-collecting area.

Claims

1. one kind has orbit aerocraft, it is characterized in that: this have orbit aerocraft mainly by can flyer and one or one group constraint Guide rail forms；Described flyer can be limited in and run on the restriction range of described guide rail and track, and described guide rail is made For described can flyer takeoff and landing runway；Each website is set in described guide rail side, so that personnel and goods and materials enter Go out above-mentioned can flyer.

2. one kind according to claim 1 has orbit aerocraft, it is characterized in that: above-mentioned by guide rail constrain can flyer Power set, are by the propeller of motor-driven.

3. one kind according to claim 1 has orbit aerocraft, it is characterized in that: above-mentioned can flyer top by with wheel Hanging (or setting up its bottom) is on guide rail, and completes its rolling start in the restriction range of guide rail, leaves the right or normal track and fly and sliding Row landing.

4. one kind according to claim 1 has orbit aerocraft, it is characterized in that: above-mentioned can flyer flying height, lead to Cross and change its flight speed and lift to be adjusted and to control；And the regulation of its flight speed and lift, except by flight Outside the various known regulation control mode of device, also adjusted control with track brake.

5. one kind according to claim 1 has orbit aerocraft, it is characterized in that: above-mentioned can flyer left and right sides position Constraint, with can magnetic force between flyer and track or both sides directive wheel be controlled by.

6. one kind according to claim 1 has orbit aerocraft, it is characterized in that: above-mentioned can flyer global shape approximate In one section of aircraft fixed-wing, but it is highly much larger than traditional aircraft fixed-wing with width, and at least its upper section is interior Portion's clear height is greater than the height of ordinary people；Its shape of cross section and construction structure are also similar to the fixed-wing of aircraft.

7. one kind according to claim 1 has orbit aerocraft, it is characterized in that: above-mentioned can flyer left and right two ends (or Middle) hung with wheel and constrained on guide rail, and run along guide rail；Its normal operating condition is the state of flight that leaves the right or normal track, And landing is completed on guide rail.

8. one kind according to claim 1 has orbit aerocraft, it is characterized in that: above-mentioned can flyer be hollow cavity knot Structure, and a part for its hollow cavity is isolated as cabin.

9. one kind according to claim 1 has orbit aerocraft, it is characterized in that: has orbit aerocraft across frame with column by this It is located at different kinds of roads overhead, neither land occupation, and does not affect surface car and pass through.

10. one kind according to claim 9 has orbit aerocraft, it is characterized in that: by solar panel or solar energy film Battery is erected in the frame structure being made up of column on the way and aircraft guide rail etc., in order to realize large solar generating Meanwhile, provide masking for surface road, to exempt the traffic problems that ice and snow on road surfaces causes and the road surface that rain drop erosion immersion causes Damage, and huge rainwater-collecting area can be provided.