CN101991954A - Suspension cable type low-altitude flying system - Google Patents

Suspension cable type low-altitude flying system Download PDF

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Publication number
CN101991954A
CN101991954A CN2010101966035A CN201010196603A CN101991954A CN 101991954 A CN101991954 A CN 101991954A CN 2010101966035 A CN2010101966035 A CN 2010101966035A CN 201010196603 A CN201010196603 A CN 201010196603A CN 101991954 A CN101991954 A CN 101991954A
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track
flying object
flying
unit
orbit
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CN2010101966035A
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Chinese (zh)
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渠仁书
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Abstract

The invention provides a suspension cable type low-altitude flying system, belonging to the levitation entertainment field. The suspension cable type low-altitude flying system comprises at least two main towers, a plurality of assisting towers, a track, a planometer, a track levelling unit, a floatage unit, a flyer and a driving unit; whether the track is in a horizontal state is detected by the floatage unit which is used for balancing the gravity of the flyer and the planometer on the track, a signal for adjusting or maintaining the track to be in the horizontal state is transmitted to the track leveling unit according to the detected state; in addition, under the driving of the driving unit on the track, a lifting electric hoist on the floatage unit controls the lifting of the floatage unit by taking up or releasing the suspension cable of the flyer, a lifter on the flyer controls the contraction of the suspension cable of the flyer to control the flying height of an airplane, so as to simulate the running of a real airplane; and therefore, the system ensures the flyer to have remote flying distance safely and effectively.

Description

Suspension low-latitude flying system
Technical field
The present invention relates to the entertainment field of going up to the air, relate in particular to a kind of suspension low-latitude flying system.
Background technology
In the lift-off show business at home and abroad, manned lift-off aircraft is one of common lift-off converter tools, and this manned lift-off aircraft is mechanical structure normally, can only move among a small circle in the original place, and displacement is generally in 100 meters.Except manned lift-off aircraft, the dirigible or the fire balloon that are filled with rare gas can carry out longer-distance flight.But the distance of these manned lift-off equipment flights is still limited, is difficult to realize take into account converter tools simultaneously as the regional traffic instrument in the short time between the destination, comes and goes delivery visitor low-speed operations, and is as tens kilometers, even farther until larger distance.
Summary of the invention
Technical problem to be solved by this invention provides a kind of suspension low-latitude flying system, realize between the destination, taking into account converter tools simultaneously in the short time as the regional traffic instrument, come and go delivery visitor low-speed operations,, even farther until larger distance as tens kilometers.
For solving the problems of the technologies described above, the invention provides a kind of suspension low-latitude flying system.This suspension low-latitude flying system comprises:
At least two king-tower framves to establishing, described king-tower frame is provided with carrier cable;
Some secondary tower framves, described secondary tower frame suspends described carrier cable in midair from both sides;
Track, described track are suspended in described carrier cable below;
Planometer, described planometer are arranged on the described track;
The track leveling unit is used for controlling described track according to the control signal of described planometer and is in level;
The buoyancy unit;
Flying object, described flying object is by the suspention of flying object hoist cable and be fixed on below, described buoyancy unit, the buoyant equilibrium of the gravity of described flying object and described buoyancy unit;
Driver element is used to drive described buoyancy unit to drive described flying object along described orbital motion, and described driver element hangs and connects described buoyancy unit.
In an optimal technical scheme of the embodiment of the invention, described secondary tower frame suspends described carrier cable in midair by secondary tower frame hoist cable, and described driver element hangs by described flying object hoist cable and connects described buoyancy unit.
In an optimal technical scheme of the embodiment of the invention, described track is suspended in described carrier cable below by described track leveling unit.
In an optimal technical scheme of the embodiment of the invention, described track leveling unit is the leveling electric hoist.
In an optimal technical scheme of the embodiment of the invention, described buoyancy unit is the air bag with birds profile or rocket profile, and described air bag with birds profile or rocket profile is provided with the lifting electric hoist of the air bag lifting of described birds profile of control or rocket profile.
In an optimal technical scheme of the embodiment of the invention; described track comprises orbit and annular shutdown track; described orbit is centered around described annular and shuts down the track periphery, and described orbit and described annular are shut down the setting of track crossing place makes the buoyancy unit shut down the electronic shift fork of track that switches between the track at described orbit and described annular.
In an optimal technical scheme of the embodiment of the invention, described driver element is the synchronous car of electric track, and the synchronous car of described electric track is set in described orbit or annular is shut down operation in the track.
In an optimal technical scheme of the embodiment of the invention, the inboard that described orbit and annular are shut down track is covered with trolley, and described trolley contacts with the brush of railcar side; Cable that the ground electrical network is hung through railcar by trolley and brush and flying object power line are to described flying object transmission of electric energy.
In an optimal technical scheme of the embodiment of the invention, suspension low-latitude flying system also comprises the platform of boarding, the described platform of boarding is provided with hoist engine, what the described platform of boarding was provided with that according to described hoist engine control forms described flying object outbound or warehouse-in goes out to put in storage baffle plate, and the cat head of described king-tower frame and secondary tower frame is equipped with the safe operation watch-dog that is used to carry out the global safety monitoring.
In an optimal technical scheme of the embodiment of the invention, described flying object is an aircraft, the head place of described aircraft is provided with first propelling screws, the empennage top of described aircraft is provided with the rudder blower fan and second propelling screws, the both wings place of described aircraft is equipped with hover fan, also is provided with on the described aircraft by controlling the lift of described flying object hoist cable with lifting.
Among the present invention, by the buoyancy unit of balance flying object gravity is set, and in orbit planometer is set detects track in real time and whether be in level, send to the track leveling unit according to detected state and adjust or orbit keeping is in the signal of level.In addition under the driving that driver element in orbit is set; the buoyancy unit is shut down on the track in orbit or annular and is moved to drive flying object with the synchronous mode of driver element; be arranged on the lifting of lifting electric hoist by folding and unfolding flying object hoist cable control buoyancy unit on the buoyancy unit; be arranged on the flexible flying height of lift control flying object hoist cable on the flying object, thereby simulate the operation of real aircraft with the control aircraft.Therefore, guaranteed that safely and effectively flying object has flying distance far away.
Description of drawings
Fig. 1 is the structural representation of suspension low-latitude flying system embodiment of the present invention;
Fig. 2 is the schematic diagram that is provided with of suspension low-latitude flying system embodiment middle orbit of the present invention;
Fig. 3 is the schematic diagram that is provided with of the electronic shift fork of suspension low-latitude flying system embodiment middle orbit of the present invention;
Fig. 4 is provided with schematic diagram for driver element in the suspension low-latitude flying system embodiment of the present invention in track;
Fig. 5 is the structural representation of buoyancy unit in the suspension low-latitude flying system embodiment of the present invention;
Fig. 6 is the structural representation of flying object among the present invention.
The specific embodiment
Below by drawings and Examples, technical scheme of the present invention is described in further detail.Fig. 1 is the structural representation of suspension low-latitude flying system embodiment of the present invention.Fig. 2 is the schematic diagram that is provided with of suspension low-latitude flying system embodiment middle orbit of the present invention.Fig. 3 is the schematic diagram that is provided with of the electronic shift fork of suspension low-latitude flying system embodiment middle orbit of the present invention.Fig. 4 is provided with schematic diagram for driver element in the suspension low-latitude flying system embodiment of the present invention in track.As shown in Figure 1, the suspension low-latitude flying system in the present embodiment comprises: at least two king-tower framves 101, several secondary tower framves 102, track 103, planometer 104, track leveling unit 105, buoyancy unit 106, flying object 107, driver element (not shown in figure 1).
Wherein, at least two king-tower framves 101 are used for fixing carrier cable 111 according to the direction setting to establishing mutually.
Secondary tower frame 102 is arranged on the both sides of carrier cable 111, reaching the effect of suspention carrier cable 111, in the present embodiment, secondary tower frame 102 can but be not limited to by secondary tower frame hoist cable 112 suspention carrier cables 111.
Track 103 is suspended in carrier cable 111 belows, provides flying object 107 sliding trajectories.In in this enforcement; as shown in Figures 2 and 3; track 103 can comprise orbit 113 and annular shutdown track 123; orbit 113 is centered around annular and shuts down track 123 peripheries, and orbit 113 and annular are shut down the setting of A place, track 123 crosspoint makes buoyancy unit 106 shut down the electronic shift fork 133 of track that switches between the track 123 at orbit 113 and annular.
Particularly, as shown in Figure 4, be the set-up mode of example explanation driver element in track with orbit 113.The inboard of orbit 113 is covered with trolley 153, and trolley 153 contacts with brush 143 as the synchronous car wheel of the electric track of driver element 163 sides; Cable that the ground electrical network is hung through driver element by trolley 153 and brush 143 and flying object power line 136 are to flying object 107 transmission of electric energy.When running to annular as the synchronous car of the electric track of driver element 108 and shut down track 123, driver element 108 set-up modes are identical with set-up mode in orbit 113.
Planometer 104 is arranged on the track 103, is used for detecting automatically track 103 and whether is in state parallel to the ground.On track 103, a planometer 104 is set every 50 to 100 meters.
In the present embodiment can but be not limited to by track leveling unit 105 track 103 be suspended in carrier cable 111 belows, track leveling unit 105 is controlled track 103 automatically according to the control signal of planometer 104 and is in level.Be that track leveling unit 105 detects track 103 and is in non-standard state at present, then send the control signal of leveling track 103 to level to track leveling unit 105, otherwise, then send the control signal that orbit keeping 103 is in level to track leveling unit 105.In the present embodiment, track leveling unit 105 can but be not limited to the leveling electric hoist.
Buoyancy unit 106 is suspended in the top of flying object 107 by flying object hoist cable 116, and buoyancy unit 106 imposes on the mutual balance of gravity of the buoyancy and the flying object 107 of flying object 107, guarantees that flying object 107 keeps balances, does not apply downward pulling force to track 103.Be under the level at track 103, flying object 107 is stably along track 103 flights.
In the present embodiment, as shown in Figure 5, buoyancy unit 106 can but be not limited to air bag with birds profile, air bag with birds profile is provided with the lifting electric hoist 126 and the flying object power line 136 of the air bag lifting of control birds profile, lifting electric hoist 126 can be arranged on the position of centre of gravity place of the air bag of birds profile, and flying object power line 136 passes the center of gravity of the air bag of birds profile.Thereby lifting electric hoist 126 flies up and down by flexible flying object hoist cable 116 control flying objects 107.Buoyancy unit 106 also can be for having the air bag of rocket profile.
Flying object 107 is by 116 suspentions of flying object hoist cable and be fixed on 106 belows, buoyancy unit.
Driver element 108 hangs and connects buoyancy unit 106, and driver element 108 drives buoyancy unit 106 to drive flying object 107 along track 103 operations.In the present embodiment, driver element 108 can but be not limited to hang and connect buoyancy unit 106 by flying object hoist cable 116.Particularly, driver element 108 can but be not limited to the synchronous car of electric track, the synchronous car of electric track is set in orbit 113 or annular is shut down in the track 123 to move with flying object 107 constant speed.
Suspension low-latitude flying system in the present embodiment has also increased the platform 109 of boarding that the annular that is arranged on one of them king-tower frame 101 1 end or two king-tower frame 101 ends is shut down the track below except comprising two king-tower framves 101, several secondary tower framves 102, track 103, planometer 104, track leveling unit 105, buoyancy unit 106, flying object 107, driver element 108, carrier cable 111, secondary tower frame hoist cable 112, flying object hoist cable 116 etc.Be provided with hoist engine 119 on this boards platform 109, this hoist engine 119 is controlled out the rise or the landing of warehouse-in baffle plate 129, thereby plays control flying object 107 outbounds or warehouse-in.Hoist engine 119 can be provided with position as shown in Figure 1 with the position that goes out to put in storage baffle plate 129.When flying object will switch to orbit, by opening out warehouse-in baffle plate 129,107 of flying objects moved along orbit.When flying object switches to annular and shuts down track, opened out warehouse-in baffle plate 129 before this and allow flying object 107 drop to board on the platform 109.If run into bad weathers such as strong wind, can start hoist engine 119 and control out 129 rises of warehouse-in baffle plate to be higher than 5 meters enclosure wall in platform 109 formation all around of boarding.Go out to put in storage baffle plate 129 and can be an electronic switching door, its direction of opening the door is towards another one king-tower frame 101.
In the present embodiment, Fig. 6 is the structural representation of flying object among the present invention.As shown in Figure 6, flying object 107 can but be not limited to an aircraft, the head place of aircraft is provided with first propelling screws 117, the empennage top of aircraft is provided with the rudder blower fan 127 and second propelling screws 137, the both wings place of aircraft is equipped with hover fan 147, also is provided with on the aircraft by the lift 157 of control flying object hoist cable 116 with lifting.Lift 157 is arranged on the center of gravity place of aircraft, along with the flight up and down of aircraft is shunk automatically or loosened flying object hoist cable 116.First propelling screws 117 and second propelling screws 137 advance aircraft to fly forward, the heading of rudder blower fan 127 control aircrafts.Hover fan 147 is used to control the horizontal tilt degree of aircraft, simulates real flight status.Particularly, when aircraft flight, the entertainer controls the deflection angle and the speed discrepancy of each blower fan, produces speed discrepancy, thereby changes the flight attitude of aircraft.As the driving cabin 167 that ccontaining entertainer also is set on the aircraft of flying object 107.
In the present embodiment, passenger board lobby and/or back-stage management chamber (not shown) can be set also on the platform 109 of boarding.
In the above-described embodiments, orbit is specifically as follows the circular orbit of a closure, and this circular orbit is positioned at the king-tower frame and brings out for 101 liang and can be provided with annular and shut down and to dodge the track (not shown), with the influence to other aircraft flights of the aircraft avoiding shutting down.
The cat head of king-tower frame 101 and secondary tower frame 102 all can be provided with the safe operation watch-dog safe operation watch-dog 121 that is used to carry out the global safety monitoring.By the mode of video monitoring, detect whether security of operation of whole system.
The above embodiment of the present invention also can apply in the every engineering transportation that is difficult between the two places in scenic spot traffic or each field of society repair the roads, build bridge.
In the above embodiment of the present invention, by the buoyancy unit of balance flying object gravity is set, and in orbit planometer is set detects track in real time and whether be in level, send to the track leveling unit according to detected state and adjust or orbit keeping is in the signal of level.In addition by the driving that driver element in orbit is set; the buoyancy unit is shut down on the track in orbit or annular and is moved to drive flying object with the synchronous mode of driver element; be arranged on the lifting of lifting electric hoist by folding and unfolding flying object hoist cable control buoyancy unit on the buoyancy unit; be arranged on the flexible flying height of lift control flying object hoist cable on the flying object, thereby simulate the operation of real aircraft with the control aircraft.Therefore, guaranteed that safely and effectively flying object has flying distance far away.
It should be noted that at last: above embodiment is only in order to technical scheme of the present invention to be described but not limit it, although the present invention is had been described in detail with reference to preferred embodiment, those of ordinary skill in the art is to be understood that: it still can make amendment or be equal to replacement technical scheme of the present invention, and these modifications or be equal to replacement and also can not make amended technical scheme break away from the spirit and scope of technical solution of the present invention.

Claims (10)

1. a suspension low-latitude flying system is characterized in that, comprising:
At least two king-tower framves to establishing, described king-tower frame is provided with carrier cable;
Some secondary tower framves, described secondary tower frame suspends described carrier cable in midair from both sides;
Track, described track are suspended in described carrier cable below;
Planometer, described planometer are arranged on the described track;
The track leveling unit is used for controlling described track according to the control signal of described planometer and is in level;
The buoyancy unit;
Flying object, described flying object is by the suspention of flying object hoist cable and be fixed on below, described buoyancy unit, the buoyant equilibrium of the gravity of described flying object and described buoyancy unit;
Driver element is used to drive described buoyancy unit to drive described flying object along described orbital motion, and described driver element hangs and connects described buoyancy unit.
2. suspension low-latitude flying according to claim 1 system is characterized in that described secondary tower frame suspends described carrier cable in midair by secondary tower frame hoist cable, and described driver element hangs by described flying object hoist cable and connects described buoyancy unit.
3. suspension low-latitude flying according to claim 2 system is characterized in that, described track is suspended in described carrier cable below by described track leveling unit.
4. suspension low-latitude flying according to claim 3 system is characterized in that described track leveling unit is the leveling electric hoist.
5. 4 described suspension low-latitude flying systems as requested, it is characterized in that, described buoyancy unit is the air bag with birds profile or rocket profile, and described air bag with birds profile or rocket profile is provided with the lifting electric hoist of the air bag lifting of described birds profile of control or rocket profile.
6. suspension low-latitude flying according to claim 1 system; it is characterized in that; described track comprises orbit and annular shutdown track; described orbit is centered around described annular and shuts down the track periphery, and described orbit and described annular are shut down the setting of track crossing place makes the buoyancy unit shut down the electronic shift fork of track that switches between the track at described orbit and described annular.
7. suspension low-latitude flying according to claim 6 system is characterized in that described driver element is the synchronous car of electric track, and the synchronous car of described electric track is set in described orbit or annular is shut down operation in the track.
8. suspension low-latitude flying according to claim 7 system is characterized in that, the inboard that described orbit and annular are shut down track is covered with trolley, and described trolley contacts with the brush of the synchronous car of electric track side; Cable that the ground electrical network is hung through the synchronous car of electric track by trolley and brush and flying object power line are to described flying object transmission of electric energy.
9. suspension low-latitude flying according to claim 8 system, it is characterized in that, also comprise the platform of boarding, the described platform of boarding is provided with hoist engine, what the described platform of boarding was provided with that according to described hoist engine control forms described flying object outbound or warehouse-in goes out to put in storage baffle plate, and the cat head of described king-tower frame and secondary tower frame is equipped with the safe operation watch-dog that is used to carry out the global safety monitoring.
10. according to the described suspension low-latitude flying of any item of claim 1 to 9 system, it is characterized in that, described flying object is an aircraft, the head place of described aircraft is provided with first propelling screws, the empennage top of described aircraft is provided with the rudder blower fan and second propelling screws, the both wings place of described aircraft is equipped with hover fan, also is provided with on the described aircraft by controlling the lift of described flying object hoist cable with lifting.
CN2010101966035A 2009-08-11 2010-06-10 Suspension cable type low-altitude flying system Pending CN101991954A (en)

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CN200910162885 2009-08-11
CN2010101966035A CN101991954A (en) 2009-08-11 2010-06-10 Suspension cable type low-altitude flying system

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108044814A (en) * 2018-01-03 2018-05-18 中铁广州工程局集团有限公司 The accurate cutter device of CFG pile heads
CN108525316A (en) * 2018-06-13 2018-09-14 酷黑科技（北京）有限公司 The method of autonomous flight system and control autonomous flight system
CN109224465A (en) * 2018-09-25 2019-01-18 程鲲 A kind of overhead cable system being easily installed erection

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CN101991954A (en) * 2009-08-11 2011-03-30 渠仁书 Suspension cable type low-altitude flying system
CN104787333B (en) * 2015-03-21 2017-04-05 王文平 A kind of low latitude single track, the electric airplane for flying thereon and its flying method
CN105564442B (en) * 2016-01-15 2018-03-02 彭红廷 Kong Tie transportation systems and empty iron transportation resources
CN106292334B (en) * 2016-09-29 2019-06-25 大连理工大学 It is a kind of along cableway aircraft device
CN107982922B (en) * 2017-12-19 2019-07-26 倪为勇 A kind of trackless roller-coaster

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CN108044814A (en) * 2018-01-03 2018-05-18 中铁广州工程局集团有限公司 The accurate cutter device of CFG pile heads
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CN109224465A (en) * 2018-09-25 2019-01-18 程鲲 A kind of overhead cable system being easily installed erection
CN109224465B (en) * 2018-09-25 2023-11-28 西南科技大学 Swift current cable system convenient to installation is erect

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Application publication date: 20110330