CN108553917A - A kind of bungee jumping aircraft and its application - Google Patents
A kind of bungee jumping aircraft and its application Download PDFInfo
- Publication number
- CN108553917A CN108553917A CN201810730185.XA CN201810730185A CN108553917A CN 108553917 A CN108553917 A CN 108553917A CN 201810730185 A CN201810730185 A CN 201810730185A CN 108553917 A CN108553917 A CN 108553917A
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- CN
- China
- Prior art keywords
- aircraft
- wire
- compound
- compound wire
- elastic string
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- 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.)
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Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63G—MERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
- A63G31/00—Amusement arrangements
- A63G31/02—Amusement arrangements with moving substructures
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63G—MERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
- A63G31/00—Amusement arrangements
- A63G2031/002—Free-fall
Landscapes
- Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)
Abstract
The present invention provides a kind of bungee jumping aircraft, which has gone out except the action of the conventional bungee jumping of experience, can be with familiarization flight, the actions such as fall, roll, rotate.
Description
Technical field
The invention belongs to fly, entertainment field, especially a kind of aircraft can be used in similar bungee jumping campaign.
Background technology
Currently, tourist very attractive of the bungee jumping to taste for adventure, self-challenge.But bungee jumping at present is merely
From falling from high altitude, tourist is only acted on by gravity and elastic force, lacks the effect of lateral power, therefore running orbit is single, lacks
The speed of weary horizontal direction.Tourist can not oneself operation and control track, lack rolling, rotation etc. actions experience.
Invention content
Goal of the invention：The shortcomings that in order to overcome bungee jumping, the present invention provides a kind of bungee jumping aircraft and its in amusement side
The application in face.
Technical scheme is as follows:
Aircraft contains motor, rotor, control unit, rack；The rotor is 2 or 2 or more, the control unit packet
It includes but is not limited to fly control, electron speed regulator, receiver.Aircraft is connected to compound wire；It can also be in aircraft or aircraft
Rack on power interface is installed, which may be used compound wire and is connected to external power supply.In this way, using remote control
Device can control the state of flight of aircraft.
The compound wire includes elastic string and conducting wire, and the elastic string in the compound wire is used with conducting wire includes but unlimited
In tie up, part bonding, circular mode combines.
The elastic string refers to stretching 30% or more the rope of plastic deformation will not still occur, and elastic string includes but not limited to
Rope skipping, stretch cord, elastic string, rubber rope and various composite ropes.The conducting wire is electrically conductive line, including but not
It is limited to copper core electric wire, copper core cable, aluminium core electric wire, aluminium cable,
In order to enhance pulling force, in the component part of the conducting wire in compound wire other than conductive part, insulating part, also pulling force
Strengthening part, the pulling force strengthening part include but not limited to steel wire, steel wire.
Preferably, the cross-sectional area of the conductive part of compound wire is more than 10 square millimeters or the compound wire
For the biggest quality for the load that can be born than also big M kilograms or more of the quality of aircraft, the range of M is 40 ~ 5000.
Compound wire is connected to the power supply except aircraft（External power supply）It powers to aircraft.The conducting wire has larger
Intensity, the pulling force more than 100N or more can be born, this can be accomplished in several ways, for example, by using thicker copper wire/copper
Cable or in conducting wire use reinforcement（Such as steel wire, steel wire etc.）Etc..
Compound wire is powered aircraft for being connected to external power supply；Or in the rack of aircraft/aircraft
Provided with power interface, external power supply can also be connected to by compound wire in this way.
The external power supply is including but not limited to generator, civilian electricity（Line）Or commercial power（Line）, electricity in building
Source sets skyborne power supply etc..As needed, external power supply can be directly connected to aircraft, or pacified on board the aircraft
Dress transformer reuses after carrying out transformation.
Preferably, power supply uses civilian or commercial power.
Compound wire also undertakes the effect of stress and safety guarantee.Since compound wire includes elastic string and two, conducting wire
Point, conductive effect is undertaken by conducting wire, and elastic string undertakes the effect of stress and safety guarantee, the conducting wire that single choice is enhanced with pulling force
When, conducting wire can also be used as safety guarantee effect（The length of fracture or elastic string reaches the length of conducting wire other than elastic string
When）.
The preparation process of compound wire is as follows：
Elastic string is straightend, conducting wire is then subjected to coiling by axis of elastic string, material is thus formed one kind using elastic string as core
Compound wire, conducting wire one encloses the land and is centered around in elastic string.The physical length of conducting wire in compound wire is far longer than elasticity
Rope.When compound wire is by external force, external force acts predominantly in elastic string, and elastic wire stress is elongated；Between each circle of conducting wire
Distance increase, this makes it possible to the elongations for adapting to entire compound wire.
In order to increase adhesion effect of the conducting wire in elastic string, can on composite rope every a distance just to conducting wire with
Elastic string, which is done, fixes, for example, with gluing, the methods such as tie up.
Can not certainly coiling, conducting wire and elastic string are just done every a distance directly and fixed.But at this time
It allows each section of the length of conducting wire to be more than the length of elastic string, such as can be 1.5-4 times.
When work, on board the aircraft by a fixation of compound wire；Other end is fixed on the eminence except aircraft, institute
The eminence stated is 3 meters or more aerial from the ground, or has the place in 3 meters or more spaces below, including but not limited to aerial, bridge
The places such as between upper, cliffside, valley, building.
In this way, the thrust of the elastic pulling force of the gravity that aircraft is subject to during amusement, compound wire, aircraft can
Bring entertainment effect.For bungee jumping, the more thrusts of an aircraft of the present invention, and this thrust be can be to
It is upper, move downwards or to horizontal all directions, also, aircraft can also make the actions such as rotation, rolling, and entertainment effect is remote
It is better than bungee jumping.Tourist can manipulate aircraft, control flight path and flight attitude, the earthquake intensity of movement with oneself.
Preferably, compound wire can also control the length of its actual use by bobbin winder device.
In this way, because of the protective effect of compound wire, even if aircraft breaks down, aircraft will not directly fall
It falls to the ground.The length of compound wire when can be by controlling aircraft work, to increase safety.For bungee jumping,
Invention increases double safety guarantee：One is the flight performance of aircraft, secondly for the pulling force of conducting wire（When using thick copper
When cable or dynamics enhancement type conducting wire, this pulling force is considerable）.
When work, compound wire is aloft connect with external power supply, the both ends connection of compound wire is in addition to ensureing power supply
Between aircraft except the conducting of electricity, the fixation on mechanics also made to the both ends of conducting wire, the fixation includes but unlimited
In fixing or be limited to aircraft/aircraft machine using the modes such as tying up, be, prick by the mechanics reinforcement in compound wire or conducting wire
Frame, power supply position place secured, that wire tension can be born.The eminence refers to 3 meters or more from the ground of place
（Including but not limited to various platforms, various holders）, or there is the place more than 3 meters of spaces (including but not limited to bridge, to hang below
Cantilever beam etc. on precipice, valley, steep cliff or valley).
It is, of course, also possible to which compound wire is fixed on lower, but pass through eminence, is connected to aircraft.It is compound in this way
Conducting wire remains able to play and compound wire is fixed to aloft similar effect, and those skilled in that art are according to the present invention
The similar transformation that scheme can be made, also within protection scope of the present invention.
Preferably, compound wire is also fixed in the rack of aircraft.
Compound wire is encountered by blade in order to prevent, and guard may be used and cover blade, in this way, on the one hand avoiding paddle
Piece encounters compound wire, on the one hand can also protect blade.
Preferably, the present invention aircraft include manned component, such as manned platform, nacelle, it might even be possible to be column,
Plate, basket or other forms.There is fixing device that the body of tourist is fixed on manned component, to protect tourist, meets flight
Application of the device in amusement etc..
The method of operation of the present invention is as follows：
The compound wire of aircraft is fixed aloft, then aircraft takes off from ground or takes off from eminence or fallen from eminence
It falls.Later, aircraft can make the actions such as flight, rotation, rolling, give full play to the characteristics of hanging rotor aircraft more.
Position generally more fixed than the position of compound wire peak or compound wire the location of when the aircraft works
Position when setting or taking off is low, aircraft mainly flight downwards during amusement, but also maintains the energy to fly upwards
Power.
For example, when using bungee jumping pattern, aircraft is directly from eminence freely falling body.When using holder on level land,
Aircraft can fly up from ground, fly to certain altitude and do freely falling body again；A platform can also be done in the air, aircraft is from flat
Direct freely falling body on platform flies again later.
Beneficial effect：
Compound wire in the present invention can not only give full play to the effect of elastic string, but also can play conductive effect.It is multiple due to having
Closing the double protection of conducting wire and the flight performance of aircraft, the safety of tourist has sufficient guarantee, is not only able to body
Test roller-coaster, bungee jumping all processes, moreover it is possible to experience some roller-coasters, the process that bungee jumping can not be experienced.Importantly, trip
Visitor can be operated with oneself.Roller-coaster, bungee jumping running route be fixed, and the running orbit of aircraft of the present invention, appearance
State then can be manipulated artificially.
To facilitate the understanding of the present invention, accompanying drawings and embodiments are provided below for explaining the present invention, but they are not constituted pair
The restriction of the present invention.
Description of the drawings
Fig. 1 is the structure and method of operation schematic diagram of bungee jumping aircraft of the present invention.
Reference sign：
1- nacelles
2- motors
3- rotors
4- racks
5- holders
6- compound wires
Fig. 2 is the flight control system of the present invention and the connection relationship diagram of motor, power supply.
Specific implementation mode
Below by detailed description of the present invention aircraft in conjunction with the embodiments.
The nacelle 1, rack 4, holder 5 for using carbon fibre material manufacture aircraft first, then install motor 2, motor 2 is
150-80 model outer rotor brushless motors.4025 model carbon fiber paddles 3 are installed on motor 2, then carbon fiber is protected using guard
Tie up paddle.Then winged control, electron speed regulator, receiver, GPS module are fixed on the rack, their connection relation presses Fig. 2 institutes
Show：Conducting wire is connected to external power supply, and then conducting wire is connected with the input power cord of electron speed regulator, the output line of electron speed regulator
It is connected to the motor.The signal wire of receiver is connected with control is flown, and the signal wire of electron speed regulator is connected to winged control, by GPS module
Signal wire with fly control be connected, using lithium battery to fly control power, by the positive and negative anodes of lithium battery with fly control power interface positive and negative anodes
It is connected.
Conducting wire 5 uses, and conducting wire 5 is fixed on to the immediate vicinity position of rack with line card, is then connect with external power supply.Outside
It connects power supply and uses high frequency switch power.In this way, after connecting the line on external power supply, flight just can be controlled using remote controler
The state of flight of device.
The making of compound wire：Prepare 2 cores of 20 centimetres of diameter, the stretch cord of fracture strength 5000N and steel wire reinforcement
Copper cable.The sectional area of copper is 1 square centimeter, 3 millimeters of steel wire diameter in cable.The length of stretch cord is 50 meters, the length of cable
Degree is 100 meters.The two is fixed using line card every 10 meters of position every 5 meters, cable in stretch cord.Thus it obtains compound
Conducting wire.
Compound wire 6 is connected with the input power cord of electron speed regulator, and by compound wire 6 in aircraft center of gravity position
It is fixed nearby, the other end of compound wire 6 is fixed on bridge 7, the state of flight of aircraft is then can control using remote controler.
Embodiment 2
Motor in embodiment 1 is changed to the external rotor electric machine of 140-100 models into, other are constant.
The above is only some examples of embodiment of the present invention, it should be pointed out that：For the technology people of the art
For member, various improvements and modifications may be made without departing from the principle of the present invention, these improvements and modifications are also answered
It is considered as protection scope of the present invention.
Claims (8)
1. a kind of aircraft, it is characterised in that：The aircraft contains the compound wire for the external power that may be coupled to aircraft, or
Power interface is reserved in the rack of person's aircraft/aircraft, in order to being connected to flight with compound wire when aircraft works
Power supply except device.
2. a kind of compound wire as described in claim 1, it is characterised in that：The cross section of the conductive part of the compound wire
The maximum weight for accumulating the load that more than 10 square millimeters or the compound wire can be born is also bigger M than the weight of aircraft
Kilogram or more, the range of M is 40 ~ 5000.
3. a kind of compound wire as described in claim 1, it is characterised in that：The compound wire includes elastic string and conducting wire,
Elastic string in the compound wire and conducting wire are combined using the modes such as tying up, bond, surround.
4. a kind of compound wire as described in claim 1, it is characterised in that：Conducting wire in the compound wire includes but not limited to
Copper core electric wire, copper core cable, aluminium core electric wire, aluminium cable, in addition to conductive part in the component part of the conducting wire in the compound wire
Divide, outside insulated part, also pulling force strengthening part, the pulling force strengthening part include but not limited to steel wire, steel wire.
5. a kind of elastic string as described in claim 1, it is characterised in that：The elastic string stretches 30% or more and will not still mould
Deformation, the elastic string include but not limited to rope skipping, stretch cord, elastic string, rubber rope and various composite ropes.
6. a kind of aircraft as described in claim 1, it is characterised in that：When the aircraft works, compound wire one end is fixed
On board the aircraft, the other end is fixed aloft；The eminence is 3 meters or more aerial from the ground, or has 3 meters or more below
The place in space, including but not limited on aerial, bridge, cliffside, the places such as valley.
7. a kind of aircraft as described in claim 1, it is characterised in that：It is general than multiple the location of when the aircraft works
Close conducting wire peak position the fixed position of compound wire or position when taking off it is low.
8. a kind of aircraft as described in claim 1 is in the application of amusement etc..
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721028816 | 2017-08-17 | ||
| CN2017210288160 | 2017-08-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108553917A true CN108553917A (en) | 2018-09-21 |
Family
ID=63555624
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810730185.XA Pending CN108553917A (en) | 2017-08-17 | 2018-07-05 | A kind of bungee jumping aircraft and its application |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108553917A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107380438A (en) * | 2017-08-17 | 2017-11-24 | 镇江市丹徒区硕源材料科技有限公司 | A kind of bungee jumping aircraft and its application |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202686760U (en) * | 2012-06-20 | 2013-01-23 | 谭大刚 | Free gliding system with safety protection device |
| CN204606235U (en) * | 2015-05-04 | 2015-09-02 | 厦门大学 | Many rotor wing unmanned aerial vehicles device when navigating based on the length hanging mooring system |
| CN106379554A (en) * | 2016-12-08 | 2017-02-08 | 中国科学院长春光学精密机械与物理研究所 | Flight test protection device and method |
| CN107380438A (en) * | 2017-08-17 | 2017-11-24 | 镇江市丹徒区硕源材料科技有限公司 | A kind of bungee jumping aircraft and its application |
-
2018
- 2018-07-05 CN CN201810730185.XA patent/CN108553917A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202686760U (en) * | 2012-06-20 | 2013-01-23 | 谭大刚 | Free gliding system with safety protection device |
| CN204606235U (en) * | 2015-05-04 | 2015-09-02 | 厦门大学 | Many rotor wing unmanned aerial vehicles device when navigating based on the length hanging mooring system |
| CN106379554A (en) * | 2016-12-08 | 2017-02-08 | 中国科学院长春光学精密机械与物理研究所 | Flight test protection device and method |
| CN107380438A (en) * | 2017-08-17 | 2017-11-24 | 镇江市丹徒区硕源材料科技有限公司 | A kind of bungee jumping aircraft and its application |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107380438A (en) * | 2017-08-17 | 2017-11-24 | 镇江市丹徒区硕源材料科技有限公司 | A kind of bungee jumping aircraft and its application |
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180921 |
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| WD01 | Invention patent application deemed withdrawn after publication |