CN206171785U - Helium balloon unmanned aerial vehicle - Google Patents
Helium balloon unmanned aerial vehicle Download PDFInfo
- Publication number
- CN206171785U CN206171785U CN201621209683.2U CN201621209683U CN206171785U CN 206171785 U CN206171785 U CN 206171785U CN 201621209683 U CN201621209683 U CN 201621209683U CN 206171785 U CN206171785 U CN 206171785U
- Authority
- CN
- China
- Prior art keywords
- air film
- film body
- steering wheel
- electronic
- helium
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model relates to a helium balloon unmanned aerial vehicle, including the air film body that is filled with a quantitative helium, the relative both sides in external week of air film are respectively pasted and are had two setting up pieces, install the steering wheel on the setting up piece, install electronic duct motor on the steering wheel, and the flight control system of electronic duct motor of control and steering wheel is installed to the internal bottom of air film, and flight control system's control wires wears out from the inflation inlet of the air film body and links to each other with electronic duct motor, steering wheel respectively. The utility model has the advantages of simple structure, convenient for realization, the air film body that is filled with the helium produces buoyancy, even consequently unmanned aerial vehicle tenesmus out of control also can slowly be fallen to the ground, can not crack up the property, the people can not wound yet, improve the safety in utilization, and buoyancy balances out partly load, electronic duct motor only need consume less power, the event is power consumptive less, time of endurance is longer, especially adaptedly be used for the control of indoor outer mill, technique production supervision and factory building tour etc, also be fit for using as removing projection screen.
Description
Technical field
This utility model is related to a kind of unmanned plane, more particularly to a kind of little power consumption, safe helium balloon unmanned plane.
Background technology
With the most use at present is four rotor wing unmanned aerial vehicles, and it has four propellers, easy to control, and flight is flexible, but its
There is also following defect：The bottom of compared with, atwirl propeller easily threatens to the personal safety of people for safety；Power consumption compared with
Greatly, also can only be flown 20 minutes or so with best battery, endurance is poor.It is unsuitable to apply to factory's monitoring, technology production prison
The field such as pipe and Factory Building tour.
The content of the invention
This utility model mainly solves that original unmanned plane power consumption is big, endurance is poor, easily causes personal injury, there is peace
The technical problem of full hidden danger；A kind of helium balloon unmanned plane is provided, its power consumption is less, and cruising time is longer, safe, Bu Huizao
Into personal injury, factory's monitoring, technology production supervision and Factory Building tour etc. are highly suitable for.
What above-mentioned technical problem of the present utility model was mainly addressed by following technical proposals：This utility model bag
The air film body filled with helium is included, air film is provided with vitro some electronic duct motors, the electronic duct motor of control is provided with air film body
Flight control system.Air film body can be made using materials such as PVC, polyethylene or aluminium films.The diameter of the air film body filled with helium is general
For 30~500cm, the air film body filled with helium produces certain buoyancy, is filled with the amount of helium by control to carry out the tune of load-carrying
Whole, the lift of helium balloon is in a basic balance by the weight of whole unmanned plane, and only the weight of remaining 20g to 200g is needed by electronic culvert
Road motor is lifted, therefore electronic duct motor just can be risen whole unmanned plane with less power, be carried out aerial
Various actions.Ground handling operator sends control signal by radio remote controller, and flight control system is received after signal, then is controlled
The operating of electronic duct motor.By change be located at different directions electronic duct motor rotating speed, so that it may realize helium balloon without
Man-machine rising, decline, rotation and the movement of left-right and front-back either direction.Therefore this utility model power consumption is less, cruising time compared with
It is long.And this utility model does not use the propeller for exposing, it is to avoid potential safety hazard, even if unmanned plane tenesmus out of control also can be floating
Slowly land under power effect, property will not be broken, also will not wound people, improve safety in utilization.
Preferably, described air film is provided with vitro some steering wheels, the electronic culvert being provided with each steering wheel described in
Road motor, steering wheel and described flight control system electrical connection.As needed, steering wheel can be first installed in vitro in air film, then in steering wheel
It is upper that electronic duct motor is installed.Steering wheel, by the direction for changing steering wheel, can just change the electricity on steering wheel equivalent to head
The setting direction of dynamic duct motor, in conjunction with the rotating speed for adjusting electronic duct motor, so as to be capable of achieving the upper of helium balloon unmanned plane
Liter, decline, rotation and the movement of left-right and front-back either direction, control convenient.
Preferably, described electronic duct motor has four, four electronic duct motors are respectively arranged on described air film
The left side of body, right side, front side and rear side, between electronic duct motor and described air film body setting-up piece is provided with.Four electronic
When duct motor all rotates at the same speed, helium balloon unmanned plane rises；When the electronic duct motor low speed rotation in front side two and rear side two
When electronic duct motor turns at a high speed, then helium balloon unmanned plane advances, otherwise then retreats；When the electronic duct motor low speed in two, left side
Then the electronic duct motor in two, right side when turning at a high speed, then helium balloon unmanned plane flies to the left, otherwise then flies to the right.By changing
Become the rotating speed of each electronic duct motor, can be achieved with the rising of helium balloon unmanned plane, decline, rotation, left-right and front-back and arbitrary
The movement in direction.
Preferably, described steering wheel and described electronic duct motor have two, two steering wheels are respectively arranged on described
The external opposite sides of air film, two electronic duct motors are separately mounted on two steering wheels, steering wheel and described air film body
Between be provided with setting-up piece.By the direction for changing two steering wheels, can just change two electronic duct horses on steering wheel
The setting direction for reaching, in conjunction with the rotating speed for adjusting electronic duct motor, so as to be capable of achieving the rising of helium balloon unmanned plane, decline,
The movement of rotation, left-right and front-back and either direction.
Preferably, described air film body is spheroid, spheroid, cylinder, square or cuboid.The technical program
In, the profile of air film body is not limited to spheroid, may be made as various animals, cartoon shape.
Preferably, being provided with horizontally disposed skeleton in described air film body, described flight control system is arranged on described
On skeleton.Skeleton, typically adopts carbon fiber skeleton, and lighter in weight, fastness is good.As needed, projection can be also installed on skeleton
The equipment such as instrument, player, carry out the activities such as advertising.
Preferably, being provided with horizontally disposed skeleton in described air film body, skeleton is in cross, four terminations of skeleton
Described air film body is passed, four described electronic duct motors are separately mounted on four terminations of skeleton.Skeleton passes through gas
The position of film body carries out encapsulation process, makes being more firmly mounted for electronic duct motor.
The beneficial effects of the utility model are：Simple structure, it is convenient to realize, the air film body filled with helium produces buoyancy, because
Even if the tenesmus out of control of this unmanned plane also can slowly land, property will not be broken, also will not wound people, improve safety in utilization, and
And power consumption is less, cruising time is longer, and factory's monitoring, technology production supervision and the Factory Building for being highly suitable for indoor and outdoor is maked an inspection tour
Deng also being suitable as mobile projector screen and use.
Description of the drawings
Fig. 1 is a kind of main structure diagram of the present utility model.
Fig. 2 is a kind of partial enlargement structural representation of the present utility model.
Fig. 3 is a kind of overlooking the structure diagram of the present utility model.
Fig. 4 is another overlooking the structure diagram of the present utility model.
Fig. 5 is another main structure diagram of the present utility model.
Fig. 6 is a kind of system attachment structure block diagram of flight control system in this utility model.
1. air film body in figure, 2. electronic duct motor, 3. flight control system, 4. steering wheel, 5. setting-up piece, 6. skeleton, 31. nothings
Line electrical remote control receiver module, 32. one-chip computer modules, 33. motor drive modules.
Specific embodiment
Below by embodiment, and accompanying drawing is combined, the technical solution of the utility model is described in further detail.
Embodiment 1：A kind of helium balloon unmanned plane of the present embodiment, as shown in Figure 1, Figure 2, Figure 3 shows, including filled with a certain amount of helium
The air film body 1 of gas, in the present embodiment, air film body 1 is a spheroid, alternatively referred to as balloon, and diameter has 2 meters, the phase of the periphery of air film body 1
Both sides are respectively pasted with two setting-up pieces 5, steering wheel 4 are installed on setting-up piece, electronic duct motor 2 is installed on steering wheel,
Bottom in air film body 1 is provided with the flight control system 3 of the electronic duct motor of control and steering wheel, the pilot of flight control system 3 from
The inflation inlet of air film body 1 is passed and is connected with electronic duct motor 2, steering wheel 4 respectively again.
As shown in fig. 6, flight control system 3 includes wireless remotecontrol receiver module 31, one-chip computer module 32 and Motor drive mould
Block 33, the outfan of wireless remotecontrol receiver module 31 is connected with the input of one-chip computer module 32, one-chip computer module 32 it is defeated
Go out end to be connected with the input of two motor drive modules, 33, two steering wheels 4 respectively, the outfan and electricity of motor drive module 33
The input of dynamic duct motor 2 is connected.
Balloon filled with helium produces certain buoyancy, is filled with the amount of helium by control to carry out the adjustment of load-carrying, helium
The lift of balloon is in a basic balance by the weight of whole aircraft, only the weight of remaining 20g to 100g, and so electronic duct motor is just
Whole aircraft can be risen with less power, carry out aerial various actions.Ground handling operator is distant by radio
Control device sends control signal, and the wireless remotecontrol receiver module of flight control system is received after signal, is conveyed to one-chip computer module, Jing
After one-chip computer module process, then control signal is sent respectively to motor drive module and steering wheel, by motor drive module control electricity
The steering of dynamic duct motor and rotating speed, by the direction of Single-chip Controlling steering wheel.Steering wheel equivalent to an axle head, by changing two
The direction of steering wheel, can just change the setting direction of two electronic duct motors on steering wheel, in conjunction with the electronic culvert of adjustment
The rotating speed of road motor, so as to be capable of achieving the movement of rising, decline, rotation, left-right and front-back and the either direction of helium balloon unmanned plane.
Embodiment 2：A kind of helium balloon unmanned plane of the present embodiment, as shown in Figure 4, Figure 5, including filled with a certain amount of helium
Air film body 1 and four electronic duct motors 2, in the present embodiment, air film body 1 is a spheroid, alternatively referred to as balloon, and diameter has 2 meters,
Horizontally disposed carbon fiber skeleton 6 is installed, skeleton 6 is provided with flight control system 3, skeleton in cross on skeleton in air film body 1
6 four terminations pass air film body 1, and four electronic duct motors 2 are separately mounted on four terminations of skeleton 6, flight control system 3
Pilot pass from air film body 1 along skeleton and be connected with four electronic duct motors 2 respectively again.Remaining structure is with embodiment 1.
The present embodiment need not install steering wheel, and by flight control system steering and the rotating speed of four electronic duct motors are controlled.
When four electronic duct motors all rotate at the same speed, helium balloon unmanned plane rises；When front side two, electronic duct motor low speed is transferred
When the electronic duct motor of rear side two turns at a high speed, then helium balloon unmanned plane advances, otherwise then retreats；When the electronic duct in two, left side
When motor low speed is transferred the electronic duct motors in two, right side and turned at a high speed, then helium balloon unmanned plane flies to the left, otherwise then flies to the right
OK.By the rotating speed for changing each electronic duct motor, before can be achieved with rising, decline, rotation, the left and right of helium balloon unmanned plane
Afterwards and either direction movement.
This utility model produces certain buoyancy by air film body filled with helium, is filled with the amount of helium to enter by control
The adjustment of row load-carrying, the lift of helium balloon is in a basic balance by the weight of whole unmanned plane, and only the weight of remaining 20g to 200g needs
Lifted by electronic duct motor, therefore electronic duct motor just can be risen whole unmanned plane with less power,
Carry out aerial various actions.This utility model power consumption is less, and cruising time is longer, and the air film body filled with helium is produced and floated
Power, even if therefore unmanned plane it is out of control tenesmus also can slowly land, property will not be broken, also will not wound people, improve using safety
Property, it is highly suitable for factory's monitoring, technology production supervision and Factory Building tour of indoor and outdoor etc..As a huge balloon also
Can play with masses, because enough safety and endurance is very strong, can for a long time shoot large-scale public activity or performance
Meeting, in crowd overhead, quiet distance is arbitrarily flown, and can be dressed up as different profiles, and inside is installed additional after projector, is also used as moving
Dynamic projection screen is used.
Claims (7)
1. a kind of helium balloon unmanned plane, it is characterised in that include the air film body (1) filled with helium, air film body (1) is externally provided with some
The flight control system (3) for controlling electronic duct motor (2) is provided with electronic duct motor (2), air film body (1).
2. a kind of helium balloon unmanned plane according to claim 1, it is characterised in that described air film body (1) is externally provided with some
Steering wheel (4), the electronic duct motor (2) being provided with each steering wheel (4) described in, steering wheel (4) and described flight control system
(3) electrically connect.
3. a kind of helium balloon unmanned plane according to claim 1 and 2, it is characterised in that described electronic duct motor (2)
There are four, four electronic duct motors (2) are respectively arranged on left side, right side, front side and the rear side of described air film body (1), electronic
Setting-up piece (5) is provided between duct motor (2) and described air film body (1).
4. a kind of helium balloon unmanned plane according to claim 2, it is characterised in that described steering wheel (4) and described electronic
Duct motor (2) has two, and two steering wheels (4) are respectively arranged on described air film body (1) opposite sides outward, two electronic culverts
Road motor (2) is separately mounted on two steering wheels (4), and between steering wheel (4) and described air film body (1) setting-up piece (5) is provided with.
5. a kind of helium balloon unmanned plane according to claim 1 and 2, it is characterised in that described air film body (1) is spheroid,
Spheroid, cylinder, square or cuboid.
6. a kind of helium balloon unmanned plane according to claim 1 and 2, it is characterised in that is provided with described air film body (1)
Horizontally disposed skeleton (6), described flight control system (3) is on described skeleton (6).
7. a kind of helium balloon unmanned plane according to claim 3, it is characterised in that is provided with level in described air film body (1)
The skeleton (6) of setting, in cross, four terminations of skeleton (6) pass described air film body (1) to skeleton (6), described four
Electronic duct motor (2) is separately mounted on four terminations of skeleton (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621209683.2U CN206171785U (en) | 2016-11-09 | 2016-11-09 | Helium balloon unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621209683.2U CN206171785U (en) | 2016-11-09 | 2016-11-09 | Helium balloon unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206171785U true CN206171785U (en) | 2017-05-17 |
Family
ID=58685103
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621209683.2U Expired - Fee Related CN206171785U (en) | 2016-11-09 | 2016-11-09 | Helium balloon unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206171785U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI641532B (en) * | 2017-09-05 | 2018-11-21 | 朝陽科技大學 | UAV and its flying method and driving device |
| CN109353486A (en) * | 2018-11-12 | 2019-02-19 | 李紫萱 | A kind of balloon soaring plane |
| CN110816803A (en) * | 2019-10-12 | 2020-02-21 | 山东科技大学 | Small helium balloon double propeller control device and method |
-
2016
- 2016-11-09 CN CN201621209683.2U patent/CN206171785U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI641532B (en) * | 2017-09-05 | 2018-11-21 | 朝陽科技大學 | UAV and its flying method and driving device |
| CN109353486A (en) * | 2018-11-12 | 2019-02-19 | 李紫萱 | A kind of balloon soaring plane |
| CN110816803A (en) * | 2019-10-12 | 2020-02-21 | 山东科技大学 | Small helium balloon double propeller control device and method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206171785U (en) | Helium balloon unmanned aerial vehicle | |
| CN104787318A (en) | Multi-rotor unmanned aerial vehicle with function of loaded long-time flying | |
| CN203434576U (en) | Remote-controlled multi-shaft unmanned plane paying-off device | |
| CN207157480U (en) | Unmanned investigation dirigible system and low latitude detecting system | |
| CN105652886A (en) | Internet unmanned aerial vehicle capable of achieving continuous endurance | |
| CN106143908A (en) | A kind of safe and reliable Intelligent unattended machine with online generating function | |
| CN107244253B (en) | Charging system for electric automobile | |
| CN106347654A (en) | Spherical unmanned aerial vehicle | |
| CN105059541A (en) | Novel multi-axis unmanned aerial vehicle | |
| CN206265280U (en) | A kind of dirigible without rudder face structure | |
| CN201321159Y (en) | Unmanned aircraft with vertical ducts | |
| CN202711065U (en) | Ducted fan unmanned plane | |
| CN204916171U (en) | Many rotor unmanned aerial vehicle with flight of load long term | |
| CN205060014U (en) | Novel multiaxis unmanned aerial vehicle | |
| CN206434864U (en) | A kind of aircraft of VTOL | |
| CN205608525U (en) | Last internet unmanned aerial vehicle of continuation of journey | |
| CN206465717U (en) | Utilize wind energy and the amphibious moveable house of solar power generation | |
| CN105818954A (en) | Spherical unmanned airship based on dual remote control system | |
| CN209700924U (en) | A kind of unmanned plane during flying body with cage shape shielded frame | |
| CN209719887U (en) | A kind of rotor with Quick Release fast-assembling and air bag composite modules lighter-than-air flight device | |
| CN205060003U (en) | Low novel multiaxis unmanned aerial vehicle of power consumption cruises | |
| CN208828081U (en) | The huge pollution-free transhipment of dirigible synchronizes the system of letting fly away | |
| CN205931255U (en) | Spherical unmanned aerial vehicle based on ARM | |
| CN104843191A (en) | Non-contact type intelligent rainproof device for unmanned aerial vehicle | |
| CN204660017U (en) | A kind of kite assisting in flying device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170517 Termination date: 20181109 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |