CN207045715U - A kind of novel and multifunctional unmanned plane - Google Patents
A kind of novel and multifunctional unmanned plane Download PDFInfo
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- CN207045715U CN207045715U CN201720758148.0U CN201720758148U CN207045715U CN 207045715 U CN207045715 U CN 207045715U CN 201720758148 U CN201720758148 U CN 201720758148U CN 207045715 U CN207045715 U CN 207045715U
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Abstract
A kind of novel and multifunctional unmanned plane, including：Unmanned plane body, suspension apparatus, battery-allocated circuit and combined battery placing structure；The suspension apparatus is arranged on the unmanned plane body lower part, and the combined battery placing structure includes：Battery case, the first clamping unit and the second clamping unit；The battery-allocated circuit is used to distribute the order that unmanned plane is dished out with the job order and battery of battery；The combined battery placing structure is designed as laying number of batteries as the natural number more than 1, and the unmanned plane possesses multi-functional tasks carrying effect, and more traditional shooting unmanned plane possesses preferable market prospects；By cell module structure design and the new concept dished out without battery control, the cruising time of existing unmanned plane is considerably increased, weakens the deficiency that unmanned plane field of batteries development limitation is acted on behalf of.
Description
Technical field
The utility model patent is related to a kind of unmanned aerial vehicle design new construction technical field, especially a kind of novel and multifunctional nothing
Man-machine, the unmanned plane uses brand-new Structural design idea so that unmanned plane stand-by time is longer, possesses multi-functional tasks carrying
Operation.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates；It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc.；
Unmanned plane presses application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.The people
Unmanned plane+sector application, it is that unmanned plane has really just needed with aspect；At present take photo by plane, agricultural, plant protection, self-timer, express transportation,
Disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture wave
The application in unrestrained etc. field, has greatly expanded the purposes of unmanned plane in itself, developed country also actively extension sector application with
Develop unmanned air vehicle technique.
Multi-rotor unmanned aerial vehicle, it is a kind of special pilotless helicopter with multiple rotor shafts, it passes through each axle
On motor rotation, drive rotor, so as to produce lift, rotor always away from typically immobilizing, rather than general helicopter
It is variable like that；By changing the relative rotation speed between different rotors, thus it is possible to vary the size of single shaft propulsive force, so as to control flight
The running orbit of device；Because multi-rotor unmanned aerial vehicle, without runway, be able to can be hovered in the air with VTOL, manipulate simple etc. more
Kind of advantage, it is increasingly deep among the production and life of people, and " in one's hands to fly ", individual are taken photo by plane machine and exploration, rescue etc.；
In the prior art, the battery design capacity of unmanned plane greatly limit the development of unmanned air vehicle technique, have
The battery capacity of limit largely determines the overall valency of the cruising time of unmanned plane, tasks carrying species and unmanned plane
Lattice.
Utility model content
The purpose of this utility model is to provide a kind of novel and multifunctional unmanned plane, solves in the prior art, unmanned plane is standby
Time taken a step not because of the development limitation of existing battery design technology before awkward situation, and by install additional seek survival rescue etc. equipment,
Realize multi-functional and the whole body new construction unmanned plane；
A kind of novel and multifunctional unmanned plane, including：Unmanned plane body, suspension apparatus, battery-allocated circuit and combined type
Battery accommodating structure；
Further, in addition to：Infrared temperature probe, radar range finder, solar recharging accessory plate and scalable machine
Arm configuration；
As a kind of for example, the infrared temperature when infrared temperature probe can be used for rescuing or investigating is imaged；
As a kind of for example, the radar range finder can be used for measuring the stranded distance of trapped personnel；
As one kind for example, the solar recharging accessory plate is arranged on unmanned plane body upper part, for battery
Auxiliary charging；
As one kind for example, the horn structure setting is folding type telescopic structure, drawer-like slideway is built-in
Neck, the elongation that can be very good to carry out horn operate with shortening, and considerably increase the application of unmanned plane；
Further, the preferably existing multi-rotor unmanned aerial vehicle of the unmanned plane body is as body；
Further, the suspension apparatus is arranged on the unmanned plane body lower part, and thing is transferred in the suspention for unmanned plane
Product operation；The suspension apparatus includes：Fixed structure, starter motor and the pull rope being fixed on below unmanned plane body；
As one kind for example, the starter motor selects DC micro starter motor；
As a kind of for example, the pull rope is from toughness and the preferable nylon rope of rigidity or steel wire rope；
Further, the combined battery placing structure includes：Battery case, the first clamping unit and the second card-tight part
Part；
Used as one kind for example, being provided with the battery case with the same number of electrical power contacts of arranging batteries
Head；
As it is a kind of for example, first clamping unit for fixed setting protrusion structure, accordingly pacify for clamping
The side of packed battery；
As it is a kind of for example, second clamping unit for activity set can protruding-type structure, for clamping phase
The opposite side of battery should be installed；
It is described activity set can protruding-type structure include：Two hot-wire coils, two metal columns as coil inside,
The hot-wire coil is symmetrical arranged on same axis；
As a kind of for example, the metal column is made using the soft intermetallic composite coating for being not easy to be magnetized；
Further, the battery-allocated circuit be used for distribute unmanned plane dished out with the job order and battery of battery it is suitable
Sequence；
As a kind of for example, the battery-allocated circuit is arranged on the inside of unmanned plane body；
As a kind of for example, it is oneself more than 1 that the combined battery placing structure, which is designed as placement number of batteries,
So number；
In order to better illustrate design principle of the present utility model, it is as follows now briefly to introduce its course of work：
First, determine that unmanned plane participates in task, exemplified by falling into high mountain gorge parietal suture trapped personnel, the combined battery
Placing structure is designed as four pieces of battery citings；Open unmanned plane to rise at winged paramount waterway between mountains valley wall seam, pass through the suspension apparatus
Food is transferred, quote water or rescues rope；
Secondly, when apart from it is far when can be powered respectively by described four pieces of batteries of battery-allocated circuit wheel flow control, together
When control two hot-wire coils in the second clamping unit, pass through the power supply respectively in identical or different direction so that the metal
Post is attracted or repelled, and reaches blocking and dishing out for battery, the overall weight of unmanned plane is reduced with this, extend the work of stand-by time
With；
In order to facilitate battery recycling, lightweight parachute is also provided with the battery, when battery is spilled over, is followed
The wind resistance of freely falling body automatically opens up；
As a kind of for example, the parachute is made using paper material；
Finally, the horn length of each occasion, after reclaiming battery, charging can be set by the flexible controllability of horn
After treat next subtask；
The beneficial effects of the utility model：
1. the unmanned plane possesses multi-functional tasks carrying effect, more traditional shooting unmanned plane possesses preferable market prospects；
2. by cell module structure design and without the new concept dished out of battery control, considerably increase it is existing nobody
In the cruising time of machine, weaken the deficiency of unmanned plane field of batteries development limitation agency.
Brief description of the drawings
Fig. 1 is a kind of overall structure diagram of novel and multifunctional unmanned plane of the utility model.
Fig. 2 is a kind of combined battery placing structure diagrammatic cross-section of novel and multifunctional unmanned plane of the utility model.
Embodiment
Preferred embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
Referring to figs. 1 to shown in Fig. 2, a kind of novel and multifunctional unmanned plane, including：Unmanned plane body 101, suspension apparatus 102,
Battery-allocated circuit 103 and combined battery placing structure 104；
Further, in addition to：Infrared temperature probe, radar range finder, solar recharging accessory plate and scalable machine
Arm configuration 105；The infrared temperature probe, radar range finder are arranged at the lower outside of unmanned plane body 101；
As a kind of for example, the infrared temperature when infrared temperature probe can be used for rescuing or investigating is imaged；
As a kind of for example, the radar range finder can be used for measuring the stranded distance of trapped personnel；
As one kind for example, the solar recharging accessory plate is arranged on the top of unmanned plane body 101, for battery
Auxiliary charging；
As a kind of for example, the horn structure 105 is arranged to folding type telescopic structure, drawer-like slideway,
Built-in neck, the elongation that can be very good to carry out horn operate with shortening, and considerably increase the application of unmanned plane；
Further, the preferably existing multi-rotor unmanned aerial vehicle of the unmanned plane body 101 is as body；
Further, the suspension apparatus 102 is arranged on the bottom of unmanned plane body 101, the suspention for unmanned plane
Lowering of articles operation；The suspension apparatus 102 includes：Be fixed on the fixed structure of the lower section of unmanned plane body 101, starter motor and
Pull rope；
As one kind for example, the starter motor selects DC micro starter motor；
As a kind of for example, the pull rope is from toughness and the preferable nylon rope of rigidity or steel wire rope；
Further, the combined battery placing structure 104 includes：Battery case 201, the first clamping unit 202 and
Two clamping units 203；
As one kind for example, be provided with the battery case 201 makes with the same number of electrical power contacts of arranging batteries
With head；
As it is a kind of for example, first clamping unit 202 for fixed setting protrusion structure, it is corresponding for clamping
The side of battery is installed；
As it is a kind of for example, second clamping unit 203 for activity set can protruding-type structure, for clamping
The opposite side of corresponding installation battery；
It is described activity set can protruding-type structure include：Two hot-wire coils, two metal columns as coil inside,
The hot-wire coil is symmetrical arranged on same axis；
As a kind of for example, the metal column is made using the soft intermetallic composite coating for being not easy to be magnetized；
Further, the battery-allocated circuit 103 is dished out for distributing unmanned plane with the job order and battery of battery
Order；
As a kind of for example, the battery-allocated circuit 103 is arranged on the inside of unmanned plane body；
As a kind of for example, the combined battery placing structure 104 is designed as laying number of batteries as more than 1
Natural number；
In order to better illustrate design principle of the present utility model, it is as follows now briefly to introduce its course of work：
First, determine that unmanned plane participates in task, exemplified by falling into high mountain gorge parietal suture trapped personnel, the combined battery
Placing structure 104 is designed as four pieces of battery citings；Open unmanned plane to rise at winged paramount waterway between mountains valley wall seam, pass through the suspention and fill
Decentralization food is put, quote water or rescues rope；
Secondly, when apart from it is far when can by the battery-allocated circuit 103 take turns four pieces of batteries of flow control power respectively,
Two hot-wire coils in the second clamping unit 203 are controlled simultaneously, pass through the power supply respectively in identical or different direction so that described
Metal column is attracted or repelled, and reaches blocking and dishing out for battery, the overall weight of unmanned plane is reduced with this, extends stand-by time
Effect；
In order to facilitate battery recycling, lightweight parachute is also provided with the battery, when battery is spilled over, is followed
The wind resistance of freely falling body automatically opens up；
As a kind of for example, the parachute is made using paper material；
Finally, the length of horn 105 of each occasion by the flexible controllability of horn 105, can be set, reclaims battery
Afterwards, next subtask is treated after charging；
The unmanned plane possesses multi-functional tasks carrying effect, and more traditional shooting unmanned plane possesses preferable market prospects；It is logical
Cell module structure design and the new concept dished out without battery control are crossed, when considerably increasing the continuation of the journey of existing unmanned plane
Between, weaken the deficiency that unmanned plane field of batteries development limitation is acted on behalf of；
Above-described is only preferred embodiment of the present utility model, should be understood that the explanation of above example only
It is to be used to help understand method and its core concept of the present utility model, is not used to limit the scope of protection of the utility model,
All any modifications made within thought of the present utility model and principle, equivalent substitution etc., it is new to should be included in this practicality
Within the protection domain of type.
Claims (10)
1. a kind of novel and multifunctional unmanned plane, including：Unmanned plane body, it is characterised in that also include：Suspension apparatus, battery point
With circuit and combined battery placing structure；
The suspension apparatus is arranged on the unmanned plane body lower part, and the suspension apparatus includes：It is fixed under unmanned plane body
Fixed structure, starter motor and the pull rope of side；
The combined battery placing structure includes：Battery case, the first clamping unit and the second clamping unit；In the battery case
It is provided with and uses head with the same number of electrical power contacts of arranging batteries；First clamping unit is tied for the prominent of fixed setting
Structure, second clamping unit can protruding-type structures for activity setting；It is described activity set can protruding-type structure include：Two
Individual hot-wire coil, two metal columns for being placed in coil inside, the hot-wire coil are symmetrical arranged on same axis；It is described
Battery-allocated circuit is used to distribute the order that unmanned plane is dished out with the job order and battery of battery；The battery-allocated circuit is set
Put on the inside of unmanned plane body；The combined battery placing structure is designed as laying number of batteries as the natural number more than 1.
2. a kind of novel and multifunctional unmanned plane according to claim 1, it is characterised in that be additionally provided with the body red
Outer temperature probe, radar range finder, solar recharging accessory plate and scalable horn structure.
3. a kind of novel and multifunctional unmanned plane according to claim 2, it is characterised in that the infrared temperature probe can use
Infrared temperature imaging when rescue or investigation；The radar range finder can be used for measuring the stranded distance of trapped personnel；
The solar recharging accessory plate is arranged on unmanned plane body upper part, the auxiliary charging for battery.
4. a kind of novel and multifunctional unmanned plane according to claim 2, it is characterised in that the horn structure setting is folding
Neck built in stacked Collapsible structure.
5. a kind of novel and multifunctional unmanned plane according to claim 4, it is characterised in that the unmanned plane body uses more
Rotor wing unmanned aerial vehicle is as body.
6. a kind of novel and multifunctional unmanned plane according to claim 5, it is characterised in that the starter motor is micro- from direct current
Type starter motor.
A kind of 7. novel and multifunctional unmanned plane according to claim 6, it is characterised in that the pull rope from toughness with
The preferable nylon rope of rigidity or steel wire rope.
A kind of 8. novel and multifunctional unmanned plane according to claim 7, it is characterised in that the metal column using it is soft not
The intermetallic composite coating being easily magnetized makes.
9. a kind of novel and multifunctional unmanned plane according to claim 8, it is characterised in that be provided with lightweight on the battery
Parachute.
10. a kind of novel and multifunctional unmanned plane according to claim 9, it is characterised in that the parachute uses papery
Material makes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720758148.0U CN207045715U (en) | 2017-06-27 | 2017-06-27 | A kind of novel and multifunctional unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720758148.0U CN207045715U (en) | 2017-06-27 | 2017-06-27 | A kind of novel and multifunctional unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045715U true CN207045715U (en) | 2018-02-27 |
Family
ID=61492515
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720758148.0U Active CN207045715U (en) | 2017-06-27 | 2017-06-27 | A kind of novel and multifunctional unmanned plane |
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| Country | Link |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109398706A (en) * | 2018-12-05 | 2019-03-01 | 智灵飞（北京）科技有限公司 | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn |
| CN113911371A (en) * | 2021-10-14 | 2022-01-11 | 贵州电网有限责任公司 | Unmanned aerial vehicle battery increase-volume anti-falling system |
| WO2022095335A1 (en) * | 2020-11-05 | 2022-05-12 | 北星空间信息技术研究院(南京)有限公司 | Multi-rotor unmanned aerial vehicle-based priority algorithm for jettisonable accessories |
-
2017
- 2017-06-27 CN CN201720758148.0U patent/CN207045715U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109398706A (en) * | 2018-12-05 | 2019-03-01 | 智灵飞（北京）科技有限公司 | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn |
| WO2022095335A1 (en) * | 2020-11-05 | 2022-05-12 | 北星空间信息技术研究院(南京)有限公司 | Multi-rotor unmanned aerial vehicle-based priority algorithm for jettisonable accessories |
| CN113911371A (en) * | 2021-10-14 | 2022-01-11 | 贵州电网有限责任公司 | Unmanned aerial vehicle battery increase-volume anti-falling system |
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