CN208775026U - A kind of unmanned plane external source auxiliary prolongs boat system - Google Patents
A kind of unmanned plane external source auxiliary prolongs boat system Download PDFInfo
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- CN208775026U CN208775026U CN201820513210.4U CN201820513210U CN208775026U CN 208775026 U CN208775026 U CN 208775026U CN 201820513210 U CN201820513210 U CN 201820513210U CN 208775026 U CN208775026 U CN 208775026U
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- unmanned plane
- magnetic force
- line cutting
- energy conversion
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Abstract
The utility model discloses a kind of unmanned plane external source auxiliary to prolong boat system, including energy conversion module, drainage conducting wire, magnetic force line cutting control holder and magnetic force line cutting module；Wherein the output end of energy conversion module is electrically connected with the input terminal of magnetic force line cutting holder, the output end of magnetic force line cutting control holder is connect with magnetic force line cutting module, energy conversion module is accessed by drainage conducting wire in the both ends of magnetic force line cutting module, and the output end of energy conversion module accesses unmanned plane original power supply system.The utility model is according to the movement velocity of unmanned plane and the angle of unmanned plane relative magnetic line, provide executing instruction for magnetic force line cutting control holder, Extensible magnetic line of force cutting module is controlled, the hollow contact tube of merogenesis moves in the magnetic field of transmission line of electricity, cutting magnetic line, induced electromotive force is generated, by draining conducting wire, accesses AD/DC rectification module and DC/DC copped wave module, it realizes energy conversion, finally provides suitable charge capacity to unmanned plane original power supply system.
Description
Technical field
The utility model relates to unmanned plane fields, prolong boat system more particularly, to a kind of unmanned plane external source auxiliary.
Background technique
Unmanned plane is widely used to overhead transmission line and makes an inspection tour operation, airborne visible light high definition camera and video camera
Deng the main means for becoming route and shaft tower and making an inspection tour, visual range is close, can multi-angled shooting, can and measured target it is quick etc. excellent
Point greatly improves the quality and efficiency of transmission line of electricity.Multiple operating condition this for night breakdown repair, using more rotors nobody
Machine is when shortening fault outage with in-situ data in time, is accurately and efficiently obtained to the fast, accurately positioning of abort situation
Between, improve electric power first-aid efficiency effective way.And a disadvantage of multi-rotor unmanned aerial vehicle itself is that cruise duration is short, is generally existed
30 minutes or so, the poor operating environment big in face of windage carried the continuation of the journey of the multi-rotor unmanned aerial vehicle of night servicing lighting
It is shorter, it is unable to satisfy the continuation of the journey demand of night line walking.The industrial level of the batteries such as current lithium battery can't increase substantially
Its energy density will greatly increase the volume and gross weight of unmanned plane if increasing battery capacity, by the side for increasing battery capacity
Formula is not effective come the cruise duration for increasing unmanned plane continuation of the journey.Therefore it needs to design a kind of unmanned plane external source auxiliary and prolongs boat system.
Summary of the invention
The purpose of this utility model is to solve said one or multiple defects, proposes that a kind of unmanned plane external source auxiliary prolongs boat system
System.
To realize the above goal of the invention, the technical solution adopted is that:
A kind of unmanned plane external source auxiliary prolongs boat system, including energy conversion module, drainage conducting wire, magnetic force line cutting control cloud
Platform and magnetic force line cutting module；Wherein the output end of energy conversion module is electrically connected with the input terminal of magnetic force line cutting holder, magnetic
The output end of line of force cut-sytle pollination holder is connect with magnetic force line cutting module, and the both ends of magnetic force line cutting module pass through drainage conducting wire
Energy conversion module is accessed, the output end of energy conversion module accesses unmanned plane original power supply system.
Preferably, the magnetic force cutting module includes the hollow contact tube of merogenesis that conductive metal material is constituted.
Preferably, the hollow contact tube of the merogenesis is retractable structure.
Preferably, the conductive metal material includes one kind of aluminium or copper.
Preferably, the energy conversion module includes main control module, AD/DC rectification module and DC/DC copped wave module；Its
The output end of middle main control module transmits a signal to magnetic force cutting holder, AD/DC rectification module and DC/DC copped wave module respectively；
The input terminal of AD/DC rectification module is connect by draining conducting wire with magnetic force line cutting module, output end and DC/DC copped wave module
Input terminal electrical connection；The output end of DC/DC copped wave module is electrically connected with unmanned plane original power supply system.
Compared with prior art, the beneficial effects of the present invention are:
1) external electric energy of this system, which obtains the transmission line of electricity for having near wireless and flight track and has no physics, connects
Touching greatly improves flexibility and safety in utilization that auxiliary prolongs boat system；
2) unmanned plane can constantly obtain the supplement of energy in entire flight course, meet night poor operating environment
The continuation of the journey demand of lower unmanned plane line walking；
3) design of magnetic force line cutting control holder is so that induced electromotive force on the hollow contact tube of merogenesis always can be with
Magnetic line of force magnetic induction intensity is linear, and the electric energy that the energy conversion links after being export high power quality lays the foundation.
Detailed description of the invention
Fig. 1 is the overall system architecture figure of the utility model；
Fig. 2 is the systematic schematic diagram of the utility model.
Specific embodiment
The attached figures are only used for illustrative purposes and cannot be understood as limitating the patent；
Below in conjunction with drawings and examples, the present invention is further elaborated.
Embodiment 1
A kind of unmanned plane external source auxiliary prolongs boat system, referring to FIG. 1, including energy conversion module 1, drainage conducting wire 2, magnetic force
Wire cutting controls holder 3 and magnetic force line cutting module 4；The wherein output end of energy conversion module 1 and magnetic force line cutting holder 3
The output end of input terminal electrical connection, magnetic force line cutting control holder 3 is connect with magnetic force line cutting module 4, magnetic force line cutting module 4
Both ends by drainage conducting wire 2 access energy conversion module 1, energy conversion module 1 output end access unmanned plane original power supply system
System.
In the present embodiment, the magnetic force cutting module 4 includes the hollow contact tube of merogenesis that conductive metal material is constituted.
In the present embodiment, the hollow contact tube of merogenesis is retractable structure.
In the present embodiment, the conductive metal material includes one kind of aluminium or copper.By the high conductivity metals material such as aluminium or copper
Texture at the hollow contact tube of merogenesis, moved in the magnetic field of transmission line of electricity, cutting magnetic line, induced electromotive force generated, can
The size of the induced electromotive force generated in flexible magnetic force line cutting module 4 is by the magnetic line of force magnetic induction intensity, the electric conductor that cut
The angle of length, the movement velocity of electric conductor and electric conductor cutting magnetic line determines.
In the present embodiment, conducting wire 2 is drained by remaining module in Extensible magnetic line of force cutting module 4, this system and nobody
Machine original power supply system is linked to be a closed circuit.Magnetic force line cutting, which controls holder 3 and controls in Extensible magnetic line of force cutting module 4, divides
Save the length of hollow contact tube and the angle of cutting magnetic line.
Referring to FIG. 2, the energy conversion module 1 includes main control module, AD/DC rectification module and DC/DC copped wave mould
Block；Wherein the output end of main control module transmits a signal to magnetic force cutting holder 3, AD/DC rectification module and DC/DC respectively and cuts
Wave module；The input terminal of AD/DC rectification module is connect by draining conducting wire 2 with magnetic force line cutting module 4, output end and DC/DC
The input terminal of copped wave module is electrically connected；The output end of DC/DC copped wave module is electrically connected with unmanned plane original power supply system.
In the present embodiment, it main control module: according to the angle of the movement velocity of unmanned plane and unmanned plane relative magnetic line, gives
Magnetic force line cutting controls executing instruction for holder 3 out, Extensible magnetic line of force cutting module 4 is controlled, so that the hollow contact tube of merogenesis
Induced electromotive force on shape electric conductor can be linear with magnetic line of force magnetic induction intensity；AD/DC rectification module: by electric conductor
The AC conversion of cutting magnetic line is direct current；DC/DC copped wave module: the output voltage of AD/DC rectification module, output are adjusted
With the matched voltage of unmanned plane original power supply system.
In the present embodiment, main control module is given according to the movement velocity of unmanned plane and the angle of unmanned plane relative magnetic line
Magnetic force line cutting controls executing instruction for holder 3 out, controls Extensible magnetic line of force cutting module 4, the hollow contact tube of merogenesis, defeated
It is moved in the magnetic field of electric line, cutting magnetic line, generates induced electromotive force, by draining conducting wire 2, access AD/DC rectification module
With DC/DC copped wave module, realizes energy conversion, finally provide suitable charge capacity to unmanned plane original power supply system.
Obviously, the above embodiment of the present invention be only to clearly illustrate example of the present invention, and not be pair
The restriction of embodiments of the present invention.For those of ordinary skill in the art, may be used also on the basis of the above description
To make other variations or changes in different ways.There is no necessity and possibility to exhaust all the enbodiments.It is all this
Made any modifications, equivalent replacements, and improvements etc., should be included in the claims in the present invention within the spirit and principle of invention
Protection scope within.
Claims (5)
1. a kind of unmanned plane external source auxiliary prolongs boat system, which is characterized in that including energy conversion module (1), drainage conducting wire (2),
Magnetic force line cutting controls holder (3) and magnetic force line cutting module (4)；The wherein output end and the magnetic line of force of energy conversion module (1)
The input terminal electrical connection of holder (3) is cut, magnetic force line cutting controls the output end of holder (3) and magnetic force line cutting module (4) connect
Connect, the both ends of magnetic force line cutting module (4) by drainage conducting wire access energy conversion module (1), energy conversion module (1) it is defeated
Outlet accesses unmanned plane original power supply system.
2. a kind of unmanned plane external source auxiliary according to claim 1 prolongs boat system, which is characterized in that the magnetic force blanking punch
Block (4) includes the hollow contact tube of merogenesis that conductive metal material is constituted.
3. a kind of unmanned plane external source auxiliary according to claim 2 prolongs boat system, which is characterized in that the merogenesis is hollow to lead
Fulgurite is retractable structure.
4. a kind of unmanned plane external source auxiliary according to claim 2 prolongs boat system, which is characterized in that the conductive metal material
Matter includes one kind of aluminium or copper.
5. a kind of unmanned plane external source auxiliary according to claim 1 prolongs boat system, which is characterized in that the energy converts mould
Block (1) includes main control module, AD/DC rectification module and DC/DC copped wave module；Wherein the output end of main control module is respectively by signal
It is transmitted to magnetic force cutting holder (3), AD/DC rectification module and DC/DC copped wave module；The input terminal of AD/DC rectification module passes through
Drainage conducting wire (2) is connect with magnetic force line cutting module (4), and output end is electrically connected with the input terminal of DC/DC copped wave module；DC/DC
The output end of copped wave module is electrically connected with unmanned plane original power supply system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820513210.4U CN208775026U (en) | 2018-04-10 | 2018-04-10 | A kind of unmanned plane external source auxiliary prolongs boat system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820513210.4U CN208775026U (en) | 2018-04-10 | 2018-04-10 | A kind of unmanned plane external source auxiliary prolongs boat system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208775026U true CN208775026U (en) | 2019-04-23 |
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ID=66140802
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820513210.4U Active CN208775026U (en) | 2018-04-10 | 2018-04-10 | A kind of unmanned plane external source auxiliary prolongs boat system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208775026U (en) |
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2018
- 2018-04-10 CN CN201820513210.4U patent/CN208775026U/en active Active
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