CN207910021U - Helicopter Safety exit light solar energy charging and discharging lithium battery control device - Google Patents
Helicopter Safety exit light solar energy charging and discharging lithium battery control device Download PDFInfo
- Publication number
- CN207910021U CN207910021U CN201820383289.3U CN201820383289U CN207910021U CN 207910021 U CN207910021 U CN 207910021U CN 201820383289 U CN201820383289 U CN 201820383289U CN 207910021 U CN207910021 U CN 207910021U
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- CN
- China
- Prior art keywords
- protective housing
- main body
- controller main
- solar energy
- lithium battery
- 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.)
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E70/00—Other energy conversion or management systems reducing GHG emissions
- Y02E70/30—Systems combining energy storage with energy generation of non-fossil origin
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Abstract
The utility model discloses a kind of Helicopter Safety exit light solar energy charging and discharging lithium battery control devices, including connecting plate, protective housing, controller main body, anti-tampering magnet ring and reflecting plate, connecting plate is fixed in protective housing bottom end, the both sides of connecting plate are equipped with several screw holes, the side on protective housing top has been pivotally mounted case lid, controller main body is fixed in protective housing, protective housing and case lid play controller main body preliminary protective action, the performance in terms of external collision and preliminary electromagnetism interference can be resisted, it is radiated by ventilation hole inside protective housing, in order to avoid extraneous electromagnetic interference, reflecting plate will effectively be gone out into ventilation hole electromagnetism by baffle reflection, using anti-tampering magnet ring, significantly reduce the possibility that electromagnetic interference is generated between conductor wire;The utility model is simple in structure, is readily produced manufacture, of low cost, has a good application prospect.
Description
Technical field
The utility model is related to charging-discharging controller fields, and in particular to a kind of Helicopter Safety exit light solar energy lithium electricity
Pond charge-discharge controller.
Background technology
With making constant progress for circuit design and enriching constantly for circuit control device, solar energy lithium battery
Various requirements such as the stability of charging-discharging controller are also higher and higher, however, charging-discharging controller equipment traditional at present
Still there is a problem of it is more, if anti-interference ability is weak, without unique anti-interference method, in actual use, be easy by
The interference of electromagnetic field, changes of magnetic field can all interfere controller as caused by thunder and lightning so that control panel performance is unreliable, leads
Cause under severe interference environment can not normal operation, therefore, a kind of charge and discharge for Helicopter Safety exit light is studied by my company
The anti-tampering equipment of electricity, solves problem above.
Utility model content
In order to overcome the deficiencies of existing technologies, the technical problem to be solved by the utility model is to provide a kind of helicopters
Exit light solar energy charging and discharging lithium battery control device can not only effectively reduce the interference of electromagnetic field, improve the sun
Can charging and discharging lithium battery controller stability, and changes of magnetic field caused by can reducing thunder and lightning is done caused by controller
It disturbs.
For this purpose, the utility model uses following technical scheme:
The utility model provides a kind of Helicopter Safety exit light solar energy charging and discharging lithium battery control device, including even
Fishplate bar, protective housing, controller main body, anti-tampering magnet ring and reflecting plate, the connecting plate is fixed in the protective housing bottom end, described
The both sides of connecting plate are equipped with several screw holes, and the side on the protective housing top has been pivotally mounted case lid, the controller master
Body is fixed in the protective housing, and the controller main body includes several conductor wires, and the anti-tampering magnet ring quantity is multiple, institute
It states several conductor wires and runs through the anti-tampering magnet ring, the side wall of the protective housing close to the conductor wire is fixed with wiring and inserts
Seat, the other end and the connector socket of several conductor wires electrically connect, and the top of the protective housing offers multiple ventilations
The side in hole, controller main body close to the ventilation hole is installed with connecting rod, and the reflecting plate is fixedly installed in institute
Connecting rod top is stated, the reflecting surface of the reflecting plate towards the ventilation hole and covers multiple ventilation holes settings.
In the utility model preferably technical solution, multiple ventilation holes are rounded to be uniformly distributed, and further includes fixing
In multiple exhaust fans of the protection chamber interior wall, multiple exhaust fans are around multiple ventilation hole settings.
In the utility model preferably technical solution, the protective housing and the case lid use acrylic board material.
In the utility model preferably technical solution, rubber pad, institute are equipped between the connecting plate and the protective housing
State inside rubber pad is honeycomb.
In the utility model preferably technical solution, peace is fixed in side of the controller main body far from the ventilation hole
Equipped with temperature sensor, and the protection box outer wall is equipped with the alarm bell electrically connected with the temperature sensor.
The beneficial effects of the utility model are:
Helicopter Safety exit light solar energy charging and discharging lithium battery control device provided by the utility model, protective housing and case
Lid plays controller main body preliminary protective action, can resist the property in terms of external collision and preliminary electromagnetism interference
Can, it is radiated by ventilation hole inside protective housing, in order to avoid extraneous electromagnetic interference, reflecting plate is set in the lower section of ventilation hole,
It will effectively can be gone out into ventilation hole electromagnetism by baffle reflection while realizing ventilated to controller main body,
Using anti-tampering magnet ring, the possibility of generation electromagnetic interference between conductor wire is significantly reduced;The utility model is simple in structure, easily
It is of low cost in the manufacturing, it has a good application prospect.
Description of the drawings
Fig. 1 is the main view schematic diagram of the utility model;
Fig. 2 is the side view figure structure schematic representation of the utility model.
In figure:1, connecting plate;11, screw hole;2, protective housing;21, case lid;22, ventilation hole;23, exhaust fan;3, controller
Main body;31, conductor wire;32, connector socket;33, connecting rod;34, temperature sensor;35, alarm bell;4, anti-tampering magnet ring;5, anti-
Penetrate plate;6, rubber pad.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
It removes, be fully described by, wherein the drawings are for illustrative purposes only and are merely schematic diagrams rather than pictorial diagram, Bu Nengli
Solution is the limitation to this patent;In order to better illustrate the utility model embodiment, the certain components of attached drawing have omission, amplification
Or reduce, do not represent the size of actual product;It will be understood by those skilled in the art that certain known features and its explanation in attached drawing
It may omit and will be understood by.
The described embodiments are only a part of the embodiments of the utility model for the utility model, rather than whole implementation
Example.Based on the embodiments of the present invention, those of ordinary skill in the art are obtained without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
Embodiment is described in detail:
As shown in Figure 1 to Figure 2, a kind of Helicopter Safety exit light solar energy charging and discharging lithium battery control is provided in embodiment
Device processed, including connecting plate 1, protective housing 2, controller main body 3, anti-tampering magnet ring 4 and reflecting plate 5,2 bottom end of the protective housing are solid
It is equipped with several screw holes 11, the side pivot joint on 2 top of the protective housing due to the both sides of the connecting plate 1, the connecting plate 1
Case lid 21 is installed, the controller main body 3 is fixed in the protective housing 2, and the controller main body 3 includes several conductor wires
31,4 quantity of anti-tampering magnet ring is multiple, and several conductor wires 31 run through the anti-tampering magnet ring 4, the protective housing 2
Side wall close to the conductor wire 31 is fixed with connector socket 32, and the other end and the wiring of several conductor wires 31 are inserted
Seat 32 electrically connects, and the top of the protective housing 2 offers multiple ventilation holes 22, and the controller main body 3 is close to the ventilation hole
22 side is installed with connecting rod 33, and the reflecting plate 5 is fixedly installed in 33 top of the connecting rod, the reflecting plate 5
Reflecting surface be arranged towards the ventilation hole 22 and the multiple ventilation holes 22 of covering.
Helicopter Safety exit light solar energy charging and discharging lithium battery control device provided by the utility model, protective housing and case
Lid plays controller main body preliminary protective action, can resist the property in terms of external collision and preliminary electromagnetism interference
Can, it is radiated by ventilation hole inside protective housing, in order to avoid extraneous electromagnetic interference, reflecting plate is set in the lower section of ventilation hole,
It will effectively can be gone out into ventilation hole electromagnetism by baffle reflection while realizing ventilated to controller main body,
Using anti-tampering magnet ring, the possibility of generation electromagnetic interference between conductor wire is significantly reduced;The utility model is simple in structure, easily
It is of low cost in the manufacturing, it has a good application prospect.
In the present embodiment, multiple ventilation holes 22 are rounded is uniformly distributed, and further includes being fixed in the protective housing 2
Multiple exhaust fans 23 of wall, multiple exhaust fans 23 are arranged around multiple ventilation holes 22;Specifically, multiple exhaust fans 23
It is fixed on the upper surface of 5 outer of reflecting plate, the air inside protective housing 2 is taken out towards the ventilation hole 22 in the air port of exhaust fan
Go out outside protective housing 2, to enhance the heat dissipation effect in protective housing 2.
In the present embodiment, the protective housing 2 and the case lid 21 use acrylic board material;The shock resistance of acrylic board
Power is strong, is 16 times of simple glass, is adapted for mount on the area for especially needing safety, and excellent insulating property, easy to maintain.
In the present embodiment, rubber pad 6 is equipped between the connecting plate 1 and the protective housing 2, inside the rubber pad 6
For honeycomb.The rubber pad 6 of internal cellular structure plays shockproof effect, avoid encountering during helicopter flight air blast or
The macroseism generated in person's descent impacts controller main body 3 and even damages.
In the present embodiment, 3 side far from the ventilation hole 22 of the controller main body is installed with temperature sensing
Device 34, and the protection box outer wall is equipped with the alarm bell 35 electrically connected with the temperature sensor 34.Temperature sensor 34 can be
Controller main body 3 senses the variation of temperature and timely sends out early warning to user by alarm bell 35 when breaking down, ensure
The safety of controller main body 3 when in use.
The utility model is described with reference to the preferred embodiments, and those skilled in the art know, is not departing from this reality
In the case of with novel principle and spirit, various changes, modification, replacement and volume can be carried out to these features and embodiment
It writes, still falls in the scope of protection of the utility model.The utility model is not limited to the particular embodiment disclosed,
The embodiment that he falls into claims hereof shall fall within the protection scope of the present invention.
Claims (5)
1. a kind of Helicopter Safety exit light solar energy charging and discharging lithium battery control device, it is characterised in that:Including connecting plate
(1), protective housing (2), controller main body (3), anti-tampering magnet ring (4) and reflecting plate (5), protective housing (2) bottom end are fixed on
The both sides of the connecting plate (1), the connecting plate (1) are equipped with several screw holes (11), the side on protective housing (2) top
It is pivotally mounted case lid (21), the controller main body (3) is fixed in the protective housing (2), controller main body (3) packet
Several conductor wires (31) are included, anti-tampering magnet ring (4) quantity is multiple, and several conductor wires (31) are through described anti-tampering
Magnet ring (4), the side wall of protective housing (2) close to the conductor wire (31) are fixed with connector socket (32), several described to lead
The other end of electric wire (31) is electrically connected with the connector socket (32), and the top of the protective housing (2) offers multiple ventilation holes
(22), the side of controller main body (3) close to the ventilation hole (22) is installed with connecting rod (33), the reflecting plate
(5) it is fixedly installed in the connecting rod (33) top, the reflecting surface of the reflecting plate (5) towards the ventilation hole (22) and covers
The multiple ventilation hole (22) settings.
2. Helicopter Safety exit light solar energy charging and discharging lithium battery control device according to claim 1, feature exist
In:Multiple ventilation holes (22) are rounded to be uniformly distributed, and further includes the multiple exhaust fans for being fixed on the protective housing (2) inner wall
(23), multiple exhaust fans (23) are around multiple ventilation hole (22) settings.
3. Helicopter Safety exit light solar energy charging and discharging lithium battery control device according to claim 1, feature exist
In:The protective housing (2) and the case lid (21) use acrylic board material.
4. Helicopter Safety exit light solar energy charging and discharging lithium battery control device according to claim 1, feature exist
In:It is equipped with rubber pad (6) between the connecting plate (1) and the protective housing (2), is honeycomb inside the rubber pad (6).
5. Helicopter Safety exit light solar energy charging and discharging lithium battery control device according to claim 1, feature exist
In:Side of the controller main body (3) far from the ventilation hole (22) is installed with temperature sensor (34), and described anti-
Protecting box outer wall is equipped with the alarm bell (35) electrically connected with the temperature sensor (34).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820383289.3U CN207910021U (en) | 2018-03-21 | 2018-03-21 | Helicopter Safety exit light solar energy charging and discharging lithium battery control device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820383289.3U CN207910021U (en) | 2018-03-21 | 2018-03-21 | Helicopter Safety exit light solar energy charging and discharging lithium battery control device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN207910021U true CN207910021U (en) | 2018-09-25 |
Family
ID=63559323
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201820383289.3U Active CN207910021U (en) | 2018-03-21 | 2018-03-21 | Helicopter Safety exit light solar energy charging and discharging lithium battery control device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN207910021U (en) |
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2018
- 2018-03-21 CN CN201820383289.3U patent/CN207910021U/en active Active
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