CN204614830U - The battery component of aircraft and comprise its aircraft - Google Patents
The battery component of aircraft and comprise its aircraft Download PDFInfo
- Publication number
- CN204614830U CN204614830U CN201520208089.0U CN201520208089U CN204614830U CN 204614830 U CN204614830 U CN 204614830U CN 201520208089 U CN201520208089 U CN 201520208089U CN 204614830 U CN204614830 U CN 204614830U
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- Prior art keywords
- battery
- aircraft
- battery case
- port
- gathering sill
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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
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Connection Of Batteries Or Terminals (AREA)
Abstract
The utility model provides a kind of battery component of aircraft and comprises its aircraft.This battery component comprises a battery case, at least one piece of battery is included in battery case, the positive terminal of battery is connected with the discharge and recharge interface be arranged on battery case with the second charging balanced line respectively by the first charging balanced line with negative pole end, and this discharge and recharge interface comprises at least one charging port and an electric discharge port.This aircraft comprises described battery component; The fuselage of aircraft is provided with the battery case for set battery assembly, and battery case is provided with insert port; The surface that battery case contacts with battery case is provided with at least one gathering sill, and the bearing of trend of described gathering sill is vertical with insert port, and battery case is provided with the gib block mated with gathering sill.The battery component of the aircraft in the utility model and to comprise its Flight Vehicle Structure simple, easy to use, effectively can be protected battery by battery case, simplify the operating procedure of discharge and recharge simultaneously.
Description
Technical field
The utility model relate in particular to a kind of aircraft battery component and comprise the aircraft of device.
Background technology
In prior art, the lithium battery of aircraft does not have shell to protect mostly, only by plastic film wrapped and use, there is very large potential safety hazard, not resistance toly to fall, not crashworthiness.In addition, the battery interface of conventional aircraft adopts an output interface and an equilibrium charging interface, is inserted on aircraft by battery, then power line is plugged the electric discharge port of battery during aircraft work.When needing to charge the battery, need first to be pulled up by the electric discharge port of power line from battery, then plug equilibrium charging port and charge the battery, find in actual use, this kind of operation has inconvenience more.
Utility model content
The technical problems to be solved in the utility model does not have external protection to overcome the battery component of aircraft in prior art, not resistance toly to fall, the defect of not crashworthiness, provides a kind of battery component of aircraft and comprise its aircraft.
The utility model solves above-mentioned technical problem by following technical proposals:
A kind of battery component of aircraft, its feature is, it comprises a battery case, at least one piece of battery is included in this battery case, the positive terminal of described battery is connected with a discharge and recharge interface with the second charging balanced line respectively by the first charging balanced line with negative pole end, and this discharge and recharge interface comprises at least one charging port and an electric discharge port; This discharge and recharge interface is located on this battery case.
Wherein, the arragement direction of described charging port and described electric discharge port is perpendicular.
Wherein, described battery component comprises the battery of three pieces of series connection, is connected between described battery respectively by one the 3rd charging balanced line with the 4th charging balanced line with this discharge and recharge interface.
The utility model additionally provides a kind of aircraft, and its feature is, it comprises the battery component of described aircraft; The fuselage of this aircraft is provided with one for the battery case of this battery component accommodating, and this battery case is provided with an insert port; The surface that this battery case contacts with this battery case is provided with at least one gathering sill, and the bearing of trend of described gathering sill is vertical with this insert port, and this battery case is provided with the gib block mated with described gathering sill.Under the cooperation of described gib block and gathering sill, there is screens mistake when can effectively avoid battery component to assemble, make assembling process more accurately convenient.In addition, described gib block also plays an extra supporting role to battery component.
Wherein, the front end of described gathering sill is equipped with a flaring targeting port.
Wherein, described battery case is provided with a bayonet socket; Described battery case is provided with the buckle with this bayonet fittings.
Wherein, this buckle is provided with one and makes this buckle depart from the press section of this bayonet socket for pressing this buckle.
Positive progressive effect of the present utility model is: the battery component of the aircraft in the utility model and to comprise its Flight Vehicle Structure simple, easy to use, effectively can be protected battery, simplify the operating procedure of discharge and recharge simultaneously by battery case.
Accompanying drawing explanation
Fig. 1 is the structural representation of the battery component inside in the utility model one embodiment.
Fig. 2 is the structural representation of the battery component in the present embodiment.
Fig. 3 is the vertical view of battery component in the present embodiment.
Fig. 4 is the structural representation of the first half after A-A hatching cutting in Fig. 3.
Fig. 5 is the upward view of battery component in the present embodiment.
Fig. 6 is the right view of battery component in the present embodiment.
Fig. 7 is the airframe structure schematic diagram of the aircraft in the utility model one preferred embodiment.
Fig. 8 is the cutaway view after battery component in the utility model is assembled to aircraft.
Fig. 9 is A portion enlarged drawing in Fig. 8.
Figure 10 is the exploded view of the battery component of aircraft in the present embodiment.
Embodiment
Lift preferred embodiment below, and come by reference to the accompanying drawings clearlyer intactly the utility model to be described.
Embodiment 1
As shown in Figure 1, the battery component in the present embodiment comprises the battery 100 of three pieces of series connection, and is connected with discharge and recharge interface 6 by the first charging balanced line 200, second charging balanced line 500, the 3rd charging balanced line 300 and the 4th charging balanced line 400.This discharge and recharge interface comprises three charging ports 61 and an electric discharge port 62.In order to prevent wire and plug grafting from putting upside down, preferably, by the arragement direction of the arragement direction of electric discharge port 62 perpendicular to charging port 61.
As shown in Fig. 2 ~ 9, this battery component also comprises a battery case 1, and above-mentioned discharge and recharge interface 6 is arranged on this battery case 1.A gathering sill 2 is respectively provided with in the both sides of battery case 1.As shown in figs. 7-9, the fuselage of this aircraft is provided with one for installing the battery case of this battery component, and this battery case is provided with one for inserting the insert port of this battery component.The bearing of trend of above-mentioned gathering sill 2 is vertical with this insert port.This battery case is provided with the gib block 7 mated with described gathering sill 2.For the ease of gathering sill 2 and gib block 7 being matched, be equipped with a flaring targeting port 3 in the front end of gathering sill 2.Under the cooperation of described gib block 7 and gathering sill 2, there is screens mistake when can effectively avoid battery component to assemble, make assembling process more accurately convenient.
In addition, the bottom of this battery case, i.e. the fuselage of this aircraft offers an engraved structure, thus the assembling to interior of aircraft accessory after being convenient to fuselage assembling.Therefore, battery case embeds the part that this engraved structure place forms fuselage cover after assembling.But owing to not having structure effectively to support battery component bottom battery case, so gib block 7 described in the present embodiment also plays an extra supporting role to battery component.
Be provided with a buckle 5 at the top of battery case 1, position corresponding with this buckle 5 on the battery case of fuselage is provided with the bayonet socket 8 coordinated with it simultaneously.When battery component to slip into along gib block 7 battery case foremost after, buckle 5 blocks bayonet socket 8 thus plays the object of securing battery cell packs.
And for the ease of the dismounting of battery component, buckle 5 is also provided with the press section 4 making it to depart from bayonet socket 8 for pressing this buckle 5.
It should be noted that, the gathering sill in the utility model and the distribution of gib block are not limited to above-mentioned layout, also can be arranged on battery case by gathering sill, are arranged on battery case by gib block.
As shown in Figure 10, the battery case 1 in the present embodiment comprises upper shell 11 and a lower house 12, and it adopts ultrasonic welding technique to be welded.
Although the foregoing describe embodiment of the present utility model, it will be understood by those of skill in the art that this only illustrates, protection range of the present utility model is defined by the appended claims.Those skilled in the art, under the prerequisite not deviating from principle of the present utility model and essence, can make various changes or modifications to these execution modes, but these change and amendment all falls into protection range of the present utility model.
Claims (7)
1. the battery component of an aircraft, it is characterized in that, it comprises a battery case, at least one piece of battery is included in this battery case, the positive terminal of described battery is connected with a discharge and recharge interface with the second charging balanced line respectively by the first charging balanced line with negative pole end, and this discharge and recharge interface comprises at least one charging port and an electric discharge port; This discharge and recharge interface is located on this battery case.
2. the battery component of aircraft as claimed in claim 1, it is characterized in that, the arragement direction of described charging port and described electric discharge port is perpendicular.
3. the battery component of aircraft as claimed in claim 1, is characterized in that, described battery component comprises the battery of three pieces of series connection, is connected between described battery respectively by one the 3rd charging balanced line with the 4th charging balanced line with this discharge and recharge interface.
4. an aircraft, is characterized in that, it comprises the battery component of the aircraft according to any one of claims 1 to 3; The fuselage of this aircraft is provided with one for the battery case of this battery component accommodating, and this battery case is provided with an insert port; The surface that this battery case contacts with this battery case is provided with at least one gathering sill, and the bearing of trend of described gathering sill is vertical with this insert port, and this battery case is provided with the gib block mated with described gathering sill.
5. aircraft as claimed in claim 4, it is characterized in that, the front end of described gathering sill is equipped with a flaring targeting port.
6. aircraft as claimed in claim 4, it is characterized in that, described battery case is provided with a bayonet socket; Described battery case is provided with the buckle with this bayonet fittings.
7. aircraft as claimed in claim 6, it is characterized in that, this buckle is provided with one makes this buckle depart from the press section of this bayonet socket for pressing this buckle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520208089.0U CN204614830U (en) | 2015-04-08 | 2015-04-08 | The battery component of aircraft and comprise its aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520208089.0U CN204614830U (en) | 2015-04-08 | 2015-04-08 | The battery component of aircraft and comprise its aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204614830U true CN204614830U (en) | 2015-09-02 |
Family
ID=53967358
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520208089.0U Active CN204614830U (en) | 2015-04-08 | 2015-04-08 | The battery component of aircraft and comprise its aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204614830U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105529421A (en) * | 2015-12-26 | 2016-04-27 | 小米科技有限责任公司 | Battery and aircraft |
| US10224526B2 (en) | 2015-12-14 | 2019-03-05 | Autel Robotics Usa Llc | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| US10442533B2 (en) | 2015-12-14 | 2019-10-15 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
-
2015
- 2015-04-08 CN CN201520208089.0U patent/CN204614830U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10224526B2 (en) | 2015-12-14 | 2019-03-05 | Autel Robotics Usa Llc | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| US10442533B2 (en) | 2015-12-14 | 2019-10-15 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
| US10745128B2 (en) | 2015-12-14 | 2020-08-18 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
| US11254429B2 (en) | 2015-12-14 | 2022-02-22 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
| CN105529421A (en) * | 2015-12-26 | 2016-04-27 | 小米科技有限责任公司 | Battery and aircraft |
| CN105529421B (en) * | 2015-12-26 | 2018-01-19 | 小米科技有限责任公司 | A kind of battery and aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |