CN205657102U - Suspension type battery and unmanned helicopter - Google Patents
Suspension type battery and unmanned helicopter Download PDFInfo
- Publication number
- CN205657102U CN205657102U CN201620282640.0U CN201620282640U CN205657102U CN 205657102 U CN205657102 U CN 205657102U CN 201620282640 U CN201620282640 U CN 201620282640U CN 205657102 U CN205657102 U CN 205657102U
- Authority
- CN
- China
- Prior art keywords
- battery
- supporting plate
- suspension type
- type battery
- groove
- 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.)
- Withdrawn - After Issue
Links
Classifications
-
- 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
Landscapes
- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses a suspension type battery and unmanned helicopter, it is equipped with the layer board, the terminal surface is equipped with a battery core at least under the layer board, the layer board both ends are the slip position, are equipped with left slip limit and right slip limit respectively. Be equipped with the baffle between layer board and the battery core. The utility model has the advantages of simple structure, it is with low costs, easy dismounting, the battery size is unrestricted.
Description
Technical field
This utility model relates to suspension type battery and depopulated helicopter.
Background technology
Traditional depopulated helicopter battery all uses cluster to fix, or uses the mode of battery compartment installation, and conventional batteries storehouse has the disadvantage in that
1, structure is complicated；
2, battery sizes is restricted；
3, dismounting inconvenience.
Utility model content
Technical problem to be solved in the utility model is to overcome the deficiencies in the prior art, it is provided that suspension type battery and depopulated helicopter, and it has simple in construction, low cost, easy accessibility, the unrestricted advantage of battery sizes.
This utility model be the technical scheme is that
Suspension type battery, it is provided with supporting plate, and described supporting plate lower surface is sliding position at least provided with a battery, described two ends of bearing plate, is respectively equipped with left sliding edge and right sliding edge.
It is provided with dividing plate between described supporting plate and battery.
Described dividing plate cross-section lengths is less than described supporting plate cross-section lengths.
Be between supporting plate with battery, the position of dividing plate one end is provided with the first breach coordinating right sliding edge to move；Be between supporting plate with battery, the position of the dividing plate other end is provided with the second breach coordinating left sliding edge to move.
Described supporting plate is provided with the engraved structure of several through holes composition.
Depopulated helicopter, it is at least provided with a suspension type battery, and described depopulated helicopter also includes fuselage, and described fuselage lower end is provided with the sliding tray for coordinating fixing suspension type battery.
Described sliding tray includes the first groove being provided with fuselage lower left and is located at bottom-right second groove of fuselage, and described first groove and the second slot opening are relative.
The beneficial effects of the utility model are: it has simple in construction, low cost, easy accessibility, the unrestricted advantage of battery sizes.
Accompanying drawing explanation
Fig. 1 is the structural representation of this utility model depopulated helicopter；
Fig. 2 is the structural representation of this utility model suspension type battery；
Fig. 3 is the structural representation of supporting plate in this utility model；
Fig. 4 is the schematic diagram that in this utility model, the first groove and the second groove decompose out.
Detailed description of the invention
As shown in Figures 1 to 4, this utility model suspension type battery, it is provided with supporting plate 3, and described supporting plate 3 lower surface is at least provided with a battery 1, and described supporting plate 3 two ends are sliding position, are respectively equipped with left sliding edge and right sliding edge.
It is provided with dividing plate 2 between described supporting plate 3 and battery 1.
Described dividing plate 2 cross-section lengths is less than described supporting plate 3 cross-section lengths.
Be between supporting plate 3 with battery 1, the position of dividing plate 2 one end is provided with the first breach coordinating right sliding edge to move；Be between supporting plate 3 with battery 1, the position of dividing plate 2 other end is provided with the second breach coordinating left sliding edge to move.
Described supporting plate 3 is provided with the engraved structure of several through holes composition.
Depopulated helicopter, it is at least provided with a described suspension type battery, and described depopulated helicopter also includes fuselage 4, and described fuselage 4 lower end is provided with the sliding tray for coordinating fixing suspension type battery.
Described sliding tray includes the first groove 5 being provided with fuselage 4 lower left and is located at bottom-right second groove 6 of fuselage 4, and described first groove 5 is relative with the second groove 6 opening.
The beneficial effects of the utility model are: it has simple in construction, low cost, easy accessibility, the unrestricted advantage of battery sizes.
Claims (6)
1. suspension type battery, it is characterised in that: it is provided with supporting plate (3), and described supporting plate (3) lower surface is at least provided with a battery (1), and described supporting plate (3) two ends are sliding position, is respectively equipped with left sliding edge and right sliding edge；Dividing plate (2) it is provided with between described supporting plate (3) and battery (1).
Suspension type battery the most according to claim 1, it is characterised in that: described dividing plate (2) cross-section lengths is less than described supporting plate (3) cross-section lengths.
Suspension type battery the most according to claim 2, it is characterised in that: be between supporting plate (3) with battery (1), the position of dividing plate (2) one end is provided with the first breach coordinating right sliding edge to move；Be between supporting plate (3) with battery (1), the position of dividing plate (2) other end is provided with the second breach coordinating left sliding edge to move.
Suspension type battery the most according to claim 3, it is characterised in that: described supporting plate (3) is provided with the engraved structure of several through holes composition.
5. depopulated helicopter, its feature exists: at least provided with a suspension type battery as described in Claims 1-4 any one, and described depopulated helicopter also includes fuselage (4), and described fuselage (4) lower end is provided with the sliding tray for coordinating fixing suspension type battery.
Depopulated helicopter the most according to claim 5, it is characterized in that: described sliding tray includes being provided with first groove (5) of fuselage (4) lower left and is located at bottom-right second groove of fuselage (4) (6), and described first groove (5) is relative with the second groove (6) opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620282640.0U CN205657102U (en) | 2016-04-07 | 2016-04-07 | Suspension type battery and unmanned helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620282640.0U CN205657102U (en) | 2016-04-07 | 2016-04-07 | Suspension type battery and unmanned helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205657102U true CN205657102U (en) | 2016-10-19 |
Family
ID=57389948
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620282640.0U Withdrawn - After Issue CN205657102U (en) | 2016-04-07 | 2016-04-07 | Suspension type battery and unmanned helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205657102U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105679980A (en) * | 2016-04-07 | 2016-06-15 | 珠海紫燕新科技有限公司 | Suspension-type battery and unmanned helicopter |
-
2016
- 2016-04-07 CN CN201620282640.0U patent/CN205657102U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105679980A (en) * | 2016-04-07 | 2016-06-15 | 珠海紫燕新科技有限公司 | Suspension-type battery and unmanned helicopter |
| CN105679980B (en) * | 2016-04-07 | 2018-09-21 | 珠海紫燕无人飞行器有限公司 | Suspension type battery and unmanned helicopter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170504 Address after: 519000 Xiangzhou, Guangdong Province, lemon Creek Taihe business center 16E Patentee after: Zhuhai Ziyan unmanned aircraft Co. Ltd. Address before: 519000, block B, Guoxin Plaza, No. 338, Xi Xi Road, Zhuhai, Guangdong, China 13F Patentee before: ZHUHAI ZIYAN NEW TECHNOLOGY CO., LTD. |
|
| TR01 | Transfer of patent right | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20161019 Effective date of abandoning: 20180921 |
|
| AV01 | Patent right actively abandoned |