CN105679980A - Suspension-type battery and unmanned helicopter - Google Patents
Suspension-type battery and unmanned helicopter Download PDFInfo
- Publication number
- CN105679980A CN105679980A CN201610212068.5A CN201610212068A CN105679980A CN 105679980 A CN105679980 A CN 105679980A CN 201610212068 A CN201610212068 A CN 201610212068A CN 105679980 A CN105679980 A CN 105679980A
- Authority
- CN
- China
- Prior art keywords
- supporting plate
- type battery
- battery
- suspension type
- 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.)
- Granted
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
-
- 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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- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Toys (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The invention discloses a suspension-type battery and an unmanned helicopter. The suspension-type battery is provided with a supporting plate, wherein the lower end surface of the supporting plate is at least provided with one battery cell, and two ends of the supporting plate are slide parts, namely, a left slide edge and a right slide edge. A separation plate is arranged between the supporting plate and the battery cell. The suspension-type battery has the advantages of simple structure, low cost, convenience in disassembly and assembly and no limitation on the size of the battery.
Description
Technical field
The present invention relates to suspension type battery and depopulated helicopter.
Background technology
Traditional depopulated helicopter battery all adopts cluster to fix, or adopts 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.
Summary of the invention
The technical problem to be solved 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, and cost is low, easy accessibility, the unrestricted advantage of battery sizes.
The technical solution adopted in the present invention is:
Suspension type battery, it is provided with supporting plate, and described supporting plate lower surface is at least provided with a battery, and described two ends of bearing plate is sliding position, 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 invention has the beneficial effects as follows: it has simple in construction, and cost is low, easy accessibility, the unrestricted advantage of battery sizes.
Accompanying drawing explanation
Fig. 1 is the structural representation of depopulated helicopter of the present invention;
Fig. 2 is the structural representation of suspension type battery of the present invention;
Fig. 3 is the structural representation of supporting plate in the present invention;
Fig. 4 is the schematic diagram that in the present invention, the first groove and the second groove decompose out.
Detailed description of the invention
As shown in Figures 1 to 4, suspension type battery of the present invention, 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 invention has the beneficial effects as follows: it has simple in construction, and cost is low, easy accessibility, the unrestricted advantage of battery sizes.
Claims (7)
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.
2. suspension type battery according to claim 1, it is characterised in that: it is provided with dividing plate (2) between described supporting plate (3) and battery (1).
3. suspension type battery according to claim 2, it is characterised in that: described dividing plate (2) cross-section lengths is less than described supporting plate (3) cross-section lengths.
4. suspension type battery according to claim 3, 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.
5. suspension type battery according to claim 4, it is characterised in that: described supporting plate (3) is provided with the engraved structure of several through holes composition.
6. depopulated helicopter, its feature exists: at least provided with a suspension type battery as described in claim 1 to 5 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.
7. depopulated helicopter according to claim 6, 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 (6) of fuselage (4), and described first groove (5) is relative with the second groove (6) opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610212068.5A CN105679980B (en) | 2016-04-07 | 2016-04-07 | Suspension type battery and unmanned helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610212068.5A CN105679980B (en) | 2016-04-07 | 2016-04-07 | Suspension type battery and unmanned helicopter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105679980A true CN105679980A (en) | 2016-06-15 |
| CN105679980B CN105679980B (en) | 2018-09-21 |
Family
ID=56308558
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610212068.5A Active CN105679980B (en) | 2016-04-07 | 2016-04-07 | Suspension type battery and unmanned helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105679980B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103350636A (en) * | 2013-05-31 | 2013-10-16 | 国家电网公司 | Underpan hanging battery box of electric passenger vehicle |
| CN203601574U (en) * | 2013-12-04 | 2014-05-21 | 广州地理研究所 | Single-rotation-wing power-driven unmanned plane balance adjusting device |
| CN203707201U (en) * | 2013-09-25 | 2014-07-09 | 深圳一电科技有限公司 | Electronic device |
| CN204577482U (en) * | 2015-03-17 | 2015-08-19 | 郑州宇通客车股份有限公司 | A kind of cell fixing device and use the vehicle of this cell fixing device |
| CN204741037U (en) * | 2015-07-24 | 2015-11-04 | 深圳市硕腾科技有限公司 | Suspension type battery protection device that shocks resistance |
| CN105216636A (en) * | 2015-10-28 | 2016-01-06 | 广西大学 | A kind of pantograph spring case of adjustable rigidity |
| CN204956912U (en) * | 2015-08-18 | 2016-01-13 | 西北工业大学明德学院 | Eight rotor crafts |
| CN205075635U (en) * | 2015-11-10 | 2016-03-09 | 哈尔滨理工大学 | Commodity circulation transport vechicle |
| CN205657102U (en) * | 2016-04-07 | 2016-10-19 | 珠海紫燕新科技有限公司 | Suspension type battery and unmanned helicopter |
-
2016
- 2016-04-07 CN CN201610212068.5A patent/CN105679980B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103350636A (en) * | 2013-05-31 | 2013-10-16 | 国家电网公司 | Underpan hanging battery box of electric passenger vehicle |
| CN203707201U (en) * | 2013-09-25 | 2014-07-09 | 深圳一电科技有限公司 | Electronic device |
| CN203601574U (en) * | 2013-12-04 | 2014-05-21 | 广州地理研究所 | Single-rotation-wing power-driven unmanned plane balance adjusting device |
| CN204577482U (en) * | 2015-03-17 | 2015-08-19 | 郑州宇通客车股份有限公司 | A kind of cell fixing device and use the vehicle of this cell fixing device |
| CN204741037U (en) * | 2015-07-24 | 2015-11-04 | 深圳市硕腾科技有限公司 | Suspension type battery protection device that shocks resistance |
| CN204956912U (en) * | 2015-08-18 | 2016-01-13 | 西北工业大学明德学院 | Eight rotor crafts |
| CN105216636A (en) * | 2015-10-28 | 2016-01-06 | 广西大学 | A kind of pantograph spring case of adjustable rigidity |
| CN205075635U (en) * | 2015-11-10 | 2016-03-09 | 哈尔滨理工大学 | Commodity circulation transport vechicle |
| CN205657102U (en) * | 2016-04-07 | 2016-10-19 | 珠海紫燕新科技有限公司 | Suspension type battery and unmanned helicopter |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105679980B (en) | 2018-09-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20170420 Address after: 519000 Xiangzhou, Guangdong Province, lemon Creek Taihe business center 16E Applicant after: Zhuhai Ziyan unmanned aircraft Co. Ltd. Address before: 519000, block B, Guoxin Plaza, No. 338, Xi Xi Road, Zhuhai, Guangdong, China 13F Applicant before: ZHUHAI ZIYAN NEW TECHNOLOGY CO., LTD. |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant |