CN105679980B - Suspension type battery and unmanned helicopter - Google Patents
Suspension type battery and unmanned helicopter Download PDFInfo
- Publication number
- CN105679980B CN105679980B CN201610212068.5A CN201610212068A CN105679980B CN 105679980 B CN105679980 B CN 105679980B CN 201610212068 A CN201610212068 A CN 201610212068A CN 105679980 B CN105679980 B CN 105679980B
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- CN
- China
- Prior art keywords
- supporting plate
- battery
- 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.)
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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
Abstract
The invention discloses suspension type battery and unmanned helicopter, suspension type battery is equipped with supporting plate, and the supporting plate lower face is sliding position at least provided with a battery, the two ends of bearing plate, is respectively equipped with left sliding edge and right sliding edge.Partition board is equipped between the supporting plate and battery.The present invention has simple in structure, at low cost, convenient for disassembly and assembly, the unrestricted advantage of battery sizes.
Description
Technical field
The present invention relates to suspension type battery and unmanned helicopters.
Background technology
Traditional unmanned helicopter battery is all made of cluster and fixes, or by the way of battery compartment installation, tradition electricity
Chi Cang has the following disadvantages:
1, complicated;
2, battery sizes are restricted;
3, dismounting is inconvenient.
Invention content
The technical problem to be solved by the present invention is to overcome the deficiencies of the prior art and provide suspension type battery and nobody goes straight up to
Machine, with simple in structure, at low cost, convenient for disassembly and assembly, the unrestricted advantage of battery sizes.
The technical solution adopted in the present invention is:
Suspension type battery is equipped with supporting plate, and the supporting plate lower face is at least provided with a battery, the two ends of bearing plate
Sliding position is respectively equipped with left sliding edge and right sliding edge.
Partition board is equipped between the supporting plate and battery.
The partition board cross-section lengths are less than the supporting plate cross-section lengths.
Between supporting plate and battery, first notch of the position of partition board one end equipped with the right sliding edge movement of cooperation;Place
Between supporting plate and battery, second notch of the position of the partition board other end equipped with the left sliding edge movement of cooperation.
The supporting plate is equipped with the engraved structure of several through-holes composition.
Unmanned helicopter, at least provided with a suspension type battery, the unmanned helicopter further includes having fuselage, the machine
Body lower end is equipped with the sliding groove for coordinating fixed suspension type battery.
The sliding groove includes the first groove equipped with fuselage lower left and the second groove set on fuselage lower right, described
First groove and the second slot opening are opposite.
The beneficial effects of the invention are as follows:It is with simple in structure, and at low cost, convenient for disassembly and assembly, battery sizes are unrestricted
Advantage.
Description of the drawings
Fig. 1 is the structural schematic diagram of unmanned helicopter of the present invention;
Fig. 2 is the structural schematic diagram of suspension type battery of the present invention;
Fig. 3 is the structural schematic diagram of supporting plate in the present invention;
Fig. 4 is that the first groove and the second groove decomposite the schematic diagram come in the present invention.
Specific implementation mode
As shown in Figures 1 to 4, suspension type battery of the present invention is equipped with supporting plate 3, and 3 lower face of the supporting plate is at least provided with one
A battery 1,3 both ends of the supporting plate are sliding position, are respectively equipped with left sliding edge and right sliding edge.
Partition board 2 is equipped between the supporting plate 3 and battery 1.
2 cross-section lengths of the partition board are less than 3 cross-section lengths of the supporting plate.
Between supporting plate 3 and battery 1, first notch of the position of 2 one end of partition board equipped with the right sliding edge movement of cooperation;
Between supporting plate 3 and battery 1, second notch of the position of 2 other end of partition board equipped with the left sliding edge movement of cooperation.
The supporting plate 3 is equipped with the engraved structure of several through-holes composition.
Unmanned helicopter, at least provided with the suspension type battery described in one, the unmanned helicopter further includes having fuselage
4,4 lower end of the fuselage is equipped with the sliding groove for coordinating fixed suspension type battery.
The sliding groove includes the first groove 5 equipped with 4 lower left of fuselage and the second groove 6 set on 4 lower right of fuselage,
First groove, 5 and second groove 6 is open relatively.
The beneficial effects of the invention are as follows:It is with simple in structure, and at low cost, convenient for disassembly and assembly, battery sizes are unrestricted
Advantage.
Claims (4)
1. suspension type battery, it is characterised in that:It is equipped with supporting plate(3), the supporting plate(3)Lower face is at least provided with a battery
(1), the supporting plate(3)Both ends are sliding position, respectively left sliding edge and right sliding edge;The supporting plate(3)With battery(1)
Between be equipped with partition board(2);In supporting plate(3)With battery(1)Between, partition board(2)The position of one end, which is equipped with, coordinates right sliding edge
The first mobile notch;In supporting plate(3)With battery(1)Between, partition board(2)The position of the other end, which is equipped with, coordinates left sliding edge
The second mobile notch;The supporting plate(3)It is equipped with the engraved structure of several through-holes composition.
2. suspension type battery according to claim 1, it is characterised in that:The partition board(2)Cross-section lengths are less than described
Supporting plate(3)Cross-section lengths.
3. unmanned helicopter, feature exists:At least provided with a suspension type battery as described in claim 1 to 2 any one,
The unmanned helicopter further includes having fuselage(4), the fuselage(4)Lower end is equipped with the sliding for coordinating fixed suspension type battery
Slot.
4. unmanned helicopter according to claim 3, it is characterised in that:The sliding groove includes being equipped with fuselage(4)Lower-left
First groove of side(5)With set on fuselage(4)Second groove of lower right(6), first groove(5)With the second groove(6)
Opening is opposite.
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 CN105679980A (en) | 2016-06-15 |
CN105679980B true 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)
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CN (1) | CN105679980B (en) |
Citations (7)
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---|---|---|---|---|
CN103350636A (en) * | 2013-05-31 | 2013-10-16 | 国家电网公司 | Underpan hanging battery box of electric passenger vehicle |
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 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
-
2016
- 2016-04-07 CN CN201610212068.5A patent/CN105679980B/en active Active
Patent Citations (7)
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 |
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 |
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CN105679980A (en) | 2016-06-15 |
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Legal Events
Date | Code | Title | Description |
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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. |
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GR01 | Patent grant | ||
GR01 | Patent grant |