CN105679980B - Suspension type battery and unmanned helicopter - Google Patents

Suspension type battery and unmanned helicopter Download PDF

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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
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Application number
CN201610212068.5A
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Chinese (zh)
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CN105679980A (en
Inventor
王江平
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhuhai Ziyan unmanned aircraft Co. Ltd.
Original Assignee
Zhuhai Ziyan Unmanned Aircraft Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhuhai Ziyan Unmanned Aircraft Co Ltd filed Critical Zhuhai Ziyan Unmanned Aircraft Co Ltd
Priority to CN201610212068.5A priority Critical patent/CN105679980B/en
Publication of CN105679980A publication Critical patent/CN105679980A/en
Application granted granted Critical
Publication of CN105679980B publication Critical patent/CN105679980B/en
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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2220/00Batteries for particular applications
    • H01M2220/20Batteries in motive systems, e.g. vehicle, ship, plane
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy 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

Suspension type battery and unmanned helicopter
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.
CN201610212068.5A 2016-04-07 2016-04-07 Suspension type battery and unmanned helicopter Active CN105679980B (en)

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

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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 (7)

* Cited by examiner, † Cited by third party
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
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (7)

* Cited by examiner, † Cited by third party
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

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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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