CN106207034A - Shock-damping structure installed by a kind of unmanned plane battery - Google Patents
Shock-damping structure installed by a kind of unmanned plane battery Download PDFInfo
- Publication number
- CN106207034A CN106207034A CN201610671770.8A CN201610671770A CN106207034A CN 106207034 A CN106207034 A CN 106207034A CN 201610671770 A CN201610671770 A CN 201610671770A CN 106207034 A CN106207034 A CN 106207034A
- Authority
- CN
- China
- Prior art keywords
- battery
- box body
- lid
- unmanned plane
- damping structure
- 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.)
- Pending
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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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The present invention relates to a kind of unmanned plane battery and install shock-damping structure, install shock-damping structure including a kind of unmanned plane battery, including box body, box body one end open is arranged, and other end surface configuration has cable-through hole；Inboard wall of cartridge is fixedly installed limited block and multiple waveform buffer bar；Also including the lid coordinated with opening, lid is rotationally connected with box body；Lid lower surface is provided with multiple buffering feet；Self-locking screw it is provided with on lid；The screw coordinated with self-locking screw it is provided with on box body；During use, battery prolongs box opening position and loads, connect power line by cable-through hole, battery front end is carried out spacing and puts in place signal as insertion by limited block simultaneously, and buffer bar deforms upon compression battery both sides, then covers tightly lid, buffering feet props up battery rear end, effectively reduce vibrations and battery is subjected to displacement situation, and install the easiest, lighter in weight；Overall structure is simple, low cost.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly, it relates to shock-damping structure installed by a kind of unmanned plane battery.
Background technology
Unmanned plane is the most manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself, civilian nothing
Man-machine taking photo by plane, agricultural, plant protection, the field such as the disaster relief have more important application；Unmanned plane, mostly from charged pool, relies on battery power
As power, currently used battery mounting box is poor to battery protection dynamics, fragile battery during generation accident collision.
Summary of the invention
The technical problem to be solved in the present invention is, for the drawbacks described above of prior art, it is provided that a kind of to battery protection
Shock-damping structure installed by effective unmanned plane battery.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of unmanned plane battery of structure installs shock-damping structure, including box body；Wherein, described box body one end open is arranged, separately
End surface is provided with cable-through hole；Described inboard wall of cartridge is fixedly installed limited block and multiple waveform buffer bar；Also include with
The lid that described opening coordinates, described lid is rotationally connected with described box body；Described lid lower surface is provided with multiple cushion pad
Foot；It is provided with self-locking screw on described lid；The screw coordinated with described self-locking screw it is provided with on described box body.
Shock-damping structure installed by unmanned plane battery of the present invention, and wherein, described limited block is excellent power blob of viscose.
Shock-damping structure installed by unmanned plane battery of the present invention, wherein, described lid is provided with and described self-locking spiral shell
The through hole that silk coordinates, is provided with annular bayonet socket in described through hole；It is provided with on described self-locking screw and the ring of described bayonet fittings
Shape groove.
Shock-damping structure installed by unmanned plane battery of the present invention, and wherein, described box body upper and lower surface is provided with multiple logical
Groove.
The beneficial effects of the present invention is: during use, battery prolongs box opening position and loads, and connects electricity by cable-through hole
Source line, battery front end is carried out spacing and puts in place signal as insertion by limited block simultaneously, and buffer bar deforms upon compression battery two
Side, then covers tightly lid, and buffering feet props up battery rear end, effectively reduces vibrations and battery is subjected to displacement situation, and install
The easiest, lighter in weight；Overall structure is simple, low cost.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below in conjunction with accompanying drawing and reality
The invention will be further described to execute example, and the accompanying drawing in describing below is only the section Example of the present invention, for this area
From the point of view of those of ordinary skill, on the premise of not paying creative work, it is also possible to obtain other accompanying drawings according to these accompanying drawings:
Fig. 1 is that shock-damping structure structural representation installed by the unmanned plane battery of present pre-ferred embodiments.
Detailed description of the invention
In order to make the purpose of the embodiment of the present invention, technical scheme and advantage clearer, implement below in conjunction with the present invention
Technical scheme in example carries out clear, complete description, it is clear that described embodiment is the section Example of the present invention, and
It is not all of embodiment.Based on embodiments of the invention, those of ordinary skill in the art are not before paying creative work
Put the every other embodiment obtained, broadly fall into protection scope of the present invention.
The unmanned plane battery of present pre-ferred embodiments installs shock-damping structure as it is shown in figure 1, include a kind of unmanned plane battery
Installing shock-damping structure, including box body 1, box body 1 one end open is arranged, and other end surface configuration has cable-through hole 10；Box body 1 inwall is solid
Surely limited block 11 and multiple waveform buffer bar 12 it are provided with；Also including the lid 2 coordinated with opening, lid 2 rotates with box body 1
Connect；Lid 2 lower surface is provided with multiple buffering feet 20；Self-locking screw 21 it is provided with on lid 2；Be provided with on box body 1 with
The screw 13 that self-locking screw 21 coordinates；During use, battery prolongs box body 1 aperture position and loads, and connects power supply by cable-through hole 10
Line, battery front end is carried out spacing and puts in place signal as insertion by limited block 11 simultaneously, and buffer bar 12 deforms upon compression battery
Both sides, then cover tightly lid 2, and buffering feet 20 props up battery rear end, effectively reduces vibrations and battery is subjected to displacement situation, and
Install the easiest, lighter in weight；Overall structure is simple, low cost.
As it is shown in figure 1, limited block 11 is excellent power blob of viscose, improves damping, buffering effect, and then improve protected effect.
As it is shown in figure 1, be provided with the through hole 22 coordinated with self-locking screw 21 on lid 2, in through hole 22, it is provided with annular snap
Mouth 220；The cannelure 210 coordinated with bayonet socket 220 it is provided with on self-locking screw 21；More convenient and difficult drop-off is installed.
As it is shown in figure 1, box body 1 upper and lower surface is provided with multiple groove (not shown), alleviates overall weight and carry simultaneously
High radiating effect.
It should be appreciated that for those of ordinary skills, can be improved according to the above description or be converted,
And all these modifications and variations all should belong to the protection domain of claims of the present invention.
Claims (4)
1. a shock-damping structure installed by unmanned plane battery, including box body；It is characterized in that, described box body one end open is arranged, separately
End surface is provided with cable-through hole；Described inboard wall of cartridge is fixedly installed limited block and multiple waveform buffer bar；Also include with
The lid that described opening coordinates, described lid is rotationally connected with described box body；Described lid lower surface is provided with multiple cushion pad
Foot；It is provided with self-locking screw on described lid；The screw coordinated with described self-locking screw it is provided with on described box body.
Shock-damping structure installed by unmanned plane battery the most according to claim 1, it is characterised in that described limited block is excellent power glue
Block.
Unmanned plane battery the most according to claim 1 install shock-damping structure, it is characterised in that be provided with on described lid with
The through hole that described self-locking screw coordinates, is provided with annular bayonet socket in described through hole；It is provided with on described self-locking screw and described card
The cannelure that mouth coordinates.
Shock-damping structure installed by unmanned plane battery the most according to claim 1, it is characterised in that described box body upper and lower surface sets
It is equipped with multiple groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610671770.8A CN106207034A (en) | 2016-08-15 | 2016-08-15 | Shock-damping structure installed by a kind of unmanned plane battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610671770.8A CN106207034A (en) | 2016-08-15 | 2016-08-15 | Shock-damping structure installed by a kind of unmanned plane battery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106207034A true CN106207034A (en) | 2016-12-07 |
Family
ID=57521569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610671770.8A Pending CN106207034A (en) | 2016-08-15 | 2016-08-15 | Shock-damping structure installed by a kind of unmanned plane battery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106207034A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106594165A (en) * | 2017-02-08 | 2017-04-26 | 湖州博润实业有限公司 | Electromechanical damping equipment |
| CN107180936A (en) * | 2017-05-26 | 2017-09-19 | 成都艾欧新能源科技有限公司 | The structure of effective available fuel cell group |
| WO2018032265A1 (en) * | 2016-08-15 | 2018-02-22 | 张琬彬 | Unmanned aerial vehicle battery mounting damping structure |
| CN108408034A (en) * | 2018-01-31 | 2018-08-17 | 芜湖市海联机械设备有限公司 | A kind of visual unmanned plane |
| CN110635080A (en) * | 2019-09-16 | 2019-12-31 | 安徽天德无人机科技有限公司 | Unmanned aerial vehicle battery fixed knot of plant protection constructs |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10284046A (en) * | 1997-04-08 | 1998-10-23 | Matsushita Electric Ind Co Ltd | Nonaqueous electrolyte secondary battery |
| CN201022086Y (en) * | 2007-02-09 | 2008-02-13 | 苏州见诚电动科技有限公司 | A novel accumulator box |
| CN201408789Y (en) * | 2009-04-02 | 2010-02-17 | 中兴通讯股份有限公司 | Rotary type battery-cover structure |
| CN202150501U (en) * | 2011-06-30 | 2012-02-22 | 上海卡能迪蓄能科技有限公司 | Battery box for protecting battery |
| CN104157800A (en) * | 2014-07-31 | 2014-11-19 | 宿迁玉笛电动车有限公司 | Multifunctional battery box of electro-tricycle |
| CN205150264U (en) * | 2015-10-30 | 2016-04-13 | 深圳高启科技有限公司 | Can dismantle unmanned aerial vehicle battery package assembly |
-
2016
- 2016-08-15 CN CN201610671770.8A patent/CN106207034A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10284046A (en) * | 1997-04-08 | 1998-10-23 | Matsushita Electric Ind Co Ltd | Nonaqueous electrolyte secondary battery |
| CN201022086Y (en) * | 2007-02-09 | 2008-02-13 | 苏州见诚电动科技有限公司 | A novel accumulator box |
| CN201408789Y (en) * | 2009-04-02 | 2010-02-17 | 中兴通讯股份有限公司 | Rotary type battery-cover structure |
| CN202150501U (en) * | 2011-06-30 | 2012-02-22 | 上海卡能迪蓄能科技有限公司 | Battery box for protecting battery |
| CN104157800A (en) * | 2014-07-31 | 2014-11-19 | 宿迁玉笛电动车有限公司 | Multifunctional battery box of electro-tricycle |
| CN205150264U (en) * | 2015-10-30 | 2016-04-13 | 深圳高启科技有限公司 | Can dismantle unmanned aerial vehicle battery package assembly |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018032265A1 (en) * | 2016-08-15 | 2018-02-22 | 张琬彬 | Unmanned aerial vehicle battery mounting damping structure |
| CN106594165A (en) * | 2017-02-08 | 2017-04-26 | 湖州博润实业有限公司 | Electromechanical damping equipment |
| CN106594165B (en) * | 2017-02-08 | 2018-09-11 | 江苏台普动力机械有限公司 | A kind of electromechanics shock-absorption device |
| CN107180936A (en) * | 2017-05-26 | 2017-09-19 | 成都艾欧新能源科技有限公司 | The structure of effective available fuel cell group |
| CN107180936B (en) * | 2017-05-26 | 2020-09-04 | 陈宇飞 | Structure for effectively fixing fuel cell stack |
| CN108408034A (en) * | 2018-01-31 | 2018-08-17 | 芜湖市海联机械设备有限公司 | A kind of visual unmanned plane |
| CN110635080A (en) * | 2019-09-16 | 2019-12-31 | 安徽天德无人机科技有限公司 | Unmanned aerial vehicle battery fixed knot of plant protection constructs |
| CN110635080B (en) * | 2019-09-16 | 2023-08-18 | 安徽天德无人机科技有限公司 | Plant protection unmanned aerial vehicle battery fixed knot constructs |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |
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| RJ01 | Rejection of invention patent application after publication |