CN204473148U - A kind of fixed sturcture of multi-rotor aerocraft battery - Google Patents
A kind of fixed sturcture of multi-rotor aerocraft battery Download PDFInfo
- Publication number
- CN204473148U CN204473148U CN201520087752.6U CN201520087752U CN204473148U CN 204473148 U CN204473148 U CN 204473148U CN 201520087752 U CN201520087752 U CN 201520087752U CN 204473148 U CN204473148 U CN 204473148U
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- CN
- China
- Prior art keywords
- battery
- rotor aerocraft
- battery compartment
- gripping members
- compartment
- 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.)
- Expired - Fee Related
Links
- 238000000034 method Methods 0.000 abstract description 4
- 230000007423 decrease Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 abstract description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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 kind of fixed sturcture of multi-rotor aerocraft battery, comprise battery compartment and battery lock gripping members; Described battery compartment is hollow square structure, side is opened wide as mouth put into by battery, and put entrance side at the battery of described battery compartment and arrange described battery lock gripping members, described battery lock gripping members is list structure, and a mouthful middle side part put into by the battery being horizontally set on described battery compartment.The utility model is fixed by the battery of battery compartment to multi-rotor aerocraft; put into mouth at the battery of battery compartment and put into battery; be fixed by battery lock gripping members; fixed form is simple and efficient; be easy to dismounting after fixing, be convenient for changing new battery; fixed effect is firm, can play a very good protection to battery in the decline process of multi-rotor aerocraft, and overall appearance is neatly generous.
Description
Technical field
The utility model belongs to multi-rotor aerocraft technical field, in particular to a kind of fixed sturcture of multi-rotor aerocraft battery.
Background technology
In recent years, the advantages such as the region that multi-rotor aerocraft much cannot arrive because of its cost is low, efficiency-cost ratio is high, no one was injured risk and can setting foot in, be with a wide range of applications in dual-use field, as low-altitude reconnaissance, meteorological exploration, aerial photography, traffic patrolling etc.But be confined to body size reason, multi-rotor aerocraft aloft the flight time very short, need often to change battery, cumbersome, waste a lot of human and material resources.The typical multi-rotor aerocraft battery fixing structure of one as shown in accompanying drawing 1, Fig. 2, is arranged battery retaining boards 12, and is fixed by panel fastener 13 above battery 11, ties up by battery bandage 14 below battery retaining boards 12 by battery 11; Adopt and in this way not only complex steps is fixed to battery, battery bottom does not support and is in vacant state, fixation procedure is inconvenient, and there will be illusive phenomenon, affect monnolithic case express, the more important thing is multi-rotor aerocraft from the process of falling in the air to battery without any protective action.
Summary of the invention
Goal of the invention: for the deficiencies in the prior art, the utility model provides a kind of fixed sturcture of multi-rotor aerocraft battery, is easy to fix, be convenient to dismounting, plays good protective action to battery simultaneously.
Technical scheme: the fixed sturcture of multi-rotor aerocraft battery described in the utility model, comprises battery compartment and battery lock gripping members; Described battery compartment is hollow square structure, side is opened wide as mouth put into by battery, and put entrance side at the battery of described battery compartment and arrange described battery lock gripping members, described battery lock gripping members is list structure, and a mouthful middle side part put into by the battery being horizontally set on described battery compartment; Described battery compartment comprises two end plates, two block length side plate and short side plates, end plate is provided with vice card groove and three to the main latch position be arranged in parallel, vice card groove is used for being connected with short side plate, the top of long side plate and bottom are respectively equipped with the fixture block mated with main latch position, and outstanding end plate after the fixture block of long side plate snaps in main latch position is also fixedly connected with by connecting rod.Put entrance side from the battery of battery compartment battery is put into, then utilize battery lock gripping members to fix, easy for installation, and can play a very good protection to battery.
The corner, top of described battery compartment is provided with battery compartment connecting element.
Described end plate, long side plate and short side plate all have square through hole.Described square through hole is two rows.
Described battery lock gripping members is strip bandage or strip baffle plate.
Beneficial effect: compared with prior art; advantage of the present utility model: the utility model is fixed by the battery of battery compartment to multi-rotor aerocraft; put into mouth at the battery of battery compartment and put into battery; be fixed by battery lock gripping members; fixed form is simple and efficient; be easy to dismounting after fixing, be convenient for changing new battery, fixed effect is firm, can play a very good protection to battery in the decline process of multi-rotor aerocraft, and overall appearance is neatly generous.
Accompanying drawing explanation
Fig. 1 is the front view of multi-rotor aerocraft battery fixing structure in prior art.
Fig. 2 is the birds-eye view of multi-rotor aerocraft battery fixing structure in prior art.
Fig. 3 is structural representation of the present utility model.
Detailed description of the invention
Below by accompanying drawing, technical solutions of the utility model are described in detail, but protection domain of the present utility model is not limited to described embodiment.
Embodiment 1: the fixed sturcture of multi-rotor aerocraft battery as shown in Figure 3, comprises battery compartment, battery compartment connecting element 22 and battery lock gripping members; Battery compartment forms hollow square structure by two end plates 241, two block length side plate 242 and short side plate 243, side is opened wide as mouth put into by battery, put entrance side 23 at the battery of battery compartment and battery lock gripping members 21 is set, battery lock gripping members 21 is strip bandage bar, and the battery being horizontally set on battery compartment is put in the middle part of entrance side 23.Battery compartment end plate 241 is provided with vice card groove and three to the main latch position be arranged in parallel, vice card groove is used for being connected with short side plate 243, the top of long side plate 242 and bottom are respectively equipped with the fixture block 252 mated with main latch position, and outstanding end plate 241 after the fixture block 252 of long side plate 242 snaps in main latch position is also fixedly connected with by connecting rod 251.Battery compartment top end plate 241 4 jiaos is provided with battery compartment connecting element 22; End plate 241, long side plate 242 and short side plate 243 all have two row's square through holes.
As mentioned above, although represented with reference to specific preferred embodiment and described the utility model, it shall not be construed as the restriction to the utility model self.Under the spirit and scope prerequisite of the present utility model not departing from claims definition, various change can be made in the form and details to it.
Claims (5)
1. a fixed sturcture for multi-rotor aerocraft battery, is characterized in that: comprise battery compartment and battery lock gripping members; Described battery compartment is hollow square structure, side is opened wide as mouth put into by battery, and put entrance side at the battery of described battery compartment and arrange described battery lock gripping members, described battery lock gripping members is list structure, and a mouthful middle side part put into by the battery being horizontally set on described battery compartment; Described battery compartment comprises two end plates, two block length side plate and short side plates, end plate is provided with vice card groove and three to the main latch position be arranged in parallel, vice card groove is used for being connected with short side plate, the top of long side plate and bottom are respectively equipped with the fixture block mated with main latch position, and outstanding end plate after the fixture block of long side plate snaps in main latch position is also fixedly connected with by connecting rod.
2. the fixed sturcture of multi-rotor aerocraft battery according to claim 1, is characterized in that: the corner, top of described battery compartment is provided with battery compartment connecting element.
3. the fixed sturcture of multi-rotor aerocraft battery according to claim 1, is characterized in that: described end plate, long side plate and short side plate all have square through hole.
4. the fixed sturcture of multi-rotor aerocraft battery according to claim 1, is characterized in that: described square through hole is two rows.
5. the fixed sturcture of multi-rotor aerocraft battery according to claim 1, is characterized in that: described battery lock gripping members is strip bandage or strip baffle plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520087752.6U CN204473148U (en) | 2015-02-06 | 2015-02-06 | A kind of fixed sturcture of multi-rotor aerocraft battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520087752.6U CN204473148U (en) | 2015-02-06 | 2015-02-06 | A kind of fixed sturcture of multi-rotor aerocraft battery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204473148U true CN204473148U (en) | 2015-07-15 |
Family
ID=53628939
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520087752.6U Expired - Fee Related CN204473148U (en) | 2015-02-06 | 2015-02-06 | A kind of fixed sturcture of multi-rotor aerocraft battery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204473148U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275460A (en) * | 2016-08-15 | 2017-01-04 | 张琬彬 | A kind of unmanned plane battery fastening structure |
| CN108091793A (en) * | 2017-11-06 | 2018-05-29 | 立峰集团有限公司 | A kind of spliced li battery shell |
| CN108190024A (en) * | 2017-12-03 | 2018-06-22 | 刘福珍 | A kind of power-supply battery stent of agricultural unmanned spraying machine |
| CN109941445A (en) * | 2017-12-21 | 2019-06-28 | 海鹰航空通用装备有限责任公司 | A kind of unmanned plane battery cabin structure |
| CN109996731A (en) * | 2016-11-24 | 2019-07-09 | 空中客车运作有限责任公司 | Structural detail, battery pack, the arrangement and re-entry space vehicle of structural detail and battery pack |
-
2015
- 2015-02-06 CN CN201520087752.6U patent/CN204473148U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275460A (en) * | 2016-08-15 | 2017-01-04 | 张琬彬 | A kind of unmanned plane battery fastening structure |
| CN109996731A (en) * | 2016-11-24 | 2019-07-09 | 空中客车运作有限责任公司 | Structural detail, battery pack, the arrangement and re-entry space vehicle of structural detail and battery pack |
| US11299024B2 (en) | 2016-11-24 | 2022-04-12 | Airbus Operations Gmbh | Structural element, a battery set, an arrangement of a structural element and a battery set, and an aerospace vehicle |
| CN108091793A (en) * | 2017-11-06 | 2018-05-29 | 立峰集团有限公司 | A kind of spliced li battery shell |
| CN108091793B (en) * | 2017-11-06 | 2023-07-07 | 立峰集团有限公司 | Spliced lithium battery shell |
| CN108190024A (en) * | 2017-12-03 | 2018-06-22 | 刘福珍 | A kind of power-supply battery stent of agricultural unmanned spraying machine |
| CN109941445A (en) * | 2017-12-21 | 2019-06-28 | 海鹰航空通用装备有限责任公司 | A kind of unmanned plane battery cabin structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150715 Termination date: 20190206 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |