CN207381454U - A kind of unmanned plane battery protecting apparatus - Google Patents
A kind of unmanned plane battery protecting apparatus Download PDFInfo
- Publication number
- CN207381454U CN207381454U CN201721454061.0U CN201721454061U CN207381454U CN 207381454 U CN207381454 U CN 207381454U CN 201721454061 U CN201721454061 U CN 201721454061U CN 207381454 U CN207381454 U CN 207381454U
- Authority
- CN
- China
- Prior art keywords
- device body
- unmanned plane
- constrictor
- protecting apparatus
- battery protecting
- 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
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- 238000009434 installation Methods 0.000 claims abstract description 7
- 230000006835 compression Effects 0.000 claims description 15
- 238000007906 compression Methods 0.000 claims description 15
- 229910000831 Steel Inorganic materials 0.000 claims description 9
- 239000010959 steel Substances 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims 1
- 230000035939 shock Effects 0.000 abstract description 6
- 238000010521 absorption reaction Methods 0.000 abstract description 3
- 230000009977 dual effect Effects 0.000 abstract description 3
- 238000013016 damping Methods 0.000 description 4
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 241000271460 Crotalus cerastes Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses a kind of unmanned plane battery protecting apparatus, including device body, rotation axis is rotatablely equipped at the top of described device body, driving gear is arranged in the rotation axis, two reversed screws being vertically arranged are rotatablely equipped in described device body, the top of the reversed screw is fixedly connected with driven gear through device body, driven gear is engaged with driving gear, there are two grip blocks for screw thread installation on the reversed screw, battery is equipped between two grip blocks, the top inner wall and bottom interior wall of described device body are fixedly mounted there are two constrictor, motion bar is slidably fitted on constrictor, one end of the motion bar is fixedly connected with grip block, horizontally disposed rail rods are welded between two constrictors, spring there are two being arranged in the rail rods.The utility model greatly enhances the shock resistance of battery protecting apparatus, improves the service life of battery by dual shock absorption mechanism, easy to use, easy to spread.
Description
Technical field
The utility model is related to unmanned air vehicle technique field more particularly to a kind of unmanned plane battery protecting apparatus.
Background technology
Battery life on unmanned plane is particularly important for the normal operation of unmanned plane, so the guarantor for unmanned machine battery
Shield is also essential, and unmanned plane can be with violent vibrations, the very big prestige of this security presence to battery during landing
The side of body, in order to solve problem above, it is necessary to which a kind of unmanned plane meets the needs of people with battery protecting apparatus.
Utility model content
The purpose of this utility model is and a kind of unmanned plane electricity consumption proposed in order to solve shortcoming in the prior art
Pond protective device.
To achieve these goals, the utility model employs following technical solution：
A kind of unmanned plane battery protecting apparatus including device body, is rotatablely equipped at the top of described device body and turns
Moving axis is arranged with driving gear in the rotation axis, two reverse silks being vertically arranged is rotatablely equipped in described device body
Bar, the top of the reversed screw are fixedly connected with driven gear through device body, and driven gear is engaged with driving gear, institute
Screw thread installation is stated on reversed screw there are two grip block, is equipped with battery between two grip blocks, in the top of described device body
Wall and bottom interior wall are fixedly mounted there are two constrictor, and motion bar, one end of the motion bar are slidably fitted on constrictor
Be fixedly connected with grip block, horizontally disposed rail rods be welded between two constrictors, be arranged in the rail rods there are two
Spring is slidably installed in the rail rods there are two sliding block, is hinged with interlocking bar on sliding block, the one end of interlocking bar away from sliding block with
Grip block is hinged, the driving gear is equipped with compression chamber, and the bottom interior wall of compression chamber is fixedly mounted that there are two be vertically arranged
Spring stack, is fixedly connected with buffer stopper at the top of the spring stack, and two side rolls of the buffer stopper are equipped with steel ball, steel ball with
Compression chamber both sides inner wall rolls connection, offers through hole at the top of the driving gear, through hole is connected with compression chamber, reversed screw
Bottom be fixedly connected through through hole with buffer stopper.
Preferably, the reversed screw is made of the first threaded rod and the second threaded rod, the first threaded rod and the second screw thread
Hand of spiral on bar is on the contrary, the top inner wall and bottom interior wall of device body are installed with bearing, and the two of reversed screw
End is fixedly connected with the inner ring of bearing.
Preferably, the both sides inner wall of the compression chamber offers track groove, and steel ball is rolled with track groove and connected.
Preferably, the constrictor and motion bar are cylindrical structural, and the cross-sectional diameter of constrictor is more than motion bar
Cross-sectional diameter.
Preferably, the spring is between constrictor and sliding block.
Preferably, the grip block is U-shaped structure, and two opposed one sides of grip block are equipped with buffer board, buffer board
It is made of rubber material.
The beneficial effects of the utility model are：By rotation axis driving gear is driven to rotate, driving gear drives driven tooth
Wheel and reversed screw rotate, and are fixedly clamped so as to fulfill two grip blocks to battery, by between constrictor and motion bar
Cooperation, provide to first layer damping, by the cooperation between rail rods, spring, sliding block, interlocking bar, provide to battery
Second layer damping, this experiment is new by dual shock absorption mechanism, greatly enhances the shock resistance of battery protecting apparatus, improves
The service life of battery, it is easy to use, it is easy to spread.
Description of the drawings
Fig. 1 be the utility model proposes a kind of unmanned plane battery protecting apparatus structure diagram；
Fig. 2 is the schematic cross-sectional view of constrictor.
In figure：1 device body, 2 rotation axis, 3 driving gears, 4 reversed screws, 5 driven gears, 6 grip blocks, 7 batteries, 8
Constrictor, 9 motion bars, 10 rail rods, 11 springs, 12 sliding blocks, 13 interlocking bar, 14 compression chambers, 15 spring stacks, 16 buffer stoppers, 17.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.
With reference to Fig. 1-2, a kind of unmanned plane battery protecting apparatus, including device body 1, the top of device body 1 rotates
Rotation axis 2 is installed, driving gear 3 is arranged in rotation axis 2, rotational installation is anti-there are two being vertically arranged in device body 1
To screw 4, the top of reversed screw 4 is fixedly connected with driven gear 5, driven gear 5 and driving gear 3 through device body 1
It engages, grip block 6 there are two screw thread installations on reversed screw 4, battery 7, the top of device body 1 is equipped between two grip blocks 6
Portion's inner wall and bottom interior wall are fixedly mounted there are two constrictor 8, and motion bar 9 is slidably fitted on constrictor 8, motion bar 9
One end is fixedly connected with grip block 6, and horizontally disposed rail rods 10 are welded between two constrictors 8, are arranged in rail rods 10
It there are two spring 11, is slidably installed in rail rods 10 there are two sliding block 12, is hinged with interlocking bar 13 on sliding block 12, interlocking bar 13 is remote
One end and grip block 6 from sliding block 12 is hinged, and driving gear 3 is equipped with compression chamber 14, and the bottom interior wall of compression chamber 14 fixes peace
The spring stack 15 that there are two dresses is vertically arranged, the top of spring stack 15 to be fixedly connected with buffer stopper 16, and the two of buffer stopper 16 sidewinders
Dynamic to be equipped with steel ball 17, steel ball 17 is rolled with 14 both sides inner wall of compression chamber and connected, and the top of driving gear 3 offers through hole, leads to
Hole is connected with compression chamber 14, and the bottom of reversed screw 4 is fixedly connected through through hole with buffer stopper 16.
In the present embodiment, reversed screw 4 is made of the first threaded rod and the second threaded rod, the first threaded rod and the second screw thread
Hand of spiral on bar on the contrary, the top inner wall and bottom interior wall of device body 1 are installed with bearing, reversed screw 4
Both ends are fixedly connected with the inner ring of bearing, and the both sides inner wall of compression chamber 14 offers track groove, steel ball 17 and track trough roller
Dynamic connection, constrictor 8 and motion bar 9 are cylindrical structural, and the cross-sectional diameter of constrictor 8 is more than the cross section of motion bar 9
Diameter, for spring 11 between constrictor 8 and sliding block 12, grip block 6 is U-shaped structure, and two 6 opposed one sides of grip block are equal
Equipped with buffer board, buffer board is made of rubber material, by rotation axis 2 drive driving gear 3 rotate, driving gear 3 drive from
Moving gear 5 and reversed screw 4 rotate, and are fixedly clamped so as to fulfill two grip blocks 6 to battery, pass through constrictor 8 and activity
Cooperation between bar 9 provides the first layer damping to 7, by between rail rods 10, spring 11, sliding block 12, interlocking bar 13
Cooperation, provides the second layer damping to battery 7, this experiment is new by dual shock absorption mechanism, greatly enhances battery 7 and protects
The shock resistance of protection unit improves the service life of battery 7, easy to use, easy to spread.
In the present embodiment, by rotation axis 2 drive driving gear 3 rotate, driving gear 3 drive driven gear 5 and reversely
Screw 4 rotates, and reversed screw 4 drives two grip blocks 6 to move toward one another, and the clamping of battery is consolidated so as to fulfill two grip blocks 6
It is fixed, by the cooperation between spring stack 15 inside constrictor 8, buffer stopper 16 and motion bar 9, provide and 7 first layer is subtracted
Shake protection, spring 11 is a kind of in compressive state, by the cooperation between rail rods 10, spring 11, sliding block 12, interlocking bar 13,
Provide the second layer shock-absorbing protecting to battery 7.
The above is only the preferable specific embodiment of the utility model, but the scope of protection of the utility model is not
This is confined to, in the technical scope that any one skilled in the art discloses in the utility model, according to this practicality
New technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
- A kind of 1. unmanned plane battery protecting apparatus, including device body (1), which is characterized in that the top of described device body (1) Portion is rotatablely equipped with rotation axis (2), and driving gear (3) is arranged on the rotation axis (2), is rotated in described device body (1) There are two the reversed screw (4) being vertically arranged, the top of the reversed screw (4) is fixedly connected through device body (1) for installation There is driven gear (5), driven gear (5) is engaged with driving gear (3), and there are two folders for screw thread installation on the reversed screw (4) Plate (6) is held, is equipped with battery (7) between two grip blocks (6), the top inner wall and bottom interior wall of described device body (1) are solid Dingan County's dress is slidably fitted with motion bar (9), one end of the motion bar (9) and folder there are two constrictor (8) on constrictor (8) It holds plate (6) to be fixedly connected, is welded with horizontally disposed rail rods (10) between two constrictors (8), on the rail rods (10) It is arranged there are two spring (11), is slidably installed on the rail rods (10) there are two sliding block (12), sliding block is hinged with connection on (12) Lever (13), the one end of interlocking bar (13) away from sliding block (12) is hinged with grip block (6), and the driving gear (3) is equipped with pressure Contracting chamber (14), there are two the spring stack (15) being vertically arranged, the spring stacks for the bottom interior wall fixed installation of compression chamber (14) (15) buffer stopper (16) is fixedly connected at the top of, two side rolls of the buffer stopper (16) are equipped with steel ball (17), steel ball (17) roll and connect with compression chamber (14) both sides inner wall, through hole, through hole and compression chamber are offered at the top of the driving gear (3) (14) connect, the bottom of reversed screw (4) is fixedly connected through through hole with buffer stopper (16).
- A kind of 2. unmanned plane battery protecting apparatus according to claim 1, which is characterized in that the reversed screw (4) It is made of the first threaded rod and the second threaded rod, the hand of spiral on the first threaded rod and the second threaded rod is on the contrary, device body (1) top inner wall and bottom interior wall is installed with bearing, and the both ends of reversed screw (4) are fixed with the inner ring of bearing to be connected It connects.
- 3. a kind of unmanned plane battery protecting apparatus according to claim 1, which is characterized in that the compression chamber (14) Both sides inner wall offers track groove, and steel ball (17) is rolled with track groove and connected.
- 4. a kind of unmanned plane battery protecting apparatus according to claim 1, which is characterized in that the constrictor (8) and Motion bar (9) is cylindrical structural, and the cross-sectional diameter of constrictor (8) is more than the cross-sectional diameter of motion bar (9).
- 5. a kind of unmanned plane battery protecting apparatus according to claim 1, which is characterized in that the spring (11) is located at Between constrictor (8) and sliding block (12).
- 6. a kind of unmanned plane battery protecting apparatus according to claim 1, which is characterized in that the grip block (6) is U Shape structure, two opposed one sides of grip block (6) are equipped with buffer board, and buffer board is made of rubber material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721454061.0U CN207381454U (en) | 2017-11-03 | 2017-11-03 | A kind of unmanned plane battery protecting apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721454061.0U CN207381454U (en) | 2017-11-03 | 2017-11-03 | A kind of unmanned plane battery protecting apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207381454U true CN207381454U (en) | 2018-05-18 |
Family
ID=62334936
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721454061.0U Expired - Fee Related CN207381454U (en) | 2017-11-03 | 2017-11-03 | A kind of unmanned plane battery protecting apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207381454U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108433651A (en) * | 2018-05-28 | 2018-08-24 | 芜湖威灵数码科技有限公司 | A kind of smart home with can self-cleaning sweeping robot |
| CN108583910A (en) * | 2018-06-25 | 2018-09-28 | 山东飞奥航空发动机有限公司 | A kind of central power type multi-rotor aerocraft and control method |
| CN109017255A (en) * | 2018-08-14 | 2018-12-18 | 胡玉平 | A kind of battery shock absorbing apparatus of new-energy automobile |
| CN109454166A (en) * | 2018-10-31 | 2019-03-12 | 大连函量科技发展有限公司 | A kind of damping of mold |
| CN109860453A (en) * | 2018-12-13 | 2019-06-07 | 湖北泰和电气有限公司 | A kind of cell apparatus for underground storage type pressure gauge |
| CN110783616A (en) * | 2019-10-23 | 2020-02-11 | 深圳市华创众成智能装备有限公司 | Sliding-rolling type pushing pressing plate formation clamp |
| CN111826865A (en) * | 2019-04-16 | 2020-10-27 | 涂友本 | Shuttle loom with adjust no bullet cloth tension stability |
| CN112542629A (en) * | 2020-12-02 | 2021-03-23 | 湖南电将军新能源有限公司 | Novel energy power battery system of high power |
| CN114597561A (en) * | 2022-03-22 | 2022-06-07 | 江西中聚宏新材料科技有限公司 | Light plastic high-safety battery compartment |
-
2017
- 2017-11-03 CN CN201721454061.0U patent/CN207381454U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108433651A (en) * | 2018-05-28 | 2018-08-24 | 芜湖威灵数码科技有限公司 | A kind of smart home with can self-cleaning sweeping robot |
| CN108583910A (en) * | 2018-06-25 | 2018-09-28 | 山东飞奥航空发动机有限公司 | A kind of central power type multi-rotor aerocraft and control method |
| CN109017255A (en) * | 2018-08-14 | 2018-12-18 | 胡玉平 | A kind of battery shock absorbing apparatus of new-energy automobile |
| CN109454166A (en) * | 2018-10-31 | 2019-03-12 | 大连函量科技发展有限公司 | A kind of damping of mold |
| CN109860453A (en) * | 2018-12-13 | 2019-06-07 | 湖北泰和电气有限公司 | A kind of cell apparatus for underground storage type pressure gauge |
| CN109860453B (en) * | 2018-12-13 | 2021-11-30 | 湖北泰和电气有限公司 | Battery device for underground storage type pressure gauge |
| CN111826865A (en) * | 2019-04-16 | 2020-10-27 | 涂友本 | Shuttle loom with adjust no bullet cloth tension stability |
| CN110783616A (en) * | 2019-10-23 | 2020-02-11 | 深圳市华创众成智能装备有限公司 | Sliding-rolling type pushing pressing plate formation clamp |
| CN112542629A (en) * | 2020-12-02 | 2021-03-23 | 湖南电将军新能源有限公司 | Novel energy power battery system of high power |
| CN114597561A (en) * | 2022-03-22 | 2022-06-07 | 江西中聚宏新材料科技有限公司 | Light plastic high-safety battery compartment |
| CN114597561B (en) * | 2022-03-22 | 2024-03-22 | 江西中聚宏新材料科技有限公司 | Light-duty high security battery compartment of plastics |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180518 |