CN212556813U - A battery energy-saving protection device for unmanned aerial vehicle - Google Patents
A battery energy-saving protection device for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN212556813U CN212556813U CN202021256598.8U CN202021256598U CN212556813U CN 212556813 U CN212556813 U CN 212556813U CN 202021256598 U CN202021256598 U CN 202021256598U CN 212556813 U CN212556813 U CN 212556813U
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- China
- Prior art keywords
- battery
- fixedly connected
- aerial vehicle
- unmanned aerial
- well cavity
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- 239000000110 cooling liquid Substances 0.000 claims description 4
- 230000007246 mechanism Effects 0.000 claims description 3
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 230000002035 prolonged effect Effects 0.000 abstract description 6
- 239000002826 coolant Substances 0.000 abstract description 5
- 230000017525 heat dissipation Effects 0.000 abstract description 5
- 239000007788 liquid Substances 0.000 abstract description 5
- 230000003139 buffering effect Effects 0.000 abstract description 4
- 238000013016 damping Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 239000000284 extract Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000008151 electrolyte solution Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
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- 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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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses an energy-conserving protection device of battery for unmanned aerial vehicle, including lower casing, the interior bottom fixedly connected with of casing is first well hollow rod down, be equipped with first well cavity in the first well cavity pole, sliding connection has the connecting rod in the first well cavity, the first spring of fixedly connected with between the interior bottom of connecting rod bottom and first well cavity, two second springs of equal fixedly connected with symmetry between U template and the first well cavity pole, the battery has been inlayed on the U template, the both sides of battery are equipped with stop gear, casing upper portion is equipped with the casing down. The utility model discloses, rational in infrastructure, through spacing and effectual buffering protection to the battery, prevent that the battery from appearing vibrations and causing the damage, prolonged the life of battery, be the coolant liquid with the U template the inside that the battery was hugged closely, can effectually carry out the heat dissipation protection to the battery, prevent that the battery from appearing high temperature and burning out and reduce the loss of battery electric energy.
Description
Technical Field
The utility model relates to a battery protection technology field especially relates to a battery energy-saving protection device for unmanned aerial vehicle.
Background
The battery refers to a part of space of a cup, a groove or other container or a composite container which is filled with electrolyte solution and a metal electrode connector to generate current, and a device which can convert chemical energy into electric energy and has a positive pole and a negative pole; the battery is used as an energy source, stable voltage and current can be obtained, stable power supply can be realized for a long time, the battery is simple in structure, convenient to carry, simple and easy to operate, stable and reliable in performance, and plays a great role in various aspects of modern social life.
The modern unmanned aerial vehicle battery has the following problems that the battery does not have the functions of buffering protection and heat dissipation protection, so that the unmanned aerial vehicle generates vibration when in use, the battery is damaged due to long-term vibration, and the service life of the battery is shortened.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the battery energy-saving protection device for unmanned aerial vehicle who proposes, it prevents through spacing and effectual buffering protection to the battery that vibrations from appearing and cause the damage, has prolonged the life of battery, is the coolant liquid with the U template the inside that the battery was hugged closely, can effectually dispel the heat the protection to the battery, prevents that the battery from appearing high temperature and burning out and reduce the loss of battery electric energy.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an energy-conserving protection device of battery for unmanned aerial vehicle, includes lower casing, the first well cavity pole of interior bottom fixedly connected with of casing down, be equipped with first well cavity in the pole in the first cavity, sliding connection has the connecting rod in the first well cavity, the first spring of fixedly connected with between the interior bottom of connecting rod bottom and first well cavity, connecting rod top fixedly connected with U template, two second springs of equal fixedly connected with symmetry between U template and the first well cavity pole, the battery has been inlayed on the U template, the both sides of battery are equipped with stop gear, casing upper portion is equipped with down, casing and last casing pass through the hinge rotation and are connected down, go up the equal fixedly connected with connecting block of looks remote site of casing and lower casing, two the connecting block passes through bolt fixed connection.
Preferably, stop gear includes with lower casing bottom fixed connection's two second cavity poles, two all be equipped with the second in the second cavity pole in the equal sliding connection of second cavity intracavity has L type pole, two L type pole all offsets with the upper end of battery, two the equal fixedly connected with piston in bottom of L type pole, two fixedly connected with third spring between the interior bottom of piston bottom and second cavity.
Preferably, a positive electrode connector and a negative electrode connector are fixedly connected to the upper case, and the positive electrode connector and the negative electrode connector respectively correspond to the positive electrode and the negative electrode of the battery.
Preferably, the connecting block is provided with a threaded through groove matched with the bolt.
Preferably, the U-shaped plate is a hollow U-shaped plate, and cooling liquid is arranged in the U-shaped plate.
Preferably, the piston is provided with a plurality of vent holes in a penetrating manner.
Compared with the prior art, the utility model, its beneficial effect does:
1. the battery vibrates upwards to drive the L-shaped rod, the piston and the third spring to perform buffer protection, meanwhile, the piston seals the second hollow cavity, air can only enter the second hollow cavity from the vent hole to form air damping, and the battery can be subjected to buffer protection; the battery shakes downwards to drive the U-shaped plate, the connecting rod and the second spring to perform buffer protection, and the connecting rod and the first spring are driven to perform buffer protection simultaneously.
2. The U-shaped plate tightly attached to the battery is a hollow plate, the cooling liquid is arranged inside the U-shaped plate, the battery can be effectively protected in a heat dissipation mode, the battery is prevented from being burnt out at high temperature, and the service life of the battery is prolonged.
To sum up, through spacing and effectual buffering protection to the battery, prevent that vibrations from appearing in the battery and cause the damage, prolonged the life of battery, be the coolant liquid with the U template the inside that the battery is hugged closely, can effectually carry out the heat dissipation protection to the battery, prevent that the high temperature from burning out and reducing the loss of battery electric energy from appearing in the battery.
Drawings
Fig. 1 is a cross-sectional view of a lower casing of a battery energy-saving protection device for an unmanned aerial vehicle according to the present invention;
fig. 2 is a side view of a U-shaped frame of a battery energy-saving protection device for an unmanned aerial vehicle according to the present invention;
fig. 3 is a sectional view of an upper housing of the battery energy-saving protection device for the unmanned aerial vehicle according to the present invention;
fig. 4 is the utility model provides a battery energy-saving protection device elevation for unmanned aerial vehicle.
In the figure: the structure of the cooling device comprises a lower shell 1, a first hollow rod 2, a first hollow cavity 3, a first spring 4, a connecting rod 5, a U-shaped plate 6, a second spring 7, a battery 8, a second hollow rod 9, a second hollow cavity 10, a third spring 11, a piston 12, a vent hole 13, a L-shaped rod 14, cooling liquid 15, an upper shell 16, a positive electrode connector 17, a negative electrode connector 18, a hinge 19, a connecting block 20 and a bolt 21.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1-4, an energy-conserving protection device of battery for unmanned aerial vehicle, including casing 1 down, the interior bottom fixedly connected with of casing 1 is first well hollow rod 2 down, be equipped with first well cavity 3 in the first well cavity 2, sliding connection has connecting rod 5 in the first well cavity 3, fixedly connected with first spring 4 between the interior bottom of connecting rod 5 bottom and first well cavity 3, connecting rod 5 top fixedly connected with U template 6, U template 6 is well cavity board, be equipped with coolant liquid 15 in the U template 6, can effectually dispel the heat the protection to battery 8, prevent that battery 8 from appearing high temperature and burning out.
Two symmetrical second springs 7 are fixedly connected between the U-shaped plate 6 and the first hollow rod 2, a battery 8 is embedded on the U-shaped plate 6, two sides of the battery 8 are provided with limiting mechanisms, each limiting mechanism comprises two second hollow rods 9 fixedly connected with the bottom of the lower shell 1, second hollow cavities 10 are arranged in the two second hollow rods 9, L-shaped rods 14 are slidably connected in the two second hollow cavities 10, the two L-shaped rods 14 are abutted against the upper ends of the battery 8, pistons 12 are fixedly connected with the bottoms of the two L-shaped rods 14, a plurality of vent holes 13 are arranged on the pistons 12 in a penetrating manner, and a third spring 11 is fixedly connected between the bottoms of the two pistons 12 and the inner bottom of the second hollow cavities 10, through the buffer protection of the L-shaped rod 14, the piston 12 and the third spring 11, air can only enter the second hollow cavity 10 from the vent hole 13 to form air damping, and the buffer protection of the battery 8 can be realized.
The upper portion of the lower shell 1 is provided with an upper shell 16, the upper shell 16 is fixedly connected with a positive electrode connector 17 and a negative electrode connector 18, the positive electrode connector 17 and the negative electrode connector 18 correspond to the positive electrode and the negative electrode of the battery 8 respectively, the lower shell 1 is rotatably connected with the upper shell 16 through a hinge 19, opposite ends of the lower shell 1 and the upper shell 16 are fixedly connected with connecting blocks 20, each connecting block 20 is provided with a threaded through groove matched with a bolt 21, the two connecting blocks 20 are fixedly connected through the bolt 21, and the upper shell and the lower shell can be opened through the rotating bolt 21 so as to replace the battery 8.
In the utility model, the worker firstly holds the handle on the bolt 21, rotates the bolt 21 to make the bolt 21 leave the connecting block 20, then rotates the upper shell 16, then extracts the L-shaped rod 14 upwards, then takes out the battery 8 for charging or replacing, then extracts the L-shaped rod 14 upwards, then puts the battery 8 into the U-shaped plate 6, puts down the L-shaped rod 14 to clamp the battery 8, wherein the U-shaped plate 6 can limit the battery 8 to move forwards and backwards, the second hollow rod 9 can limit the battery 8 to move leftwards and rightwards, when the battery 8 moves upwards and downwards, if the battery 8 moves upwards to drive the L-shaped rod 14 to move upwards, the L-shaped rod 14 drives the piston 12 to move upwards, the piston 12 moves upwards to limit the battery 8 under the action of the third spring 11, if the battery 8 moves downwards to drive the U-shaped plate 6 to move downwards, the U-shaped rod 6 moves downwards to limit the battery 8 under the action of the second spring 7, simultaneously U template 6 moves down and drives connecting rod 5 and move down, and connecting rod 5 is spacing to battery 8 under the effect of first spring 4.
During the flight, if a shock occurs, if the battery 8 moves upwards to drive the L-shaped rod 14 to move upwards, the L-shaped rod 14 moves upwards to drive the piston 12 to move upwards, the piston 12 moves upwards to drive the third spring 11 to stretch upwards for buffer protection, meanwhile, in the process that the piston 12 moves upwards, because the piston 12 seals the second hollow cavity 10 of the second hollow rod 9, air can only enter the second hollow cavity 10 from the vent hole 13 to form air damping, so that the battery 8 can be buffer protected, and if the battery 8 moves downwards to drive the U-shaped plate 6 to move downwards, the U-shaped plate 6 moves downwards to drive the second spring 7 to compress for buffer protection, meanwhile, the U-shaped plate 6 moves downwards to drive the connecting rod 5 to move downwards, the connecting rod 5 moves downwards to drive the first spring 4 to compress downwards for buffer protection, and through the limit and effective buffer protection of the battery 8, the damage caused by the vibration of the battery 8 is prevented, and the service life of the battery 8 is prolonged; if unmanned aerial vehicle works for a long time, battery 8 can dispel the heat, and the U template 6 of hugging closely with battery 8 is the cavity board, and the inside is coolant liquid 15, can effectually dispel the heat the protection to battery 8, prevents that battery 8 from appearing high temperature burnout, has prolonged battery 8's life to battery 8 buffer protection and heat dissipation protection's advantage has been reached.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The utility model provides an energy-conserving protection device of battery for unmanned aerial vehicle, includes casing (1) down, its characterized in that, the interior bottom fixedly connected with of casing (1) is first well cavity pole (2) down, be equipped with first well cavity (3) in first well cavity pole (2), sliding connection has connecting rod (5) in first well cavity (3), fixedly connected with first spring (4) between the interior bottom of connecting rod (5) bottom and first well cavity (3), connecting rod (5) top fixedly connected with U template (6), equal two second springs (7) of fixedly connected with symmetry between U template (6) and first well cavity pole (2), battery (8) have been inlayed on U template (6), the both sides of battery (8) are equipped with stop gear, casing (1) upper portion is equipped with upper housing (16) down, casing (1) and upper housing (16) are connected through hinge (19) rotation down, the opposite ends of the upper shell (16) and the lower shell (1) are fixedly connected with connecting blocks (20), and the two connecting blocks (20) are fixedly connected through bolts (21).
2. The battery energy-saving protection device for the unmanned aerial vehicle according to claim 1, wherein the limiting mechanism comprises two second hollow rods (9) fixedly connected with the bottom of the lower shell (1), two hollow rods (10) are arranged in the second hollow rods (9), two L-shaped rods (14) are slidably connected in the second hollow rods (10), two L-shaped rods (14) are abutted against the upper end of the battery (8), two pistons (12) are fixedly connected to the bottoms of the L-shaped rods (14), and two third springs (11) are fixedly connected between the bottoms of the pistons (12) and the inner bottom of the second hollow rods (10).
3. The battery energy-saving protection device for the unmanned aerial vehicle as claimed in claim 1, wherein a positive electrode connector (17) and a negative electrode connector (18) are fixedly connected to the upper housing (16), and the positive electrode connector (17) and the negative electrode connector (18) respectively correspond to the positive electrode and the negative electrode of the battery (8).
4. The battery energy-saving protection device for the unmanned aerial vehicle as claimed in claim 1, wherein the connecting block (20) is provided with a threaded through groove matched with the bolt (21).
5. The battery energy-saving protection device for the unmanned aerial vehicle according to claim 1, wherein the U-shaped plate (6) is a hollow U-shaped plate, and a cooling liquid (15) is arranged in the U-shaped plate (6).
6. The battery energy-saving protection device for the unmanned aerial vehicle according to claim 2, wherein a plurality of vent holes (13) are formed in the piston (12) in a penetrating manner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021256598.8U CN212556813U (en) | 2020-07-02 | 2020-07-02 | A battery energy-saving protection device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021256598.8U CN212556813U (en) | 2020-07-02 | 2020-07-02 | A battery energy-saving protection device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212556813U true CN212556813U (en) | 2021-02-19 |
Family
ID=74614972
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021256598.8U Expired - Fee Related CN212556813U (en) | 2020-07-02 | 2020-07-02 | A battery energy-saving protection device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212556813U (en) |
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2020
- 2020-07-02 CN CN202021256598.8U patent/CN212556813U/en not_active Expired - Fee Related
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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: 20210219 |