CN220984733U - Portable power source installation mechanism - Google Patents
Portable power source installation mechanism Download PDFInfo
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- CN220984733U CN220984733U CN202322698485.3U CN202322698485U CN220984733U CN 220984733 U CN220984733 U CN 220984733U CN 202322698485 U CN202322698485 U CN 202322698485U CN 220984733 U CN220984733 U CN 220984733U
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- air bag
- protective
- protective cover
- protective shell
- mounting groove
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- 238000009434 installation Methods 0.000 title claims abstract description 32
- 230000007246 mechanism Effects 0.000 title claims abstract description 31
- 230000001681 protective effect Effects 0.000 claims abstract description 89
- 238000005192 partition Methods 0.000 claims description 17
- 238000001816 cooling Methods 0.000 claims description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 229910021389 graphene Inorganic materials 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 7
- 230000009471 action Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- -1 graphite alkene Chemical class 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model relates to the technical field of unmanned aerial vehicles and discloses a mobile power supply installation mechanism, which comprises a power supply piece, wherein the power supply piece is detachably arranged at the side part of an unmanned aerial vehicle, the power supply piece comprises a battery, a protective shell, a protective cover and a protective cover, the battery is arranged in the protective shell, the protective cover is arranged at the side part of the protective shell, the protective cover is sleeved outside the protective shell, a driving device is arranged at the side part of the protective cover, an auxiliary assembly is arranged in the middle of the protective shell, when the protective shell is detached, a torsion rotation knob is twisted, a fixing block can move to two sides and simultaneously push a first baffle plate and a second baffle plate, the first baffle plate and the second baffle plate can squeeze the first bellows-shaped air bag and the second bellows-shaped air bag, gas in the first bellows-shaped air bag and the second bellows-shaped air bag can flow to a common air bag, when the common air bag is inflated, the baffle plate is stressed to squeeze a second spring, and the second spring can push the battery out.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a mobile power supply installation mechanism.
Background
Unmanned aerial vehicle is an unmanned aerial vehicle that does not have a person to take. It can perform flight tasks through remote control or preset autonomous flight plans, and unmanned aerial vehicles are typically composed of flight control systems, power systems, and sensors. They can be used for a variety of purposes including aerial photography, agricultural inspection, logistics transportation, scientific research, and the like. The unmanned aerial vehicle can fly in a multi-rotor, fixed wing or hybrid mode.
Some unmanned aerial vehicle designs can use removable power supply, and this kind of design makes unmanned aerial vehicle's power can easily change to extension flight time or carry out quick replacement, common removable power supply includes rechargeable battery or fuel cell. By replacing the new power supply, the drone may be recharged or refueled in a short period of time to continue performing tasks without stopping. Such a design is very useful for long-term tasks or applications requiring continuous flight, such as aerial photography, search rescue, etc.
Most of the existing unmanned aerial vehicle battery disassembling modes are spring piece buckle type, when the battery is installed in the mode, a certain gap exists between the battery and the unmanned aerial vehicle, the installation is not firm, once vibration occurs, the unmanned aerial vehicle is likely to be broken, the existing installation structure between most unmanned aerial vehicle and the battery is complex, the disassembly and the assembly are inconvenient, and the shockproof effect is poor; therefore, the existing requirements are not met, and a mobile power supply installation mechanism is provided for the mobile power supply installation mechanism.
Disclosure of utility model
The utility model provides a mobile power supply mounting mechanism, which has the beneficial effects that the problems that most of the existing unmanned aerial vehicle battery dismounting modes in the background technology are spring piece buckle type, a certain gap exists between a battery and an unmanned aerial vehicle when the unmanned aerial vehicle is mounted in the mode, the mounting is not firm, the unmanned aerial vehicle is likely to be broken once vibration occurs, the mounting structure between most of the existing unmanned aerial vehicles and the battery is complex, the dismounting is inconvenient, and the shockproof effect is poor are solved.
The utility model provides the following technical scheme: the utility model provides a portable power source installation mechanism, includes power supply piece, power supply piece demountable installation is in unmanned aerial vehicle lateral part, power supply piece includes battery, protective housing, visor and protective sheath, the battery is installed inside the protective housing, the visor is installed the protective housing lateral part, the protective housing outside has cup jointed the protective sheath, drive arrangement is installed to the visor lateral part, auxiliary assembly is installed at protective housing mid-section;
The side part of the protective cover is provided with a first mounting groove, a second mounting groove and a third mounting groove, a first spring is mounted in the first mounting groove, and the second mounting groove and the third mounting groove are respectively provided with a first bellows-shaped air bag and a second bellows-shaped air bag.
As an alternative to the mobile power supply installation mechanism of the present utility model, the following is adopted: the first baffle is fixedly connected with the end part of the first bellows-shaped air bag, the second baffle is fixedly connected with the end part of the second bellows-shaped air bag, the middle part of the protective cover is provided with a fixed block, and the side part of the fixed block is provided with a first mounting groove.
As an alternative to the mobile power supply installation mechanism of the present utility model, the following is adopted: the auxiliary assembly comprises a partition plate, a vent pipe, an air outlet, a second spring and a common air bag, wherein the partition plate is arranged at the bottom of the protective shell, the partition plate is arranged at the side part of the common air bag, the second spring is connected between the partition plate and the battery, the air outlet is arranged at the side part of the common air bag, the air outlet is connected with the vent pipe, and the bottom of the vent pipe is communicated with the first corrugated air bag and the second corrugated air bag.
As an alternative to the mobile power supply installation mechanism of the present utility model, the following is adopted: the protective sheath middle part is provided with the cooling layer, the protective sheath sets up to weave the cover, the cooling layer sets up to the graphite alkene layer.
As an alternative to the mobile power supply installation mechanism of the present utility model, the following is adopted: the driving device comprises a rotating knob, a driving piece, a rotating shaft and a connecting rod, wherein the driving piece is arranged in the middle of the fixed block, the rotating knob is fixedly connected with the connecting rod, the rotating shaft is rotationally connected with the driving piece, the rotating shaft is arranged in the protective shell, the connecting rod is connected with the protective cover in an inserting mode, and the connecting rod is also connected with the driving piece in an inserting mode.
As an alternative to the mobile power supply installation mechanism of the present utility model, the following is adopted: the notch is offered to the protective housing lateral part, the notch with fixed block.
As an alternative to the mobile power supply installation mechanism of the present utility model, the following is adopted: the first mounting groove, the second mounting groove and the third mounting groove are rectangular grooves.
As an alternative to the mobile power supply installation mechanism of the present utility model, the following is adopted: mounting holes are formed in the periphery of the protective shell and the periphery of the protective cover, and the protective shell and the protective cover are fixedly mounted through the mounting holes.
The utility model has the following beneficial effects:
1. This portable power source installation mechanism, auxiliary assembly's installation for this portable power source installation mechanism is convenient for install and dismantles, when dismantling, twists reverse the rotation knob, and the fixed block can remove to both sides, promotes first baffle and second baffle simultaneously, and first baffle and second baffle just can extrude first bellows gasbag and second bellows gasbag, and the gaseous ordinary gasbag of air pipe flow direction in first bellows gasbag and the second bellows gasbag can be extruded the baffle when ordinary gasbag inflation, and the baffle atress can extrude the second spring, and the second spring can promote the battery and release the battery.
When installing in with battery propulsion protective housing, gas in the ordinary gasbag can be discharged through the gas outlet, when rotatory rotation knob, the driving piece can rotate, and first baffle can stimulate first bellows gasbag and second bellows gasbag with the second baffle, inhale first bellows gasbag and second bellows gasbag with the gas in the ordinary gasbag for the second spring resumes the relaxation state, simultaneously, also can play the fixed action to the battery through the setting of spring and baffle.
2. This portable power source installation mechanism, through the setting of protective sheath for this portable power source installation mechanism can have better cushioning effect, plays physical protection, and the setting of cooling layer in the protective sheath makes unmanned aerial vehicle play the effect of cooling to the battery when long-time use, can be better play the guard action to the battery, and the material of protective sheath is woven the cover, makes this protective sheath have elasticity, can adapt to the battery of equidimension not.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle according to the present utility model.
Fig. 2 is a schematic view of a protective cover removing structure according to the present utility model.
Fig. 3 is a schematic structural view of a protective shell according to the present utility model.
FIG. 4 is a schematic view of a protective cover according to the present utility model.
Fig. 5 is a schematic structural view of a protective sleeve according to the present utility model.
Fig. 6 is a schematic diagram showing the structure of the auxiliary assembly in a second spring compressed state.
FIG. 7 is a schematic view of the secondary assembly of the present utility model in a second spring relaxed state.
In the figure: 400. a power supply member; 370. a connecting rod; 380. a rotating shaft; 390. a notch; 410. a partition plate; 420. a vent pipe; 430. a second spring; 440. a common air bag; 450. an air outlet; 200. a first bellows-like balloon; 210. a second bellows-like balloon; 220. a first baffle; 230. a second baffle; 240. a driving member; 250. a first spring; 260. a mounting hole; 270. a fixed block; 280. a first mounting groove; 290. a second mounting groove; 300. a third mounting groove; 310. a protective shell; 320. a protective cover; 330. a driving device; 340. a protective sleeve; 350. a cooling layer; 360. a rotary knob; 460. a battery; 470. an auxiliary assembly.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1
The embodiment is intended to facilitate solving the problem that when the existing unmanned aerial vehicle battery disassembling mode is mostly elastic sheet buckle type, a certain gap exists between the battery and the unmanned aerial vehicle when the unmanned aerial vehicle battery disassembling mode is installed, the installation is not firm, and once vibration occurs, the problem that the unmanned aerial vehicle is likely to be broken is likely to occur, referring to fig. 1-7, a mobile power supply installing mechanism comprises a power supply piece 400, the power supply piece 400 is detachably installed at the side part of the unmanned aerial vehicle, the power supply piece 400 comprises a battery 460, a protective shell 310, a protective cover 320 and a protective sleeve 340, the battery 460 is installed inside the protective shell 310, the protective cover 320 is installed at the side part of the protective shell 310, the protective sleeve 340 is sleeved outside the protective shell 310, the driving device 330 is installed at the side part of the protective cover 320, and the auxiliary component 470 is installed in the middle of the protective shell 310; the first mounting groove 280, the second mounting groove 290 and the third mounting groove 300 are formed in the side portion of the protective cover 320, the first spring 250 is mounted in the first mounting groove 280, the first bellows-shaped air bag 200 and the second bellows-shaped air bag 210 are mounted in the second mounting groove 290 and the third mounting groove 300 respectively, the first baffle 220 is fixedly connected to the end portion of the first bellows-shaped air bag 200, the second baffle 230 is fixedly connected to the end portion of the second bellows-shaped air bag 210, the fixing block 270 is arranged in the middle of the protective cover 320, and the first mounting groove 280 is formed in the side portion of the fixing block 270.
The auxiliary assembly 470 includes a partition 410, a vent pipe 420, an air outlet 450, a second spring 430 and a common air bag 440, the partition 410 is installed at the bottom of the protective case 310, the partition 410 is installed at the side of the common air bag 440, the second spring 430 is connected between the partition 410 and the battery 460, the air outlet 450 is arranged at the side of the common air bag 440, the air outlet 450 is connected with the vent pipe 420, the bottom of the vent pipe 420 is communicated with the first bellows-shaped air bag 200 and the second bellows-shaped air bag 210, a cooling layer 350 is arranged at the middle of the protective case 340, the protective case 340 is provided as a woven sleeve, and the cooling layer 350 is provided as a graphene layer.
In this embodiment: the installation of the auxiliary assembly 470 of the portable power source installation mechanism facilitates the installation and the disassembly, when the installation is performed, the rotary knob 360 is twisted, the fixing block 270 moves to two sides and pushes the first baffle 220 and the second baffle 230, the first baffle 220 and the second baffle 230 can squeeze the first bellows-shaped air bag 200 and the second bellows-shaped air bag 210, the air in the first bellows-shaped air bag 200 and the second bellows-shaped air bag 210 can flow to the common air bag 440 through the ventilation pipe 420, when the common air bag 440 expands and can squeeze the partition 410, the partition 410 is stressed and can squeeze the second spring 430, the second spring 430 can push the battery 460 out, when the installation is performed, the battery 460 is pushed into the protective shell 310, the air in the common air bag 440 can be discharged through the air outlet 450, when the rotary knob 360 is rotated, the driving piece 240 can rotate, the air in the first bellows-shaped air bag 200 and the second bellows-shaped air bag 210 can be pulled by the first baffle 220 and the second baffle 230, the air in the common air bag 440 can be sucked into the first bellows-shaped air bag 200 and the second bellows-shaped air bag 210, when the common air bag 440 expands and can squeeze the partition 410, the second spring 430 can also play a role of fixing the function of the partition 430 and the battery 460.
Example 2
The present embodiment is intended to facilitate solving the problems that most of the existing unmanned aerial vehicle and battery mounting structures are complex, inconvenient to disassemble and assemble, and poor in shockproof effect, and the present embodiment is an improvement made on the basis of embodiment 1, and referring to fig. 1-7, the driving device 330 includes a rotation knob 360, a driving element 240, a rotation shaft 380 and a connecting rod 370, the driving element 240 is mounted in the middle of the fixing block 270, the rotation knob 360 is fixedly connected with the connecting rod 370, the rotation shaft 380 is rotatably connected with the driving element 240, the rotation shaft 380 is mounted inside the protective cover 310, the connecting rod 370 is spliced with the protective cover 320, the connecting rod 370 is spliced with the driving element 240, the side portion of the protective cover 310 is provided with a notch 390, the notch 390 is fixedly clamped with the fixing block 270, the periphery of the protective cover 310 and the periphery of the protective cover 320 are provided with mounting holes 260, and the protective cover 310 and the protective cover 320 are fixedly mounted through the mounting holes 260.
In this embodiment: this portable power source installation mechanism, through the setting of protective sheath 340 for this portable power source installation mechanism can have better cushioning effect, plays physical protection, and the setting of cooling layer 350 in protective sheath 340 makes unmanned aerial vehicle play the effect of cooling to battery 460 when long-time use, can be better play the guard action to battery 460, and the material of protective sheath 340 is the cover of weaving, makes this protective sheath 340 have elasticity, can adapt to not equidimension battery 460.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
The foregoing is merely a preferred embodiment of the present utility model, and it should be noted that it will be apparent to those skilled in the art that several modifications and variations can be made without departing from the technical principle of the present utility model, and these modifications and variations should also be regarded as the scope of the utility model.
Claims (8)
1. The utility model provides a portable power source installation mechanism, includes power spare (400), power spare (400) demountable installation is in unmanned aerial vehicle lateral part, its characterized in that: the power supply piece (400) comprises a battery (460), a protective shell (310), a protective cover (320) and a protective sleeve (340), wherein the battery (460) is installed inside the protective shell (310), the protective cover (320) is installed on the side part of the protective shell (310), the protective sleeve (340) is sleeved outside the protective shell (310), a driving device (330) is installed on the side part of the protective cover (320), and an auxiliary assembly (470) is installed in the middle of the protective shell (310);
The side part of the protective cover (320) is provided with a first mounting groove (280), a second mounting groove (290) and a third mounting groove (300), a first spring (250) is mounted in the first mounting groove (280), and the second mounting groove (290) and the third mounting groove (300) are respectively provided with a first bellows-shaped air bag (200) and a second bellows-shaped air bag (210).
2. The portable power source mounting mechanism of claim 1, wherein: the first baffle (220) is fixedly connected to the end part of the first bellows-shaped air bag (200), the second baffle (230) is fixedly connected to the end part of the second bellows-shaped air bag (210), the middle part of the protective cover (320) is provided with a fixed block (270), and the side part of the fixed block (270) is provided with a first mounting groove (280).
3. The portable power source mounting mechanism of claim 1, wherein: the auxiliary assembly (470) comprises a partition plate (410), a vent pipe (420), an air outlet (450), a second spring (430) and a common air bag (440), wherein the partition plate (410) is installed at the bottom of the protective shell (310), the partition plate (410) is installed at the side part of the common air bag (440), the second spring (430) is connected between the partition plate (410) and the battery (460), the air outlet (450) is arranged at the side part of the common air bag (440), the air outlet (450) is connected with the vent pipe (420), and the bottom of the vent pipe (420) is communicated with the first corrugated air bag (200) and the second corrugated air bag (210).
4. The portable power source mounting mechanism of claim 1, wherein: the cooling layer (350) is arranged in the middle of the protection sleeve (340), the protection sleeve (340) is a woven sleeve, and the cooling layer (350) is a graphene layer.
5. A portable power source mounting mechanism as claimed in claim 2, wherein: the driving device (330) comprises a rotating knob (360), a driving piece (240), a rotating shaft (380) and a connecting rod (370), wherein the driving piece (240) is installed in the middle of the fixed block (270), the rotating knob (360) is fixedly connected with the connecting rod (370), the rotating shaft (380) is rotationally connected with the driving piece (240), the rotating shaft (380) is installed inside the protective shell (310), the connecting rod (370) is connected with the protective cover (320) in an inserting mode, and the connecting rod (370) is also connected with the driving piece (240) in an inserting mode.
6. A portable power source mounting mechanism as claimed in claim 2, wherein: notch (390) have been seted up to protective housing (310) lateral part, notch (390) with fixed block (270) fixed block.
7. The portable power source mounting mechanism of claim 1, wherein: the first mounting groove (280), the second mounting groove (290) and the third mounting groove (300) are all rectangular grooves.
8. The portable power source mounting mechanism of claim 1, wherein: mounting holes (260) are formed in the periphery of the protective shell (310) and the periphery of the protective cover (320), and the protective shell (310) and the protective cover (320) are fixedly mounted through the mounting holes (260).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322698485.3U CN220984733U (en) | 2023-10-09 | 2023-10-09 | Portable power source installation mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322698485.3U CN220984733U (en) | 2023-10-09 | 2023-10-09 | Portable power source installation mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220984733U true CN220984733U (en) | 2024-05-17 |
Family
ID=91038427
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322698485.3U Active CN220984733U (en) | 2023-10-09 | 2023-10-09 | Portable power source installation mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220984733U (en) |
-
2023
- 2023-10-09 CN CN202322698485.3U patent/CN220984733U/en active Active
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