CN218564908U - Unmanned aerial vehicle data memory - Google Patents
Unmanned aerial vehicle data memory Download PDFInfo
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- CN218564908U CN218564908U CN202222926406.5U CN202222926406U CN218564908U CN 218564908 U CN218564908 U CN 218564908U CN 202222926406 U CN202222926406 U CN 202222926406U CN 218564908 U CN218564908 U CN 218564908U
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Abstract
The utility model discloses an unmanned aerial vehicle data memory belongs to unmanned aerial vehicle data storage field. The utility model discloses an unmanned aerial vehicle data storage device, which comprises a storage device shell, wherein one side of the storage device shell is provided with a first connecting end; the both ends of centre gripping fixed plate all are provided with the connection fixed plate, two connect fixed plate and be a body structure with the centre gripping fixed plate, one side of connecting the fixed plate is provided with the unmanned aerial vehicle inner wall, two connect equal vertical evenly distributed between fixed plate and the unmanned aerial vehicle inner wall and have a plurality of bumper shock absorber. The utility model provides a long-time shake of current unmanned aerial vehicle data memory can cause accumulator data transmission efficiency lower, and the shake at first can be carried out the shock attenuation by the bumper shock absorber, and the parcel by first shock attenuation cotton and second shock attenuation cotton can make the shake of bearing fixed frame itself transmit to the accumulator shell afterwards, improves the stability of being connected between first link and the second link.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle data storage field specifically is an unmanned aerial vehicle data memory.
Background
Unmanned aerial vehicle is called unmanned aerial vehicle for short, it is an unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, or is operated by vehicle-mounted computer completely or intermittently and autonomously, with the popularization of unmanned aerial vehicle, people can utilize unmanned aerial vehicle to carry on multiple uses, and the data produced in the application process is often stored in the data storage temporarily, the data storage can last long-time to the data collected by unmanned aerial vehicle and store, in order to deal with the long-time use of unmanned aerial vehicle and the high-speed record of a large amount of data, people design a kind of unmanned aerial vehicle data storage;
chinese utility model patent of No. CN114852356A discloses a multi-functional file contrast instrument, including unmanned aerial vehicle internal baffle, horizontal shockproof sliding plate and data memory main part, unmanned aerial vehicle internal baffle fixed connection is inside unmanned aerial vehicle, the fixed frame of bottom fixedly connected with horizontal buffering of unmanned aerial vehicle internal baffle, this built-in unmanned aerial vehicle data memory is when using, and unmanned aerial vehicle internal baffle provides six shockproof to the data memory main part, and when unmanned aerial vehicle carried out the function, the power of the level or the vertical direction of production all can obtain the buffering through horizontal shockproof mechanism and vertical shockproof mechanism, and the influence that vibrations caused to the data memory main part in the at utmost reduction flight process guaranteed the stability of being connected of data memory main part and unmanned aerial vehicle internal element, guaranteed stable data transmission to improve the life of data memory main part.
However, in the actual use process of the existing data storage device for the unmanned aerial vehicle, the unmanned aerial vehicle itself shakes due to the flow of fan blades of the unmanned aerial vehicle and external air, the shake is transferred to the connected data storage device in the shaking process, the long-time shaking of the storage device causes the data transmission efficiency of the storage device to be low, and the long-time shaking of the storage device causes the service life of the storage device to be reduced; thus, the existing requirements are not met, for which we propose a drone data storage.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle data memory, the shake that unmanned aerial vehicle produced can be transmitted to the accumulator shell by the bumper shock absorber transmission and just can be transmitted to bearing fixed frame by the centre gripping fixed plate, the shake at first can be carried out the shock attenuation by the bumper shock absorber, the shock attenuation is avoided the accumulator shell to be in long-time shake state, on the other hand, the parcel by first shock attenuation cotton and second shock attenuation cotton can make the shake of bearing fixed frame itself transmit to the accumulator shell, can avoid the accumulator shell to bear the shake that unmanned aerial vehicle produced when moving for a long time at the in-process of fixed accumulator shell, improve the life of accumulator shell, and through the shock attenuation, improve the stability of being connected between first link and the second link, the problem of proposing in the above-mentioned background art has been solved.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle data storage device comprises a storage device shell, wherein a first connecting end is arranged on one side of the storage device shell;
still include the centre gripping fixed plate, it sets up in the opposite side of accumulator shell, the both ends of centre gripping fixed plate all are provided with the connection fixed plate, two connect fixed plate and be a body structure with the centre gripping fixed plate, one side of connecting the fixed plate is provided with the unmanned aerial vehicle inner wall, two connect equal vertical evenly distributed between fixed plate and the unmanned aerial vehicle inner wall have a plurality of bumper shock absorber, be provided with between centre gripping fixed plate and the unmanned aerial vehicle inner wall and bear fixed frame.
Preferably, bear the both ends of fixed frame respectively with unmanned aerial vehicle inner wall and centre gripping fixed plate welded fastening, the outside both ends of bumper shock absorber all are provided with the go-between.
Preferably, bear and be provided with second shock attenuation cotton between fixed frame and the accumulator shell, be provided with first shock attenuation cotton between accumulator shell and the unmanned aerial vehicle inner wall, one side of first shock attenuation cotton is fixed with the one side adhesion of accumulator shell, second shock attenuation cotton is fixed with the upper end adhesion that bears fixed frame.
Preferably, the upper end of the storage device shell is provided with a first cooling fin, one side between the storage device shell and the clamping fixing plate is provided with a second cooling fin, and the second cooling fin and the first cooling fin are both fixedly adhered to the outside of the storage device shell.
Preferably, one side of the outside of the clamping fixing plate is provided with a protruding frame, one side of the protruding frame is provided with a second heat dissipation cavity, and the lower end of one side of the protruding frame is provided with a first heat dissipation cavity.
Preferably, the inside centre of protrusion frame is provided with the heat dissipation flabellum, one side of heat dissipation flabellum is provided with dustproof filter screen, the outside of dustproof filter screen is fixed with the inside adhesion of protrusion frame.
Preferably, the lower extreme of first heat dissipation chamber outside is provided with the air exit, and the air exit runs through and extends to the upper and lower both ends of bearing fixed frame.
Preferably, the two sides of the front end of the protruding frame are provided with two air flow limiting plates, and one end of each of the two air flow limiting plates is welded and fixed with the protruding frame.
Preferably, a second connecting end is arranged outside the first connecting end, and the second connecting end, the first connecting end and the storage shell are all electrically connected.
Preferably, the connecting rings are internally provided with fixing pieces, and one sides of the fixing pieces are fixedly connected with the two ends of the shock absorber through bolts.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses an one end at the unmanned aerial vehicle inner wall is provided with the accumulator shell, the one end of accumulator shell is provided with the centre gripping fixed plate, both sides between centre gripping fixed plate and the unmanned aerial vehicle inner wall all vertically are provided with three bumper shock absorber, unmanned aerial vehicle removes and when carrying the accumulator shell in the air, the shake that unmanned aerial vehicle produced can be transmitted to bearing fixed frame just can transmit to the accumulator shell by the bumper shock absorber transmission and by the centre gripping fixed plate, the shake at first can be carried out the shock attenuation by the bumper shock absorber, the shock attenuation is avoided the accumulator shell to be in long-time shake state, on the other hand, the parcel by first shock attenuation cotton and second shock attenuation cotton can make the shake of bearing fixed frame itself transmit to the accumulator shell, can avoid the accumulator shell to bear the shake that unmanned aerial vehicle produced when moving for a long time at the in-process of fixed accumulator shell, improve the life of accumulator shell, and through the shock attenuation, improve the stability of being connected between first link and the second link.
2. The utility model discloses an inside at dustproof filter screen is provided with the radiating fan blade, one side of radiating fan blade is provided with second heat dissipation chamber, the lower extreme of radiating fan blade one side is provided with first heat dissipation chamber, when data storage ware stores for a long time and produces the heat, the radiating fan blade by single laminating storage ware shell one side rotates, the rotation of radiating fan blade can drive the air flow and make the air flow respectively to second heat dissipation chamber and first heat dissipation chamber, the first fin and the second fin that the flow of air and direct contact correspond, raise the radiating efficiency and radiating effect, furthest's improvement heat-sinking capability, it is higher to avoid the storage shell temperature when storing data for a long time, thereby reduce the temperature of storage shell and improve the life of storage shell and the data transmission effect of storage shell.
Drawings
FIG. 1 is a perspective view of the overall external structure of the present invention;
fig. 2 is a schematic view of the transmission structure in the first heat dissipation cavity of the present invention;
FIG. 3 is a schematic view of the internal structure of the first shock absorbing cotton of the present invention;
fig. 4 is a partially enlarged view of the area a in fig. 3 according to the present invention.
In the figure: 1. the inner wall of the unmanned aerial vehicle; 2. a reservoir housing; 3. first shock absorbing cotton; 4. bearing the fixed frame; 5. clamping the fixing plate; 6. an air flow restricting plate; 7. a protruding frame; 8. a dustproof filter screen; 9. connecting the fixed plate; 10. a connecting ring; 11. a shock absorber; 12. a fixing sheet; 13. a first heat sink; 14. a second heat sink; 15. a heat dissipating fan blade; 16. a first heat dissipation chamber; 17. an air outlet; 18. second shock absorption cotton; 19. a second heat dissipation chamber; 20. a first connection end; 21. a second connection end.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
For further understanding of the present invention, please refer to fig. 1, fig. 2, fig. 3 and fig. 4, the present embodiment provides the following technical solutions:
an unmanned aerial vehicle data memory comprises a memory shell 2, wherein a first connecting end 20 is arranged on one side of the memory shell 2;
still include centre gripping fixed plate 5, it sets up in the opposite side of accumulator shell 2, the both ends of centre gripping fixed plate 5 all are provided with connection fixed plate 9, two connection fixed plate 9 are a body structure with centre gripping fixed plate 5, one side of connecting fixed plate 9 is provided with unmanned aerial vehicle inner wall 1, equal vertical evenly distributed has a plurality of bumper shock absorber 11 between two connection fixed plate 9 all and the unmanned aerial vehicle inner wall 1, be provided with between centre gripping fixed plate 5 and the unmanned aerial vehicle inner wall 1 and bear fixed frame 4.
In order to solve the technical problems that during the actual use of the existing data storage of the unmanned aerial vehicle, the unmanned aerial vehicle itself shakes due to the flow of fan blades of the unmanned aerial vehicle and the external air, during the shaking process, the shaking is transmitted to the connected data storage, the long-time shaking of the storage causes the data transmission efficiency of the storage to be low, and the long-time shaking of the storage causes the service life of the storage to be reduced, please refer to fig. 1, fig. 2, fig. 3 and fig. 4, the embodiment provides the following technical solutions:
bear the both ends of fixed frame 4 respectively with unmanned aerial vehicle inner wall 1 and 5 welded fastening of centre gripping fixed plate, 11 outside both ends of bumper shock absorber all are provided with go-between 10.
In particular, the vibration of the drive can be damped by means of the damper 11, which can prevent long-term high-frequency vibrations of the reservoir housing 2.
Further, referring to fig. 1, fig. 2, fig. 3 and fig. 4, the present embodiment provides the following technical solutions:
bear and be provided with second shock attenuation cotton 18 between fixed frame 4 and the accumulator shell 2, be provided with first shock attenuation cotton 3 between accumulator shell 2 and the unmanned aerial vehicle inner wall 1, one side of first shock attenuation cotton 3 is fixed with the one side adhesion of accumulator shell 2, and second shock attenuation cotton 18 is fixed with the upper end adhesion of bearing fixed frame 4.
Specifically, the contact between the second damping cotton 18 and the first damping cotton 3 can improve the damping effect and avoid the long-term high-frequency shaking of the storage casing 2.
Further, referring to fig. 1, fig. 2, fig. 3 and fig. 4, the present embodiment provides the following technical solutions:
the upper end of the storage casing 2 is provided with a first radiating fin 13, one side between the storage casing 2 and the clamping fixing plate 5 is provided with a second radiating fin 14, and the second radiating fin 14 and the first radiating fin 13 are both fixedly adhered to the outside of the storage casing 2.
Specifically, the contact area between the heat generating position of the reservoir housing 2 and the outside air can be increased by the first heat dissipation fins 13 and the second heat dissipation fins 14, and the increase in the contact area can improve the heat dissipation effect of the device.
Further, referring to fig. 1, fig. 2, fig. 3 and fig. 4, the present embodiment provides the following technical solutions:
the outer side of the clamping and fixing plate 5 is provided with a protruding frame 7, one side of the protruding frame 7 is provided with a second heat dissipation cavity 19, and the lower end of one side of the protruding frame 7 is provided with a first heat dissipation cavity 16.
Specifically, the transmitted air can be shunted and enter the second heat dissipation cavity 19 and the first heat dissipation cavity 16 through the self-restriction of the storage casing 2, so that the heat at the corresponding position is discharged, and the heat dissipation effect of the device is improved.
Further, referring to fig. 1, fig. 2 and fig. 3, the present embodiment provides the following technical solutions:
the inside centre of protrusion frame 7 is provided with heat dissipation flabellum 15, and one side of heat dissipation flabellum 15 is provided with dustproof filter screen 8, and the outside of dustproof filter screen 8 is fixed with the inside adhesion of protrusion frame 7.
Specifically, the whole floor space of the device can be reduced by the attached radiating fan blades 15, and the overall structure is prevented from being large in size.
Further, referring to fig. 2, fig. 3 and fig. 4, the present embodiment provides the following technical solutions:
the lower end of the outer part of the first heat dissipation cavity 16 is provided with an air outlet 17, and the air outlet 17 penetrates through and extends to the upper end and the lower end of the bearing fixing frame 4.
In particular, the heat transferred can be discharged through the air outlet 17.
Further, referring to fig. 1, fig. 2, fig. 3 and fig. 4, the present embodiment provides the following technical solutions:
the both sides of protrusion frame 7 front end all are provided with air flow limiting plate 6, and air flow limiting plate 6 is provided with two, and the one end of two air flow limiting plate 6 all with protrusion frame 7 welded fastening.
Specifically, the air flow direction of the air extracted from the outside can be limited by the air flow limiting plate 6, so that the extracted air can contact the first heat radiating fin 13 and the second heat radiating fin 14 in a comprehensive manner, and the heat radiating effect is improved.
Further, referring to fig. 1, fig. 2 and fig. 3, the present embodiment provides the following technical solutions:
the second connection end 21 is disposed outside the first connection end 20, and the second connection end 21, the first connection end 20 and the storage casing 2 are all electrically connected.
Specifically, the data can be stored inside the storage case 2 by electrically connecting the first connection terminal 20 and the second connection terminal 21.
Further, referring to fig. 1, the present embodiment provides the following technical solutions:
the inside of two go-between 10 all is provided with stationary blade 12, and one side of stationary blade 12 all passes through bolt fixed connection with the both ends of bumper shock absorber 11.
Specifically, the fixing of the damper 11 can be completed by the connection of the fixing piece 12, and the damping effect of the damper 11 can be improved by the fixing.
The working principle is as follows: when the unmanned aerial vehicle storage is used in actual use, according to fig. 1, fig. 2, fig. 3 and fig. 4, in order to avoid the influence of jitter generated during the operation of the unmanned aerial vehicle on the use and service life of the storage shell 2, the jitter of the unmanned aerial vehicle is transmitted to the shock absorber 11 through the inner wall 1 of the unmanned aerial vehicle, the jitter of the shock absorber 11 is transmitted to the connecting and fixing plate 9, the connecting and fixing plate 9 transmits the jitter to the bearing and fixing frame 4 through the clamping and fixing plate 5 and finally contacts the storage shell 2, the jitter force can be directly reduced through the shock absorption of the shock absorber 11, on the other hand, the second shock absorbing cotton 18 and the first shock absorbing cotton 3 are respectively contacted and supported with the lower end outside the storage shell 2 and the connecting positions of the first connecting end 20 and the second connecting end 21, when the storage shell 2 is fixed, the shock absorption can be further performed, the stability of the connection between the first connecting end 20 and the second connecting end 21 can be improved, in order to avoid the problem that the self temperature is high due to long-time storage shell 2 storage shell storage, thereby the influence on the data transmission effect, the rotation of the heat dissipation fan 15 extracts the outside air after contacting the storage shell 2, the air can be separated and separated from the heat dissipation cavity 19, the heat dissipation fan blade 15, thereby the heat dissipation area of the heat dissipation of the storage shell can be reduced, and the heat dissipation area of the whole of the unmanned aerial vehicle can be reduced, and the heat dissipation fan blade 15, and the heat dissipation of the unmanned aerial vehicle can be reduced, and the whole volume of the heat dissipation fan blade can be reduced, and the whole of the unmanned aerial vehicle, and the heat dissipation fan blade can be reduced.
It is noted that, herein, relational terms such as first and second, and the like may be 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. Also, 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.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides an unmanned aerial vehicle data storage ware, includes storage shell (2), one side of storage shell (2) is provided with first connection end (20), its characterized in that:
still include centre gripping fixed plate (5), it sets up in the opposite side of accumulator shell (2), the both ends of centre gripping fixed plate (5) all are provided with connection fixed plate (9), two connection fixed plate (9) are a body structure with centre gripping fixed plate (5), one side of connecting fixed plate (9) is provided with unmanned aerial vehicle inner wall (1), two equal vertical evenly distributed has a plurality of bumper shock absorber (11) between connection fixed plate (9) all and unmanned aerial vehicle inner wall (1), be provided with between centre gripping fixed plate (5) and the unmanned aerial vehicle inner wall (1) and bear fixed frame (4).
2. A drone data storage according to claim 1, characterized in that: bear the both ends of fixed frame (4) respectively with unmanned aerial vehicle inner wall (1) and centre gripping fixed plate (5) welded fastening, the outside both ends of bumper shock absorber (11) all are provided with go-between (10).
3. A drone data storage according to claim 1, characterized in that: bear and be provided with second shock attenuation cotton (18) between fixed frame (4) and reservoir shell (2), be provided with first shock attenuation cotton (3) between reservoir shell (2) and unmanned aerial vehicle inner wall (1), one side of first shock attenuation cotton (3) is fixed with the one side adhesion of reservoir shell (2), second shock attenuation cotton (18) are fixed with the upper end adhesion of bearing fixed frame (4).
4. A drone data storage according to claim 1, characterized in that: the upper end of the storage device shell (2) is provided with a first radiating fin (13), one side between the storage device shell (2) and the clamping fixing plate (5) is provided with a second radiating fin (14), and the second radiating fin (14) and the first radiating fin (13) are both fixed with the outside of the storage device shell (2) in an adhesion manner.
5. A drone data storage according to claim 1, characterized in that: the clamping fixing plate is characterized in that a protruding frame (7) is arranged on one side of the outer portion of the clamping fixing plate (5), a second heat dissipation cavity (19) is arranged on one side of the protruding frame (7), and a first heat dissipation cavity (16) is arranged at the lower end of one side of the protruding frame (7).
6. A UAV data storage according to claim 5 wherein: the middle of the inside of the protruding frame (7) is provided with a radiating fan blade (15), one side of the radiating fan blade (15) is provided with a dustproof filter screen (8), and the outside of the dustproof filter screen (8) is fixed with the inside adhesion of the protruding frame (7).
7. The drone data storage of claim 6, wherein: the outside lower extreme in first heat dissipation chamber (16) is provided with air exit (17), and air exit (17) run through and extend to the upper and lower both ends of bearing fixed frame (4).
8. The drone data storage of claim 7, wherein: the air flow limiting plates (6) are arranged on two sides of the front end of the protruding frame (7), two air flow limiting plates (6) are arranged, and one ends of the two air flow limiting plates (6) are welded and fixed with the protruding frame (7).
9. A drone data storage according to claim 1, characterized in that: the second connecting end (21) is arranged outside the first connecting end (20), and the second connecting end (21), the first connecting end (20) and the storage shell (2) are all electrically connected.
10. A drone data storage according to claim 2, characterized in that: two the inside of go-between (10) all is provided with stationary blade (12), and one side of stationary blade (12) all passes through bolt fixed connection with the both ends of bumper shock absorber (11).
Priority Applications (1)
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CN202222926406.5U CN218564908U (en) | 2022-11-03 | 2022-11-03 | Unmanned aerial vehicle data memory |
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CN202222926406.5U CN218564908U (en) | 2022-11-03 | 2022-11-03 | Unmanned aerial vehicle data memory |
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CN202222926406.5U Active CN218564908U (en) | 2022-11-03 | 2022-11-03 | Unmanned aerial vehicle data memory |
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