CN212829028U - Unmanned aerial vehicle's casing and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle's casing and unmanned aerial vehicle Download PDFInfo
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- CN212829028U CN212829028U CN202021362461.0U CN202021362461U CN212829028U CN 212829028 U CN212829028 U CN 212829028U CN 202021362461 U CN202021362461 U CN 202021362461U CN 212829028 U CN212829028 U CN 212829028U
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- unmanned aerial
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Abstract
The utility model discloses an unmanned aerial vehicle's casing and unmanned aerial vehicle, wherein, this unmanned aerial vehicle's casing includes: the surface of the frame can be used for mounting electronic components of the unmanned aerial vehicle, and part of the surface of the frame is concavely provided with a mounting groove for mounting a battery of the unmanned aerial vehicle; the baffle is used for sealing and covering the mounting groove so as to limit the battery of the unmanned aerial vehicle; and the locking assembly comprises a locking device arranged on the rack and a locking device arranged on the baffle, and the locking device is detachably connected with the locking device so as to fixedly connect the baffle with the rack. The utility model discloses technical scheme sets up battery and electronic components in the different spaces of frame, and when unmanned aerial vehicle's casing received the striking, unmanned aerial vehicle's battery can not cause the interference to unmanned aerial vehicle's electronic components.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to unmanned aerial vehicle's casing and unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, and has the advantages of simple operation and control, high reliability, capability of vertically taking off and landing without a runway, capability of hovering in the air after taking off and the like. Unmanned aerial vehicle can be divided into for military use unmanned aerial vehicle and civilian unmanned aerial vehicle. In the aspect of civil unmanned aerial vehicles, the unmanned aerial vehicles are mainly used in combination with industry. At present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded by combining with industrial application.
Because unmanned aerial vehicle's application range is wider and wider, various problems also ensued to, current unmanned aerial vehicle's mainboard, GPS orientation module, pilot lamp, automatic pilot module, electronic components such as GPS module and unmanned aerial vehicle's battery are all installed in the same surface of unmanned aerial vehicle's casing, the battery takes place the condition of droing easily when unmanned aerial vehicle receives the striking, the battery drops then can influence other electronic components that lie in around the battery, and then lead to the unable normal flight of unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle's casing and unmanned aerial vehicle, do not bring the influence of butterfly effect formula to the inside other components of unmanned aerial vehicle when aiming at the battery to drop.
In order to achieve the above object, the utility model provides a pair of unmanned aerial vehicle's casing, it includes: the surface of the rack can be used for mounting electronic components of the unmanned aerial vehicle, and part of the surface of the rack is concavely provided with a mounting groove for mounting a battery of the unmanned aerial vehicle; the baffle is used for covering the mounting groove so as to limit the battery of the unmanned aerial vehicle; the locking assembly comprises a locking device arranged on the rack and a locking device arranged on the baffle, and the locking device is detachably connected with the locking device so as to fixedly connect the baffle with the rack.
Optionally, the locking device includes a locking housing, a locking post and a power element, the locking housing is mounted on the frame, an abdicating opening is concavely formed on the surface of the locking housing, the locking post is movably mounted on the locking housing and can move along the direction in which two opposite side walls of the abdicating opening are close to or far away from each other, and the power element is mounted on the locking housing and is in transmission connection with the locking post; the locking device comprises a fixing part fixedly connected with the baffle and a locking ring connected with the fixing part, and the locking ring can extend into the abdicating opening to be matched with the locking column.
Optionally, the locking column is made of a metal material, and a limiting protrusion is arranged on the outer peripheral wall of one end of the locking column; the locking shell is provided with a containing cavity and a abdicating hole for communicating the containing cavity with the abdicating opening, and one end of the locking column, which is far away from the limiting bulge, extends into the abdicating hole; the power part comprises an electromagnet and a spring, the electromagnet is installed in the containing cavity and can magnetically adsorb the locking column, the spring is sleeved on the locking column, one end of the spring is abutted to the limiting protrusion, and the other end of the spring is abutted to the outer surface of the locking shell.
Optionally, the electro-magnet is connected with unmanned aerial vehicle's battery and unmanned aerial vehicle's equal electricity of main control box.
Optionally, the frame is further provided with a fixing plate in a protruding manner, and the fixing plate and the locking device are respectively arranged on two opposite sides of the notch of the mounting groove; one side of the baffle is abutted to the fixed plate, and the other side of the baffle is detachably connected with the locking device through the locking device.
Optionally, the surface of the fixed plate abutted against the baffle is provided with a limiting structure, and the limiting structure is used for limiting the baffle to move towards the direction deviating from the mounting groove.
Optionally, the limiting structure is a plurality of stop protrusions convexly arranged on the surface of the fixing plate, which is abutted to the baffle plate; or the limiting structure is a positioning groove which is concavely arranged on the surface of the fixed plate, which is abutted to the baffle.
Optionally, a groove wall of the mounting groove is arranged in a penetrating manner to form a plurality of through holes.
Optionally, a handle is arranged on the surface of the baffle plate, which faces away from the mounting groove.
The utility model also provides an unmanned aerial vehicle, including unmanned aerial vehicle's battery, unmanned aerial vehicle's main control box and unmanned aerial vehicle's frame, unmanned aerial vehicle's battery is installed in the mounting groove of main part, unmanned aerial vehicle's main control box is installed in the surface of main part.
The utility model discloses a surface of unmanned aerial vehicle's frame supplies unmanned aerial vehicle's electronic components to install, the concave mounting groove that forms the battery installation that supplies unmanned aerial vehicle of establishing of surface part of unmanned aerial vehicle's frame, the baffle is used for the mounting groove closing cap, so can locate two spaces with unmanned aerial vehicle's battery and unmanned aerial vehicle's electronic components branch in, even unmanned aerial vehicle's casing receives the impact, thereby unmanned aerial vehicle's battery can not drop yet and avoid unmanned aerial vehicle's electronic components to cause the damage of butterfly effect formula. Simultaneously, the frame and the baffle of the unmanned aerial vehicle are detachably connected through the locking device and the locking device of the locking assembly, so that the battery is conveniently mounted and dismounted.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an embodiment of a housing of the unmanned aerial vehicle of the present invention;
FIG. 2 is a cross-sectional view of the locking device of FIG. 1;
fig. 3 is a cross-sectional view of the latching device of fig. 1.
The reference numbers illustrate:
| reference numerals | Name (R) | Reference numerals | Name (R) | |
| 1000 | Unmanned aerial vehicle's |
322 | |
|
| 100 | |
| Spacing protrusion | |
| 110 | |
| Abdication opening | |
| 200 | |
| Containing chamber | |
| 300 | Locking assembly | 312a | |
|
| 310 | Locking | 312b | Spring | |
| 320 | |
120 | |
|
| 311 | |
121 | Stop bulge | |
| 312 | |
130 | Through |
|
| 313 | |
210 | |
|
| 321 | Fixing part |
The objects, features and advantages of the present invention will be further described with reference to the accompanying drawings.
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 efforts belong to the protection scope of the present invention.
It should be noted that all the directional indicators (such as upper, lower, left, right, front and rear … …) in the embodiment of the present invention are only used to explain the relative position relationship between the components, the motion situation, etc. in a specific posture (as shown in the drawings), and if the specific posture is changed, the directional indicator is changed accordingly.
In addition, the descriptions related to "first", "second", etc. in the present invention are for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicit ly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should not be considered to exist, and is not within the protection scope of the present invention.
The utility model provides an unmanned aerial vehicle's casing, it can separate unmanned aerial vehicle's electronic components and unmanned aerial vehicle's battery, and unmanned aerial vehicle's battery interference to unmanned aerial vehicle's electronic components when having effectively avoided unmanned aerial vehicle to receive when strikeing to ensure that unmanned aerial vehicle receives and still can normally fly after strikeing.
Referring to fig. 1, the housing 1000 of the drone includes a frame 100, a baffle 200, and a locking assembly 300, and the frame 100 and the baffle 200 are connected and fixed by the locking assembly 300.
This frame 100 is an installation carrier, and it can supply unmanned aerial vehicle's electronic components (mainboard, GPS orientation module, pilot lamp, Autopilot module, GPS module etc.), unmanned aerial vehicle's battery, unmanned aerial vehicle's wing and other part installations. The rack 100 includes a mounting surface for mounting electronic components and a support frame detachably connected to the mounting surface.
The surface of this frame 100 can supply unmanned aerial vehicle's electronic components (mainboard, GPS orientation module, etc.) installation, and unmanned aerial vehicle's electronic components can concentrate and install on the installation face of frame 100, also can locate on the installation face of frame 100 and the support frame outside separately, does not do specific restriction here.
The surface portion of this frame 100 is concavely provided with the mounting groove 110 that is formed with the battery installation that supplies unmanned aerial vehicle, and the size and the shape of this mounting groove 110 all with unmanned aerial vehicle's battery size and shape looks adaptation. This mounting groove 110 can be installed unmanned aerial vehicle's electronic components's the concave formation of establishing of surface portion by frame 100, and this mounting groove 110 also can be installed unmanned aerial vehicle's electronic components's the concave formation of establishing of surface portion by frame 100, does not do specific restriction here.
The baffle 200 is a notch plate structure covering the mounting groove 110, the size of the baffle 200 can be larger than or equal to the notch setting of the mounting groove 110, the shape of the baffle 200 is related to the size of the baffle 200, if the size of the baffle 200 is larger than the notch setting of the mounting groove 110, the shape of the baffle 200 can be arbitrarily set, as long as the notch of the mounting groove 110 is sealed, if the size of the baffle 200 is equal to the notch of the mounting groove 110, the shape of the baffle 200 is the same as the notch formation of the mounting groove 110. The baffle 200 may be disposed to protrude from a surface of the rack 100, and the baffle 200 may be flush with the surface of the rack 100, which is not particularly limited herein.
The locking assembly 300 is used for fixedly connecting the baffle plate 200 and the rack 100, the locking assembly 300 comprises a locking device 310 arranged on the rack 100 and a locking device 320 arranged on the baffle plate 200, the locking device 310 is connected with the locking device 320, so that the rack 100 and the baffle plate 200 can be fixedly connected, and the locking device 310 and the locking device 320 are unlocked, so that the baffle plate 200 and the rack 100 can be unlocked. The locking device 310 and the locking device 320 can be of various types, for example, the locking device 310 is a hook, the locking device 320 is a buckle, and if the locking device 310 is an electromagnet 312a, the locking device 320 is a metal lock cylinder, the locking device 310 and the locking device 320 can also be other types of detachable connection structures, which are not limited herein.
The utility model discloses an unmanned aerial vehicle's frame 100's surface supplies unmanned aerial vehicle's electronic components installation, the concave mounting groove 110 that forms the battery installation that supplies unmanned aerial vehicle of establishing of unmanned aerial vehicle's frame 100's surface part, baffle 200 is used for the mounting groove 110 closing cap, so can locate unmanned aerial vehicle's battery and unmanned aerial vehicle's electronic components branch in two spaces, even unmanned aerial vehicle's casing 1000 receives the impact, unmanned aerial vehicle's battery also can not drop and cause the damage of butterfly effect formula to unmanned aerial vehicle's electronic components. Meanwhile, the frame 100 and the baffle 200 of the unmanned aerial vehicle are detachably connected through the locking device 310 and the locking device 320 of the locking assembly 300, so that the battery can be conveniently mounted and dismounted.
In an embodiment of the present invention, the locking device 310 and the locking device 320 are detachably connected by a cylindrical structure and a ring structure, please refer to fig. 2 and fig. 3, the locking device 310 includes a locking housing 311, a power component 312 and a locking post 313, and the locking device 320 includes a fixing portion 321 and a locking ring 322.
The locking housing 311 is fixedly mounted on the frame 100, and may be fixed to the frame 100 by screw connection, rivet riveting, welding, and other methods. The surface of the locking housing 311 is concavely provided with a relief opening 311a, the relief opening 311a may be disposed at a position where the locking housing 311 faces the baffle 200, and the relief opening 311a may also be disposed at a side surface of the locking housing 311, which is not limited herein. The abdicating opening 311a may have two sets of oppositely disposed side wall structures, i.e. similar to a groove structure, or the abdicating opening 311a may have one set of oppositely disposed side wall structures, i.e. similar to a notch structure, which is not limited herein.
The locking post 313 is mounted on the locking housing 311, and may be disposed inside the locking housing 311, or may be disposed on the surface of the locking housing 311, as long as it can move along the direction that the two opposite sidewalls of the abdicating opening 311a are close to or far away from each other, so as to cross the abdicating opening 311 a.
The power element 312 is mounted on the locking housing 311, the power element 312 may be fixed to the locking housing 311 by screw connection, rivet riveting, welding or other methods, the power element 312 may be an air pump, a piston rod, a piston, and a piston cylinder, the power element 312 may also be composed of a motor, a rocker, and a slider, and the power element 312 may also be other components capable of driving the locking post 313 to make linear motion, which is not limited herein.
The fixing portion 321 is fixedly connected to the baffle 200, and may be fixed to the baffle 200 by screw connection, rivet riveting, welding, and other methods.
The locking ring 322 is fixedly connected to the fixing portion 321, and may also be fixed to the fixing portion 321 by screw connection, rivet riveting, welding, and other methods, and the locking ring 322 is in an annular configuration, which may be in an elliptical ring, a rectangular ring, a circular ring, and other annular configurations.
In the locking process, the baffle 200 covers the notch of the mounting groove 110 of the rack 100, the locker 320 fixed on the baffle 200 is gradually close to the locker 310 fixed on the rack 100, the locking ring 322 is inserted into the abdicating opening 311a, the power part 312 drives the locking post 313 to move, so that one end of the locking post 313 penetrates through the locking ring 322 in the moving process and finally abuts against the locking shell 311, the locking post 313 can abut against the side wall of the abdicating opening 311a, and the locking post 313 can also abut against other positions of the locking shell 311, so that the locking ring 322 is connected with the locking post 313, and the purpose of locking the baffle 200 is achieved.
In the unlocking process, the power member 312 drives the locking post 313 to move, so that the locking post 313 moves along the direction that the two opposite side walls of the abdicating opening 311a are away from each other, and the locking post 313 passes through one end of the locking ring 322 and is dislocated with the locking ring 322, so that the restriction on the locking ring 322 is released, and the unlocking purpose is achieved.
Furthermore, the locking column 313 is made of a metal material, a limiting protrusion 313a is arranged on the outer peripheral wall of one end of the locking column 313, the locking shell 311 is provided with a containing cavity 311b and a yielding hole (not marked) for communicating the containing cavity 311b with the yielding opening 311a, and one end of the locking column 313, which is far away from the limiting protrusion 313a, extends into the yielding hole; the power component 312 includes an electromagnet 312a and a spring 312b, the electromagnet 312a is installed in the accommodating cavity 311b and can magnetically attract the locking column 313, the spring 312b is sleeved on the locking column 313, one end of the spring is abutted against the limiting protrusion 313a, and the other end of the spring is abutted against the outer surface of the locking housing 311.
In the locking process, the baffle 200 covers the notch of the mounting groove 110 of the rack 100, the locker 320 fixed on the baffle 200 is gradually close to the locker 310 fixed on the rack 100, the locking ring 322 is inserted into the abdicating opening 311a, the power supply cut off by the electromagnet 312a enables the locking column 313 to be only under the action of the spring 312b, the spring 312b recovers elastic deformation when the locking column 313 loses magnetic force action so as to drive the locking column 313 to move along the direction that the two opposite side walls of the abdicating opening 311a are close to or far away from each other, the locking column 313 penetrates through the locking ring 322 in the moving process, so that the locking ring 322 is connected with the locking column 313, and the purpose of locking the baffle 200 is achieved.
In the unlocking process, the electromagnet 312a is powered on, the locking column 313 receives the acting force of the spring 312b and the acting force of the electromagnet 312a at the same time, the elastic force of the spring 312b is opposite to the magnetic attraction force of the electromagnet 312a, the acting force generated by the electromagnet 312a is larger than the acting force of the spring 312b, the locking column 313 moves along the direction that two oppositely-arranged side walls of the abdicating opening 311a are away from each other under the acting force of the electromagnet 312a at the moment, so that the locking column 313 and the locking ring 322 are separated from each other at the moment, and the unlocking purpose is achieved.
It is worth noting that the power-on and the outage of electro-magnet 312a can be controlled through the controller, for the convenient power-on and outage of control electro-magnet 312a the utility model discloses an in the embodiment, this electro-magnet 312a is connected with unmanned aerial vehicle's battery and unmanned aerial vehicle's the equal electricity of main control box, so sets up, not only can realize intelligent control to electro-magnet 312a, but also can simplify unmanned aerial vehicle's overall structure, has saved the setting of the main control board of independent control electro-magnet 312a promptly.
In an embodiment of the present invention, referring to fig. 1, one side of the baffle 200 is fixedly connected to the frame 100 by the connection of the locking device 310 and the locking device 320, and the other side of the baffle 200 can be positioned by friction. Specifically, the frame 100 is further provided with a fixing plate 120 in a protruding manner, the fixing plate 120 and the locking device 310 are respectively disposed on two opposite sides of the notch of the mounting groove 110, one side of the baffle plate 200 abuts against the fixing plate 120, and the other side of the baffle plate 200 is detachably connected to the locking device 310 through a locking device 320. So set up for be connected more firmly between baffle 200 and the frame 100, avoided baffle 200 to drop from frame 100, especially drop from frame 100 when unmanned aerial vehicle's casing 1000 receives the impact.
Further, the surface of the fixing plate 120 abutting against the baffle 200 is provided with a limiting structure, and the limiting structure is used for limiting the baffle 200 to move towards the direction away from the mounting groove 110, that is, the limiting structure limits the baffle 200 to move towards the direction that the groove bottom of the mounting groove 110 is close to or away from the groove opening, so that the baffle 200 is better limited on the rack 100.
It should be noted that, the limiting structure may be a plurality of stopping protrusions 121 protruding from the surface of the fixing plate 120 abutting against the baffle 200, and the stopping protrusions 121 are all abutted against the surface of the baffle 200 facing away from the mounting groove 110 to limit the baffle 200. The position-limiting structure may also be a positioning groove (not shown) concavely disposed on the surface of the fixing plate 120 abutting against the baffle 200, and the positioning groove is inserted into and matched with the side end of the baffle 200 far away from the locking device 320, so as to limit the baffle 200. The limiting structure may be other structures, which are not listed here.
In other embodiments of the present invention, one side of the baffle 200 is fixedly connected to the frame 100 by the connection of the locking device 310 and the locking device 320, and the other side of the baffle 200 can be connected to the frame 100 by the pivot. The pivot may be a hinge, or other structure, not to be taken as an exhaustive list.
In an embodiment of the present invention, please refer to fig. 1, the slot wall of the mounting groove 110 is provided with a plurality of through holes 130 in a penetrating manner, the through holes 130 can communicate the mounting groove 110 with the external atmosphere, and the through holes 130 can be used for heat exchange between the connecting wires and the external atmosphere through the through holes 130, so as to ensure the heat dissipation speed of the battery, avoid the problem that the battery cannot normally work due to the over-high temperature, and reduce the weight of the rack. The through hole 130 also facilitates the manual and quick removal of the battery from the mounting groove 110 when the battery is disassembled.
In an embodiment of the present invention, referring to fig. 1, the surface of the baffle 200 opposite to the mounting groove 110 is provided with a handle 210, and the handle 210 provides a force application point for a user, so as to facilitate the taking and placing of the baffle 200.
It should be noted that, in the embodiments of the present invention, the bottom of the mounting groove 110 may also be disposed through, that is, the mounting groove 110 has two notches, correspondingly, the two baffles 200 are disposed in two, the two baffles 200 are respectively used for covering the notch of the mounting groove 110, and the two baffles 200 are respectively fixedly connected to the frame 100 through the locking device.
The utility model also provides an unmanned aerial vehicle, this unmanned aerial vehicle include unmanned aerial vehicle's battery, unmanned aerial vehicle's main control box and unmanned aerial vehicle's frame, and unmanned aerial vehicle's battery is installed in the mounting groove of main part, and unmanned aerial vehicle's main control box is installed in the surface of main part. This unmanned aerial vehicle's concrete structure refers to above-mentioned embodiment, because this unmanned aerial vehicle has adopted all technical scheme of above-mentioned all embodiments, consequently has all beneficial effects that the technical scheme of above-mentioned embodiment brought at least, no longer gives unnecessary details one by one here.
The above is only the optional embodiment of the present invention, and not therefore the scope of the present invention is limited, all the equivalent structure changes made by the contents of the specification and the drawings are utilized under the inventive concept of the present invention, or the application directly/indirectly in other related technical fields are included in the patent protection scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle's casing, its characterized in that includes:
the surface of the rack can be used for mounting electronic components of the unmanned aerial vehicle, and part of the surface of the rack is concavely provided with a mounting groove for mounting a battery of the unmanned aerial vehicle;
the baffle is used for covering the mounting groove so as to limit the battery of the unmanned aerial vehicle;
the locking assembly comprises a locking device arranged on the rack and a locking device arranged on the baffle, and the locking device is detachably connected with the locking device so as to fixedly connect the baffle with the rack.
2. The unmanned aerial vehicle casing of claim 1, wherein the locking device comprises a locking housing, a locking post and a power member, the locking housing is mounted on the frame, an abdication opening is concavely formed on a surface of the locking housing, the locking post is movably mounted on the locking housing and can move along a direction that two opposite side walls of the abdication opening are close to or far away from each other, and the power member is mounted on the locking housing and is in transmission connection with the locking post;
the locking device comprises a fixing part fixedly connected with the baffle and a locking ring connected with the fixing part, and the locking ring can extend into the abdicating opening to be matched with the locking column.
3. The unmanned aerial vehicle casing of claim 2, wherein the locking post is made of metal material, and a limiting protrusion is arranged on the outer peripheral wall of one end of the locking post;
the locking shell is provided with a containing cavity and a abdicating hole for communicating the containing cavity with the abdicating opening, and one end of the locking column, which is far away from the limiting bulge, extends into the abdicating hole;
the power part comprises an electromagnet and a spring, the electromagnet is installed in the containing cavity and can magnetically adsorb the locking column, the spring is sleeved on the locking column, one end of the spring is abutted to the limiting protrusion, and the other end of the spring is abutted to the outer surface of the locking shell.
4. The chassis of the drone of claim 3, wherein the electromagnet is electrically connected to both the battery of the drone and the main control box of the drone.
5. The unmanned aerial vehicle casing of claim 1, wherein the frame is further provided with a fixing plate in a protruding manner, and the fixing plate and the locking device are respectively arranged on two opposite sides of the notch of the mounting groove;
one side of the baffle is abutted to the fixed plate, and the other side of the baffle is detachably connected with the locking device through the locking device.
6. The unmanned aerial vehicle's casing of claim 5, wherein the surface that the fixed plate and baffle butt is provided with limit structure, limit structure is used for restricting the baffle to move towards the direction that deviates from the mounting groove.
7. The unmanned aerial vehicle's casing of claim 6, wherein, the limit structure is a plurality of stop protrusions convexly provided on the surface of the fixed plate abutting against the baffle; or
The limiting structure is a positioning groove which is concavely arranged on the surface of the fixed plate and abutted to the baffle.
8. The unmanned aerial vehicle's casing of claim 1, wherein the slot wall of the mounting groove is disposed therethrough, forming a plurality of through-holes.
9. The unmanned aerial vehicle's casing of claim 1, wherein the baffle sets up the handle in the surface that faces away from the mounting groove.
10. An unmanned aerial vehicle, characterized in that, including unmanned aerial vehicle's battery, unmanned aerial vehicle's main control box and the unmanned aerial vehicle's casing of any one of claims 1-9, unmanned aerial vehicle's battery is installed in the mounting groove of main part, unmanned aerial vehicle's main control box is installed in the surface of main part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021362461.0U CN212829028U (en) | 2020-07-10 | 2020-07-10 | Unmanned aerial vehicle's casing and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021362461.0U CN212829028U (en) | 2020-07-10 | 2020-07-10 | Unmanned aerial vehicle's casing and unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN212829028U true CN212829028U (en) | 2021-03-30 |
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| CN202021362461.0U Active CN212829028U (en) | 2020-07-10 | 2020-07-10 | Unmanned aerial vehicle's casing and unmanned aerial vehicle |
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| Country | Link |
|---|---|
| CN (1) | CN212829028U (en) |
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- 2020-07-10 CN CN202021362461.0U patent/CN212829028U/en active Active
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