CN217575624U - Unmanned aerial vehicle airport device of uncapping - Google Patents
Unmanned aerial vehicle airport device of uncapping Download PDFInfo
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- CN217575624U CN217575624U CN202220472451.5U CN202220472451U CN217575624U CN 217575624 U CN217575624 U CN 217575624U CN 202220472451 U CN202220472451 U CN 202220472451U CN 217575624 U CN217575624 U CN 217575624U
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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Abstract
The utility model discloses an unmanned aerial vehicle airport cover opening device, in the utility model, if the top covers on both sides are opened, the unmanned aerial vehicle can fly away from the airport to operate, or wait for the unmanned aerial vehicle to return to the airport; when the unmanned aerial vehicle returns to the airport, the top covers on the two sides are closed, so that the unmanned aerial vehicle can be protected; the back is opened to both sides to the top cap, leaves the gap in the middle of top cap and the air park, and the lower air current of washing of unmanned aerial vehicle's screw passes through the gap and discharges to the cabin cover below, can not return the screw top, and difficult formation vortex ring leads to producing the vortex ring effect, has avoided influencing the problem of unmanned aerial vehicle's gesture when unmanned aerial vehicle takes off and descends.
Description
[ technical field ] A method for producing a semiconductor device
The utility model belongs to the technical field of the unmanned aerial vehicle airport, in particular to unmanned aerial vehicle airport device of uncapping.
[ background of the invention ]
The unmanned aerial vehicle is used for operating scenes such as photovoltaic panels, reservoirs, enclosing walls and power transmission lines, is an important point in the application of the current unmanned aerial vehicle industry, and the application of the unmanned aerial vehicle is also a supplement to the operation of the traditional ground robot. With the continuous development of the unmanned aerial vehicle technology, the flexibility and the maneuverability of the unmanned aerial vehicle are gradually irreplaceable, so that the unmanned aerial vehicle is more and more widely applied;
the mode of uncapping for both sides is the form of sliding open at present unmanned aerial vehicle airport, and when unmanned aerial vehicle descended, screw top atmospheric pressure was less than the below, and the downwash air current that the oar dish produced receives sheltering from on ground, receives the low-pressure area attraction of oar dish top simultaneously, produces and rolls up, forms the vortex ring effect easily, and when vortex ring formed, the lift that the screw produced reduced, and no longer is linear relation between lift and the rotational speed, seriously influences unmanned aerial vehicle's attitude control.
In view of this, the utility model discloses in, the back is opened to both sides to the top cap, leaves the gap in the middle of top cap and the air park, and the lower air current of washing of unmanned aerial vehicle's screw passes through the gap and discharges to the cabin cover below, can not return the screw top, is difficult for forming vortex ring, leads to producing the vortex ring effect, has avoided taking off at unmanned aerial vehicle and has influenced the problem of unmanned aerial vehicle's gesture when descending, consequently, this device can become necessary demand for unmanned aerial vehicle airport technical field.
[ Utility model ] content
Defect more than to prior art or improve the demand, along with the continuous development of unmanned aerial vehicle technique, unmanned aerial vehicle's flexibility, mobility is gradually irreplaceable, make unmanned aerial vehicle use more and more extensively, current unmanned aerial vehicle airport mode of uncapping is the form that both sides slide, when unmanned aerial vehicle descends, screw top atmospheric pressure is less than the below, the downwash air current that the oar dish produced receives sheltering from on ground, receive the low-pressure zone attraction of oar dish top simultaneously, produce and roll up, form the vortex ring effect easily, need avoid unmanned aerial vehicle take off and influence the problem of unmanned aerial vehicle gesture because the vortex ring effect when descending.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle airport device of uncapping, includes air park 1, still includes:
the linkage structure is arranged below the parking apron 1, and the linkage structure 4 drives the top cover to open or close;
when the top cover is opened, a preset distance exists between the top cover and the parking apron 1, and the preset distance is used for enabling an airflow circulation space to be formed between the top cover and the parking apron 1.
Preferably, the top cover comprises a first top cover 2 and a second top cover 3, and the first top cover 2 and the second top cover 3 are symmetrically arranged; wherein the first cap 2 and the second cap 3 open in opposite directions when open and the first cap 2 and the second cap 3 close in opposite directions when closed.
Preferably, the linkage structure 4 includes a first linkage assembly 41 and a second linkage assembly 42, the first linkage assembly 41 and the second linkage assembly 42 are symmetrically arranged and are respectively connected with the first top cover 2 and the second top cover 3;
wherein, the first linkage assembly 41 and the second linkage assembly 42 are respectively used for driving the first top cover 2 and the second top cover 3 to open and close.
Preferably, the linkage structure 4 further includes a first fixed plate assembly 43 and a second fixed plate assembly 44, the first fixed plate assembly 43 and the second fixed plate assembly 44 are symmetrically disposed, and the first fixed plate assembly 43 and the second fixed plate assembly 44 are used for supporting the first linkage assembly 41 and the second linkage assembly 42.
Preferably, the first linkage assembly 41 includes a first connecting rod 411, a second connecting rod 412, a first transmission assembly 413, a first motor 414, a first worm gear 415 and a second transmission assembly 416;
one end of the first connecting rod 411 is connected with one end of the first top cover 2, and the other end of the first connecting rod 411 is connected with the first transmission component 413; one end of the second connecting rod 412 is connected with the other end of the first top cover 2, and the other end of the second connecting rod 412 is connected with the second transmission assembly 416; two ends of the first worm gear 415 are respectively connected with the first transmission component 413 and the second transmission component 416; the first motor 414 is connected to the first worm gear 415 for driving the first worm gear 415 so as to link the first link 411 and the second link 412 to drive the first top cover 2 to open or close.
Preferably, the second linkage assembly 42 includes a third link 421, a fourth link 422, a third transmission assembly 423, a second motor 424, a second worm gear 425 and a fourth transmission assembly 426;
one end of the third connecting rod 421 is connected to one end of the second top cover 3, and the other end of the third connecting rod 421 is connected to the third transmission assembly 423; one end of the fourth connecting rod 422 is connected with the other end of the second top cover 3, and the other end of the fourth connecting rod 422 is connected with the fourth transmission assembly 426; the two ends of the second worm gear 425 are respectively connected with the third transmission assembly 423 and the fourth transmission assembly 426; the second motor 424 is connected to the second worm gear 425 for driving the second worm gear 425 to link the third link 421 and the fourth link 422 to drive the second top cover 3 to open or close.
Preferably, the first fixed plate assembly 43 and the second fixed plate assembly 44 further include:
the first fixing plate assembly 43 comprises a first fixing plate 431 and a second fixing plate 432, and the first fixing plate 431 and the second fixing plate 432 are arranged in a flush manner; the first transmission assembly 413 and the third transmission assembly 423 are respectively fixed between the interlayers at two ends of the first fixing plate 431 and the second fixing plate 432; the first fixing plate 431 and the second fixing plate 432 are used for fixing the first transmission assembly 413 and the third transmission assembly 423 on the same plane;
the second fixing plate assembly 44 includes a third fixing plate 441 and a fourth fixing plate 442, and the third fixing plate 441 and the fourth fixing plate 442 are arranged in parallel; the second transmission assembly 416 and the fourth transmission assembly 426 are respectively fixed between the interlayers at the two ends of the first fixing plate 441 and the second fixing plate 442; the third fixing plate 441 and the fourth fixing plate 442 are used for fixing the second transmission assembly 416 and the fourth transmission assembly 426 on the same plane;
the first fixing plate 431, the second fixing plate 432, the third fixing plate 441 and the fourth fixing plate 442 are used for fixing the first transmission assembly 413, the second transmission assembly 416, the third transmission assembly 423 and the fourth transmission assembly 426 on the same horizontal plane.
Preferably, after the top cover is opened, the opening angle of the first top cover 2 and the second top cover 3 is a preset angle.
Preferably, a peripheral plate 5 and a bottom plate 6 are arranged below the apron 1.
Preferably, the bottom plate 6 cooperates with the peripheral plate 5 to form a receiving space.
The utility model provides an unmanned aerial vehicle airport device of uncapping, the back is opened to both sides to the top cap, leaves the gap in the middle of top cap and the air park, and the lower air current of washing of unmanned aerial vehicle's screw passes through the gap and discharges to the cabin cover below, can not return the screw top, and difficult formation vortex ring leads to producing the vortex ring effect, has avoided influencing the problem of unmanned aerial vehicle's gesture when unmanned aerial vehicle takes off and descends.
[ description of the drawings ]
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the embodiments of the present invention will be briefly described below. It is obvious that the drawings described below are only some embodiments of the invention, and that for a person skilled in the art, other drawings can be derived from them without inventive effort.
Fig. 1 is a schematic view of the lifting of an unmanned aerial vehicle when the unmanned aerial vehicle airport cover opening device of the utility model is opened;
fig. 2 is a schematic diagram of the unmanned aerial vehicle airport cover opening device of the present invention when opened;
fig. 3 is a schematic diagram of the internal device of the unmanned aerial vehicle airport cover opening device when the unmanned aerial vehicle airport cover opening device is opened;
fig. 4 is a schematic diagram of the unmanned aerial vehicle airport cover opening device of the present invention when closed;
fig. 5 is a top view of the unmanned aerial vehicle airport cover opening device of the present invention;
fig. 6 is a bottom view of the unmanned aerial vehicle airport cover opening device of the present invention;
fig. 7 is a schematic structural view of the linkage structure of the unmanned aerial vehicle airport cover opening device of the present invention;
fig. 8 is a schematic structural diagram of a first linkage assembly of the unmanned aerial vehicle airport cover opening device of the present invention;
fig. 9 is a schematic structural diagram of a second linkage assembly of the unmanned aerial vehicle airport cover opening device of the present invention;
fig. 10 is an exploded view of a first fixed plate assembly of an unmanned aerial vehicle airport door opening device of the present invention;
fig. 11 is an exploded view of a second fixing plate of the unmanned aerial vehicle airport cover opening device of the present invention;
in all the figures, the reference numerals are as follows:
1-apron; 2-a first cap; 3-a second top cover; 4-linkage structure; 5-peripheral plate; 6-a bottom plate;
41-a first linkage assembly; 42-a second linkage assembly; 43-a first fixed plate assembly; 44 a second fixed plate assembly;
411-a first link; 412-a second link; 413-a first transmission assembly; 414-a first motor; 415-a first worm gear; 416-a second transmission assembly;
421-a third link; 422-fourth link; 423-a third transmission assembly; 424-a second motor; 425-a second worm gear; 426-a fourth transmission assembly;
431-a first fixing plate; 432-a second fixation plate; 441-a third fixing plate; 442-fourth fixing plate.
[ detailed description ] embodiments
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
In the description of the present invention, the terms "inside", "outside", "longitudinal", "lateral", "up", "down", "top", "bottom", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for convenience of describing the present invention but do not require that the present invention must be constructed and operated in a particular orientation, and thus should not be construed as limiting the present invention.
Furthermore, the technical features mentioned in the embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.
Example 1:
the embodiment of the utility model provides an unmanned aerial vehicle airport device of uncapping, a serial communication port, including air park 1, still include:
the linkage structure is arranged below the parking apron 1, and the linkage structure 4 drives the top cover to open or close;
when the top cover is opened, a preset distance exists between the top cover and the parking apron 1, and the preset distance is used for enabling an airflow circulation space to be formed between the top cover and the parking apron 1.
As shown in fig. 1-6, the apron 1 is used for supporting the placement of the drone and providing a parking space for the drone; the linkage structure 4 is positioned below the air park 1 and arranged around the air park 1, and does not occupy the space when the unmanned aerial vehicle is parked; the linkage structure 4 is connected with the top cover, a motor in the linkage structure 4 drives the linkage structure according to a background instruction, the background instruction is set by a person skilled in the art by himself, and the protection range of the utility model is not limited, so that the top cover is controlled to be opened and closed;
in the prior art, the top cover of the unmanned aerial vehicle airport is opened in a sliding mode from two sides, no gap exists between the top cover and the machine halt, when the unmanned aerial vehicle in the unmanned aerial vehicle needs to land, after the top cover is opened, no gap communicated with the outside exists in a certain range around the unmanned aerial vehicle in the unmanned aerial vehicle, an airflow circulation space is formed, the air pressure above the propeller is lower than that below the propeller, downwash airflow generated by the propeller disc is shielded by the ground and is simultaneously attracted by a low-pressure area above the propeller disc to generate upward rolling, a vortex ring effect is easily formed, when a vortex ring is formed, the lift force generated by the propeller is reduced, the lift force and the rotating speed are not in a linear relation any more, and the attitude control of the unmanned aerial vehicle is seriously influenced;
the utility model discloses in, the back can be left between top cap and the air park 1 to the top cap at the unmanned aerial vehicle airport after opening completely, preset distance is set for by oneself according to actual conditions by technical personnel in the field, can avoid unmanned aerial vehicle to take off or produce the vortex ring effect when descending can, here should not restrict the utility model discloses protection range.
The top covers comprise a first top cover 2 and a second top cover 3, and the first top cover 2 and the second top cover 3 are symmetrically arranged; wherein the first and second caps 2, 3 open in opposite directions when open and the first and second caps 2, 3 close in opposite directions when closed.
In order to ensure that the space required by the unmanned aerial vehicle airport is the minimum when the unmanned aerial vehicle airport is opened and closed, the top covers are arranged into a first top cover 2 and a second top cover 3, the first top cover 2 and the second top cover 3 are the same in size and shape and are symmetrically arranged, the first top cover 2 and the second top cover 3 are both concave towards the inside of the unmanned aerial vehicle airport and convex towards the outside of the unmanned aerial vehicle airport, the placing space of the unmanned aerial vehicle at the unmanned aerial vehicle airport is further maximized, when the unmanned aerial vehicle airport is opened, the first top cover 2 and the second top cover 3 are opened in opposite directions, and when the top covers are completely opened, the distance between the first top cover 2 and the second top cover 3 is larger than the length of the unmanned aerial vehicle, or the distance is set by a person skilled in the art;
since the top cover includes the first top cover 2 and the second top cover 3, the first top cover 2 and the second top cover 3 need to use two linkage structures to control the opening and closing of the first top cover 2 and the second top cover 3, respectively, and therefore the embodiment further includes the following preferred design:
as shown in fig. 7, the linkage structure 4 includes a first linkage assembly 41 and a second linkage assembly 42, the first linkage assembly 41 and the second linkage assembly 42 are symmetrically disposed and are respectively connected to the first top cover 2 and the second top cover 3;
wherein, the first linkage assembly 41 and the second linkage assembly 42 are respectively used for driving the first top cover 2 and the second top cover 3 to open and close.
The first top cover 2 and the second top cover 3 are controlled by different linkage structures, because the first top cover 2 and the second top cover 3 are identical in size and shape and symmetrically arranged and operate in the same manner, the linkage structure 4 is also divided into a first linkage assembly 41 and a second linkage assembly 42 which are symmetrically arranged, the first linkage assembly 41 and the second linkage assembly 42 are identical in shape and size, the first linkage assembly 41 controls the first top cover 2, and the second linkage assembly 42 controls the second top cover 3.
the linkage structure 4 further comprises a first fixed plate assembly 43 and a second fixed plate assembly 44, the first fixed plate assembly 43 and the second fixed plate assembly 44 are symmetrically arranged, and the first fixed plate assembly 43 and the second fixed plate assembly 44 are used for supporting the first linkage assembly 41 and the second linkage assembly 42.
The first linkage assembly 41 and the second linkage assembly 42 are fixedly combined by the first fixing plate assembly 43 and the second fixing plate assembly 44, wherein the first linkage assembly 41, the first fixing plate assembly 43, the second linkage assembly 42 and the second fixing plate assembly 44 are sequentially connected, and finally the second fixing plate assembly 44 is connected with the first linkage assembly 41 to form a closed loop, wherein when the first linkage assembly 41, the first fixing plate assembly 43, the second linkage assembly 42 and the second fixing plate assembly 44 are connected, an angle between two adjacent assemblies is 90 degrees, a fixing part exists on the surface of the first fixing plate assembly 43 and the second fixing plate assembly 44 for fixing the linkage structure 4 on the peripheral plate 5, the fixing part may specifically be provided with screw holes on the first fixing plate assembly 43 and the second fixing plate assembly 44, and the first fixing plate assembly 43 and the second fixing plate assembly 44 are fixedly combined with the peripheral plate 5 by using screws, or the fixing part may be designed by a person skilled in the art according to an actual situation, and may achieve the effect of fixing the first fixing plate assembly 43 and the second fixing plate assembly 44 on the peripheral plate 5 by itself.
When the top cover is opened or closed, the first top cover 2 and the second top cover 3 need to be kept parallel to the state when the top cover is closed in the movement process regardless of vertical movement or parallel movement, so that the stability of the top cover in the opening or closing process is ensured, and the unmanned aerial vehicle is prevented from colliding with the top cover when taking off or landing; simultaneously opening and closing of top cap is automatic operation and need not manually, consequently, the utility model discloses still relate to following preferred design:
as shown in fig. 8, the first linkage assembly 41 includes a first link 411, a second link 412, a first transmission assembly 413, a first motor 414, a first worm gear 415 and a second transmission assembly 416;
one end of the first connecting rod 411 is connected with one end of the first top cover 2, and the other end of the first connecting rod 411 is connected with the first transmission component 413; one end of the second connecting rod 412 is connected with the other end of the first top cover 2, and the other end of the second connecting rod 412 is connected with the second transmission component 416; two ends of the first worm 415 are respectively connected with the first transmission assembly 413 and the second transmission assembly 413; the first motor 414 is connected to the first worm gear 415 for driving the first worm gear 415 so as to link the first link 411 and the second link 412 to drive the first top cover 2 to open or close.
As shown in fig. 9, the second linkage assembly 42 includes a third link 421, a fourth link 422, a third transmission assembly 423, a second motor 424, a second worm gear 425 and a fourth transmission assembly 426;
one end of the third connecting rod 421 is connected to one end of the second top cover 3, and the other end of the third connecting rod 421 is connected to the third transmission assembly 423; one end of the fourth connecting rod 422 is connected with the other end of the second top cover 3, and the other end of the fourth connecting rod 422 is connected with the fourth transmission component 426; the two ends of the second worm gear 425 are respectively connected with the third transmission assembly 423 and the fourth transmission assembly 426; the second motor 424 is connected to the second worm gear 425 for driving the second worm gear 425 to link the third link 421 and the fourth link 422 to drive the second top cover 3 to open or close.
When the first connecting rod 411, the second connecting rod 412, the third connecting rod 421 and the fourth connecting rod 422 further include two branch connecting rods, the two branch connecting rods are arranged in parallel and connected to the back of one side of the first top cover 2 or the second top cover 3; when the other end of the branch connecting rod is fixed and does not move, the top cover cannot rotate around the direction perpendicular to the connecting rod as an axis, so when the first linkage assembly 41 and the second linkage assembly 42 are connected with the top cover by using two or more than two connecting rods, the first top cover 2 and the second top cover 3 can be ensured to be parallel to the state when the top cover is closed in the process of moving regardless of vertical movement or parallel movement.
The two branch connecting rods are connected with each other through the transmission assembly, so that one transmission assembly further comprises a driving wheel and a driven wheel, the driving wheel is connected with one of the two branch connecting rods, and the driven wheel is connected with the other of the two branch connecting rods; in order to keep the two branch connecting rods parallel all the time in the moving process, the moving rates of the two branch connecting rods need to be kept consistent, so that the circumferences of a driving wheel and a driven wheel in the transmission assembly are consistent.
The first worm gear 415 and the second worm gear 425 both have a self-locking function, and when the first worm gear 415 and the second worm gear 425 operate to a certain state, the operation is stopped, so that the first top cover 2 and the second top cover 3 are opened to a certain extent or completely closed; the self-locking state of the first worm gear 415 and the second worm gear 425 is set by a person skilled in the art, and the scope of the present invention should not be limited herein.
The first connecting rod 411, the second connecting rod 412, the third connecting rod 421 and the fourth connecting rod 422 are movably connected with other parts.
Since the first fixing plate assembly 43 and the second fixing plate assembly 44 are used for fixing and connecting the first linkage assembly 41 and the second linkage assembly 42, the first transmission assembly 413, the second transmission assembly 416, the third transmission assembly 423 and the fourth transmission wheel 426 are required to be fixedly arranged on the first fixing plate assembly 43 or the second fixing plate assembly 44, therefore, the present invention also relates to the following preferred design:
as shown in fig. 10 and 11, the first fixed plate assembly 43 and the second fixed plate assembly 44 further include:
the first fixing plate assembly 43 comprises a first fixing plate 431 and a second fixing plate 432, and the first fixing plate 431 and the second fixing plate 432 are arranged in a flush manner; the first transmission assembly 413 and the third transmission assembly 423 are respectively fixed between the interlayers at two ends of the first fixing plate 431 and the second fixing plate 432; the first fixing plate 431 and the second fixing plate 432 are used for fixing the first transmission assembly 413 and the third transmission assembly 423 on the same plane;
the second fixing plate assembly 44 includes a third fixing plate 441 and a fourth fixing plate 442, and the third fixing plate 441 and the fourth fixing plate 442 are arranged in parallel; the second transmission assembly 416 and the fourth transmission assembly 426 are respectively fixed between the interlayers at the two ends of the first fixing plate 441 and the second fixing plate 442; the third fixing plate 441 and the fourth fixing plate 442 are used for fixing the second transmission assembly 416 and the fourth transmission assembly 426 on the same plane;
the first fixing plate 431, the second fixing plate 432, the third fixing plate 441 and the fourth fixing plate 442 are used for fixing the first transmission assembly 413, the second transmission assembly 416, the third transmission assembly 423 and the fourth transmission assembly 426 on the same horizontal plane.
Since the four transmission assemblies are required to be fixed on the same horizontal plane to ensure that the first linkage assembly 41 and the second linkage assembly 42 are on the same horizontal plane, and further ensure that the first top cover 2 and the second top cover 3 are on the same horizontal plane in the closed state, if only one fixing plate is present in each fixing plate assembly, the transmission assemblies are not sufficiently fixed, and therefore, each of the first fixing plate assembly 43 and the second fixing plate assembly 44 includes at least two fixing plates; the first transmission assembly 413 is disposed at a first preset position of two fixed plates of the first fixed plate assembly 43, a third transmission assembly 423 is disposed at a second preset position of two fixed plates of the first fixed plate assembly 43, and the first transmission assembly 413 and the third transmission assembly 423 are disposed between the two fixed plate interlayers to fix the first transmission assembly 413 and the third transmission assembly 423; arranging the second transmission assembly 416 at a third preset position of the two fixed plates of the second fixed plate assembly 44, arranging a fourth transmission assembly 426 at a fourth preset position of the two fixed plates of the second fixed plate assembly 44, and arranging the second transmission assembly 416 and the fourth transmission assembly 426 between the two fixed plate interlayers to fix the second transmission assembly 416 and the fourth transmission assembly 426; the first preset position, the second preset position, the third preset position and the fourth preset position are all designed by a person skilled in the art according to actual situations, so that the first transmission assembly 413, the second transmission assembly 416, the third transmission assembly 423 and the fourth transmission assembly 426 are ensured to be located on the same horizontal plane;
in order to ensure that the apron 1 is horizontally disposed, the first fixing plate assembly 43 is disposed flush with the second fixing plate assembly 44, and the apron 1 is disposed on the first fixing plate assembly 43 and the second fixing plate assembly 44, so that the distance between the first fixing plate assembly 43 and the second fixing plate assembly 44 should be smaller than the length or width of the apron 1.
Because first top cap 2 and second top cap 3 are when opening completely, first top cap 2 with second top cap 3 all with parking apron 1 has certain clearance, consequently, the utility model discloses still relate to following preferred design:
after the top cover is opened, the opening angle of the first top cover 2 and the second top cover 3 is a preset angle.
In order to guarantee first top cap 2 with second top cap 3 opens the back unmanned aerial vehicle safely and has enough space to come in and go out, consequently first top cap 2 with the angle that second top cap 3 was opened is for predetermineeing the angle, predetermine the angle and be greater than 90 degrees, perhaps predetermine the angle and reserve the air current flow space and come from the design of going when descending for unmanned aerial vehicle by technical personnel according to unmanned aerial vehicle size and needs, here should not restrict the utility model discloses a protection scope.
The utility model discloses an inside periphery and the bottom in unmanned aerial vehicle airport need be protected and external the isolation, consequently the utility model discloses still relate to following preferred method:
a peripheral plate 5 and a bottom plate 6 are arranged below the parking apron 1; the bottom plate 6 cooperates with the peripheral plate 5 to form a receiving space.
The storage space is used for storing connecting wires for the motor and can also store spare parts or maintenance tools of the unmanned aerial vehicle.
Example 2:
the embodiment of the utility model provides an unmanned aerial vehicle airport device of uncapping is provided, embodiment 1 is compared to this embodiment and is followed unmanned aerial vehicle and fly from the airport and demonstrate the utility model discloses a use method.
In the embodiment, the opening angle of the top cover of the unmanned aerial vehicle airport is 100 degrees;
when the unmanned aerial vehicle does not need to take off from the unmanned aerial vehicle airport, the first top cover 2 and the second top cover 3 are in a closed state;
when the unmanned aerial vehicle needs to take off, the motor drives the first top cover 2 and the second top cover 3 to open the top cover of the unmanned aerial vehicle airport;
the motor 414 in the first linkage assembly 41 drives the first worm gear 415 in the first linkage assembly 41 to operate, the first worm gear 415 in the first linkage assembly 41 is linked with the first connecting rod 411 and the second connecting rod 412 in the first linkage assembly 41, and the first connecting rod 411 and the second connecting rod 412 in the first linkage assembly 41 drive the first top cover 2 to open; a motor 424 in the second linkage assembly 42 drives a second worm gear 425 in the second linkage assembly 42 to operate, the second worm gear 425 in the second linkage assembly 42 and a third connecting rod 421 and a fourth connecting rod 422 in the second linkage assembly 42 form linkage, and the third connecting rod 421 and the fourth connecting rod 422 in the second linkage assembly 42 drive the second top cover 3 to open;
when first top cap 2 with the second top cap 3 opening angle all reaches 100 degrees, unmanned aerial vehicle airport top cap is opened completely, and unmanned aerial vehicle takes off and leaves the airport.
Example 3:
the embodiment of the utility model provides an unmanned aerial vehicle airport device of uncapping is provided, embodiment 1 is compared to this embodiment and is demonstrateed from unmanned aerial vehicle descending from the airport the utility model discloses a use method.
In the embodiment, the opening angle of the top cover of the unmanned aerial vehicle airport is 95 degrees;
when the unmanned aerial vehicle takes off and is not placed in an unmanned aerial vehicle airport, the first top cover 2 and the second top cover 3 are in an opening state, and the opening angle is 95 degrees;
when the unmanned aerial vehicle needs to land, the unmanned aerial vehicle is positioned and lands in the unmanned aerial vehicle airport, airflow generated by a propeller of the unmanned aerial vehicle circulates from a gap between the top cover and the parking apron 1, and when the unmanned aerial vehicle stably lands at a designated position of the unmanned aerial vehicle airport and stops running, the motor drives the first top cover 2 and the second top cover 3 to close the top cover of the unmanned aerial vehicle airport;
the motor 414 in the first linkage assembly 41 drives the first worm and gear 415 in the first linkage assembly 41 to operate, the first worm and gear 415 in the first linkage assembly 41 is linked with the first connecting rod 411 and the second connecting rod 412 in the first linkage assembly 41, and the first connecting rod 411 and the second connecting rod 412 in the first linkage assembly 41 drive the first top cover 2 to close; a motor 424 in the second linkage assembly 42 drives a second worm gear 425 in the second linkage assembly 42 to operate, the second worm gear 425 in the second linkage assembly 42 and a third connecting rod 421 and a fourth connecting rod 422 in the second linkage assembly 42 form linkage, and the third connecting rod 421 and the fourth connecting rod 422 in the second linkage assembly 42 drive the second top cover 3 to close;
when the first top cover 2 and the second top cover 3 are operated inwards and rotated by 95 degrees, the first top cover 2 and the second top cover 3 are completely closed.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle airport device of uncapping which characterized in that includes air park (1), still includes:
the linkage structure comprises a top cover arranged above the parking apron (1) and a linkage structure arranged below the parking apron (1), wherein the linkage structure (4) drives the top cover to open or close;
when the top cover is opened, a preset distance exists between the top cover and the parking apron (1), and the preset distance is used for enabling an airflow circulation space to be formed between the top cover and the parking apron (1).
2. The unmanned aerial vehicle airport cover opening device of claim 1, wherein the roof comprises a first roof (2) and a second roof (3), the first roof (2) and the second roof (3) being symmetrically arranged; wherein the first (2) and second (3) caps open in opposite directions when open, and the first (2) and second (3) caps close in opposite directions when closed.
3. The unmanned aerial vehicle airport cover opening device of claim 2, wherein the linkage structure (4) comprises a first linkage assembly (41) and a second linkage assembly (42), the first linkage assembly (41) and the second linkage assembly (42) are symmetrically arranged and are respectively connected with the first top cover (2) and the second top cover (3);
wherein the first linkage assembly (41) and the second linkage assembly (42) are respectively used for driving the first top cover (2) and the second top cover (3) to open and close.
4. The unmanned aerial vehicle airport door opener of claim 3, wherein the linkage structure (4) further comprises a first fixed plate assembly (43) and a second fixed plate assembly (44), the first fixed plate assembly (43) and the second fixed plate assembly (44) are symmetrically arranged, and the first fixed plate assembly (43) and the second fixed plate assembly (44) are used for supporting the first linkage assembly (41) and the second linkage assembly (42).
5. The unmanned aerial vehicle airport door opener of claim 4, wherein the first linkage assembly (41) comprises a first link (411), a second link (412), a first transmission assembly (413), a first motor (414), a first worm gear (415), and a second transmission assembly (416);
one end of the first connecting rod (411) is connected with one end of the first top cover (2), and the other end of the first connecting rod (411) is connected with the first transmission component (413); one end of the second connecting rod (412) is connected with the other end of the first top cover (2), and the other end of the second connecting rod (412) is connected with the second transmission assembly (416); two ends of the first worm gear (415) are respectively connected with the first transmission component (413) and the second transmission component (416); the first motor (414) is connected with the first worm gear (415) and used for driving the first worm gear (415) so as to link the first connecting rod (411) and the second connecting rod (412) to drive the first top cover (2) to open or close.
6. The unmanned aerial vehicle airport door opener of claim 5, wherein the second linkage assembly (42) comprises a third link (421), a fourth link (422), a third transmission assembly (423), a second motor (424), a second worm gear (425), and a fourth transmission assembly (426);
one end of the third connecting rod (421) is connected with one end of the second top cover (3), and the other end of the third connecting rod (421) is connected with the third transmission component (423); one end of the fourth connecting rod (422) is connected with the other end of the second top cover (3), and the other end of the fourth connecting rod (422) is connected with the fourth transmission component (426); two ends of the second worm gear (425) are respectively connected with the third transmission assembly (423) and the fourth transmission assembly (426); the second motor (424) is connected with the second worm gear (425) and used for driving the second worm gear (425) to link the third connecting rod (421) with the fourth connecting rod (422) to drive the second top cover (3) to open or close.
7. The unmanned aerial vehicle airport door opener of claim 6, wherein the first and second fixed plate assemblies (43, 44) further comprise:
the first fixing plate assembly (43) comprises a first fixing plate (431) and a second fixing plate (432), and the first fixing plate (431) and the second fixing plate (432) are arranged in a flush manner; wherein the first transmission assembly (413) and the third transmission assembly (423) are respectively fixed between the interlayers at two ends of the first fixing plate (431) and the second fixing plate (432); the first fixing plate (431) and the second fixing plate (432) are used for fixing the first transmission assembly (413) and the third transmission assembly (423) on the same plane;
the second fixing plate assembly (44) comprises a third fixing plate (441) and a fourth fixing plate (442), and the third fixing plate (441) and the fourth fixing plate (442) are arranged in a flush manner; wherein the second transmission assembly (416) and the fourth transmission assembly (426) are respectively fixed between the interlayers at two ends of the first fixing plate (431) and the second fixing plate (432); the third fixing plate (441) and the fourth fixing plate (442) are used for fixing the second transmission assembly (416) and the fourth transmission assembly (426) on the same plane;
the first fixing plate (431), the second fixing plate (432), the third fixing plate (441) and the fourth fixing plate (442) are used for fixing the first transmission assembly (413), the second transmission assembly (416), the third transmission assembly (423) and the fourth transmission assembly (426) on the same horizontal plane.
8. An unmanned aerial vehicle airport cover opening device as claimed in claim 3, wherein the angle at which the first roof (2) and the second roof (3) are opened is a predetermined angle when the roof is opened.
9. The unmanned aerial vehicle airport cover opening device of claim 1, wherein a peripheral plate (5) and a bottom plate (6) are arranged below the apron (1).
10. Unmanned aerial vehicle airport door opener according to claim 9, wherein the bottom plate (6) cooperates with the peripheral plate (5) to form a receiving space.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220472451.5U CN217575624U (en) | 2022-03-03 | 2022-03-03 | Unmanned aerial vehicle airport device of uncapping |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220472451.5U CN217575624U (en) | 2022-03-03 | 2022-03-03 | Unmanned aerial vehicle airport device of uncapping |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217575624U true CN217575624U (en) | 2022-10-14 |
Family
ID=83538598
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220472451.5U Active CN217575624U (en) | 2022-03-03 | 2022-03-03 | Unmanned aerial vehicle airport device of uncapping |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217575624U (en) |
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2022
- 2022-03-03 CN CN202220472451.5U patent/CN217575624U/en active Active
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