CN216275289U - Power inspection unmanned aerial vehicle descending nest equipment - Google Patents
Power inspection unmanned aerial vehicle descending nest equipment Download PDFInfo
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- CN216275289U CN216275289U CN202122559684.7U CN202122559684U CN216275289U CN 216275289 U CN216275289 U CN 216275289U CN 202122559684 U CN202122559684 U CN 202122559684U CN 216275289 U CN216275289 U CN 216275289U
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Abstract
The utility model discloses a nest device for landing of an electric power inspection unmanned aerial vehicle, which comprises a base platform, a liftable support column arranged at the bottom of the base platform and a rainy day protection cover arranged on the surface of the base platform; the rainy-day protective cover comprises a plurality of cambered-surface shed sheets, a base, hemispherical awning cloth, a driving assembly and other structures; above-mentioned unmanned aerial vehicle is patrolled and examined to electric power descends and uses quick-witted nest equipment, and it has supplementary unmanned aerial vehicle safety descending, prevents wind and rain's function, can ensure its reliable safe use in rugged environment to unmanned aerial vehicle patrols and examines efficiency indirectly has been ensured.
Description
Technical Field
The utility model relates to the technical field of power inspection, in particular to a nest device for landing of an unmanned aerial vehicle for power inspection.
Background
Along with the development of laser radar technology, the unmanned aerial vehicle carries on laser radar system operation and becomes the new means of electric power inspection gradually. Researchers find that using unmanned aerial vehicle to carry out power inspection has the technical advantages of safety, high efficiency, low personnel operation cost and the like in many aspects.
However, researchers find that the landing of the unmanned aerial vehicle and the function of a landing platform of the unmanned aerial vehicle are still hot problems of the landing of the unmanned aerial vehicle; particularly, under the severe environment of wind and rain, the traditional ground landing platform is easily influenced by rainwater, and the safe landing of the unmanned aerial vehicle is influenced by the accumulated water of the platform, the sliding of the platform and the like; of course, if the unmanned aerial vehicle lands on uneven ground, the road is muddy, and other problems, the unmanned aerial vehicle can also bring difficulty to the landing, and unnecessary loss can be caused by improper landing.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a nest device for landing of an electric power inspection unmanned aerial vehicle, and the nest device is used for solving the problems.
In order to achieve the purpose, the technical scheme of the utility model is realized as follows:
the utility model provides a nest device for landing of an electric power inspection unmanned aerial vehicle, which comprises a base platform, a lifting support column arranged at the bottom of the base platform and a rainy day protection cover arranged on the surface of the base platform; landing identification marks are arranged on the surface of the basic platform;
the rainy-day protective cover is a hemispherical protective cover and comprises a plurality of cambered-surface shed sheets, a base, hemispherical tarpaulin and a driving assembly; the base is arranged on the surface of the base platform; the cambered surfaces of the cambered surface shed sheets are connected along the inner wall surface of the awning cloth in a sticking way according to the surface of the hemispherical awning cloth, and the cambered surface shed sheets are arranged at intervals along the surface latitude line of the hemispherical awning cloth; the driving component is a servo driving motor;
the base comprises a base body, a bearing seat arranged at the upper part of the base body and a bearing arranged at the bearing seat; inserting shafts are arranged at two ends of the cambered surface shed sheet positioned in the middle of the cambered surface shed sheets, and an output shaft of the servo driving motor is inserted into a bearing hole formed by a bearing of the bearing block to realize rotating fit; and the output shaft of the servo drive motor is coaxially and rotatably connected (in key connection) with the plug shaft and is used for driving the cambered shed sheet positioned in the middle position to rotate by taking a connecting line between the two bases as an axis.
Preferably, as one possible embodiment; a slide way, a slide block and a linear motor are also arranged in the interlayer of the basic platform; an extension auxiliary landing plate is arranged on the surface of the basic platform; the output end of the linear motor is fixedly connected with the sliding block, the top surface of the sliding block is higher than the plane of the basic platform, and the extension auxiliary landing plate is detachably connected to the top surface of the sliding block; the linear motor is used for driving the extension auxiliary landing plate to freely stretch and slide in the extension direction of the slide way.
Preferably, as one possible embodiment; the surface of the extension auxiliary landing plate is also provided with the landing identification mark.
Preferably, as one possible embodiment; the surface of the extension auxiliary landing plate is also provided with an anti-skid cushion layer; the anti-skid cushion layer is divided into three layers from top to bottom, and sequentially comprises a first cushion layer, a supporting layer and a base layer; the first cushion layer is a rubber wear-resistant cushion layer; the supporting layer is a steel bar mesh; the base layer is a concrete base layer.
Preferably, as one possible embodiment; the surface of the rubber wear-resistant cushion layer is also coated with a hydrophobic coating.
Preferably, as one possible embodiment; in the structure of the cambered surface shed sheets, a heavy-weight structural member is arranged at the highest position point of the cambered surface shed sheet positioned in the middle; the heavy weight structural member is connected with the highest position point of the cambered surface shed sheet through a rope; the heavy weight structural part is of a cone structure.
Preferably, as one possible embodiment; the heavy weight structure part is detachably connected with the rope.
Preferably, as one possible embodiment; the tarpaulin in the rainy day safety cover is transparent tarpaulin.
Preferably, as one possible embodiment; an air dryer is further arranged on the surface of the basic platform; and the air outlet of the air dryer faces to the surface of the basic platform.
Preferably, as one possible embodiment; the surface of the basic platform is also provided with a solar photovoltaic panel and a storage battery pack; the solar photovoltaic panel is electrically connected with the storage battery pack, and the storage battery pack is electrically connected with the driving assembly.
Compared with the prior art, the embodiment of the utility model has the advantages that:
the utility model provides a nest device for landing of an electric power inspection unmanned aerial vehicle, which can be known by analyzing the main technical contents as follows: the nest equipment for descending the electric power inspection unmanned aerial vehicle mainly comprises a basic platform, a liftable support column, a rainy day protective cover and other mechanisms, wherein the rainy day protective cover is arranged on the surface of the basic platform; a landing identification mark is arranged on the basic platform; the rainy-day protective cover is a hemispherical protective cover and comprises a plurality of cambered-surface shed sheets, a base, hemispherical tarpaulin and a driving assembly; the base is arranged on the surface of the base platform; the cambered surfaces of the cambered surface shed sheets are connected along the inner wall surface of the awning cloth in a sticking way according to the surface of the hemispherical awning cloth, and the cambered surface shed sheets are arranged at intervals along the surface latitude line of the hemispherical awning cloth; the base comprises a base body, a bearing seat arranged at the upper part of the base body and a bearing arranged at the bearing seat; inserting shafts are arranged at two ends of the cambered surface shed sheet positioned in the middle of the cambered surface shed sheets, and an output shaft of the servo driving motor is inserted into a bearing hole formed by a bearing of the bearing block to realize rotating fit; the driving component is a servo driving motor, and the output shaft of the servo driving motor is coaxially and rotatably connected (in key connection) with the plug shaft and is used for driving the cambered surface shed sheet positioned in the middle position to rotate by taking a connecting line between the two bases as an axis.
When specifically using, can close the rainy day safety cover and carry out rain-proof protection to equipment and the basic platform on its basic platform when meetting rainy weather, avoid ponding on its basic platform, avoid basic platform surface slip influence to descend. Meanwhile, the cambered surface shed sheet at the middle position can be driven to rotate freely by the driving assembly, however, the axis of the rotation motion is a virtual line, namely, the rotation motion is performed by taking the connecting line between the two bases as the axis, so that the hemispherical protective cover is ensured to realize the motions of unfolding, opening, closing and closing.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and other drawings can be obtained by those skilled in the art without creative efforts.
Fig. 1 is a schematic perspective view of a nest device for landing of an electric inspection unmanned aerial vehicle according to a first embodiment of the present invention;
FIG. 2 is a partially enlarged schematic view of FIG. 1;
fig. 3 is a schematic perspective structural view of a nest device for landing of an electric inspection unmanned aerial vehicle at a viewing angle according to a first embodiment of the present invention;
FIG. 4 is a schematic view of the enlarged partial perspective structure of FIG. 3;
fig. 5 is a schematic structural diagram of a driving assembly and a base in a nest device for landing of an electric inspection unmanned aerial vehicle according to a first embodiment of the present invention;
fig. 6 is a schematic structural view of a cylindrical guide plate in a nest device for landing of an electric inspection unmanned aerial vehicle according to a first embodiment of the present invention;
fig. 7 is a schematic structural view of an arc-shaped canopy piece located at a middle position in the nest device for landing of the power inspection unmanned aerial vehicle according to the first embodiment of the present invention;
fig. 8 is a schematic view of an assembly structure of a base platform, a slide way, a slide block and a linear motor in the nest device for landing of the power inspection unmanned aerial vehicle according to the first embodiment of the utility model;
FIG. 9 is an enlarged partial schematic view of FIG. 8;
fig. 10 is a schematic structural view of a linear motor in a nest device for landing of an electric inspection unmanned aerial vehicle according to a first embodiment of the present invention;
fig. 11 is a schematic perspective view of a nest device for landing of an electric inspection unmanned aerial vehicle, which is provided by the first embodiment of the present invention and is provided with a heavy weight structure;
fig. 12 is a schematic cross-sectional structural view of an anti-skid mat layer in a nest device for landing of an electric inspection unmanned aerial vehicle according to an embodiment of the present invention.
Reference numbers: 1-a base platform; 2-lifting support columns; 3-protecting the cover in rainy days; 31-cambered surface shed sheet; 311-plug shaft; 32-a base; 320-a base body; 321-a bearing seat; 322-a bearing; 33-tarpaulin; 34-a drive assembly; 35-cylindrical guide disc; 36-a guide groove; 41-a slideway; 42-a slide block; 43-linear motor; 44-extension auxiliary landing plate; 441-a first underlayer; 442-a support layer; 443-a base layer; 45-heavy weight structure; 46-a rope.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the accompanying drawings, and it should be understood that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that certain terms of orientation or positional relationship are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the referred devices or elements must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.
In the description of the present invention, it should be noted that "connected" is to be understood broadly, for example, it may be fixed, detachable, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The present invention will be described in further detail below with reference to specific embodiments and with reference to the attached drawings.
Example one
Referring to fig. 1 to 4, an embodiment of the utility model provides a nest device for landing of an electric inspection unmanned aerial vehicle, which comprises a base platform 1, a liftable support column 2 arranged at the bottom of the base platform, and a rainy day protection cover 3 arranged on the surface of the base platform; landing identification marks are arranged on the surface of the basic platform;
the rainy-day protective cover 3 is a hemispherical protective cover, and the rainy-day protective cover 3 comprises a plurality of cambered-surface shed sheets 31, a base 32, hemispherical tarpaulin 33 and a driving assembly 34; the base is arranged on the surface of the base platform; the cambered surfaces of the cambered surface shed sheets are connected along the inner wall surface of the awning cloth in a sticking way according to the surface of the hemispherical awning cloth, and the cambered surface shed sheets are arranged at intervals along the surface latitude line of the hemispherical awning cloth;
referring also to fig. 5 to 7, the base 32 includes a base body 320, and a bearing seat 321 provided at an upper position of the base body, a bearing 322 provided at the bearing seat; the two ends of the arc canopy sheet 31 (see fig. 7) positioned in the middle of the plurality of arc canopy sheets are provided with insertion shafts 311, and the output shaft of the servo drive motor is inserted into a bearing hole formed by the bearing 322 of the bearing seat to realize rotating fit; the driving component 34 is a servo driving motor; the output shaft of the servo drive motor is also coaxially and rotationally connected (key-connected) with the plug-in shaft 311 and is used for driving the arc canopy piece 31 located at the middle position to rotate by taking a connecting line between the two bases 32 as an axis (meanwhile, the servo drive motor), the servo drive motor can only drive the plug-in shaft 311 at one side, and certainly, can also drive the plug-in shafts 311 at two sides simultaneously;
meanwhile, a cylindrical guide disc 35 is further disposed on the right side of the base 32 (see also fig. 6, the bottom of the cylindrical guide disc 35 is fixedly connected to the surface of the base platform 1), a guide groove 36 is disposed on the circumferential surface of the cylindrical guide disc 35, the guide groove 36 can be used for accommodating one end of the intermediate cambered shed sheet 31 to extend into, and the end of the intermediate cambered shed sheet 31 is coaxial with the cylindrical guide disc 35 (preferably, a circular hole can be formed on the upper end surface of the cylindrical guide disc 35, so that the insertion shaft 311 is inserted into the circular hole of the cylindrical guide disc 35); the guide groove 36 can be used for limiting the rotation of the insertion end of the cambered canopy plate 31 at the middle position, so that the cambered canopy plate can rotate in the groove of the guide groove along the arc edge of the guide groove in a limiting manner.
It should be noted that, in the specific technical solution of the embodiment of the present invention, the nest device for landing of the power inspection unmanned aerial vehicle adopts an independent nest structure design, the base platform and the part above the base platform are both installed on the top of the liftable support column, and the liftable support column can carry the structure to realize height position adjustment of the base platform, and the design can ensure that the base platform is independent of the ground, and cannot be submerged by ground water, so as to avoid influence of water accumulation to the maximum extent; similarly, a rain day protective cover is also designed on the basic platform, and the rain day protective cover adopts a unique design, so that when the rain day protective cover is opened, the space on the basic platform can be released to the greatest extent, and the taking-off is not influenced; when meeting overcast and rainy weather, can close the rainy day safety cover and carry out rain-proof protection to equipment and basic platform on its basic platform, avoid ponding on its basic platform, avoid basic platform surface to skid the influence and descend.
Furthermore, the rainy-day protective cover is a hemispherical protective cover, and the rainy-day protective cover mainly comprises a plurality of cambered-surface shed sheets, a base, hemispherical awning cloth, a driving assembly and other mechanisms; the base is arranged on the surface of the base platform; the cambered surface shed sheets are arranged along the inner wall surface of the tarpaulin according to the surface latitude line of the hemispherical (unfolded) tarpaulin and are attached along the inner wall surface of the tarpaulin, so that the cambered surface shed sheets form a reliable supporting framework integrally, the integral structure stability of the protective cover in rainy days is guaranteed, and the space between any two adjacent cambered surface shed sheets is a blank section of tarpaulin for connection, so that the design can also save the material of the shed sheets and the cost, and the directly driven structure in the cambered surface shed sheets is only the cambered surface shed sheet at the middle position; the design can ensure that the cambered surface shed sheets at a single middle position are driven to rotate to one side (turn left or right), so that a plurality of cambered surface shed sheets at half surfaces can act together at least under the driving action of the cambered surface shed sheets, and because a section of blank tarpaulin is connected among the cambered surface shed sheets, the cambered surface shed sheets can be influenced by pulling, and in addition, the embodiment of the application does not require that the whole tarpaulin is completely opened;
the driving assembly is a main driving structure, and the axis of the rotating action of the driving assembly is a virtual line, namely, the axis of the rotating action is a connecting line between the two bases, so that the hemispherical protective cover is ensured to realize the actions of opening, closing and closing. The driving assembly can be replaced by a driving system formed by structures such as a servo motor, a reduction gear box, a transmission system and the like, and the details are not repeated.
The specific structure and the specific technical effects of the nest device for landing of the power inspection unmanned aerial vehicle provided by the embodiment of the utility model are explained in detail as follows:
referring to fig. 8, 9 and 10, a slide rail 41, a slide block 42 and a linear motor 43 are further disposed in the interlayer of the base platform; an extension auxiliary landing plate 44 is arranged on the surface of the basic platform; the output end of the linear motor is fixedly connected with the sliding block 42, the top surface of the sliding block 42 is higher than the plane of the basic platform (or slightly higher than the plane of the basic platform), and the extension auxiliary landing plate 44 is detachably connected to the top surface of the sliding block 42 (the extension auxiliary landing plate 44 may be optionally not installed, and can be installed or detached as required); the linear motor is used for driving the extension auxiliary landing plate 44 to freely stretch and slide in the extension direction of the slideway 41. The linear motor is used for driving the extension auxiliary landing plate 44 to freely extend and retract in the extension direction of the slideway (the extension auxiliary landing plate can be round or square). The surface of the extension auxiliary landing plate is also provided with the landing identification mark.
What need explain is, when carrying out urgent descending (especially time heavy rain weather) in the rainy day, if open rainy day safety cover is whole this moment, then unmanned aerial vehicle descends and will pour into basic platform simultaneously a large amount of rainwater on basic platform in, it is serious to cause basic platform surface ponding serious seriously, influences unmanned aerial vehicle take off and land safety. Furthermore, in order to ensure the tidiness of the base platform and avoid a large amount of rainwater from falling into the base platform, an extension auxiliary landing plate is further designed on the basis of the technical scheme, the extension auxiliary landing plate is contracted into a rainy day protection cover of the base platform when not used, however, when the extension auxiliary landing plate is used in a rainy day, the extension auxiliary landing plate can be controlled by a linear motor to extend out along the base platform, meanwhile, a landing identification mark on the surface of the extension auxiliary landing plate is used for guiding the unmanned aerial vehicle to land, and then (the rainy day protection cover only needs to be opened by a small angle at the moment) the extension auxiliary landing plate is controlled by the linear motor to contract back to the original initial position along the base platform, so that the extension auxiliary landing plate is ensured to enter the rainy day protection cover, and then the rainy day protection cover is completely closed;
the rainy-day protective cover greatly shortens the time for opening the rainy-day protective cover by the cooperation of the extension auxiliary falling plate, and only needs to firstly fall on the extension auxiliary falling plate (the rain is fallen on the extension auxiliary falling plate with most of the time cost for falling), and then the extension auxiliary falling plate is driven to enter the cabin (namely, the rainy-day protective cover).
Referring to fig. 12, the surface of the extension auxiliary landing plate 44 is further provided with an anti-skid cushion layer; the anti-slip cushion layer is divided into three layers from top to bottom, and sequentially comprises a first cushion layer 441, a support layer 442 and a base layer 443; the first cushion layer 441 is a rubber wear-resistant cushion layer; the support layer 442 is a steel mesh; the base layer 443 is a concrete base layer.
It should be noted that, in order to further improve the landing safety of the extension auxiliary landing plate, the extension auxiliary landing plate is designed into a composite structure layer; wherein, above-mentioned reinforcing bar net piece mainly acts as the effect of supporting layer, and it can pour and place on the surface at the concrete foundation layer, then bonds the wear-resisting bed course of rubber at above-mentioned reinforcing bar net piece top again, and this wear-resisting bed course of rubber is main plays certain cushioning effect, reduces the impact force when unmanned aerial vehicle descends, can also play better anti-skidding effect simultaneously, has fully ensured unmanned aerial vehicle descending and has assisted the security of falling the board in the extension.
Preferably, as one possible embodiment; the surface of the rubber wear-resistant cushion layer is also coated with a hydrophobic coating.
Furthermore, in order to avoid a large amount of rainwater falling into the extension auxiliary landing plate and even the foundation platform, the extension auxiliary landing plate is further designed on the basis of the technical scheme,
the above-mentioned extension is assisted its rubber wear layer surface of descending board still need the coating have the hydrophobic coating of one deck or also can select to bond and have the hydrophobic membrane of one deck, prevents that the rainwater from staying at the surface of the supplementary board that falls of the above-mentioned extension to also can further ensure unmanned aerial vehicle's descending security. In the utility model, the extension auxiliary landing plate has stronger hydrophobicity, is convenient to install and has good auxiliary landing effect.
Referring to fig. 11, in the structure of the plurality of arc-shaped shed sheets, a heavy weight structural member 45 is arranged at the highest position point of the arc-shaped shed sheet located at the middle position; the heavy weight structural member 45 is connected with the highest position point of the cambered surface shed sheet 31 through a rope 46. The heavy bob structural member 45 is a conical structural member.
Preferably, as one possible embodiment; the heavy weight structure part is detachably connected with the rope.
Furthermore, in order to ensure the capability of the protective cover on the basic platform to adapt to rainy days and cloudy days and avoid the influence of strong wind damage, a heavy weight structure is further designed on the basis of the technical scheme; above-mentioned heavy structure of weighing down mainly plays the effect of preventing wind and rain of guarantee rainy day safety cover, promote its wind resistance, when it suffers the strong wind influence, because heavy structure of weighing down can stabilize its center and drop to the tenesmus, the rainy day safety cover has been reduced by a wide margin and has been lifted the possibility that drops basic platform, it suffers the strong wind and will arouse heavy structure of weighing down and sway about simultaneously, slow down the volatility that the strong wind blown, can effectively slow down the transient pulse load effect that the rainy day safety cover surface received when the strong wind process and assault.
Meanwhile, the cambered surface shed sheet positioned in the middle is larger in diameter size relative to the cambered surface shed sheets positioned in other positions and is thicker (even a reinforcing pipe sleeve can be sleeved) so as to guarantee the deformation resistance strength and guarantee the long-term installation and use of the heavy-weight structural member.
Preferably, as one possible embodiment; the tarpaulin in the rainy day safety cover is transparent tarpaulin. It should be noted that, in the specific technical solution of the embodiment of the present invention, the main result of the rain protective cover is the tarpaulin, and the specific transparent tarpaulin design adopted by the tarpaulin can ensure that when the rain protective cover is unfolded and closed (at this time, the basic platform is covered), the unmanned aerial vehicle can still recognize the landing recognition mark on the basic platform through the tarpaulin; the landing identification mark can be two-dimensional code, and the unique design of the rainy day protective cover does not influence the machine nest position identification before landing.
Preferably, as one possible embodiment; an air dryer (not shown in the figure) is also arranged on the surface of the basic platform; and the air outlet of the air dryer faces to the surface of the basic platform.
It should be noted that the air dryer is used for carrying out air drying treatment on the surface of the basic platform, so that rainwater entering the basic platform is prevented from causing the falling surface to skid. Further, in order to ensure the cleanness and tidiness of the basic platform, the influence of rainwater on the landing is avoided, and therefore the air dryer is additionally arranged on the basis of the technical scheme, the main effect of the air dryer is to implement air drying treatment on the surface of the basic platform, and the anti-skid performance of the ground inside the air dryer is guaranteed to be better to the greatest extent.
Preferably, as one possible embodiment; the surface of the basic platform is also provided with a solar photovoltaic panel and a storage battery pack; the solar photovoltaic panel is electrically connected with the storage battery pack, and the storage battery pack is electrically connected with the driving assembly.
It should be noted that, many auxiliary electrical devices are arranged on the surface and inside of the base platform, for example, a simple solar power supply system composed of a solar photovoltaic panel and a storage battery pack, the solar photovoltaic panel realizes reasonable utilization of light energy, the light energy is converted into electric energy to be stored in the storage battery pack, and the storage battery pack realizes power supply of driving devices such as a driving assembly and a linear motor.
The nest equipment for landing of the power inspection unmanned aerial vehicle has the following technical advantages: the nest equipment provided by the embodiment of the utility model can provide operations such as takeoff, landing, charging and the like for the unmanned aerial vehicle, and is also specially designed with a rainy-day protective cover; above-mentioned rainy day safety cover meets the rainy day environment, can close the safety cover, guarantees unmanned aerial vehicle and platform safety, can not damage unmanned aerial vehicle and platform power supply line.
The nest equipment provided by the embodiment of the utility model can fully automatically complete the power inspection operation without manually interfering the operation of the unmanned aerial vehicle, thereby improving the inspection efficiency, solving the problem of repeated flight waste caused by manual control, saving time and being suitable for mass operation of the unmanned aerial vehicle.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the utility model has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions of the embodiments of the present invention.
Claims (10)
1. A nest device for landing of an electric inspection unmanned aerial vehicle is characterized by comprising a base platform, a lifting support column arranged at the bottom of the base platform and a rainy day protection cover arranged on the surface of the base platform; landing identification marks are arranged on the surface of the basic platform;
the rainy-day protective cover is a hemispherical protective cover and comprises a plurality of cambered-surface shed sheets, a base, hemispherical tarpaulin and a driving assembly; the base is arranged on the surface of the base platform; the cambered surfaces of the cambered surface shed sheets are connected along the inner wall surface of the awning cloth in a sticking way according to the surface of the hemispherical awning cloth, and the cambered surface shed sheets are arranged at intervals along the surface latitude line of the hemispherical awning cloth; the driving component is a servo driving motor;
the base comprises a base body, a bearing seat arranged at the upper part of the base body and a bearing arranged at the bearing seat; inserting shafts are arranged at two ends of the cambered surface shed sheet positioned in the middle of the cambered surface shed sheets, and an output shaft of the servo driving motor is inserted into a bearing hole formed by a bearing of the bearing block to realize rotating fit; and the output shaft of the servo drive motor is coaxially and rotatably connected with the plug shaft and is used for driving the cambered-surface shed sheet positioned in the middle to rotate by taking a connecting line between the two bases as an axis.
2. The nest device for electric power inspection unmanned aerial vehicle landing according to claim 1, wherein a slide way, a slide block and a linear motor are further arranged in the interlayer of the base platform; an extension auxiliary landing plate is arranged on the surface of the basic platform; the output end of the linear motor is fixedly connected with the sliding block, the top surface of the sliding block is higher than the plane of the basic platform, and the extension auxiliary landing plate is detachably connected to the top surface of the sliding block; the linear motor is used for driving the extension auxiliary landing plate to freely stretch and slide in the extension direction of the slide way.
3. The nest apparatus for electric power inspection unmanned aerial vehicle landing according to claim 2, wherein the landing recognition mark is also provided on the surface of the extended auxiliary landing plate.
4. The nest device for electric power inspection unmanned aerial vehicle landing according to claim 2, wherein the surface of the extension auxiliary landing plate is further provided with an anti-skid cushion layer; the anti-skid cushion layer is divided into three layers from top to bottom, and sequentially comprises a first cushion layer, a supporting layer and a base layer; the first cushion layer is a rubber wear-resistant cushion layer; the supporting layer is a steel bar mesh; the base layer is a concrete base layer.
5. The nest device for electric power inspection unmanned aerial vehicle landing of claim 4, wherein the surface of the rubber wear pad layer is further coated with a hydrophobic coating.
6. The nest device for descending of the power inspection unmanned aerial vehicle according to claim 1, wherein in the structure of the plurality of cambered shed sheets, a heavy-weight structural member is arranged at the highest position point of the cambered shed sheet positioned in the middle; the heavy weight structural member is connected with the highest position point of the cambered surface shed sheet through a rope; the heavy weight structural part is of a cone structure.
7. The nest device for electric power inspection unmanned aerial vehicle landing of claim 6, wherein the heavy weight structure is detachably connected with the rope.
8. The nest device for electric power inspection unmanned aerial vehicle landing of claim 1, wherein the tarpaulin in the rainy day protection cover is a transparent tarpaulin.
9. The nest device for electric power inspection unmanned aerial vehicle landing according to claim 1, wherein an air dryer is further arranged on the surface of the base platform; and the air outlet of the air dryer faces to the surface of the basic platform.
10. The nest device for electric power inspection unmanned aerial vehicle landing according to claim 1, wherein a solar photovoltaic panel and a storage battery pack are further arranged on the surface of the base platform; the solar photovoltaic panel is electrically connected with the storage battery pack, and the storage battery pack is electrically connected with the driving assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122559684.7U CN216275289U (en) | 2021-10-22 | 2021-10-22 | Power inspection unmanned aerial vehicle descending nest equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122559684.7U CN216275289U (en) | 2021-10-22 | 2021-10-22 | Power inspection unmanned aerial vehicle descending nest equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216275289U true CN216275289U (en) | 2022-04-12 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122559684.7U Active CN216275289U (en) | 2021-10-22 | 2021-10-22 | Power inspection unmanned aerial vehicle descending nest equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216275289U (en) |
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2021
- 2021-10-22 CN CN202122559684.7U patent/CN216275289U/en active Active
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