CN211766356U - Unmanned aerial vehicle take-off and landing device - Google Patents
Unmanned aerial vehicle take-off and landing device Download PDFInfo
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- CN211766356U CN211766356U CN201922137860.0U CN201922137860U CN211766356U CN 211766356 U CN211766356 U CN 211766356U CN 201922137860 U CN201922137860 U CN 201922137860U CN 211766356 U CN211766356 U CN 211766356U
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Abstract
The utility model discloses an unmanned aerial vehicle take-off and landing device, including box, wheel, anemoscope and electromagnetic wave tester, the bottom of box is provided with the bottom plate, one side of bottom plate is provided with the front bezel, the another side of bottom plate is provided with the back plate, the right of bottom plate is provided with the right side board, the left side of bottom plate is provided with the left side board, one side of left side board is provided with the roof, one side of left side board is provided with first interior plate. Let the user can remove to look for the point of taking off and land on one side, the wind speed and the electromagnetic wave interference of real-time supervision environment on the other side to look for the point of taking off and land that environmental impact factor is minimum, the box can expand into a smooth platform of taking off and land completely, thereby solves the problem of the unevenness of the point of taking off and land.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, in particular to unmanned aerial vehicle take off and land device.
Background
In recent years, an unmanned aerial vehicle is taken as intelligent flight equipment, and because of its small volume, light in weight, the cost is lower than that of the traditional method, and the effect is better, therefore all obtain extensive application in each field, filled up the missing of aviation survey and drawing in the survey and drawing field more. However, the factors influencing the take-off and landing of the unmanned aerial vehicle are many, for example, overlarge wind speed can cause the left-right swinging instability of the take-off and landing of the unmanned aerial vehicle, the uneven ground can cause the ground to easily impact the ground and dust particles to fly all day by day when the unmanned aerial vehicle takes off and lands, the environment of electromagnetic interference can cause the unmanned aerial vehicle to lose control, and therefore the wind speed, the electromagnetic interference and the uneven ground are main environmental influences influencing the take-off and landing of the unmanned aerial vehicle, and how to select the take-off and landing point with the.
Therefore, it is necessary to invent a take-off and landing device for unmanned aerial vehicles to solve the above problems.
Disclosure of Invention
An object of the utility model is to provide an unmanned aerial vehicle device that takes off and land to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
an unmanned aerial vehicle lifting device comprises a box body, wheels, an anemoscope and an electromagnetic wave tester, wherein a bottom plate is arranged at the bottom of the box body, a front plate is arranged on one side of the bottom plate, a rear plate is arranged on the other side of the bottom plate, a right side plate is arranged on the right side of the bottom plate, a left side plate is arranged on the left side of the bottom plate, a top plate is arranged on one side of the left side plate, a first inner side plate is arranged on one side of the left side plate, a second inner side plate is arranged on the other side of the left side plate, a fastening screw is arranged in the middle of one side of the left side plate and used for fixing the first inner side plate and the second inner side plate after being folded, a first inner top plate is arranged on one side of the top plate, a second inner top plate is arranged on the other side of the top plate, a wrap angle is arranged on, make things convenient for the box to remove, the roof is close to the edge and is provided with the supporting legs, right margin fixedly connected with bolt section of thick bamboo on the roof, the left side on the roof is provided with the electromagnetic wave tester, be provided with the anemoscope on the electromagnetic wave tester, it has the spirit level to embed in the middle of the lower surface of roof, the spirit level surface with the roof surface flushes.
Preferably, the wrap angle comprises three mutually perpendicular faces, a wrap angle hole is formed in the middle of each face, a fixing piece capable of being attracted by magnetism is arranged in each wrap angle hole, a fixing groove corresponding to each wrap angle hole is formed in the box body, magnetic sheet-shaped objects are arranged in the fixing groove, and the fixing piece penetrates through the wrap angle hole and is connected with the magnetic sheet-shaped objects in the fixing groove in a magnetic mode.
Preferably, the fixing grooves are formed in four corners of the bottom plate, the left side plate, the right side plate, the top plate, the rear plate and the front plate.
Preferably, the side edge that goes up of electromagnetic wave tester is provided with power button, power button's the side that goes up is provided with the signal lamp, fixedly connected with strip axis of rotation on the electromagnetic wave tester, the one end of anemograph is through rotating connection strip axis of rotation. The inside power that is provided with of the other end of anemoscope, the thickness of the other end just in time equals the thickness sum of the first end of anemoscope and electromagnetic wave tester to the anemoscope can be on a parallel with the roof and collects, the one side of anemoscope is provided with electronic screen and fan blade, the anemoscope the power button the electronic screen reaches electromagnetic wave tester electric connection the power.
Preferably, the supporting legs comprise an outer cylinder and an inner column, one end of the outer cylinder is in threaded connection with the inner column, one end of the inner column is rotatably connected to the fixing sheet through a double-faced rivet, and the fixing sheet is fixed in the groove in the plate.
Preferably, the bottom plate, the top plate, the front plate, the first inner side plate, the first inner top plate, the second inner side plate and the rear plate are provided with bolt cylinders, bolts are arranged in the bolt cylinders, the bolts connect two adjacent bolt cylinders on different plates in series, and the unfolded plates can be fixed on a plane.
Preferably, the bottom plate, the left side plate, the top plate, the front plate, the first inner side plate, the first inner top plate, the second inner side plate, and the rear plate are connected by hinges, and the hinged plates can only rotate along the hinge rotation direction.
Preferably, the first face of right side board is provided with the saddlebag, and second face four corners department all is provided with the fixed slot, the trilateral seal of saddlebag, elasticity package mouth during last face edge can deposit instrument parts such as bolt, cornerite, mounting, remote controller in the package.
Preferably, be provided with the damping layer on the bottom plate, the edge on damping layer is provided with four elasticity ropes, the elasticity rope can be binded unmanned aerial vehicle and fix on the bottom plate, the damping layer then can play absorbing effect.
The utility model discloses a technological effect and advantage:
1. the utility model discloses a wheel, handle, hinge, cornerite, mounting, cornerite hole, fixed slot, magnetism sheet, box, bottom plate, right side board, left side board, roof, front bezel, first interior plate, first interior roof, second interior plate, back plate, electromagnetic wave tester, power button, signal lamp, strip axis of rotation, anemoscope, power, electronic screen, supporting legs, urceolus, inner prop, stationary blade, two-sided rivet, a bolt section of thick bamboo, bolt, spirit level, fastening screw, saddlebag, damping layer, elasticity rope. The box body moves, the wind speed and the electromagnetic wave interference of the environment are monitored in real time, if the box body is not suitable for the unmanned aerial vehicle to take off and land, the taking off and landing place is continuously searched, if the wind speed and the electromagnetic interference are detected to be suitable for taking off and landing, the box body stops moving, the box body is unfolded, the taking off and landing platform is built, and the taking off and landing are prepared; the utility model discloses a box can expand completely and fix into a smooth platform of taking off and land, adjusts the level back, can solve the problem of the place unevenness of taking off and land.
Drawings
Fig. 1 is a front view of the present invention.
Fig. 2 is a schematic view of the wrap angle structure of the present invention.
Fig. 3 is an enlarged view of the position a of the present invention.
Fig. 4 is a schematic view of the inside of the box body of the present invention.
Fig. 5 is an enlarged view of the position B of the present invention.
Fig. 6 is an expanded bottom view of the present invention.
Fig. 7 is an expanded plan view of the present invention.
In the figure: 1 wheel, 2 handles, 3 hinges, 4 wrap angles, 401 fasteners, 402 wrap angle holes, 403 fixing grooves, 404 magnetic sheet objects, a box body, 501 bottom plates, 502 right side plates, 503 left side plates, 504 top plates, 505 front plates, 506 first inner side plates, 507 first inner top plates, 508 second inner top plates, 509 second inner side plates, 510 rear plates, 6 electromagnetic wave testers, 601 power buttons, 602 signal lamps, 603 strip-shaped rotating shafts, 7 anemometers, 701 power supplies, 702 electronic screens, 8 supporting legs, 801 outer cylinders, 802 inner columns, fixing plates 803, 804 double-sided rivets, 901 pin cylinders, 902 pins, 10 gradienters, 11 fastening screws, 12 toolkits, 13 damping layers and 14 elastic ropes.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The utility model provides an unmanned aerial vehicle taking off and landing device as shown in the figure, which comprises a box body, wheels 1, an anemograph 7 and an electromagnetic wave tester 6, wherein the bottom of the box body is provided with a bottom plate 501, one side of the bottom plate 501 is provided with a front plate 505, the other side of the bottom plate 501 is provided with a rear plate 510, the right side of the bottom plate 501 is provided with a right side plate 502, the left side of the bottom plate 501 is provided with a left side plate 503, one side of the left side plate 503 is provided with a top plate 504, one side of the left side plate 503 is provided with a first inner side plate 506, the other side of the left side plate 503 is provided with a second inner side plate 509, a fastening screw 11 is arranged in the middle of one side of the left side plate 503 and used for fixing the folded first inner side plate 506 and the second inner side plate 509 so as to facilitate the folding of the left, the another side of roof 504 is provided with second inside roof 508, be provided with cornerite 4 on the case angle of box, the one side of bottom plate 501 is provided with wheel 1, department is provided with handle 2 in the middle of the roof 504, makes things convenient for the box to remove, roof 504 is close to the edge and is provided with supporting legs 8, right side edge fixedly connected with latch section of thick bamboo 901 on the roof 504, the left side on the roof 504 is provided with electromagnetic wave tester 6, be provided with anemoscope 7 on the electromagnetic wave tester 6, embedded spirit level 10 in the middle of the lower surface of roof 504, spirit level 10 surface with roof 504 surface flushes.
Further, in the above technical solution, the wrap angle 4 includes three mutually perpendicular surfaces, a wrap angle hole 402 is provided in the middle of each surface, a fixing member 401 capable of being magnetically attracted is provided in the wrap angle hole 402, a fixing groove corresponding to the wrap angle hole 402 is provided on the box body 5, a magnetic sheet 404 is provided in the fixing groove 403, and the fixing member 401 passes through the wrap angle hole 402 and is magnetically connected with the magnetic sheet 404 in the fixing groove 403;
further, in the above technical solution, the fixing grooves 403 are formed at four corners of the bottom plate 501, the left side plate 503, the right side plate 502, the top plate 504, the rear plate 510 and the front plate 505;
further, in the above technical solution, a power button 601 is disposed at an edge of an upper side of the electromagnetic wave tester 6, a signal lamp 602 is disposed on the upper side of the power button 601, a strip-shaped rotating shaft 603 is fixedly connected to the electromagnetic wave tester 6, and one end of the anemoscope 7 is rotatably connected to the strip-shaped rotating shaft 603; a power supply 701 is arranged in the other end of the anemoscope 7, the thickness of the other end is just equal to the sum of the thicknesses of the first end of the anemoscope 7 and the electromagnetic wave tester 6, so that the anemoscope 7 can be folded in parallel with the top plate 504, an electronic screen 702 and fan blades are arranged on one surface of the anemoscope 7, and the anemoscope 7, the power supply button 601, the electronic screen 702 and the electromagnetic wave tester 6 are electrically connected with the power supply 701;
further, in the above technical solution, the supporting foot 8 includes an outer cylinder 801 and an inner column 802, one end of the outer cylinder 801 is connected to the inner column 802 by a thread, one end of the inner column 802 is rotatably connected to a fixing plate 803 by a double-faced rivet 804, and the fixing plate 803 is fixed in a groove on a plate;
further, in the above technical solution, the bottom plate 501, the top plate 504, the front plate 505, the first inner side plate 506, the first inner top plate 507, the second inner top plate 508, the second inner side plate 509, and the rear plate 510 are provided with latch cylinders 901, the latch 902 is provided in the latch cylinder 901, the latch 902 connects two adjacent latch cylinders 901 on different plates in series, and the unfolded plates can be fixed on a plane;
further, in the above technical solution, the bottom plate 501, the left side plate 503, the top plate 504, the front plate 505, the first inner side plate 506, the first inner top plate 507, the second inner top plate 508, the second inner side plate 509, and the rear plate 510 are connected by a hinge 3, and the plates connected by the hinge 3 can only rotate along the rotation direction of the hinge 3;
further, in the above technical solution, a first surface of the right side plate 502 is provided with a tool bag 12, four corners of a second surface are provided with fixing grooves 403, three sides of the tool bag 12 are sealed, and the edge of the last surface is provided with an elastic bag opening, so that tool components such as a bolt 902, a bag corner 4, a fixing member 401, a remote controller and the like can be stored in the bag;
further, in the above technical scheme, a damping layer 13 is arranged on the bottom plate 501, four elastic ropes 14 are arranged on the edges of the damping layer 13, the elastic ropes 14 can bind and fix the unmanned aerial vehicle on the bottom plate 501, and the damping layer 13 can play a role in shock absorption.
This practical theory of operation:
as shown in the figure, when the utility model is used, the anemoscope 7 is rotated along the strip-shaped rotating shaft 603 to be vertical, the power button 601 is pressed, the anemoscope 7 and the electromagnetic wave detector 6 are started, the signal lamp 602 is on, the anemoscope faces the wind direction, the wind speed and the electromagnetic wave interference condition are monitored in real time, the wind speed and the electromagnetic interference data are displayed on the electronic screen 702, and the wind speed smaller than the maximum wind speed of the unmanned aerial vehicle which can take off and land is suitable for the wind speed of taking off and landing; lifting the box body with the lifting handle 2 to move or pushing the box body 5 to search for a proper take-off and landing point, continuously moving if the box body is not suitable for the unmanned aerial vehicle to take off and land on the way of moving, and stopping moving if the monitored data is suitable for taking off and landing. Pressing a power button 601, shutting down an anemoscope 7 and an electromagnetic wave detector 6, transversely folding and retracting the anemoscope 7, supporting a supporting leg 8, then taking down a fixing piece 401 and a wrap angle 4 on a box body corner, paving the rest plates on the ground along the rotation direction of a hinge 3, unscrewing fastening screws 11 on a left side plate 503 and a top plate 504, taking down a right side plate 502, putting the fixing piece 401, the wrap angle 4 and the fastening screws 11 into a tool bag 12, unfolding a first inner top plate 506, a second inner top plate 509, a first inner top plate 507 and a second inner top plate 508, taking out a bolt 902 from the tool bag 12, inserting the bolt 902 into two adjacent bolt cylinders 901, connecting the plates in the same plane after all the bolts 902 are inserted, adjusting the length of the supporting leg 8 according to a level 10 and an outer cylinder 801, adjusting the plates to be horizontal, unfastening an elastic rope 14 from an unmanned aerial vehicle, and binding the elastic rope, and carrying out take-off operation. When unmanned aerial vehicle descends, the operation is opposite to the preceding operation.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (9)
1. The utility model provides an unmanned aerial vehicle take-off and landing device, includes box (5), wheel (1), anemoscope (7) and electromagnetic wave tester (6), its characterized in that: the bottom of the box body is provided with a bottom plate (501), one side of the bottom plate (501) is provided with a front plate (505), the other side of the bottom plate (501) is provided with a rear plate (510), the right side of the bottom plate (501) is provided with a right side plate (502), the left side of the bottom plate (501) is provided with a left side plate (503), one side of the left side plate (503) is provided with a top plate (504), one side of the left side plate (503) is provided with a first inner side plate (506), the other side of the left side plate (503) is provided with a second inner side plate (509), a fastening screw (11) is arranged in the middle of one side of the left side plate (503), one side of the top plate (504) is provided with a first inner top plate (507), the other side of the top plate (504) is provided with a second inner top plate (508), a corner wrap (4) is arranged on, the utility model discloses an electromagnetic wave testing device, including roof (504), roof (504) middle department is provided with handle (2), roof (504) are close to the edge and are provided with supporting legs (8), right edge fixedly connected with bolt section of thick bamboo (901) on roof (504), the left side on roof (504) is provided with electromagnetic wave tester (6), be provided with anemoscope (7) on electromagnetic wave tester (6), spirit level (10) are embedded in the middle of the lower surface of roof (504).
2. An unmanned aerial vehicle take-off and landing device according to claim 1, wherein: be provided with in the middle of every face of cornerite (4) and wrap angle hole (402), be provided with in cornerite hole (402) and can be by magnetic attraction's mounting (401), be provided with on box (5) and wrap corresponding fixed slot (403) in angle hole (402), be provided with magnetism sheet (404) in fixed slot (403), mounting (401) run through cornerite hole (402) and are connected with magnetism sheet (404) magnetism in fixed slot (403).
3. An unmanned aerial vehicle take-off and landing device according to claim 2, wherein: the fixing grooves (403) are formed in four corners of the bottom plate (501), the left side plate (503), the right side plate (502), the top plate (504), the rear plate (510) and the front plate (505).
4. An unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the side edge that goes up of electromagnetic wave tester (6) is provided with power button (601), the side that goes up of power button (601) is provided with signal lamp (602), fixedly connected with strip axis of rotation (603) on electromagnetic wave tester (6), strip axis of rotation (603) is connected through rotating to the one end of anemoscope (7), the inside power (701) that is provided with of the other end of anemoscope (7), the one side of anemoscope (7) is provided with electronic screen (702), anemoscope (7) power button (601) electronic screen (702) reach electromagnetic wave tester (6) electric connection power (701).
5. An unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the supporting legs (8) comprise an outer cylinder (801) and an inner column (802), one end of the outer cylinder (801) is in threaded connection with the inner column (802), one end of the inner column (802) is rotatably connected onto a fixing sheet (803) through a double-faced rivet (804), and the fixing sheet (803) is fixed in a groove in the plate.
6. An unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the bottom plate (501), the top plate (504), the front plate (505), the first inner side plate (506), the first inner top plate (507), the second inner top plate (508), the second inner side plate (509) and the rear plate (510) are provided with plug pin cylinders (901), and plug pins (902) are arranged in the plug pin cylinders (901).
7. An unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the bottom plate (501), the left side plate (503), the top plate (504), the front plate (505), the first inner side plate (506), the first inner top plate (507), the second inner top plate (508), the second inner side plate (509), and the rear plate (510) are connected by a hinge (3).
8. An unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the tool bag is characterized in that a first surface of the right side plate (502) is provided with a tool bag (12), and four corners of the other surface of the right side plate (502) are provided with fixing grooves (403).
9. An unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the damping layer (13) is arranged on the bottom plate (501), and an elastic rope (14) is arranged on the edge of the damping layer (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922137860.0U CN211766356U (en) | 2019-12-03 | 2019-12-03 | Unmanned aerial vehicle take-off and landing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922137860.0U CN211766356U (en) | 2019-12-03 | 2019-12-03 | Unmanned aerial vehicle take-off and landing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211766356U true CN211766356U (en) | 2020-10-27 |
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ID=72972996
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922137860.0U Active CN211766356U (en) | 2019-12-03 | 2019-12-03 | Unmanned aerial vehicle take-off and landing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211766356U (en) |
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2019
- 2019-12-03 CN CN201922137860.0U patent/CN211766356U/en active Active
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