CN217624162U - Unmanned aerial vehicle aircraft platform with multifunctional module - Google Patents

Unmanned aerial vehicle aircraft platform with multifunctional module Download PDF

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Publication number
CN217624162U
CN217624162U CN202221149848.7U CN202221149848U CN217624162U CN 217624162 U CN217624162 U CN 217624162U CN 202221149848 U CN202221149848 U CN 202221149848U CN 217624162 U CN217624162 U CN 217624162U
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China
Prior art keywords
aerial vehicle
unmanned aerial
platform
containing box
lead screw
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CN202221149848.7U
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裴忠军
刘恩懋
沈子豪
魏琪杰
徐超
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Anhui Huiguang Intelligent Technology Co ltd
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Anhui Huiguang Intelligent Technology Co ltd
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries

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Abstract

The utility model discloses an unmanned aerial vehicle aircraft platform with multifunctional modules, which comprises a base and a lead screw, wherein rollers are arranged around the bottom of the base, and a storage box is arranged at the top of a support; the lead screw sets up in first recess, the lateral wall below both ends of containing box are provided with the movable rod. This unmanned aerial vehicle aircraft platform with multifunctional module passes through the angle adjustment subassembly, platform lift subassembly and accomodate the multifunctional module that the closing cap subassembly is constituteed, make when unmanned aerial vehicle descends, can reduce the produced vibrations of platform that rises and falls, improve unmanned aerial vehicle's stability, the accessible removes the inside to the containing box with platform and unmanned aerial vehicle that rises and falls after descending, and be close to each other through two sets of laps and carry out the closing cap to the containing box, so that can accomodate the protection to unmanned aerial vehicle, and still can adjust the angle of platform that rises and falls when slope department uses, make the platform that rises and falls to keep the level, thereby make things convenient for unmanned aerial vehicle to descend.

Description

Unmanned aerial vehicle aircraft platform with multifunctional module
Technical Field
The utility model relates to an unmanned aerial vehicle takes off and land the relevant technical field of platform specifically is an unmanned aerial vehicle aircraft platform with multifunctional module.
Background
Unmanned aerial vehicle is the unmanned aerial vehicle who utilizes radio remote control equipment and the program control device of self-contained to control, perhaps independently operate by vehicle-mounted computer totally or intermittently, when unmanned aerial vehicle takes off and lands, need use the platform of rising and falling to park unmanned aerial vehicle, through the magnanimity retrieval, discover among the prior art that unmanned aerial vehicle platform of rising and falling is typical like publication No. CN108146649A, a portable lift platform for unmanned aerial vehicle, including the elevating platform, the upper end of elevating platform is provided with the unmanned aerial vehicle body, and the lower extreme of elevating platform is provided with the pressure-bearing pole, one side fixed mounting that the lower extreme of elevating platform is close to the pressure-bearing pole has first fixed block, the lower extreme of pressure-bearing pole is connected with the surge-box, the inside of surge-box is close to one side of pressure-bearing pole and is installed the second spring. This portable lift platform for unmanned aerial vehicle, through having set up foot switch and electronic hydraulic stem, the user can be very convenient make electronic hydraulic stem rise or descend, can provide suitable height of taking off for the unmanned aerial vehicle body when taking off, the pulley has been set up, convenient to use person removes the lower plate and then removes the position of elevating platform, the baffle-box and the pressure-bearing pole have been set up, when the elevating platform receives to rock, can play buffering external force and absorbing effect, greatly reduced the vibration of elevating platform.
To sum up, current unmanned aerial vehicle platform that rises and falls is inconvenient to accomodate it after unmanned aerial vehicle descends, leads to unmanned aerial vehicle to drop the damage easily on the platform, and current unmanned aerial vehicle platform that rises and falls can not keep the level form when slope department uses, leads to unmanned aerial vehicle to slide easily after descending and falls, and the practicality is relatively poor.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle aircraft platform with multifunctional module to solve the current unmanned aerial vehicle platform of rising and falling that proposes among the above-mentioned background art and accomodate it inconveniently after unmanned aerial vehicle descends, and can not keep the problem of level form when slope department uses.
In order to achieve the above purpose, the utility model provides a following technical scheme: an unmanned aerial vehicle aircraft platform with a multifunctional module comprises a base and a screw rod,
the lifting platform comprises a base, a lifting platform, a support, a cylinder, a lifting platform, a lifting mechanism and a lifting mechanism, wherein the periphery of the bottom of the base is provided with rollers, two sides of the top of the base are respectively provided with a screw rod and a mounting plate, the inner side of the mounting plate is rotatably connected with a movable plate, two ends of the top of the movable plate are fixedly provided with the support, the top of the support is provided with a containing box, the bottom of the containing box is provided with the cylinder in a penetrating manner, the cylinder is connected with the sleeve, and the sleeve is fixedly arranged at the bottom of the lifting platform;
the lead screw sets up in first recess, and first recess sets up the lateral wall at the containing box, the both sides threaded connection of lead screw has the movable block, and the movable block setting is in the both sides of first recess, the lateral wall below both ends of containing box are provided with the movable rod, and the movable rod is connected with the apron, and the apron sets up the top both ends at the containing box simultaneously.
Preferably, the lateral wall of fly leaf has seted up the second recess, and rotates in the second recess and be connected with the connecting block, connecting block and screw rod threaded connection, and screw rod and connecting block constitute angle adjustment subassembly jointly.
Through adopting above-mentioned technical scheme, can adjust the angle of fly leaf and rise and fall platform for rise and fall platform can keep the level when using in slope department.
Preferably, telescopic inside is provided with damping spring, and damping spring is connected with the cylinder, and cylinder, sleeve and damping spring constitute platform lifting unit jointly simultaneously.
Through adopting above-mentioned technical scheme, can reduce the produced vibrations of unmanned aerial vehicle when descending, improve stability.
Preferably, the surface of the landing platform is provided with guide lamps, and the landing platform is provided with a plurality of groups.
Through adopting above-mentioned technical scheme, can guide unmanned aerial vehicle to descend night.
Preferably, the lateral wall of containing box is provided with the motor, and the output of motor is connected with the lead screw, and lead screw, movable block and movable rod constitute jointly simultaneously and accomodate the closing cap subassembly.
By adopting the technical scheme, the two groups of movable blocks can be driven to be close to or far away from each other.
Preferably, the outside of movable block is provided with spacing post, and spacing post is connected with the guide way, and the guide way is seted up on the surface of movable rod simultaneously.
Through adopting above-mentioned technical scheme, can drive two sets of apron and be close to each other to accomodate unmanned aerial vehicle.
Compared with the prior art, the beneficial effects of the utility model are that: the unmanned aerial vehicle platform with the multifunctional module,
through the angle adjustment subassembly, platform lifting unit and the multifunctional module who accomodates the closing cap subassembly and constitute, make when unmanned aerial vehicle descends, can reduce the produced vibrations of platform that rises and falls, improve unmanned aerial vehicle's stability, the accessible will rise and fall the platform and unmanned aerial vehicle removes to the inside of containing box after descending, and carry out the closing cap through two sets of apron each other being close to the containing box, so that can accomodate the protection to unmanned aerial vehicle, and still can adjust the angle of the platform that rises and falls when slope department uses, make the platform that rises and falls can keep the level, thereby make things convenient for unmanned aerial vehicle to descend.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic top view of the base and the movable plate of the present invention;
FIG. 3 is a schematic structural view of the sleeve and the landing platform of the present invention;
fig. 4 is the rear view structure diagram of the storage box of the present invention.
In the figure: 1. the base, 2, gyro wheel, 3, screw rod, 4, mounting panel, 5, fly leaf, 6, connecting block, 7, support, 8, containing box, 9, cylinder, 10, sleeve, 11, damping spring, 12, the platform that rises and falls, 13, guide lamp, 14, motor, 15, lead screw, 16, movable block, 17, spacing post, 18, movable rod, 19, guide way, 20, apron.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle aircraft platform with multifunctional module, as shown in fig. 1 and fig. 2, base 1's bottom is provided with gyro wheel 2 all around, and base 1's top both sides are provided with screw rod 3 and mounting panel 4 respectively, the inboard of mounting panel 4 is rotated and is connected with fly leaf 5, and the top both ends of fly leaf 5 are fixed with support 7, the second recess has been seted up to the lateral wall of fly leaf 5, and rotate in the second recess and be connected with connecting block 6, connecting block 6 and screw rod 3 threaded connection, and screw rod 3 constitutes angle adjustment subassembly with connecting block 6 jointly, when using in slope department, rotatable base 1 left screw rod 3 drives and its threaded connection's connecting block 6 rises or descends, can make connecting block 6 drive the one end of fly leaf 5 rise or descend, thereby make the other end of fly leaf 5 rotate at mounting panel 4's inboard, thereby adjust fly leaf 5 and containing box 8 and the angle of platform 12, make platform 12 can keep the level when using in slope department, thereby make things convenient for unmanned aerial vehicle to descend.
As shown in fig. 1 and 3, a storage box 8 is arranged at the top of the support 7, an air cylinder 9 is arranged at the bottom of the storage box 8 in a penetrating manner, the air cylinder 9 is connected with a sleeve 10, and the sleeve 10 is fixed at the bottom of a landing platform 12; sleeve 10's inside is provided with damping spring 11, and damping spring 11 is connected with cylinder 9, cylinder 9 simultaneously, sleeve 10 and damping spring 11 constitute platform lifting unit jointly, after unmanned aerial vehicle descends to platform 12 that rises and falls, sleeve 10 inside damping spring 11 can reduce unmanned aerial vehicle descending to the produced vibrations of platform 12 that rises and falls on, thereby improve stability, after descending, the cylinder 9 pressure release of 8 bottoms of accessible containing box, make cylinder 9 drive platform 12 that rises and falls descend, so that remove unmanned aerial vehicle to the inside of containing box 8, avoid unmanned aerial vehicle to drop the damage after descending.
As shown in fig. 1 and 3, the surface of the landing platform 12 is provided with the guide lamp 13, and it is provided with a plurality of groups, when using at night, the guide lamp 13 on the landing platform 12 can flash, thereby the convenience of use adjusts the landing position of the unmanned aerial vehicle, improves the precision when landing.
As shown in FIG. 1 and FIG. 4, a screw rod 15 is disposed in a first groove, the first groove is opened on the side wall of the containing box 8, two sides of the screw rod 15 are connected with movable blocks 16 by screw threads, the movable blocks 16 are disposed on two sides of the first groove, two ends of the side wall of the containing box 8 are provided with movable rods 18, the movable rods 18 are connected with cover plates 20, the cover plates 20 are disposed at two ends of the top of the containing box 8, the side wall of the containing box 8 is provided with a motor 14, the output end of the motor 14 is connected with the screw rod 15, the movable blocks 16 and the movable rods 18 together form a containing and sealing assembly, a limiting column 17 is disposed on the outer side of the movable block 16, and the limiting column 17 is connected with a guide groove 19, simultaneously the surface at movable rod 18 is seted up to guide way 19, remove unmanned aerial vehicle to containing box 8 inside back, the motor 14 of opening the 8 lateral walls of containing box drives lead screw 15 and rotates, make lead screw 15 drive two sets of movable blocks 16 rather than threaded connection be close to each other, when two sets of movable blocks 16 are close to each other, the spacing post 17 in the movable block 16 outside can slide in the guide way 19 on movable rod 18 surface, and drive movable rod 18 and revolve round and rotate with 8 nodical departments of containing box, thereby make two sets of apron 20 at movable rod 18 drive containing box 8 tops be close to each other, so that carry out the closing cap to containing box 8, thereby accomodate unmanned aerial vehicle.
The working principle is as follows: when using this unmanned aerial vehicle aircraft platform with multifunctional module, rotate screw rod 3 and drive connecting block 6 and rise or descend, make connecting block 6 drive one side of fly leaf 5 and rise or descend, make the opposite side of fly leaf 5 rotate in mounting panel 4, can adjust fly leaf 5 and platform 12 that rises and falls to the level form when slope department uses, make things convenient for unmanned aerial vehicle to descend, after unmanned aerial vehicle falls, to the cylinder 9 pressure release of containing box 8 bottom, make cylinder 9 drive platform 12 that rises and falls and the containing box 8 is inside, can accomodate unmanned aerial vehicle, prevent to drop the damage, this is accomplished whole operation, and the content that does not make detailed description in this specification belongs to the prior art that professional technical personnel publicly know in this field.
The terms "central," "longitudinal," "lateral," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like refer to orientations or positional relationships illustrated in the drawings, and are used merely to simplify the description of the present disclosure, rather than to indicate or imply that the device or element so referred to must have a particular orientation, be constructed and operated in a particular orientation, and are not to be construed as limiting the scope of the present disclosure.
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 may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.

Claims (6)

1. The utility model provides an unmanned aerial vehicle aircraft platform with multifunctional module, includes base (1) and lead screw (15), its characterized in that:
the roller wheels (2) are arranged on the periphery of the bottom of the base (1), the screw rods (3) and the mounting plates (4) are arranged on two sides of the top of the base (1) respectively, the movable plate (5) is rotatably connected to the inner side of the mounting plates (4), the supports (7) are fixed to two ends of the top of the movable plate (5), the storage box (8) is arranged on the top of each support (7), the air cylinder (9) penetrates through the bottom of each storage box (8), the air cylinder (9) is connected with the sleeve (10), and the sleeve (10) is fixed to the bottom of the lifting platform (12);
lead screw (15) set up in first recess, and the lateral wall at containing box (8) is seted up to first recess, the both sides threaded connection of lead screw (15) has movable block (16), and movable block (16) set up the both sides at first recess, the lateral wall below both ends of containing box (8) are provided with movable rod (18), and movable rod (18) are connected with apron (20), and apron (20) set up the top both ends at containing box (8) simultaneously.
2. An unmanned aerial vehicle platform with multi-functional module of claim 1, characterized in that: the lateral wall of fly leaf (5) has been seted up the second recess, and rotates in the second recess and be connected with connecting block (6), connecting block (6) and screw rod (3) threaded connection, and screw rod (3) and connecting block (6) constitute angle adjustment subassembly jointly.
3. An unmanned aerial vehicle platform with a multifunctional module of claim 1, wherein: damping spring (11) is arranged in sleeve (10), and damping spring (11) are connected with cylinder (9), and cylinder (9), sleeve (10) and damping spring (11) constitute platform lifting unit jointly simultaneously.
4. An unmanned aerial vehicle platform with a multifunctional module of claim 1, wherein: the surface of the lifting platform (12) is provided with a plurality of groups of guide lamps (13).
5. An unmanned aerial vehicle platform with multi-functional module of claim 1, characterized in that: the lateral wall of containing box (8) is provided with motor (14), and the output of motor (14) is connected with lead screw (15), and lead screw (15), movable block (16) and movable rod (18) constitute jointly simultaneously and accomodate the closing cap subassembly.
6. An unmanned aerial vehicle platform with a multifunctional module of claim 1, wherein: the outer side of the movable block (16) is provided with a limiting column (17), the limiting column (17) is connected with a guide groove (19), and the guide groove (19) is formed in the surface of the movable rod (18).
CN202221149848.7U 2022-05-13 2022-05-13 Unmanned aerial vehicle aircraft platform with multifunctional module Active CN217624162U (en)

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Application Number Priority Date Filing Date Title
CN202221149848.7U CN217624162U (en) 2022-05-13 2022-05-13 Unmanned aerial vehicle aircraft platform with multifunctional module

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221149848.7U CN217624162U (en) 2022-05-13 2022-05-13 Unmanned aerial vehicle aircraft platform with multifunctional module

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CN217624162U true CN217624162U (en) 2022-10-21

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117193337A (en) * 2023-09-18 2023-12-08 清华大学 Variable-angle vehicle-mounted unmanned aerial vehicle take-off and landing system and method under condition of high-speed movement of vehicle
CN117775467A (en) * 2024-02-27 2024-03-29 民航成都电子技术有限责任公司 Unmanned aerial vehicle storage box, unmanned aerial vehicle system and unmanned aerial vehicle path planning method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117193337A (en) * 2023-09-18 2023-12-08 清华大学 Variable-angle vehicle-mounted unmanned aerial vehicle take-off and landing system and method under condition of high-speed movement of vehicle
CN117193337B (en) * 2023-09-18 2024-04-26 清华大学 Variable-angle vehicle-mounted unmanned aerial vehicle take-off and landing system and method under condition of high-speed movement of vehicle
CN117775467A (en) * 2024-02-27 2024-03-29 民航成都电子技术有限责任公司 Unmanned aerial vehicle storage box, unmanned aerial vehicle system and unmanned aerial vehicle path planning method

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