CN214729758U - Civil unmanned aerial vehicle take-off and landing support device - Google Patents
Civil unmanned aerial vehicle take-off and landing support device Download PDFInfo
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- CN214729758U CN214729758U CN202120819384.5U CN202120819384U CN214729758U CN 214729758 U CN214729758 U CN 214729758U CN 202120819384 U CN202120819384 U CN 202120819384U CN 214729758 U CN214729758 U CN 214729758U
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- aerial vehicle
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Abstract
The utility model discloses a civil unmanned aerial vehicle strutting arrangement that takes off and land, the loach carrying platform comprises a support, the top of support is seted up flutedly, the both sides of recess are provided with fixed subassembly, fixed subassembly's one end movable mounting has splint, four edge fixed mounting in bottom of support have lifting unit, lifting unit's bottom is provided with the removal subassembly, fixed subassembly is including the thread bush that runs through recess side fixed mounting, the inside of thread bush runs through movable mounting and has the screw rod. This civil unmanned aerial vehicle strutting arrangement that takes off and land, carrying out the in-process of daily use, place unmanned aerial vehicle on the support, through adjusting fixed subassembly, press from both sides unmanned aerial vehicle's base support between splint and dog, play fixed unmanned aerial vehicle's effect, prevent that unmanned aerial vehicle from dropping the occurence of failure who damages, improve life, through the cushion buffering clamp that adopts the rubber material degree of hitting, protection unmanned aerial vehicle does not receive the damage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a civil unmanned aerial vehicle strutting arrangement that takes off and land.
Background
Unmanned aerial vehicle is the unmanned vehicles who utilizes radio remote control equipment and self-contained program control device to control, unmanned aerial vehicle is the general name of unmanned vehicles in fact, unmanned aerial vehicle according to the application, can be for military use and civilian use, for military use, unmanned aerial vehicle divide into reconnaissance plane and target drone, civilian aspect, the application of unmanned aerial vehicle trade, be the real just needed of unmanned aerial vehicle, at present take a photograph of by plane, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, the relief of disaster, the movie & TV is shot, the application in fields such as manufacturing romantic, great expansion unmanned aerial vehicle's use itself, unmanned aerial vehicle's take off and land usually need accomplish on take off and land strutting arrangement.
Current unmanned aerial vehicle strutting arrangement that takes off and land adopts comparatively crude supporting structure, receives the slight collision of external force when the support, and unmanned aerial vehicle just can remove, drops on the ground even and damages, has shortened unmanned aerial vehicle's life and has caused owner's loss of property, and strutting arrangement is high and big moreover, brings more hemp trouble for removing and transporting.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a civil unmanned aerial vehicle strutting arrangement that takes off and land to solve the current unmanned aerial vehicle strutting arrangement that takes off and land that proposes in the above-mentioned background art and adopt comparatively crude supporting structure, receive the slight collision of external force when the support, unmanned aerial vehicle just can remove, and the even drops on the ground and damages, has shortened unmanned aerial vehicle's life and has caused owner's loss of property, and strutting arrangement is high and big moreover, brings the problem of more hemp vexing for removing and transporting.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a civil unmanned aerial vehicle strutting arrangement that takes off and land, includes the support, the top of support is seted up flutedly, the both sides of recess are provided with fixed subassembly, fixed subassembly's one end movable mounting has splint, four edges and corners fixed mounting in bottom of support has lifting unit, lifting unit's bottom is provided with the removal subassembly.
Preferably, the fixed subassembly is including running through the thread bush of recess side fixed mounting, movable mounting is run through to the inside of thread bush has the screw rod, the other end fixed mounting of screw rod has the hand wheel.
Preferably, the moving assembly comprises a base fixedly installed at the bottom of the lifting assembly, and universal wheels are fixedly installed at four corners of the bottom of the base.
Preferably, the top of the support is fixedly provided with a stop block, and the two sides of the stop block and one side of the clamping plate are fixedly provided with cushion blocks.
Preferably, lifting unit includes the gear seat of fixed mounting in four edges of base department, the fixed movable mounting in top of gear seat has the cylinder body, the top movable mounting of cylinder body has the telescopic link, one side fixed mounting of cylinder body has the motor.
Preferably, a bearing is fixedly installed on the surface of one side of the clamping plate, and the inside of the bearing is rotatably connected with one end of the screw rod.
Preferably, a control button is fixedly mounted on the surface of one side of the base, and the output end of the control button is electrically connected with the input end of the motor through a wire.
Preferably, the top fixed mounting of base has the battery, the output of battery passes through the wire and the input electric connection of motor.
Compared with the prior art, the beneficial effects of the utility model are that:
this civil unmanned aerial vehicle strutting arrangement that takes off and land, carrying out the in-process of daily use, place unmanned aerial vehicle on the support, through adjusting fixed subassembly, press from both sides unmanned aerial vehicle's base support between splint and dog, play fixed unmanned aerial vehicle's effect, prevent that unmanned aerial vehicle from dropping the occurence of failure who damages, improve life, through the cushion buffering clamp that adopts the rubber material degree of hitting, protection unmanned aerial vehicle does not receive the damage.
This civil unmanned aerial vehicle strutting arrangement that takes off and land is carrying out daily use in-process, through opening control button, starter motor lifts the support to suitable height, makes things convenient for unmanned aerial vehicle to take off and land, makes things convenient for the device to remove through the universal wheel, packs up the device through lowering lifting unit, and the person of facilitating the use removes, transports labour saving and time saving, has improved the practicality of taking off and land device greatly.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a part of the fixing assembly of the present invention;
FIG. 3 is a front view of the present invention;
fig. 4 is a schematic structural view of the base portion of the present invention.
In the figure: 1. a support; 2. a groove; 3. a fixing assembly; 4. a splint; 5. a lifting assembly; 6. a moving assembly; 7. a threaded sleeve; 8. a screw; 9. a hand wheel; 10. a base; 11. a universal wheel; 12. a stopper; 13. cushion blocks; 14. a gear seat; 15. a cylinder body; 16. a telescopic rod; 17. a motor; 18. a bearing; 19. a control button; 20. and (4) a storage battery.
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.
Referring to fig. 1-4, the present invention provides a technical solution: a civil unmanned aerial vehicle taking-off and landing supporting device comprises a support 1, a groove 2 is formed in the top of the support 1, fixing components 3 are arranged on two sides of the groove 2, a clamping plate 4 is movably installed at one end of each fixing component 3, lifting components 5 are fixedly installed at four corners of the bottom of the support 1, each lifting component 5 is an electric driving device which converts the rotary motion of a motor into the linear reciprocating motion of a push rod and can be used as an executing machine in various simple or complex process flows to realize remote control, centralized control or automatic control, the motor drives a pair of screw nuts after being decelerated by gears to convert the rotary motion of the motor into the linear motion, the push rod motion is completed by utilizing the forward and reverse rotation of the motor, complex motions such as rotation, shaking and the like can be completed by various levers, rockers or connecting rods and the like, and the lever arm length is changed, the travel can be increased or enlarged, the type of the lifting component 5 can be XTL100, the bottom of the lifting component 5 is provided with a moving component 6, a fixed component 3 comprises a threaded sleeve 7 fixedly installed through the side surface of the groove 2, a screw 8 is movably installed inside the threaded sleeve 7 in a penetrating manner, the other end of the screw 8 is fixedly provided with a hand wheel 9, an unmanned aerial vehicle is placed in the groove 2 at the top of the support 1, the screw 8 slides through the threaded sleeve 7 by rotating the hand wheel 9 to drive the clamp plate 4 to axially move, the clamp plate 4 moves towards the stop block 12 to tighten and fix the unmanned aerial vehicle, the accident that the unmanned aerial vehicle falls and is damaged is prevented, the service life is prolonged, the moving component 6 comprises a base 10 fixedly installed at the bottom of the lifting component 5, universal wheels 11 are fixedly installed at four corners at the bottom of the base 10, the lifting component 5 makes telescopic motion by opening a control button 19, the lifting component 5 lifts the support 1 to a proper height by controlling the lifting component 5, make things convenient for unmanned aerial vehicle to take off and land, through descending lifting unit 5, can reduce this device and accomodate, for removing the transportation and provide convenience, remove through 11 convenience of equipment of universal wheel, labour saving and time saving has improved the practicality of taking off and land device greatly.
The top of the support 1 is fixedly provided with a stop block 12, two sides of the stop block 12 and one side of the clamping plate 4 are both fixedly provided with cushion blocks 13, the cushion blocks 13 are made of rubber materials, the pressure generated by extrusion of the clamping plate 4 and the stop block 12 is buffered, the unmanned aerial vehicle is better protected, the lifting assembly 5 comprises gear seats 14 fixedly arranged at four corners of the base 10, metal gears are arranged inside the lifting assembly, the powder metallurgy technology is adopted, the pure metal gears are improved in strength and toughness in a double mode, a cylinder body 15 is fixedly and movably arranged at the top of the gear seat 14, the cylinder body 15 is made of aluminum alloy materials, the surface is subjected to twenty-seven polishing processes, the structural design is compact, the top end of the cylinder body 15 is movably provided with an expansion rod 16, one side of the cylinder body 15 is fixedly provided with a motor 17, the lifting assembly 5 can automatically stop when reaching the top point in daily work, the motor 17 is ensured not to be idle-fired, and any position can stop, the self-carrying machine lock has the characteristics of durability, stability and the like, the protection level is IP54, a bearing 18 is fixedly arranged on one side surface of a clamping plate 4 to ensure that a screw rod 8 can rotate to displace, the inside of the bearing 18 is rotatably connected with one end of the screw rod 8, a control button 19 is fixedly arranged on one side surface of a base 10, the output end of the control button 19 is electrically connected with the input end of a motor 17 through a lead, a storage battery 20 is fixedly arranged at the top of the base 10, the storage battery 20 adopts a maintenance-free storage battery, the maintenance-free storage battery has very small electrolyte consumption due to the advantages of self structure, distilled water is not required to be supplemented basically in the service life, the self-carrying machine lock also has the characteristics of shock resistance, high temperature resistance, small volume and small self discharge, the risk of shock damage can be avoided when the unmanned aerial vehicle is moved to lift and lower the supporting device, the service life is generally twice that of a common storage battery, a lead-calcium alloy grid is adopted, the water produced during charging is little, the water evaporation is low, and the shell adopts a sealing structure, the released sulfuric acid gas is also little, so compared with the traditional storage battery, the storage battery has the advantages of no need of adding any liquid, little corrosion to the wiring pile head and the electric wire, strong overcharge resistance, large starting current, long electric quantity storage time and the like, whether the storage battery 20 is fixed or not is checked before the lifting support device is used, whether the surface of the shell is damaged or not is checked, the charging condition and the quality state are checked through an electric eye on the storage battery 20, green shows qualified, black shows power shortage, white shows that the battery is damaged and needs to be replaced, the storage battery 20 is charged in time after the support device is used, so that the storage battery 20 is used next time and is protected from being damaged due to long-term power shortage, the output end of the storage battery 20 is electrically connected with the input end of the control button 19 through a lead, the control button 19 controls the lifting assembly 5 to lift, the storage battery 20 is carried along with the device, so that field operation is facilitated, and the problem of power connection difficulty is solved.
The working principle is as follows: when the unmanned aerial vehicle lifting support device is needed to be used, the unmanned aerial vehicle is parked on the groove 2 at the top of the support 1, the screw rod 8 slides through the threaded sleeve 7 by rotating the hand wheel 9, the clamp plate 4 is pushed to move to slowly approach the stop block 12, the hand wheel 9 stops rotating after the stop of the clamping, the unmanned aerial vehicle is clamped and fixed, the unmanned aerial vehicle is prevented from falling and being damaged, the service life is prolonged, the clamp plate 4, the stop block 12 and the unmanned aerial vehicle are buffered through the cushion block 13 made of rubber materials, the unmanned aerial vehicle is prevented from being damaged due to overlarge pressure, the output end of the storage battery 20 is electrically connected with the input end of the control button 19 through a lead, the output end of the control button 19 is electrically connected with the input end of the motor 17 through a lead, the control button 19 is electrified with the motor 17 to start the control lifting assembly 5 to move, the support 1 is lifted to a proper height, the unmanned aerial vehicle is convenient to lift, and the lifting assembly 5 is lifted, can reduce this device and accomodate, provide convenience for removing the transportation, four edges fixed mounting in bottom through base 10 have universal wheel 11, make things convenient for the device to remove, labour saving and time saving, improved the practicality of take-off and landing device greatly.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides a civil unmanned aerial vehicle strutting arrangement that takes off and land, includes support (1), its characterized in that: the top of support (1) is seted up flutedly (2), the both sides of recess (2) are provided with fixed subassembly (3), the one end movable mounting of fixed subassembly (3) has splint (4), four edges and corners fixed mounting in bottom of support (1) have lifting unit (5), the bottom of lifting unit (5) is provided with removes subassembly (6).
2. The civil unmanned aerial vehicle take-off and landing support device of claim 1, wherein: fixed subassembly (3) are including running through recess (2) side fixed mounting's thread bush (7), the inside of thread bush (7) runs through movable mounting has screw rod (8), the other end fixed mounting of screw rod (8) has hand wheel (9).
3. The civil unmanned aerial vehicle take-off and landing support device of claim 1, wherein: the moving assembly (6) comprises a base (10) fixedly installed at the bottom of the lifting assembly (5), and universal wheels (11) are fixedly installed at four corners of the bottom of the base (10).
4. The civil unmanned aerial vehicle take-off and landing support device of claim 1, wherein: the top fixed mounting of support (1) has dog (12), both sides of dog (12) and one side of splint (4) all fixed mounting have cushion (13).
5. The civil unmanned aerial vehicle take-off and landing support device of claim 3, wherein: lifting unit (5) include gear seat (14) of fixed mounting in four edges of base (10), the top fixed movable mounting of gear seat (14) has cylinder body (15), the top movable mounting of cylinder body (15) has telescopic link (16), one side fixed mounting of cylinder body (15) has motor (17).
6. The civil unmanned aerial vehicle take-off and landing support device of claim 1, wherein: and a bearing (18) is fixedly arranged on the surface of one side of the clamping plate (4), and the inside of the bearing (18) is rotatably connected with one end of the screw rod (8).
7. The civil unmanned aerial vehicle take-off and landing support device of claim 3, wherein: one side fixed surface of base (10) installs control button (19), the output of control button (19) passes through the input electric connection of wire and motor (17).
8. The civil unmanned aerial vehicle take-off and landing support device of claim 3, wherein: the top fixed mounting of base (10) has battery (20), the output of battery (20) passes through the input electric connection of wire and motor (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120819384.5U CN214729758U (en) | 2021-04-21 | 2021-04-21 | Civil unmanned aerial vehicle take-off and landing support device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120819384.5U CN214729758U (en) | 2021-04-21 | 2021-04-21 | Civil unmanned aerial vehicle take-off and landing support device |
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| Publication Number | Publication Date |
|---|---|
| CN214729758U true CN214729758U (en) | 2021-11-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120819384.5U Active CN214729758U (en) | 2021-04-21 | 2021-04-21 | Civil unmanned aerial vehicle take-off and landing support device |
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| CN (1) | CN214729758U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115096142A (en) * | 2022-06-01 | 2022-09-23 | 苏州高宝科技有限公司 | Unmanned aerial vehicle defense device |
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2021
- 2021-04-21 CN CN202120819384.5U patent/CN214729758U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115096142A (en) * | 2022-06-01 | 2022-09-23 | 苏州高宝科技有限公司 | Unmanned aerial vehicle defense device |
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Effective date of registration: 20231007 Address after: Room 485, Building E3, Xingzhuang Science and Technology Industrial Park, No. 288 Qinhuai Avenue, Yongyang Street, Lishui District, Nanjing City, Jiangsu Province, 211200 Patentee after: Nanjing Tan Xufa Network Technology Co.,Ltd. Address before: Room 011-385, room 01, 6 / F, building 1, sage technology R & D center, 26 Binhu Road, Donghu New Technology Development Zone, Wuhan City, Hubei Province, 430000 Patentee before: Hubei Zhenye Technology Co.,Ltd. |