CN210681185U - Unmanned aerial vehicle platform - Google Patents

Unmanned aerial vehicle platform Download PDF

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Publication number
CN210681185U
CN210681185U CN201921796064.1U CN201921796064U CN210681185U CN 210681185 U CN210681185 U CN 210681185U CN 201921796064 U CN201921796064 U CN 201921796064U CN 210681185 U CN210681185 U CN 210681185U
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aerial vehicle
unmanned aerial
platform
frame
rotating shaft
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CN201921796064.1U
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Chinese (zh)
Inventor
刘道国
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Shenzhen Still Core Technology Co Ltd
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Shenzhen Still Core Technology Co Ltd
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Abstract

The utility model discloses an unmanned aerial vehicle platform, including base, elevating platform, race rail, positioning seat, positioning signal ware, mainframe box, the interface that charges, screen and button, the top of base is equipped with the elevating platform, and the inside of elevating platform is equipped with the race rail. The utility model discloses unmanned aerial vehicle platform, gyro wheel on the unmanned aerial vehicle falls into the track groove in the track frame, track frame pressurized drives the movable frame downstream through accepting the seat, the spring takes place to kick-back, alleviate the vibrations when unmanned aerial vehicle falls to the ground, the mainframe box is through and be connected with the driving motor between the electricity, driving motor drives the initiative runner through the initiative pivot, the initiative runner drives the driven runner and rotates, the lifter plate is the upward movement in the driven pivot, the lifter plate upward movement is followed to the baffle, the baffle passes the notch and carries on spacingly to unmanned aerial vehicle, can reduce to take place to rock and shake and the condition emergence of displacement or tumble after making unmanned aerial vehicle shut down, avoid causing the unnecessary loss.

Description

Unmanned aerial vehicle platform
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle platform.
Background
The pilotless airplane, namely the unmanned aerial vehicle, is an unmanned airplane operated by utilizing a radio remote control device and a self-contained program control device, has the advantages of low cost, good efficiency-cost ratio, low risk, strong viability, good maneuvering performance and the like, is widely applied to the fields of high-altitude shooting, electric power monitoring and the like, and has a very strong application prospect in the field of express delivery. The unmanned aerial vehicle is generally powered by a battery carried on the unmanned aerial vehicle, is limited by the limited weight of the carried battery, and has the power consumption which is continuously increased along with the increase of auxiliary equipment, so that the single flight is short, and the application prospect and the development of the unmanned aerial vehicle are limited. The needle does not have fixing device after present unmanned aerial vehicle shuts down, leads to unmanned aerial vehicle to shut down the back if meet the platform because of external environment vibration, when rocking, unmanned aerial vehicle takes place the displacement easily, condition such as tumble causes unnecessary loss.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle platform makes can reduce after unmanned aerial vehicle shuts down and takes place to rock and vibrations and displacement or the condition of tumbleing and take place, avoids causing the unnecessary loss, can solve the problem among the prior art.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle platform comprises a base, a lifting platform, a running rail, a positioning seat, a positioning annunciator, a main case, a charging interface, a screen and a button, wherein the lifting platform is arranged at the top end of the base, the running rail is arranged inside the lifting platform, the positioning seat is arranged on the inner side of the running rail, the positioning annunciator is fixedly installed on the positioning seat, the main case is arranged on one side of the lifting platform, the charging interface is fixedly installed on one side, close to the lifting platform, of the main case, the screen is arranged at the top end of the main case, and the button is arranged on one side of the screen;
the elevating platform includes frame, motor cabinet, driving motor, initiative pivot, initiative runner, driven shaft, thread groove, lifter plate, dead lever, baffle and notch, the inside of frame is equipped with the motor cabinet, the inside fixed mounting of motor cabinet has driving motor, driving motor's one end is connected with the initiative pivot, driving motor's one end fixedly connected with initiative runner is kept away from in the initiative pivot, one side of initiative runner is equipped with driven runner, driven runner is run through by driven shaft, the thread groove has been seted up in the driven shaft, movable mounting has the lifter plate on the thread groove, the lifter plate is run through by the dead lever, the top fixed mounting of lifter plate has the baffle, the notch has been seted up on the frame on baffle top.
Preferably, the running rail comprises a rail frame, a rail groove, a bearing seat, a movable frame and a spring, the rail groove is formed in the rail frame, the bearing seat is fixedly connected to the bottom end of the rail frame, the bottom end of the bearing seat is fixedly installed on the movable frame, the spring is fixedly installed in the movable frame, and the bottom end of the spring is fixedly installed on the outer frame.
Preferably, the driven rotating wheel is fixedly connected with the driven rotating shaft.
Preferably, the lifting plate is in threaded connection with the thread groove.
Compared with the prior art, the beneficial effects of the utility model are as follows:
the utility model discloses unmanned aerial vehicle platform, through descending unmanned aerial vehicle to the frame, the gyro wheel on the unmanned aerial vehicle falls into the track groove in the track frame, the track frame is pressed and is passed through the accepting seat and drive the movable frame downstream, the movable frame drives the spring and pushes down, the spring rebounds, vibrations when alleviateing unmanned aerial vehicle and falling to the ground, when unmanned aerial vehicle removes to positioning seat department, positioning signal ware detects unmanned aerial vehicle and arrives after the appointed position, transmit the signal to the mainframe box, the mainframe box is through being connected with the driving motor between the electricity, driving motor drives the initiative runner through the initiative pivot, through the interlock of initiative runner and driven runner each other, the initiative runner drives driven runner and rotates, driven runner drives driven shaft and rotates, the lifter plate is through the threaded connection between and the thread groove and upward movement on driven shaft, the baffle follows the lifter plate upward movement, the baffle passes the notch and, after the unmanned aerial vehicle is stopped, the situations that the unmanned aerial vehicle shakes and vibrates and displaces or falls can be reduced, and unnecessary loss is avoided.
Drawings
Fig. 1 is a top view of the present invention;
fig. 2 is a side sectional view of the elevating platform of the present invention;
fig. 3 is a transverse sectional view of the running rail of the present invention.
In the figure: 1. a base; 2. a lifting platform; 21. an outer frame; 22. a motor base; 23. a drive motor; 24. a driving rotating shaft; 25. a driving runner; 26. a driven runner; 27. a driven rotating shaft; 28. a thread groove; 29. a lifting plate; 210. fixing the rod; 211. a baffle plate; 212. a notch; 3. running a rail; 31. a track frame; 32. a track groove; 33. a bearing seat; 34. a movable frame; 35. a spring; 4. positioning seats; 5. a positioning annunciator; 6. a main chassis; 7. a charging interface; 8. a screen; 9. a button.
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. 1-2, an unmanned aerial vehicle platform comprises a base 1, a lifting platform 2, a running rail 3, a positioning seat 4, a positioning annunciator 5, a mainframe box 6, a charging interface 7, a screen 8 and a button 9, wherein the lifting platform 2 is arranged at the top end of the base 1, the running rail 3 is arranged inside the lifting platform 2, the positioning seat 4 is arranged at the inner side of the running rail 3, the positioning annunciator 5 is fixedly installed on the positioning seat 4, the mainframe box 6 is arranged at one side of the lifting platform 2, the charging interface 7 is fixedly installed at one side of the mainframe box 6 close to the lifting platform 2, the screen 8 is arranged at the top end of the mainframe box 6, the button 9 is arranged at one side of the screen 8, the lifting platform 2 comprises an outer frame 21, a motor seat 22, a driving motor 23, a driving rotating shaft 24, a driving rotating wheel 25, a driven rotating wheel 26, a driven rotating shaft 27, a thread groove 28, a lifting plate 29, a driving motor 23 is fixedly installed inside the motor base 22, one end of the driving motor 23 is connected with a driving rotating shaft 24, one end of the driving rotating shaft 24, which is far away from the driving motor 23, is fixedly connected with a driving rotating wheel 25, one side of the driving rotating wheel 25 is provided with a driven rotating wheel 26, the driving rotating wheel 25 is engaged with the driven rotating wheel 26, the driven rotating wheel 26 is penetrated through by the driven rotating shaft 27, the driven rotating wheel 26 is fixedly connected with the driven rotating shaft 27, the driven rotating shaft 27 is provided with a thread groove 28, a lifting plate 29 is movably installed on the thread groove 28, the lifting plate 29 is in threaded connection with the thread groove 28, the lifting plate 29 is penetrated through by a fixing rod 210, the top end of the lifting plate 29 is fixedly installed with a baffle 211, an outer frame 21 at the top end of the baffle 211 is provided with a notch 212, the driving motor 23 drives the driving rotating wheel 25 through the driving rotating, driven runner 26 drives driven rotating shaft 27 and rotates, and lifter plate 29 is through and threaded connection between the thread groove 28 upward movement on driven rotating shaft 27, and lifter plate 29 upward movement is followed to baffle 211, and baffle 211 passes notch 212 and carries on spacingly to unmanned aerial vehicle.
Please refer to fig. 3, the running rail 3 includes the rail frame 31, the rail groove 32, the bearing seat 33, the movable frame 34 and the spring 35, the rail groove 32 has been seted up to the inside of rail frame 31, the bottom fixedly connected with of rail frame 31 bears the bearing seat 33, the bottom fixed mounting who bears the bearing seat 33 is on the movable frame 34, the inside fixed mounting of movable frame 34 has the spring 35, the bottom fixed mounting of spring 35 is on frame 21, the gyro wheel on the unmanned aerial vehicle falls into the rail groove 32 in the rail frame 31, rail frame 31 is pressed and is driven the downward motion of movable frame 34 through bearing seat 33, movable frame 34 drives the spring 35 and pushes down, the spring 35 takes place to kick-back, alleviate the vibrations when unmanned aerial vehicle lands.
The working principle is as follows: by landing the unmanned aerial vehicle on the outer frame 21, the rollers on the unmanned aerial vehicle fall into the track grooves 32 in the track frame 31, the track frame 31 is pressed to drive the movable frame 34 to move downwards through the bearing seat 33, the movable frame 34 drives the spring 35 to press downwards, the spring 35 rebounds to reduce the vibration when the unmanned aerial vehicle lands, when the unmanned aerial vehicle moves to the positioning seat 4, the positioning annunciator 5 detects that the unmanned aerial vehicle reaches a designated position and transmits signals to the main case 6, the main case 6 is electrically connected with the driving motor 23, the driving motor 23 drives the driving rotating wheel 25 through the driving rotating shaft 24, the driving rotating wheel 25 is meshed with the driven rotating wheel 26 through the driving rotating wheel 25, the driving rotating wheel 25 drives the driven rotating shaft 26 to rotate, the driven rotating wheel 26 drives the driven rotating shaft 27 to rotate, the lifting plate 29 moves upwards on the driven rotating shaft 27 through the threaded connection between the lifting plate 29 and the threaded groove 28, baffle 211 passes notch 212 and carries out spacing to unmanned aerial vehicle.
In summary, the following steps: the utility model discloses unmanned aerial vehicle platform, through landing unmanned aerial vehicle to frame 21, the gyro wheel on the unmanned aerial vehicle falls into track groove 32 in track frame 31, track frame 31 is pressed and is passed through the socket 33 and drive movable frame 34 downstream, movable frame 34 drives spring 35 and pushes down, spring 35 takes place to kick-back, alleviate the vibrations when unmanned aerial vehicle lands, when unmanned aerial vehicle moves to positioning seat 4 department, after locating signal ware 5 detects that unmanned aerial vehicle reachs the designated position, transmit the signal to main case 6, main case 6 is through being connected with driving motor 23 between the electricity, driving motor 23 drives driving runner 25 through initiative pivot 24, through the mutual interlock of driving runner 25 and driven runner 26, driving runner 25 drives driven runner 26 and rotates, driven runner 26 drives driven shaft 27 and rotates, lifter plate 29 moves upward on driven shaft 27 through the threaded connection between and thread groove 28, baffle 211 follows lifter plate 29 upward movement, and baffle 211 passes notch 212 and carries on spacingly to unmanned aerial vehicle, can reduce after making unmanned aerial vehicle shut down to take place to rock and shake and the condition emergence of displacement or tumble, avoids causing the unnecessary loss.
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 (4)

1. The utility model provides an unmanned aerial vehicle platform, includes base (1), elevating platform (2), runs rail (3), positioning seat (4), positioning signal ware (5), mainframe box (6), the interface that charges (7), screen (8) and button (9), its characterized in that: the portable intelligent charging device is characterized in that a lifting table (2) is arranged at the top end of the base (1), a running rail (3) is arranged inside the lifting table (2), a positioning seat (4) is arranged on the inner side of the running rail (3), a positioning annunciator (5) is fixedly mounted on the positioning seat (4), a mainframe box (6) is arranged on one side of the lifting table (2), a charging interface (7) is fixedly mounted on one side, close to the lifting table (2), of the mainframe box (6), a screen (8) is arranged at the top end of the mainframe box (6), and a button (9) is arranged on one side of the screen (8);
the lifting platform (2) comprises an outer frame (21), a motor base (22), a driving motor (23), a driving rotating shaft (24), a driving rotating wheel (25), a driven rotating wheel (26), a driven rotating shaft (27), a thread groove (28), a lifting plate (29), a fixing rod (210), a baffle (211) and a notch (212), wherein the motor base (22) is arranged in the outer frame (21), the driving motor (23) is fixedly arranged in the motor base (22), one end of the driving motor (23) is connected with the driving rotating shaft (24), one end, far away from the driving motor (23), of the driving rotating shaft (24) is fixedly connected with the driving rotating wheel (25), one side of the driving rotating wheel (25) is provided with the driven rotating wheel (26), the driven rotating wheel (26) is penetrated by the driven rotating shaft (27), and the thread groove (28) is formed in the driven rotating shaft (27), the lifting plate (29) is movably mounted on the threaded groove (28), the lifting plate (29) is penetrated by the fixing rod (210), the top end of the lifting plate (29) is fixedly provided with a baffle (211), and a notch (212) is formed in an outer frame (21) at the top end of the baffle (211).
2. The drone platform of claim 1, wherein: run rail (3) including track frame (31), track groove (32), accept seat (33), movable frame (34) and spring (35), track groove (32) have been seted up to the inside of track frame (31), the bottom fixedly connected with of track frame (31) accepts seat (33), the bottom fixed mounting who accepts seat (33) is on movable frame (34), the inside fixed mounting of movable frame (34) has spring (35), the bottom fixed mounting of spring (35) is on frame (21).
3. The drone platform of claim 1, wherein: the driven rotating wheel (26) is fixedly connected with the driven rotating shaft (27).
4. The drone platform of claim 1, wherein: the lifting plate (29) is in threaded connection with the threaded groove (28).
CN201921796064.1U 2019-10-23 2019-10-23 Unmanned aerial vehicle platform Active CN210681185U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921796064.1U CN210681185U (en) 2019-10-23 2019-10-23 Unmanned aerial vehicle platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921796064.1U CN210681185U (en) 2019-10-23 2019-10-23 Unmanned aerial vehicle platform

Publications (1)

Publication Number Publication Date
CN210681185U true CN210681185U (en) 2020-06-05

Family

ID=70903674

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921796064.1U Active CN210681185U (en) 2019-10-23 2019-10-23 Unmanned aerial vehicle platform

Country Status (1)

Country Link
CN (1) CN210681185U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A UAV platform

Effective date of registration: 20210720

Granted publication date: 20200605

Pledgee: Shenzhen small and medium sized small loan Co.,Ltd.

Pledgor: Shenzhen still core technology Co.,Ltd.

Registration number: Y2021440020054

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20221031

Granted publication date: 20200605

Pledgee: Shenzhen small and medium sized small loan Co.,Ltd.

Pledgor: Shenzhen still core technology Co.,Ltd.

Registration number: Y2021440020054

PC01 Cancellation of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A drone platform

Effective date of registration: 20230815

Granted publication date: 20200605

Pledgee: Shenzhen small and medium sized small loan Co.,Ltd.

Pledgor: Shenzhen still core technology Co.,Ltd.

Registration number: Y2023980052158

PE01 Entry into force of the registration of the contract for pledge of patent right