CN210455254U - Many rotor unmanned aerial vehicle descending device - Google Patents
Many rotor unmanned aerial vehicle descending device Download PDFInfo
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- CN210455254U CN210455254U CN201921487042.7U CN201921487042U CN210455254U CN 210455254 U CN210455254 U CN 210455254U CN 201921487042 U CN201921487042 U CN 201921487042U CN 210455254 U CN210455254 U CN 210455254U
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- aerial vehicle
- unmanned aerial
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- servo motor
- frame
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
The utility model discloses a many rotor unmanned aerial vehicle descending device, including descending platform, elevating system, frame, hatch door and antenna, elevating system fixed mounting is on the frame, linear guide is installed to the elevating system both sides, linear guide fixes on the frame, descending platform fixed mounting is on elevating system's slider, be provided with many rotor unmanned aerial vehicle on the descending platform, the descending platform includes unmanned aerial vehicle foot rest clamping mechanism and platform self rotary mechanism, the hatch door sets up the top at the frame, the antenna mounting is on the hatch door, be provided with rack and pinion mechanism on the hatch door. The utility model discloses possess the function of taking off and land, descending platform simultaneously rotates 90 degrees to 180 degrees to in change battery and load, also do benefit to the different models of length and width size and more conveniently accomodate the inside of frame, can realize the relative motion of clamping direction, the synchronism when the W type pinch-off blades of assurance are tight.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a many rotor unmanned aerial vehicle descending device.
Background
At present many rotor unmanned aerial vehicle's application area is very extensive, plays more and more important effect in fields such as survey and drawing, fire control and urban planning, under the huge prospect of industrial application, unmanned aerial vehicle need take off and land the restriction and the storage of condition and accomodate the scheduling problem, and current unmanned aerial vehicle landing device mostly only possesses the function of taking off and land, and can not adjust unmanned aerial vehicle's position after descending, can not carry out the automation and accomodate.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a many rotor unmanned aerial vehicle descending device possesses the function of taking off and land, descends the platform simultaneously and rotates 90 degrees to 180 degrees to in change battery and load, also do benefit to the different models of length and width size and more conveniently accomodate the inside of frame, can realize the relative motion of clamping direction, the synchronism when the W type pinch-off blades of assurance press from both sides tightly, with the problem of proposing in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides a many rotor unmanned aerial vehicle descending device, includes descending platform, elevating system, frame, hatch door and antenna, elevating system fixed mounting is on the frame, linear guide is installed to the elevating system both sides, linear guide fixes on the frame, descending platform fixed mounting is on elevating system's slider, be provided with many rotor unmanned aerial vehicle on the descending platform, the descending platform includes unmanned aerial vehicle foot rest clamping mechanism and platform self rotary mechanism, the hatch door sets up the top at the frame, the antenna is installed on the hatch door, be provided with rack and pinion mechanism on the hatch door.
Preferably, unmanned aerial vehicle foot rest clamping mechanism includes positive and negative lead screw module, first servo motor, infrared sensor and W type clamp plate, positive and negative lead screw module passes through the coupling joint with first servo motor's output, infrared sensor fixed mounting is in one side of positive and negative lead screw module, W type clamp plate is fixed on the slider of positive and negative lead screw module.
Preferably, platform self rotary mechanism includes second servo motor, worm gear subassembly and revolving stage, second servo motor passes through the worm gear subassembly and is connected with the revolving stage transmission, it installs on the revolving stage to descend the platform.
Preferably, the lifting mechanism comprises a third servo motor, a speed reducer, a screw rod module and a position detection sensor, the third servo motor is connected with the speed reducer, the speed reducer is in transmission connection with the screw rod module, and the position detection sensor is fixedly installed on one side of the screw rod module.
Preferably, the rack-and-pinion mechanism comprises a fourth servo motor, a gear and a rack, the fourth servo motor is fixedly installed on the frame, the gear is connected to an output shaft of the fourth servo motor in a key mode, the rack is fixedly installed inside the cabin door, and the rack is meshed with the gear.
Preferably, be provided with the joint that charges on the unmanned aerial vehicle foot rest clamping mechanism, be provided with on many rotor unmanned aerial vehicle's the foot rest with the joint assorted interface that charges.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses possess the function of taking off and land, the platform that descends simultaneously can self rotate 90 degrees to 180 degrees under platform self rotary mechanism's drive to in change battery and load, also do benefit to the different models of length and width size and more conveniently accomodate the inside of frame, drive positive and negative lead screw module through a servo motor, can realize the relative motion of clamping direction through a motor, the synchronism when the W type pinch-off blades of assurance press from both sides tightly.
Drawings
FIG. 1 is a general schematic view of the present invention;
fig. 2 is a schematic structural view of the unmanned aerial vehicle foot stool clamping mechanism of the present invention;
fig. 3 is a schematic view of the automatic charging principle of the foot rest of the present invention
Fig. 4 is a schematic structural view of the lifting mechanism of the present invention;
fig. 5 is a schematic structural view of the split hatch of the present invention.
In the figure: 1. landing the platform; 101. an unmanned aerial vehicle foot stool clamping mechanism; 1011. a positive and negative lead screw module; 1012. a first servo motor; 1013. an infrared sensor; 1014. a W-shaped clamping plate; 102. a platform self-rotating mechanism; 1021. a worm gear assembly; 1022. a rotating table; 2. a lifting mechanism; 201. a third servo motor; 202. a speed reducer; 203. a screw rod module; 3. a frame; 4. a cabin door; 5. an antenna; 6. a rack and pinion mechanism; 601. a gear; 602. a rack; 7. a linear guide rail; 8. a charging connector; 9. a charging interface; 10. many rotor unmanned aerial vehicle.
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. 1-5, the present invention provides a technical solution:
as shown in fig. 1, a landing device of a multi-rotor unmanned aerial vehicle comprises a landing platform 1, a lifting mechanism 2, a frame 3, a cabin door 4 and an antenna 5, wherein the lifting mechanism 2 is fixedly installed on the frame 3, linear guide rails 7 are installed on two sides of the lifting mechanism 2, the linear guide rails 7 are fixed on the frame 3, the linear guide rails 7 have good guiding function, the landing platform 1 is fixedly installed on a sliding block of the lifting mechanism 2, the landing platform 1 is provided with a multi-rotor unmanned aerial vehicle 10, the landing platform 1 comprises an unmanned aerial vehicle foot stool clamping mechanism 101 and a platform self-rotating mechanism 102, when the multi-rotor unmanned aerial vehicle 10 lands on the landing platform 1, the unmanned aerial vehicle foot stool clamping mechanism 101 resets the multi-rotor unmanned aerial vehicle 10 to the central position of the landing platform 1, and locks the foot stool of the multi-rotor unmanned aerial vehicle 10 at the same time, the antenna 5 is installed on the cabin door 4, the gear and rack mechanism 6 is arranged on the cabin door 4, the cabin door 4 is opened in a split mode through the gear and rack mechanism 6, and the antenna 5 is matched to achieve automatic opening and closing.
As shown in fig. 2, the unmanned aerial vehicle foot stool clamping mechanism 101 includes positive and negative lead screw module 1011, first servo motor 1012, infrared sensor 1013 and W-shaped clamp plate 1014, positive and negative lead screw module 1011 passes through the coupling joint with the output of first servo motor 1012, infrared sensor 1013 fixed mounting is in one side of positive and negative lead screw module 1011, infrared sensor 1013 is used for examining initial position and final position, W-shaped clamp plate 1014 is fixed on the slider of positive and negative lead screw module 1011, adopt first servo motor 1012 to drive positive and negative lead screw module 1011 that comprises two lead screws with opposite rotation directions, two lead screws adopt the coupling joint on a straight line, W-shaped clamp plate 1014 is fixed respectively on two lead screw sliders and is relative motion, when multi-rotor unmanned aerial vehicle 10 lands on 1012 platform 1, be in the non-center position on the landing platform 1, first servo motor receives the instruction and begins to rotate, the W-shaped clamp plate 1014 is simultaneously close to the middle, the multi-rotor drone 10 is pushed to the middle of the landing platform 1 by the edge slope of the W-shaped clamp plate 1014 and clamped and locked, and the clamping contraction stroke is positioned by means of the two infrared sensors 1013.
As shown in fig. 3, the platform self-rotating mechanism 102 includes a second servo motor, a worm and gear assembly 1021, and a rotating platform 1022, the second servo motor is in transmission connection with the rotating platform 1022 through the worm and gear assembly 1021, the landing platform 1 is installed on the rotating platform 1022, and the second servo motor drives the rotating platform 1022 to rotate through the worm and gear assembly 1021, thereby driving the landing platform 1 to rotate.
Be provided with the joint 8 that charges on unmanned aerial vehicle foot rest clamping mechanism 101, be provided with on many rotor unmanned aerial vehicle 10's the foot rest with the joint 8 assorted that charges interface 9, through the joint 8 that charges on the unmanned aerial vehicle foot rest clamping mechanism 101 and the contact of the interface 9 that charges on many rotor unmanned aerial vehicle 10's the foot rest realize many rotor unmanned aerial vehicle 10 automatic charging function. When two W type clamp plates 1014 press from both sides tightly, the interface 9 that charges on many rotor unmanned aerial vehicle 10's the foot rest with charge the joint 8 to inserting the completion preparation work of charging, inside charges for the inside battery of organism through the foot rest hollow tube.
As shown in fig. 4, elevating system 2 includes third servo motor 201, speed reducer 202, lead screw module 203 and position detection sensor, third servo motor 201 is connected with speed reducer 202, speed reducer 202 is connected with the transmission of lead screw module 203, position detection sensor fixed mounting is in one side of lead screw module 203, and position detection sensor is provided with two, and two position sensors are fixed respectively at the initial stroke end of lead screw module 203, and when signal detection terminated position, motor stop motion, landing platform 1 rose to the highest position this moment, and multi-rotor unmanned aerial vehicle 10 is outside being lifted frame 3, alright carry out the executive task of taking off.
As shown in fig. 5, rack and pinion mechanism 6 includes fourth servo motor, gear 601 and rack 602, fourth servo motor fixed mounting is on frame 3, gear 601 key-type connection is on fourth servo motor's output shaft, rack 602 fixed mounting is inside hatch door 4, rack 602 meshes with gear 601 mutually, and when many rotor unmanned aerial vehicle 10 navigated back and descends to landing platform 1, the system received the signal of navigating back, and the back is opened to hatch door 4, and many rotor unmanned aerial vehicle 10 can descend to the platform on.
The structure principle is as follows: the utility model discloses possess the function of taking off and land, landing platform 1 simultaneously can self rotate 90 degrees to 180 degrees under platform self rotary mechanism 102's drive to in change battery and load, also do benefit to the unequal model of length and width size more conveniently and accomodate the inside of frame 3, drive positive and negative lead screw module 1011 through first servo motor 1012, can realize the relative motion of clamping direction through a motor, the synchronism when the W type clamp plate 1014 of assurance is tight.
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 (6)
1. The utility model provides a many rotor unmanned aerial vehicle descending device, includes descending platform (1), elevating system (2), frame (3), hatch door (4) and antenna (5), its characterized in that: elevating system (2) fixed mounting is on frame (3), linear guide (7) are installed to elevating system (2) both sides, linear guide (7) are fixed on frame (3), descending platform (1) fixed mounting is on the slider of elevating system (2), be provided with many rotor unmanned aerial vehicle (10) on descending platform (1), descending platform (1) includes unmanned aerial vehicle foot rest clamping mechanism (101) and platform self rotary mechanism (102), hatch door (4) set up the top in frame (3), install on hatch door (4) antenna (5), be provided with rack and pinion mechanism (6) on hatch door (4).
2. A multi-rotor drone landing gear according to claim 1, wherein: unmanned aerial vehicle foot rest clamping mechanism (101) are including positive and negative lead screw module (1011), first servo motor (1012), infrared sensor (1013) and W type clamp plate (1014), the output of positive and negative lead screw module (1011) and first servo motor (1012) passes through the coupling joint, one side at positive and negative lead screw module (1011) is fixed in infrared sensor (1013), W type clamp plate (1014) is fixed on the slider of positive and negative lead screw module (1011).
3. A multi-rotor drone landing gear according to claim 1, wherein: the self-rotating mechanism (102) of the platform comprises a second servo motor, a worm and gear assembly (1021) and a rotating platform (1022), the second servo motor is in transmission connection with the rotating platform (1022) through the worm and gear assembly (1021), and the landing platform (1) is installed on the rotating platform (1022).
4. A multi-rotor drone landing gear according to claim 1, wherein: the lifting mechanism (2) comprises a third servo motor (201), a speed reducer (202), a screw rod module (203) and a position detection sensor, the third servo motor (201) is connected with the speed reducer (202), the speed reducer (202) is in transmission connection with the screw rod module (203), and the position detection sensor is fixedly installed on one side of the screw rod module (203).
5. A multi-rotor drone landing gear according to claim 1, wherein: the gear rack mechanism (6) comprises a fourth servo motor, a gear (601) and a rack (602), the fourth servo motor is fixedly installed on the frame (3), the gear (601) is connected to an output shaft of the fourth servo motor in a key mode, the rack (602) is fixedly installed inside the cabin door (4), and the rack (602) is meshed with the gear (601).
6. A multi-rotor drone landing gear according to claim 1, wherein: be provided with joint (8) that charges on unmanned aerial vehicle foot rest clamping mechanism (101), be provided with on the foot rest of many rotor unmanned aerial vehicle (10) with the joint (8) assorted interface (9) that charges.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921487042.7U CN210455254U (en) | 2019-09-09 | 2019-09-09 | Many rotor unmanned aerial vehicle descending device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921487042.7U CN210455254U (en) | 2019-09-09 | 2019-09-09 | Many rotor unmanned aerial vehicle descending device |
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| Publication Number | Publication Date |
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| CN210455254U true CN210455254U (en) | 2020-05-05 |
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| CN201921487042.7U Active CN210455254U (en) | 2019-09-09 | 2019-09-09 | Many rotor unmanned aerial vehicle descending device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110435910A (en) * | 2019-09-09 | 2019-11-12 | 深圳市科卫泰实业发展有限公司 | A kind of multi-rotor unmanned aerial vehicle landing-gear |
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2019
- 2019-09-09 CN CN201921487042.7U patent/CN210455254U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110435910A (en) * | 2019-09-09 | 2019-11-12 | 深圳市科卫泰实业发展有限公司 | A kind of multi-rotor unmanned aerial vehicle landing-gear |
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