CN116654265B - Civil express delivery load unmanned aerial vehicle - Google Patents
Civil express delivery load unmanned aerial vehicle Download PDFInfo
- Publication number
- CN116654265B CN116654265B CN202310963232.6A CN202310963232A CN116654265B CN 116654265 B CN116654265 B CN 116654265B CN 202310963232 A CN202310963232 A CN 202310963232A CN 116654265 B CN116654265 B CN 116654265B
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- unmanned aerial
- aerial vehicle
- clamping
- express delivery
- rod
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- 230000005540 biological transmission Effects 0.000 claims abstract description 38
- 210000000078 claw Anatomy 0.000 claims abstract description 25
- 230000035939 shock Effects 0.000 claims description 33
- 238000010521 absorption reaction Methods 0.000 claims description 22
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 238000013016 damping Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 230000000670 limiting effect Effects 0.000 description 4
- 239000006096 absorbing agent Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D43/00—Lids or covers for rigid or semi-rigid containers
- B65D43/26—Mechanisms for opening or closing, e.g. pedal-operated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/02—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
- B65D81/05—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
- B65D81/07—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents using resilient suspension means
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Warehouses Or Storage Devices (AREA)
- Vibration Dampers (AREA)
Abstract
The invention discloses a civil express delivery load unmanned aerial vehicle, which relates to the technical field of load unmanned aerial vehicles and comprises an unmanned aerial vehicle component, wherein a clamping component is arranged at the bottom end of the unmanned aerial vehicle component, an express delivery transport component is arranged below the unmanned aerial vehicle component, and a buffer component is arranged at the bottom end of the express delivery transport component. The invention solves the problem of poor stability of the existing clamping jaw through the arrangement of the clamping assembly, the transmission case, the clamping claws, the transmission rod, the inner slide block, the magnetic end-sucking rod, the conical rings and the connecting rod, can drive the two groups of conical rings to rotate by starting the double-shaft motor, can push the multiple groups of clamping claws to rotate under the reset force of the reset spring and under the cooperation of the transmission rod and the inner slide block, can play the role of loosening the express box, effectively avoids the problem of power consumption of the traditional unmanned truck for independently driving the multiple groups of clamping claws, and can simultaneously loosen the express box due to the symmetrical arrangement of the two pairs of clamping claws, thereby greatly improving the stability of the unmanned truck.
Description
Technical Field
The invention relates to the technical field of load-carrying unmanned aerial vehicles, in particular to a civil express load-carrying unmanned aerial vehicle.
Background
Unmanned aerial vehicles are called "unmanned aerial vehicles" for short, english abbreviations are "UAVs", unmanned aerial vehicles which are operated by radio remote control equipment and self-provided program control devices or are operated by vehicle-mounted computers completely or intermittently and autonomously, and compared with unmanned aerial vehicles, unmanned aerial vehicles are more suitable for tasks which are too "fool, dirty or dangerous", the unmanned aerial vehicles can be divided into military and civil use according to application fields, military aspects, unmanned aerial vehicles are divided into reconnaissance and target-aircraft civil aspects, and unmanned aerial vehicle + industry application is really just needed; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies.
The existing unmanned aerial vehicle type is more including the load unmanned aerial vehicle that can transport the express delivery therein, and current load unmanned aerial vehicle side is provided with the multiunit clamping jaw generally, need drive multiunit clamping jaw one by one when using to the express delivery case centre gripping, leads to its power consumption great to lead to its stability greatly reduced, when meetting strong wind, the condition that the express delivery case emptys appears easily, exists certain limitation.
The existing express delivery load unmanned aerial vehicle bottom is provided with the express delivery case generally, and the express delivery case when using, needs manual closing its end cover, and load unmanned aerial vehicle is placing the back to the express delivery case, needs the manual work to open its end cover, has certain inconvenience.
Disclosure of Invention
Based on the above, the invention aims to provide a civil express delivery loading unmanned aerial vehicle so as to solve the technical problems in the background.
In order to achieve the above purpose, the present invention provides the following technical solutions: the civil express delivery load unmanned aerial vehicle comprises an unmanned aerial vehicle assembly, wherein a clamping assembly is arranged at the bottom end of the unmanned aerial vehicle assembly, an express delivery transportation assembly is arranged below the unmanned aerial vehicle assembly, and a buffer assembly is arranged at the bottom end of the express delivery transportation assembly;
the unmanned aerial vehicle assembly comprises an unmanned aerial vehicle body;
the clamping assembly comprises a transmission case fixed at the bottom end of the unmanned aerial vehicle body, the clamping assembly comprises two pairs of clamping claws rotationally connected with the side wall of the unmanned aerial vehicle body, a transmission rod is rotationally arranged below the unmanned aerial vehicle body on the side wall of the clamping claws, the other end of the transmission rod extends to the inside of the transmission case to rotationally connect with an inner slide block, the inner slide block slides on the inner wall of the transmission case, the inner wall of the transmission case rotationally has a connecting rod penetrating through the magnetic end rod, and the end part of the connecting rod is fixedly provided with a taper ring contacted with the side wall of the magnetic end rod;
the express delivery transportation assembly comprises a clamping side block fixed on the side wall of the clamping claw, an end cover is arranged on the side wall of the clamping side block, and an express delivery box body slides at the bottom end of the end cover;
the buffer component comprises a shock absorption box sliding at the bottom end of the express box body.
Preferably, unmanned aerial vehicle body top is provided with multiunit unmanned aerial vehicle wing, and multiunit unmanned aerial vehicle wing is rectangle permutation and distributes, unmanned aerial vehicle camera is installed on unmanned aerial vehicle body top.
Preferably, the two pairs of clamping claws are symmetrically arranged relative to the vertical central axis of the unmanned aerial vehicle body, clamping grooves matched with the magnetic attraction end rods are formed in the end parts of the conical rings, and straight sliding grooves matched with the magnetic attraction end rods are formed in the inner wall of the transmission case.
Preferably, the transmission case is internally provided with a double-shaft motor between the two groups of taper rings, the double-shaft motor is connected with the connecting rod through a coupler, and the side wall of the magnetic attraction end rod is provided with a through hole matched with the connecting rod.
Preferably, the clamping groove matched with the clamping side block is formed in the side wall of the end cover, the rotating plate is arranged on the side wall of the end cover in a rotating mode, the pushing plate is arranged on the other side of the rotating plate in a rotating mode, the connecting sliding rod connected with the inner wall of the end cover in a sliding mode is arranged on the other side of the pushing plate in a rotating mode, multiple groups of inserting blocks are fixed on the side wall of the connecting sliding rod, inserting plates are fixed on one side, located inside the express box body, of the connecting sliding rod, and multiple groups of inserting grooves matched with the inserting blocks are formed in the side wall of the inserting plates.
Preferably, a stop bar is fixed on one side of the side wall of the end cover, which is positioned on one side of the rotating plate; and the stop bar is contacted with the side wall of the rotating plate, and a torsion spring is fixed between the rotating plate and the clamping groove.
Preferably, the inner wall of the shock absorption box is fixed with an inner fixing rod, two groups of shock absorption rods are rotated at the bottom end of the express box body, shock absorption sliding sleeves sleeved on the side walls of the inner fixing rods are rotated at the bottom ends of the shock absorption rods, shock absorption springs are fixed between the two groups of shock absorption sliding sleeves, and a damper is fixed between the bottom end of the express box body and the inner wall of the shock absorption box.
Preferably, the multiunit unmanned aerial vehicle wing bottom is located the inside driving motor that is provided with of unmanned aerial vehicle body.
In summary, the invention has the following advantages:
the invention solves the problem of poor stability of the existing clamping jaw through the arrangement of the clamping assembly, the transmission case, the clamping claws, the transmission rod, the inner slide block, the magnetic end-sucking rod, the conical rings and the connecting rod, can drive the two groups of conical rings to rotate by starting the double-shaft motor, can push the multiple groups of clamping claws to rotate under the reset force of the reset spring and under the cooperation of the transmission rod and the inner slide block, can play a role of loosening the express box, effectively avoids the problem of power consumption of the traditional load unmanned plane for independently driving the multiple groups of clamping claws, and can simultaneously loosen the express box due to the symmetrical arrangement of the two pairs of clamping claws, thereby greatly improving the stability of the express box;
according to the invention, through the arrangement of the end cover, the express box body, the clamping side blocks, the rotating plate, the pushing plate, the connecting sliding rod, the plug-in block and the plug-in plate, the problem that the existing load unmanned aerial vehicle is inconvenient to open and close the express box is solved, the clamping claw can push the rotating plate to turn over when clamping the end cover, and the plug-in block and the plug-in plate can be clamped with the plug-in plate under the mutual cooperation of the pushing plate, the connecting sliding rod, the plug-in block and the plug-in plate, so that the effect of clamping the end cover and the express box body can be achieved, and inconvenience in the traditional manual closing of the express box is avoided;
according to the invention, through the arrangement of the shock absorption box, the shock absorption rods, the shock absorption sliding sleeves, the inner fixing rods, the shock absorption springs and the dampers, the problem that the shock absorption effect is poor due to the simple structure of the conventional load unmanned aerial vehicle express box is solved, when the shock absorption box collides, the shock absorption rods can be extruded to rotate, the shock absorption springs fixed between the two groups of shock absorption sliding sleeves can be extruded to compress, and under the cooperation of the dampers, the vertical force can be converted into the inclined force, so that the shock absorption effect is greatly improved, and the damage to articles in the express box is avoided.
Drawings
Fig. 1 is a front perspective view of a drone body of the present invention;
fig. 2 is a perspective view of the bottom surface of the unmanned aerial vehicle body of the present invention;
fig. 3 is a front cross-sectional view of the unmanned aerial vehicle body of the present invention;
FIG. 4 is an enlarged view of a portion of FIG. 3A in accordance with the present invention;
FIG. 5 is a perspective view of a cone ring according to the present invention;
fig. 6 is a side cross-sectional view of the unmanned aerial vehicle body of the present invention;
FIG. 7 is an enlarged view of a portion of B of FIG. 6 in accordance with the present invention;
FIG. 8 is a top cross-sectional view of an end cap of the present invention;
FIG. 9 is a schematic view of a buffer assembly according to the present invention.
In the figure: 100. an unmanned aerial vehicle assembly; 110. an unmanned aerial vehicle body; 120. unmanned aerial vehicle wings;
200. a clamping assembly; 210. a transmission case; 220. clamping claws; 230. a transmission rod; 240. an inner slide; 250. a magnetic end rod; 260. a conical ring; 270. a connecting rod;
300. an express delivery transport component; 310. an end cap; 320. an express box body; 330. clamping the side blocks; 340. a rotating plate; 350. a pushing plate; 360. connecting a slide bar; 370. a plug block; 380. a plug board;
400. a buffer assembly; 410. a damper box; 420. a shock-absorbing rod; 430. damping sliding sleeve; 440. an inner fixing rod; 450. a damping spring; 460. a damper.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. The embodiments described below by referring to the drawings are illustrative only and are not to be construed as limiting the invention.
Hereinafter, an embodiment of the present invention will be described in accordance with its entire structure.
1-9, the civil express carrying unmanned aerial vehicle comprises an unmanned aerial vehicle assembly 100, wherein a clamping assembly 200 is arranged at the bottom end of the unmanned aerial vehicle assembly 100, an express transportation assembly 300 is arranged below the unmanned aerial vehicle assembly 100, and a buffer assembly 400 is arranged at the bottom end of the express transportation assembly 300;
the unmanned aerial vehicle assembly 100 comprises a unmanned aerial vehicle body 110;
the clamping assembly 200 comprises a transmission case 210 fixed at the bottom end of the unmanned aerial vehicle body 110, the clamping assembly 200 comprises two pairs of clamping claws 220 rotationally connected with the side wall of the unmanned aerial vehicle body 110, a transmission rod 230 is rotationally arranged below the unmanned aerial vehicle body 110 on the side wall of the clamping claws 220, the other end of the transmission rod 230 extends to the inside of the transmission case 210 and is rotationally connected with an inner sliding block 240, the inner sliding block 240 slides on the inner wall of the transmission case 210, a connecting rod 270 penetrating through the magnetic attraction end rod 250 is rotationally arranged on the inner wall of the transmission case 210, and a conical ring 260 contacted with the side wall of the magnetic attraction end rod 250 is fixed at the end part of the connecting rod 270;
the express delivery transportation assembly 300 comprises a clamping side block 330 fixed on the side wall of the clamping claw 220, an end cover 310 is arranged on the side wall of the clamping side block 330, and an express delivery box body 320 is arranged at the bottom end of the end cover 310 in a sliding manner;
the buffer assembly 400 includes a shock-absorbing box 410 sliding on the bottom end of the express box body 320;
the unmanned aerial vehicle comprises an unmanned aerial vehicle body 110, a plurality of groups of unmanned aerial vehicle wings 120 are arranged at the top end of the unmanned aerial vehicle body 110, the plurality of groups of unmanned aerial vehicle wings 120 are distributed in a rectangular array, unmanned aerial vehicle cameras are arranged at the top end of the unmanned aerial vehicle body 110, two pairs of clamping claws 220 are symmetrically arranged about the vertical central axis of the unmanned aerial vehicle body 110, clamping grooves matched with magnetic suction end rods 250 are formed in the end parts of conical rings 260, straight sliding grooves matched with the magnetic suction end rods 250 are formed in the inner walls of a transmission case 210, a double-shaft motor is arranged between the two groups of conical rings 260 in the transmission case 210, the double-shaft motor is connected with a connecting rod 270 through a coupling, through holes matched with the connecting rod 270 are formed in the side walls of the magnetic suction end rods 250, clamping grooves matched with clamping side blocks 330 are formed in the side walls of an end cover 310, a rotating plate 340 is arranged on the side walls of the end cover 310, a pushing plate 350 is arranged on the other side of the rotating plate 340, connecting sliding rods 360 connected with the inner walls of the end cover 310 in a sliding mode, a plurality of groups of plug-in blocks 370 are fixed on the side of the connecting sliding rods 360, a plug-in block 360 side is fixed on one side of the connecting rod, plug-in side of the connecting box 320, plug-in blocks 380 side are arranged on the side of the side wall, and matched side walls of the plug-in the side with the side of the plug-in plate 310; and the shelves contact with the revolving plate 340 lateral wall, be fixed with the torsional spring between revolving plate 340 and the grip slot, damper box 410 inner wall is fixed with internal fixation pole 440, the express delivery case body 320 bottom is rotated there are two sets of damper rods 420, damper rod 420 bottom is rotated there is cup joints in the damping sliding sleeve 430 of internal fixation pole 440 lateral wall, be fixed with damping spring 450 between two sets of damping sliding sleeve 430, be fixed with attenuator 460 between express delivery case body 320 bottom and the damper box 410 inner wall, multiunit unmanned aerial vehicle wing 120 bottom is located unmanned aerial vehicle body 110 inside and is provided with driving motor, be fixed with reset spring between inner sliding block 240 and the transmission case 210.
When the express box needs to be clamped, the double-shaft motor can be started to drive the two groups of connecting rods 270 to rotate around the contact position with the inner wall of the transmission box 210, then drive the two groups of taper rings 260 with fixed ends to rotate around the contact position with the inner wall of the transmission box 210, then push the magnetic attraction end rod 250 with fixed side walls, push the inner sliding block 240 with fixed side walls of the magnetic attraction end rod 250 to slide on the inner wall of the transmission box 210, then push the transmission rod 230 to rotate around the contact position with the clamping claws 220, push the clamping side blocks 330 with fixed side walls of the clamping claws 220 to contact with the end cover 310, so that the clamping effect can be achieved, meanwhile, the side walls of the clamping side blocks 330 are contacted with the side walls of the rotating plate 340, the connecting sliding rods 360 with fixed side walls of the connecting sliding rods 360 can slide on the inner wall of the end cover 310, then the multiple groups of the connecting sliding rods 370 are clamped with the connecting plates 380, the bottom ends of the shock absorbing box 410 are in a limiting effect, when the bottom ends of the express box are impacted, the bottom ends of the shock absorbing box 410 are contacted with the ground, the shock absorbing box body 320 is shortened, the distance between the shock absorbing box 410 and the side blocks 320 is shortened, the shock absorbing body is in the shock absorbing body 430 can be compressed by the shock absorbing body 430, and the shock absorbing body 430 can be matched with the shock absorbing body 430, and the shock absorber body 430 can be compressed with the shock absorber body 430.
When in use, when the express delivery case needs to be clamped, the double-shaft motor can be started to drive the two groups of connecting rods 270 to rotate around the contact position with the inner wall of the transmission case 210, and the clamping side blocks 330 fixed on the side walls of the multiple groups of clamping claws 220 can be pushed to be in contact with the end covers 310 under the cooperation of the clamping assembly 200, so that the clamping effect can be achieved, meanwhile, under the cooperation of the express delivery transportation assembly 300, the multiple groups of plug-in blocks 370 fixed on the side walls of the connecting sliding rods 360 can be clamped with the plug-in plates 380, the limiting effect is achieved, when the bottom end of the express delivery case is impacted, the bottom end of the shock absorption case 410 is in contact with the ground, the distance between the shock absorption case 410 and the express delivery case body 320 is shortened, and the shock absorption and buffering effects can be achieved under the cooperation of the buffer assembly 400.
Although embodiments of the invention have been shown and described, the detailed description is to be construed as exemplary only and is not limiting of the invention as the particular features, structures, materials, or characteristics may be combined in any suitable manner in any one or more embodiments or examples, and modifications, substitutions, variations, etc. may be made in the embodiments as desired by those skilled in the art without departing from the principles and spirit of the invention, provided that such modifications are within the scope of the appended claims.
Claims (6)
1. The utility model provides a civilian express delivery load unmanned aerial vehicle, includes unmanned aerial vehicle subassembly (100), its characterized in that: the automatic delivery system comprises an unmanned aerial vehicle assembly (100), wherein a clamping assembly (200) is arranged at the bottom end of the unmanned aerial vehicle assembly (100), an express delivery transportation assembly (300) is arranged below the unmanned aerial vehicle assembly (100), and a buffer assembly (400) is arranged at the bottom end of the express delivery transportation assembly (300);
the unmanned aerial vehicle assembly (100) comprises an unmanned aerial vehicle body (110);
the clamping assembly (200) comprises a transmission case (210) fixed at the bottom end of the unmanned aerial vehicle body (110), the clamping assembly (200) comprises two pairs of clamping claws (220) rotationally connected with the side wall of the unmanned aerial vehicle body (110), a transmission rod (230) is rotationally arranged below the unmanned aerial vehicle body (110) on the side wall of the clamping claws (220), an inner sliding block (240) is rotationally connected to the inside of the transmission case (210) from the other end of the transmission rod (230), the inner sliding block (240) slides on the inner wall of the transmission case (210), a connecting rod (270) penetrating through a magnetic end rod (250) is rotationally arranged on the inner wall of the transmission case (210), conical rings (260) in contact with the side wall of the magnetic end rod (250) are fixed at the end parts of the connecting rod (270), a double-shaft motor is arranged between the two groups of the conical rings (260) inside the transmission case (210), the double-shaft motor is connected with the connecting rod (270) through a coupler, and a through hole matched with the connecting rod (270) is formed on the side wall of the magnetic end rod (250);
the express delivery transportation assembly (300) comprises clamping side blocks (330) fixed on the side walls of the clamping claws (220), end covers (310) are arranged on the side walls of the clamping side blocks (330), express delivery box bodies (320) are arranged at the bottom ends of the end covers (310) in a sliding mode, clamping grooves matched with the clamping side blocks (330) are formed in the side walls of the end covers (310), rotating plates (340) are arranged on the side walls of the end covers (310) in a rotating mode, pushing plates (350) are arranged on the other sides of the rotating plates (340) in a rotating mode, connecting sliding rods (360) are arranged on the other sides of the pushing plates (350) in a rotating mode and are connected with the inner walls of the end covers (310) in a sliding mode, multiple groups of inserting blocks (370) are fixed on the side walls of the connecting sliding rods (360), and multiple groups of inserting grooves matched with the inserting blocks (370) are formed in the side walls of the inserting blocks (380).
The buffer assembly (400) comprises a shock absorption box (410) sliding at the bottom end of the express box body (320).
2. The civil express delivery load unmanned aerial vehicle of claim 1, wherein: unmanned aerial vehicle body (110) top is provided with multiunit unmanned aerial vehicle wing (120), and multiunit unmanned aerial vehicle wing (120) are rectangle permutation and distribute, unmanned aerial vehicle camera is installed on unmanned aerial vehicle body (110) top.
3. The civil express delivery load unmanned aerial vehicle of claim 1, wherein: two pairs of clamping claws (220) are symmetrically arranged about the vertical central axis of the unmanned aerial vehicle body (110), clamping grooves matched with the magnetic attraction end rod (250) are formed in the end parts of the conical rings (260), and straight sliding grooves matched with the magnetic attraction end rod (250) are formed in the inner wall of the transmission case (210).
4. The civil express delivery load unmanned aerial vehicle of claim 1, wherein: a stop bar is fixed on one side of the side wall of the end cover (310) positioned on one side of the rotating plate (340); and the baffle strip is contacted with the side wall of the rotating plate (340), and a torsion spring is fixed between the rotating plate (340) and the clamping groove.
5. The civil express delivery load unmanned aerial vehicle of claim 1, wherein: the novel automatic shock-absorbing box is characterized in that an inner fixing rod (440) is fixed on the inner wall of the shock-absorbing box (410), two groups of shock-absorbing rods (420) are arranged at the bottom end of the express box body (320) in a rotating mode, shock-absorbing sliding sleeves (430) sleeved on the side walls of the inner fixing rod (440) are arranged at the bottom ends of the shock-absorbing rods (420) in a rotating mode, shock-absorbing springs (450) are fixed between the two groups of shock-absorbing sliding sleeves (430), and dampers (460) are fixed between the bottom end of the express box body (320) and the inner wall of the shock-absorbing box (410).
6. The civil express delivery load unmanned aerial vehicle of claim 2, wherein: the multiunit unmanned aerial vehicle wing (120) bottom is located unmanned aerial vehicle body (110) inside and is provided with driving motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310963232.6A CN116654265B (en) | 2023-08-02 | 2023-08-02 | Civil express delivery load unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310963232.6A CN116654265B (en) | 2023-08-02 | 2023-08-02 | Civil express delivery load unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN116654265A CN116654265A (en) | 2023-08-29 |
| CN116654265B true CN116654265B (en) | 2023-11-17 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202310963232.6A Active CN116654265B (en) | 2023-08-02 | 2023-08-02 | Civil express delivery load unmanned aerial vehicle |
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| CN116654265A (en) | 2023-08-29 |
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