CN212605789U - Unmanned aerial vehicle commodity circulation conveyer - Google Patents

Abstract

The utility model relates to an unmanned aerial vehicle logistics transportation device, which comprises an unmanned aerial vehicle, wherein the bottom of the unmanned aerial vehicle is provided with a bottom cover, the bottom surface of the bottom cover is provided with a coaming plate, the bottom surface of the bottom cover at the inner side of the coaming plate is provided with an adjusting mechanism, the adjusting mechanism is connected with and drives an adjusting seat, four sides of the adjusting seat are respectively provided with an upper hinging table, the upper hinging table is hinged with a clamping jaw, the bottom surface of the end surface of the four sides of the coaming plate is provided with a lower hinging table, the lower hinging table is connected with and hinged with the middle part of the clamping jaw, the bottom of the clamping jaw is provided with a clamping plate, compared with the prior art, the stability of goods is poorer in the process of loading and transporting the unmanned aerial vehicle, the utility model adopts four clamping jaws which are distributed in an annular shape, namely, the adjusting seat is driven to, the goods are more stable, improve work efficiency effectively.

Description

Unmanned aerial vehicle commodity circulation conveyer

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle commodity circulation conveyer.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The ground personnel can track, locate, remotely control, telemeter and digitally transmit the ground personnel through radio equipment and the like.

In recent years, along with electronic commerce's development, freight delivery work development is rapid, artifical delivery goods cost time is longer, the cost is higher, and under the goods accumulational condition, can not in time reach the customer effectively in hand, the introduction of unmanned aerial vehicle technique, the efficiency of goods delivery has been improved greatly, avoid the delay problem of goods simultaneously effectively, in the prior art, unmanned aerial vehicle loads in the transportation, the stability of goods is relatively poor, and unmanned aerial vehicle's the in-process of taking off and land, bear the impact on ground and increase, can't guarantee the stability of goods.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing an unmanned aerial vehicle commodity circulation conveyer to in solving prior art unmanned aerial vehicle loading transportation, the stability of goods is relatively poor, and unmanned aerial vehicle's the in-process of taking off and land, the impact that bears ground increases, can't guarantee the stable problem of goods.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle commodity circulation conveyer, includes unmanned aerial vehicle, unmanned aerial vehicle's bottom is equipped with the bottom, the bottom surface of bottom is equipped with the bounding wall, damper is installed to the outer terminal surface of bounding wall both sides, guiding mechanism is installed to the bottom surface of bounding wall inboard, be equipped with the motor in the unmanned aerial vehicle, the motor is connected and is driven guiding mechanism, guiding mechanism connects and drives there is the adjustment seat, four sides of adjustment seat all are equipped with articulated platform, it has the jack catch to go up articulated platform articulated, the bottom surface of four side terminal surfaces of bounding wall all is equipped with down articulated platform, it is articulated with the middle part of jack catch to articulate the platform connection down, the bottom of jack catch is equipped.

Preferably, damper is provided with four, four damper distributes in pairs in the both sides of bounding wall, damper is including leading the seat, be equipped with the inner guide pole in leading the seat, the bottom sliding connection of inner guide pole has the support column, the bottom of leading the seat is equipped with the limiting plate, can carry out spacingly to the support column through limiting plate and the cooperation of leading the seat, and the structure is more stable.

Preferably, the top of support column is equipped with interior guide cavity, interior guide cavity and the cooperation of interior guide arm, the top of support column is equipped with the spring, and is concrete, the outside of guide arm including the spring housing is established, can further lead the support column through the cooperation of interior guide arm and interior guide cavity to carry out elastic support by the spring, thereby improve unmanned aerial vehicle anti-seismic performance effectively.

Preferably, the adjusting mechanism comprises a top seat, a guide pillar is arranged on the bottom surface of the top seat, the guide pillar is connected with the adjusting seat in a sliding mode, the bottom end of the guide pillar is connected with the base, a screw rod is connected between the base and the top seat in a rotating mode, the screw rod is in threaded connection with the adjusting seat, the adjusting seat can be guided through the guide pillar, the stability of the adjusting seat is improved, the screw rod rotates and drives the adjusting seat to vertically lift along the guide pillar, and the structure is more stable.

Preferably, the clamping jaws are four, the four clamping jaws are distributed on four sides of the adjusting seat in an annular mode, the top ends of the clamping jaws are provided with guide grooves, the guide grooves correspond to the upper hinge table, the hinge joints can be guided through the guide grooves, the structure is more reliable, and clamping jaw locking and interference are avoided.

Preferably, the tip of motor is equipped with the gear shell, the gear shell is connected with the top surface of bottom, be equipped with driving gear and driven gear in the gear shell, can encapsulate through the gear shell.

Preferably, the driving gear and the driven gear are respectively installed at the shaft ends of the motor and the screw rod, the driving gear is meshed with the driven gear, the driving gear can be driven by the motor to rotate, and then the driving gear is meshed with the driven gear to drive the screw rod to rotate, so that the structure is more stable.

The utility model discloses possess following beneficial effect at least:

1. the utility model adopts four claws distributed annularly, namely the adjusting seat is driven by the adjusting mechanism to vertically lift, and then the claws are driven by the adjusting seat to rotate around the lower hinged platform, so that the goods are clamped by the claws and are further supported and fixed by the clamping plates, the goods are more stable, and the working efficiency is effectively improved;

2. the utility model discloses set up four group and the crisscross damper of jack catch, avoid interfering with the motion of jack catch to it is more convenient that the dismouting is maintained, through limiting plate and guide holder cooperation, carries on spacingly to the support column, and through interior guide arm and interior guide chamber cooperation, further leads the support column, can carry out elastic support by the spring, thereby improves unmanned aerial vehicle anti-seismic performance effectively, and the structure is more stable.

Drawings

Fig. 1 is a schematic view of the structure of the present invention;

FIG. 2 is a schematic cross-sectional view of FIG. 1;

FIG. 3 is a schematic sectional view of the structure at A-A in FIG. 2.

In the reference symbols: 1. an unmanned aerial vehicle; 2. a bottom cover; 3. enclosing plates; 4. a damping mechanism; 41. a guide seat; 42. A support pillar; 43. an inner guide rod; 44. an inner guide cavity; 45. a spring; 46. a limiting plate; 5. a claw; 6. A splint; 7. a lower hinge table; 8. an adjustment mechanism; 81. a top seat; 82. a base; 83. a screw; 84. a guide post; 9. an adjusting seat; 10. an upper hinge table; 11. a gear housing; 12. a motor; 13. a driving gear; 14. A driven gear; 15. a guide groove.

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 efforts belong to the protection scope of the present invention.

Examples

Referring to fig. 1-3, the present invention provides a technical solution: an unmanned aerial vehicle logistics transportation device comprises an unmanned aerial vehicle 1, wherein the bottom of the unmanned aerial vehicle 1 is provided with a bottom cover 2, the bottom surface of the bottom cover 2 is provided with a coaming 3, the outer end surfaces of two sides of the coaming 3 are provided with damping mechanisms 4, the bottom surface of the bottom cover 2 at the inner side of the coaming 3 is provided with an adjusting mechanism 8, the unmanned aerial vehicle 1 is internally provided with a motor 12, the motor 12 is connected with and drives the adjusting mechanism 8, the adjusting mechanism 8 is connected with and drives an adjusting seat 9, four sides of the adjusting seat 9 are respectively provided with an upper hinge table 10, the upper hinge tables 10 are hinged with a clamping jaw 5, particularly, the adjusting seat 9 is hinged with the top end of the clamping jaw 5, the bottom surfaces of the end surfaces of the four sides of the coaming 3 are respectively provided with a lower hinge table 7, the lower hinge tables 7 are connected with and hinged with the middle, life is higher to drive the vertical lift of adjustment seat 9 through guiding mechanism 8, and then drive jack catch 5 and rotate around hinge platform 7 down, can carry out the centre gripping by jack catch 5 to the goods, and further support fixedly through splint 6, the goods is more stable, improves work efficiency effectively.

Wherein, damper 4 is provided with four, four damper 4 distributes in pairs in the both sides of bounding wall 3, damper 4 is specific including guide 41, guide 41 is connected with bounding wall 3, be equipped with interior guide arm 43 in the guide 41, the bottom sliding connection of interior guide arm 43 has support column 42, guide 41's bottom is equipped with limiting plate 46, can be through limiting plate 46 and guide 41 cooperation, carries on spacingly to support column 42, and the structure is more stable.

Wherein, the top of support column 42 is equipped with interior guide cavity 44, interior guide cavity 44 cooperates with interior guide arm 43, the top of support column 42 is equipped with spring 45, and is specific, the outside of guide arm 43 is established including spring 45 cover, can further lead support column 42 through interior guide arm 43 and interior guide cavity 44 cooperation to carry out elastic support by spring 45, thereby improve unmanned aerial vehicle 1 anti-seismic performance effectively.

The adjusting mechanism 8 comprises a top seat 81, and is characterized in that the top seat 81 is installed on the bottom surface of the bottom cover 2, a guide pillar 84 is arranged on the bottom surface of the top seat 81, the guide pillar 84 is slidably connected with the adjusting seat 9, a base 82 is connected to the bottom end of the guide pillar 84, the adjusting seat 9 is located between the top seat 81 and the base 82, a screw 83 is rotatably connected between the base 82 and the top seat 81, the screw 83 is in threaded connection with the adjusting seat 9, the adjusting seat 9 can be guided through the guide pillar 84, the stability of the adjusting seat 9 is improved, the screw 83 rotates and drives the adjusting seat 9 to vertically lift along the guide pillar 84, and the structure is more stable.

The four clamping jaws 5 are annularly distributed on four sides of the adjusting seat 9, the top end of each clamping jaw 5 is provided with a guide groove 15, the guide grooves 15 correspond to the upper hinge table 10, the hinge points can be guided through the guide grooves 15, the structure is more reliable, and meanwhile the clamping jaws 5 are prevented from being locked and interfered.

Wherein, the tip of motor 12 is equipped with gear shell 11, gear shell 11 is connected with the top surface of bottom 2, be equipped with driving gear 13 and driven gear 14 in the gear shell 11, can encapsulate through gear shell 11.

Wherein, driving gear 13 and driven gear 14 are installed respectively at the axle head of motor 12 and screw rod 83, just driving gear 13 and driven gear 14 meshing, drive driving gear 13 by motor 12 and rotate, drive screw rod 83 and rotate by driving gear 13 and driven gear 14 meshing, and the structure is more stable.

The working principle is as follows: when the clamping device is used, the driving gear 13 is driven to rotate through the motor 12, the driving gear 13 is meshed with the driven gear 14, the screw 83 is driven to rotate, the adjusting seat 9 is driven to vertically lift along the guide post 84 by the screw 83, the clamping jaw 5 is driven to rotate around the lower hinge table 7, then the clamping jaw 5 can clamp goods, the goods are further supported and fixed through the clamping plate 6, the goods are more stable, and the working efficiency is effectively improved;

and, the in-process takes off and land of unmanned aerial vehicle 1, ground impact passes through support column 42 conduction to lead the chamber 44 cooperation in through interior guide arm 43 and interior, lead, can carry out elastic support by spring 45, thereby improve 1 anti-seismic performance of unmanned aerial vehicle effectively.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

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 (7)

1. An unmanned aerial vehicle logistics transportation device is characterized by comprising an unmanned aerial vehicle (1), wherein the bottom of the unmanned aerial vehicle (1) is provided with a bottom cover (2), the bottom surface of the bottom cover (2) is provided with a coaming plate (3), the outer end faces of two sides of the coaming plate (3) are provided with damping mechanisms (4), the bottom surface of the bottom cover (2) on the inner side of the coaming plate (3) is provided with an adjusting mechanism (8), the unmanned aerial vehicle (1) is internally provided with a motor (12), the motor (12) is connected with and drives the adjusting mechanism (8), the adjusting mechanism (8) is connected with and drives an adjusting seat (9), four sides of the adjusting seat (9) are respectively provided with an upper hinge table (10), the upper hinge table (10) is hinged with a clamping jaw (5), the bottom surfaces of the end faces of four sides of the coaming plate (3) are respectively provided with a lower hinge table (7), the lower, the bottom of the clamping jaw (5) is provided with a clamping plate (6).

2. The unmanned aerial vehicle logistics transportation device of claim 1, wherein: damper (4) are provided with four, four damper (4) distribute in pairs in the both sides of bounding wall (3), damper (4) are including leading seat (41), be equipped with interior guide arm (43) in leading seat (41), the bottom sliding connection of interior guide arm (43) has support column (42), the bottom of leading seat (41) is equipped with limiting plate (46).

3. The unmanned aerial vehicle logistics transportation device of claim 2, wherein: the top of support column (42) is equipped with interior guide chamber (44), interior guide chamber (44) and interior guide arm (43) cooperation, the top of support column (42) is equipped with spring (45), and is specific, the outside of guide arm (43) including is established to spring (45) cover.

4. The unmanned aerial vehicle logistics transportation device of claim 1, wherein: the adjusting mechanism (8) comprises a top seat (81), a guide pillar (84) is arranged on the bottom surface of the top seat (81), the guide pillar (84) is in sliding connection with the adjusting seat (9), the bottom end of the guide pillar (84) is connected with a base (82), a screw rod (83) is rotatably connected between the base (82) and the top seat (81), and the screw rod (83) is in threaded connection with the adjusting seat (9).

5. The unmanned aerial vehicle logistics transportation device of claim 1, wherein: the four clamping jaws (5) are annularly distributed on four sides of the adjusting seat (9), a guide groove (15) is formed in the top end of each clamping jaw (5), and the guide groove (15) corresponds to the upper hinge table (10).

6. The unmanned aerial vehicle logistics transportation device of claim 1, wherein: the end of the motor (12) is provided with a gear shell (11), the gear shell (11) is connected with the top surface of the bottom cover (2), and a driving gear (13) and a driven gear (14) are arranged in the gear shell (11).

7. The unmanned aerial vehicle logistics transportation device of claim 6, wherein: the driving gear (13) and the driven gear (14) are respectively arranged at the shaft ends of the motor (12) and the screw (83), and the driving gear (13) is meshed with the driven gear (14).

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