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CN-224211261-U - Unmanned aerial vehicle carries goods nacelle structure

CN224211261UCN 224211261 UCN224211261 UCN 224211261UCN-224211261-U

Abstract

The utility model discloses an unmanned aerial vehicle cargo nacelle structure, which relates to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle and a preliminary limiting assembly, wherein the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a landing gear, a top cross rod, a bottom cross rod and a supporting baffle rod, the preliminary limiting assembly is used for providing preliminary limiting operation for bottoms at two ends of a cargo box, a telescopic reinforcing assembly is arranged between the top cross rod and the bottom cross rod and used for limiting the side face of the cargo box, and meanwhile, when the unmanned aerial vehicle is lifted off during operation, the tops at two ends of the cargo box are reinforced and limited through the telescopic reinforcing assembly. According to the utility model, six-face limiting of the container can be realized by arranging the primary limiting assembly, the telescopic reinforcing assembly and the supporting baffle rod, the locking operation is not required during the installation of the container, and only one convex baffle plate is required to be pressed during the disassembly of the container, so that the whole operation is simple and convenient, and the quick transfer requirement of the container can be met.

Inventors

  • LIU HAI

Assignees

  • 北京天桥华昌科技有限公司

Dates

Publication Date
20260508
Application Date
20250430

Claims (5)

  1. 1. The utility model provides an unmanned aerial vehicle carries cargo pod structure, includes unmanned aerial vehicle (1) that comprises unmanned aerial vehicle main part (101), undercarriage (102) are provided with four, four undercarriage (102) are the rectangle and distribute and be fixed in unmanned aerial vehicle main part (101) bottom, its characterized in that, two that horizontal transverse distributes undercarriage (102) are middle to be fixed with top horizontal pole (103), bottom horizontal pole (104) distribute in the below of top horizontal pole (103), two all be fixed with a plurality of support shelves pole (105) between top horizontal pole (103) and two bottom horizontal poles (104), undercarriage (102), top horizontal pole (103), bottom horizontal pole (104), support shelves pole (105) constitute the goods shelves structure that supplies packing box (4) to place; The two ends of the two bottom cross bars (104) are provided with preliminary limiting assemblies (2), and the preliminary limiting assemblies (2) are used for providing preliminary limiting operation for bottoms of two ends of a container (4); The utility model discloses a cargo box, including top horizontal pole (103), bottom horizontal pole (104), top horizontal pole (103) and bottom horizontal pole (104) are connected in series, be provided with flexible reinforcement subassembly (3) between top horizontal pole (103) and bottom horizontal pole (104), flexible reinforcement subassembly (3) are used for spacing the side of packing box (4), simultaneously, when unmanned aerial vehicle (1) operation lift-off, consolidate spacingly through flexible reinforcement subassembly (3) to the both ends top of packing box (4).
  2. 2. The unmanned aerial vehicle cargo pod structure according to claim 1, wherein the preliminary limit assembly (2) comprises a vertical rail (201), a bottom plate (202), a convex baffle (203), a limit slider (204), and a Z-shaped spring piece (205); The two vertical rails (201) are symmetrically fixed at the bottom ends of one ends of the two bottom crossbars (104), and the bottom plate (202) is fixed at the bottoms of the two vertical rails (201); The limiting sliding blocks (204) are symmetrically fixed on two sides of the convex baffle plates (203), and the convex baffle plates (203) are distributed between the two vertical tracks (201) and are in sliding connection with the vertical tracks (201) through the limiting sliding blocks (204); The Z-shaped elastic pieces (205) are distributed between the convex baffle (203) and the bottom plate (202), and the upper end and the lower end of the Z-shaped elastic pieces (205) are fixedly connected with the bottom of the convex baffle (203) and the top of the bottom plate (202) respectively; the two groups of the preliminary limiting assemblies (2) are symmetrically distributed at two ends of the bottom cross rod (104), and two convex baffles (203) in the two groups of the preliminary limiting assemblies (2) are used for limiting bottoms of two ends of the container (4).
  3. 3. An unmanned aerial vehicle cargo pod structure according to claim 2, wherein the tops of the protruding baffles (203) protrude above the supporting bars (105), and the ends of the tops of the two protruding baffles (203) that are remote from each other are in a cambered surface structure.
  4. 4. An unmanned aerial vehicle cargo pod structure according to claim 2, wherein the telescopic reinforcement assembly (3) comprises side baffles (301), vertical straight slots (302), L-shaped shells (303), buffer bottom blocks (304), W-shaped spring plates (305), inverted concave reinforcement plates (306); The vertical straight notch (302) is formed in the side face of the side baffle (301) and completely penetrates through the other side of the side baffle (301), and the side baffle (301) is distributed on the inner sides of the top cross rod (103) and the bottom cross rod (104) and is in sliding connection with the supporting baffle rods (105) on the top cross rod (103) and the bottom cross rod (104) through the vertical straight notch (302); The L-shaped shell (303) is distributed on the outer sides of the top cross rod (103) and the bottom cross rod (104) and is fixedly connected with the side baffle (301), the buffer bottom block (304) is fixed on the bottoms of the side baffle (301) and the vertical straight notch (302), the W-shaped elastic sheet (305) is distributed between the side baffle (301) and the vertical straight notch (302) and is positioned between the bottom cross rod (104) and the buffer bottom block (304), and the upper end and the lower end of the W-shaped elastic sheet (305) are respectively fixed with the bottoms of the bottom cross rod (104) and the buffer bottom block (304); The inverted concave reinforcing plates (306) are distributed above the supporting baffle rods (105) on the top cross rod (103), and the inverted concave reinforcing plates (306) are fixedly connected with the two side baffles (301) through connecting plates; When unmanned aerial vehicle (1) lift-off, side baffle (301), vertical straight notch (302), buffering bottom block (304), undercut reinforcing plate (306) wholly move downwards under the elasticity effect of W type shell fragment (305), move the both ends of laminating packing box (4) downwards through the vertical portion in both ends of undercut reinforcing plate (306) for realize the spacing reinforcement on packing box (4) both ends upper portion.
  5. 5. The unmanned aerial vehicle cargo pod structure according to claim 4, wherein the distance between the two vertical portions of the inverted concave reinforcement plate (306) and the distance between the two convex baffles (203) are matched with the length of the cargo box (4), the height of the cargo box (4) is matched with the distance between the upper and lower sets of support bars (105), and the distance between the two side baffles (301) is matched with the width of the cargo box (4).

Description

Unmanned aerial vehicle carries goods nacelle structure Technical Field The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle cargo nacelle structure. Background Unmanned aerial vehicle is called "unmanned aerial vehicle" for short, is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, perhaps by the on-board computer completely or intermittently independently, along with unmanned aerial vehicle's technological development, utilize unmanned aerial vehicle to carry cargo transportation's operation more and more, for example unmanned aerial vehicle express delivery, through the unmanned low altitude aircraft delivery parcel that utilizes radio remote control equipment and self-contained program control device to operate, automatic delivery arrives at the destination, its advantage mainly lies in solving the delivery problem in remote area, improves delivery efficiency, simultaneously reduces the human cost. When carrying out cargo through unmanned aerial vehicle, in order to guarantee the stability of goods, need fix between goods and the unmanned aerial vehicle, convenient fixed, the split convenience between its goods and the unmanned aerial vehicle directly influence the goods transport efficiency, consequently, in order to realize the convenient dismouting of packing box and unmanned aerial vehicle, provide an unmanned aerial vehicle machine cargo pod structure. Disclosure of utility model The utility model aims to solve the problems in the background and provide an unmanned aerial vehicle cargo pod structure. The unmanned aerial vehicle cargo pod structure comprises an unmanned aerial vehicle consisting of an unmanned aerial vehicle main body and landing gears, wherein four landing gears are arranged and fixed at the bottom of the unmanned aerial vehicle main body in a rectangular distribution manner, a top cross rod and a bottom cross rod are fixed between two landing gears which are horizontally and transversely distributed, the bottom cross rod is distributed below the top cross rod, a plurality of supporting baffle rods are fixed between the two top cross rods and the two bottom cross rods, and the landing gears, the top cross rods, the bottom cross rods and the supporting baffle rods form a cargo rack structure for placing a cargo box; Preliminary limiting assemblies are arranged at the two ends of the two bottom cross bars, and the preliminary limiting assemblies are used for providing preliminary limiting operation for the bottoms of the two ends of the container; The top horizontal pole is provided with flexible reinforcement subassembly between the bottom horizontal pole, flexible reinforcement subassembly is used for spacing to the side of packing box, simultaneously, when unmanned aerial vehicle operation lift-off, consolidates spacingly through flexible reinforcement subassembly to the both ends top of packing box. As a still further proposal of the utility model, the preliminary limiting component comprises a vertical rail, a bottom plate, a convex baffle, a limiting slide block and a Z-shaped elastic sheet; The two vertical rails are symmetrically fixed at the bottom ends of one ends of the two bottom cross bars, and the bottom plate is fixed at the bottoms of the two vertical rails; The limiting sliding blocks are symmetrically fixed on two sides of the convex baffle, and the convex baffle is distributed between the two vertical tracks and is in sliding connection with the vertical tracks through the limiting sliding blocks; The Z-shaped elastic pieces are distributed between the convex baffle and the bottom plate, and the upper end and the lower end of the Z-shaped elastic pieces are fixedly connected with the bottom of the convex baffle and the top of the bottom plate respectively; the two groups of the primary limiting assemblies are symmetrically distributed at two ends of the bottom cross rod, and two convex baffles in the two groups of the primary limiting assemblies are used for limiting bottoms of two ends of a container. As a still further proposal of the utility model, the tops of the convex baffle plates are protruded above the supporting baffle rods, and the ends of the tops of the two convex baffle plates, which are far away from each other, are in cambered surface structures. As a still further proposal of the utility model, the telescopic reinforcement component comprises a side baffle, a vertical straight notch, an L-shaped shell, a buffer bottom block, a W-shaped elastic sheet and an inverted concave reinforcement plate; The vertical straight slot is arranged on the side surface of the side baffle and completely penetrates through the other side of the side baffle, and the side baffle is distributed on the inner sides of the top cross rod and the bottom cross rod and is in sliding connection with the supporting baffle rods on the top c