Unmanned aerial vehicle fuselage section transportation bracket

Abstract

The utility model discloses an unmanned aerial vehicle fuselage section transportation bracket which comprises a fuselage transportation tray, a front supporting frame, a rear supporting frame and an unmanned aerial vehicle fuselage section, the front supporting frame and the rear supporting frame are vertically arranged on the fuselage transportation tray at intervals, the front supporting frame and the rear supporting frame each comprise a movable supporting plate, and supporting vertical frames are arranged on the two sides of each movable supporting plate respectively. A movable connector is arranged on the supporting vertical frame; four fuselage connecting plugs corresponding to the movable connectors in position are arranged below the unmanned aerial vehicle fuselage section, the unmanned aerial vehicle fuselage section is connected and installed on the movable connectors through the fuselage connecting plugs, and the lower portion of the unmanned aerial vehicle fuselage section is erected on the movable supporting plate. The front supporting frame and the rear supporting frame are provided with movable connectors which are fixedly connected, the movable connectors can be firmly and movably connected with fuselage connecting plugs on the fuselage section of the unmanned aerial vehicle, the abdomen of the fuselage section of the unmanned aerial vehicle can be erected on a movable supporting plate in a matched mode, and the movable supporting plate is made of wood plates and further has the elastic buffering function. And timely replacement is also facilitated.

Description

Technical Field

[0001] The utility model relates to the technical field of UAV transportation equipment, and particularly relates to a transportation bracket for a UAV fuselage section. Background Art

[0002] A UAV fuselage consignment rack is a special equipment for loading and transporting the UAV fuselage. It usually has a stable structure and a convenient operation design to ensure the safety and stability of the UAV during transportation. Main functions: Loading and fixing: The UAV fuselage consignment rack can stably load the UAV fuselage and firmly fix the UAV on the consignment rack through various fixing devices (such as cable tighteners, straps, etc.) to prevent shaking or displacement during transportation.

[0003] II. Structural Features

[0004] Main structure: The main structure of the UAV fuselage consignment rack is usually made of high-strength materials such as aluminum alloy, carbon fiber, etc. to ensure its load-bearing capacity and stability. The design of the main structure usually takes into account the size and weight of the UAV to ensure that it can stably carry the UAV fuselage.

[0005] Fixing devices: The consignment rack is equipped with various fixing devices such as cable tighteners, straps, card slots, etc. for firmly fixing the UAV fuselage on the consignment rack. The design of these fixing devices usually takes into account the requirements of easy operation and quick fixing.

[0006] Shock-absorbing materials: In order to reduce damage to the UAV fuselage, the consignment rack is usually also equipped with shock-absorbing materials. These shock-absorbing materials can effectively absorb vibrations and impacts during transportation and protect the UAV fuselage from damage.

[0007] Selecting a suitable consignment rack: When selecting a UAV fuselage consignment rack, it should be selected according to the size, weight and transportation requirements of the UAV to ensure that the consignment rack can stably carry the UAV fuselage. Correctly fixing the UAV: When fixing the UAV fuselage, it should be ensured that the fixing device is firm and reliable to prevent shaking or displacement during transportation.

[0008] In summary, the UAV fuselage consignment rack is an important and indispensable equipment in the UAV transportation process. By selecting a suitable consignment rack, correctly fixing the UAV fuselage and paying attention to transportation safety and other measures, the safety and stability of the UAV during transportation can be ensured. Content of the Utility Model

[0009] The purpose of the utility model is to overcome the deficiencies of the prior art and provide a transportation bracket for a UAV fuselage section to solve the problem of safe transportation of the existing UAV fuselage consignment rack.

[0010] The utility model is realized through the following technical solutions:

[0011] An unmanned aerial vehicle (UAV) fuselage section transportation bracket, comprising a fuselage transportation tray, a front support frame, a rear support frame and a UAV fuselage section. The front support frame and the rear support frame are erected at intervals on the fuselage transportation tray. Both the front support frame and the rear support frame include movable support plates. Support upright frames are respectively arranged on both sides of the movable support plates, and movable connection heads are arranged on the support upright frames;

[0012] Four fuselage socket joints corresponding to the positions of the movable connection heads are arranged below the UAV fuselage section. The UAV fuselage section is connected and installed on the movable connection heads through the fuselage socket joints, and the lower part of the UAV fuselage section is erected on the movable support plates.

[0013] Preferably, a plurality of lifting rings are arranged around the fuselage transportation tray.

[0014] Preferably, sleeper mounting brackets are respectively arranged at the four corners of the bottom surface of the fuselage transportation tray, and sleeper blocks are installed in the sleeper mounting brackets.

[0015] Preferably, hooks for connecting the UAV fuselage section are arranged on the sleeper mounting brackets.

[0016] Preferably, the movable connection head includes a connection bottom plate and a concave joint pressing plate. The connection bottom plate is arranged at the top of the support upright frame, and both side parts of the concave joint pressing plate are connected to the connection bottom plate through fastening bolts.

[0017] Preferably, connection adjustment side plates are respectively arranged on one side and the outer side of the end of the connection bottom plate, and adjustment screws are arranged on the connection adjustment side plates.

[0018] Preferably, the upper support surface of the movable support plate is a concave arc surface.

[0019] Preferably, the stress test frame includes an I-shaped connection frame. The I-shaped connection frame includes a transverse frame and a longitudinal frame. L-shaped socket plates that are movably connected to the movable connection heads are respectively arranged at the four corner positions of the I-shaped connection frame. A docking support plate that is matched and docked with the movable support plate is arranged on one side of the transverse frame.

[0020] Preferably, a positioning groove is arranged in the middle of the concave arc surface of one of the movable support plates, and a positioning protrusion is arranged on the docking support plate that cooperates with the movable support plate.

[0021] Preferably, vertical plate joints for connecting the UAV fuselage section are respectively arranged on the fuselage transportation tray on both sides of the front support frame and the rear support frame.

[0022] Compared with the prior art, the utility model has the following advantages and beneficial effects:

[0023] 1. A transport bracket for the fuselage section of a drone according to the present utility model. By providing a front support frame and a rear support frame, as well as a stress test frame that is quickly and firmly connected to the front support frame and the rear support frame, movable support plates are also provided on the front support frame and the rear support frame. The movable support plates mainly play a role in supporting and docking. The movable support plates and the docking support plates can be matched and docked for support. Through the stress test frame, rapid stress testing of the transport bracket is achieved, ensuring the structural safety of the transport bracket.

[0024] 2. A transport bracket for the fuselage section of a drone according to the present utility model. Movable connection heads are fixedly connected to the front support frame and the rear support frame. The movable connection heads can be firmly and movably connected to the fuselage plug joints on the fuselage section of the drone. The abdomen of the fuselage section of the drone can be matched and placed on the movable support plates. The movable support plates are made of wood and also have an elastic buffering effect, and are also convenient for timely replacement. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] The drawings described herein are used to provide a further understanding of the embodiments of the present utility model, form a part of this application, and do not constitute a limitation to the embodiments of the present utility model. In the drawings:

[0026] Figure 1 It is a schematic connection structure diagram of the fuselage transport tray of the present utility model with the front support frame and the rear support frame.

[0027] Figure 2 It is a schematic structural diagram of a transport bracket for the fuselage section of a drone according to the present utility model.

[0028] Figure 3 It is a schematic structural diagram of the stress test frame of the present utility model Figure 1 。

[0029] Figure 4 It is a schematic structural diagram of the stress test frame of the present utility model Figure 2 。

[0030] Figure 5 It is a schematic structural diagram of the movable connection head of the present utility model.

[0031] Figure 6 It is a schematic layout structure diagram of the fuselage plug joints on the fuselage section of the present practical drone.

[0032] Marks in the drawings and corresponding component names:

[0033] 1 - Body transportation tray, 2 - Front support frame, 3 - Rear support frame, 4 - Stress test frame, 5 - Movable support plate, 6 - Support vertical frame, 7 - Movable connection head, 8 - Body plug connector, 9 - Lifting ring, 10 - Sleeper mounting frame, 11 - Sleeper block, 12 - Hook, 13 - Connection bottom plate, 14 - Concave joint pressure plate, 15 - Fastening bolt, 16 - Connection adjustment side plate, 17 - Adjusting screw rod, 18 - Concave arc surface, 19 - I-shaped connection frame, 20 - Transverse frame, 21 - Longitudinal frame, 22 - L-shaped plug-in board, 23 - Docking support plate, 24 - Positioning groove, 25 - Positioning protrusion, 26 - Vertical plate joint. Detailed implementation mode

[0034] The technical solution of the present invention will be further described below in conjunction with the drawings and through specific implementation modes.

[0035] Among them, the drawings are only for illustrative purposes, showing only schematic diagrams, not physical diagrams, and cannot be understood as a limitation to the present invention; in order to better illustrate the embodiments of the present invention, some components in the drawings will be omitted, enlarged or reduced, and do not represent the dimensions of actual products; for those skilled in the art, it is understandable that some well-known structures and their descriptions in the drawings may be omitted.

[0036] In the drawings of the embodiments of the present invention, the same or similar reference numerals correspond to the same or similar components; in the description of the present invention, it should be understood that if terms such as "upper", "lower", "left", "right", "inner", "outer", etc. are used to indicate the orientation or positional relationship, it is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, so the terms describing the positional relationship in the drawings are only for illustrative purposes and cannot be understood as a limitation to the present invention. For those of ordinary skill in the art, the specific meanings of the above terms can be understood according to specific circumstances.

[0037] In the description of the present invention, unless otherwise clearly specified and limited, if terms such as "connection" are used to indicate the connection relationship between components, this term should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or integrated; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two components or the interaction relationship between two components. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0038] Embodiment 1

[0039] Such as Figures 1-6As shown, the utility model is a transport bracket for fuselage sections of unmanned aerial vehicles, comprising a fuselage transport pallet 1, a front support frame 2, a rear support frame 3 and a stress testing frame 4. The outer contour of the fuselage transport pallet 1 matches the size of the fuselage section of the unmanned aerial vehicle, and the weight of the fuselage section of the unmanned aerial vehicle is mainly borne by the front support frame 2 and the rear support frame 3. The front support frame 2 and the rear support frame 3 not only bear the load, but also play the role of fixing and limiting the fuselage section of the unmanned aerial vehicle. The fuselage transport pallet 1 is vertically provided with a front support frame 2 and a rear support frame 3 at intervals, and the front support frame 2 and the rear support frame 3 both include a movable support plate 5, and support frames 6 are respectively provided on both sides of the movable support plate 5, and a movable connecting head 7 is provided on the support frame 6.

[0040] like Figure 1 As shown, by setting a front support frame 2 and a rear support frame 3, and a stress testing frame 4 which is quickly and firmly connected to the front support frame 2 and the rear support frame 3, a movable support plate 5 is also provided on the front support frame 2 and the rear support frame 3, and the movable support plate 5 mainly plays a supporting docking role. The movable support plate 5 and the docking support plate 23 can match the docking support, and a rapid stress test of the transport bracket can be achieved through the stress testing frame 4 to ensure the structural safety of the transport bracket.

[0041] Four fuselage plug connectors 8 corresponding to the positions of the movable connector 7 are provided below the drone fuselage section. The fuselage plug connector 8 is a connection structure provided by the drone. The drone fuselage section is connected and installed on the movable connector 7 via the fuselage plug connector 23, and the lower part of the drone fuselage section is mounted on the movable support plate 5.

[0042] The front support frame 2 and the rear support frame 3 are provided with a fixedly connected movable connector 7, which can be firmly and flexibly connected with the fuselage plug connector 8 on the fuselage section of the UAV. The lower part of the fuselage section of the UAV can be matched and mounted on the movable support plate 5. The movable support plate 5 is made of wood and has an elastic buffering effect, which is also convenient for timely replacement.

[0043] like Figures 1-6 As shown, the utility model is a transport bracket for UAV fuselage sections. A complete set of transport brackets needs to be stress tested when transporting UAVs or UAV fuselage sections to detect the structural safety of the transport bracket. The stress test process is as follows: the stress test frame 4 is lifted and connected to the front support frame 2 and the rear support frame 3, and an external force (basically the same as the actual UAV gravity) is set to act on the stress test frame 4. If the transport bracket structure is not deformed or damaged, the surface transport bracket structure is reasonably designed, and the quality meets the requirements, the UAV can be loaded and transported.

[0044] During use, the hoisting unmanned aircraft fuselage section is connected to the corresponding movable connectors 7 on the front support frame 2 and the rear support frame 3 through the fuselage plug connector 8. The lower contour of the unmanned aircraft fuselage section presses on the movable support plate 5, and the unmanned aircraft or the unmanned aircraft fuselage section is firmly connected to the transport bracket through safety ropes. Then, the hoisting rings 9 around the fuselage transport tray 1 are used to start the bracket and the unmanned aircraft fuselage section for transportation and loading.

[0045] At the four corner positions of the bottom surface of the fuselage transport tray 1, sleeper mounting frames 10 are respectively provided, and sleeper blocks 11 are installed in the sleeper mounting frames 10. The sleeper blocks 11 are movably installed, and the sleeper blocks 11 mainly play a role of buffering and supporting, and the movable setting also facilitates replacement.

[0046] On the sleeper mounting frame 10, a hook 12 for connecting the unmanned aircraft fuselage section is provided. The hook 12 is connected to the unmanned aircraft fuselage section through a cable (safety rope), which can play a role in assisting in fixing the unmanned aircraft fuselage section. In addition, the function of the vertical plate joint 26 is the same as that of the hook 12.

[0047] Embodiment 2

[0048] As Figures 1-6 shown, for a transport bracket for an unmanned aircraft fuselage section of the present utility model, on the basis of the above embodiment, the movable connector 7 includes a connection bottom plate 13 and a concave joint pressing plate 14. The connection bottom plate 13 is arranged at the top of the support vertical frame 6, and both side portions of the concave joint pressing plate 14 are connected to the connection bottom plate 13 through fastening bolts 15. The movable connector 7 is connected to the L-shaped plug-in plate 22. By pressing the concave joint pressing plate 14 on the movable connector 7 against the transverse joint plate of the L-shaped plug-in plate 22 and then connecting through the fastening bolts 15, the fixed connection between the movable connector 7 and the stress test frame 4 can be realized. Similarly, it can be realized that the movable connector 7 can be quickly and firmly connected to the fuselage plug connector 8 provided below the unmanned aircraft fuselage section. The L-shaped plug-in plate 22 on the stress test frame 4 has the same structure as the fuselage plug connector 8, and the stress test frame 4 is arranged by simulating the structure of the unmanned aircraft.

[0049] As Figure 5 shown, on one side and the outside of the end of the connection bottom plate 13, connection adjustment side plates 16 are respectively provided, and adjustment screws 17 are provided on the connection adjustment side plates 16. The adjustment screw 17 arranged on one side of the end of the connection bottom plate 13 is mainly used to limit the concave joint pressing plate 14 to prevent the concave joint pressing plate 14 from moving horizontally, while the adjustment screw 17 arranged on the outside of the connection bottom plate 13 is mainly used to press against the end position of the transverse joint plate of the L-shaped plug-in plate 22 to prevent the entire stress test frame 4 from moving left and right.

[0050] Similarly, the adjusting screw 17 arranged on the outer side of the connecting base plate 13 is mainly used to press against the end position of the transverse joint plate of the fuselage socket 8 at low pressure, avoiding the left and right movement of the entire UAV fuselage section or the UAV, and ensuring the transportation safety of the UAV fuselage section or the UAV.

[0051] The upper support surface of the movable support plate 5 is a concave arc surface 18, and the concave arc surface 18 is a semi-circular groove structure. When the semi-circular protrusion on the docking support plate 23 is docked with the semi-circular groove structure, the stress test frame 4 can be conveniently and quickly installed in the set position. The stress test frame 4 includes an I-shaped connecting frame 19, the I-shaped connecting frame 19 includes a transverse frame 20 and a longitudinal frame 21, and L-shaped plug-in plates 22 that are movably connected to the movable connection heads 7 are respectively arranged at the four corners of the I-shaped connecting frame 19. One side of the transverse frame 20 is provided with a docking support plate 23 that is matched and docked with the movable support plate 5.

[0052] A positioning groove 24 is provided in the middle of the concave arc surface 18 of one of the movable support plates 5, and a positioning protrusion 25 is provided on the docking support plate 23 that cooperates with the movable support plate 5. The positioning protrusion 25 plays a role in limiting.

[0053] Vertical plate joints 26 connected to the UAV fuselage section are respectively provided on the fuselage transportation trays 1 on both sides of the front support frame 2 and the rear support frame 3.

[0054] Movable connection heads 7 are fixedly connected to the front support frame 2 and the rear support frame 3. The movable connection heads 7 can be firmly and movably connected to the fuselage socket 8 on the UAV fuselage section. In addition, movable support plates 5 are also provided on the front support frame 2 and the rear support frame 3. The movable support plates 5 mainly play a role in supporting and docking. The movable support plates 5 can be matched and docked with the UAV fuselage for support. When the movable support plates 5 support the UAV, rubber pads are laid on the movable support plates 5 to prevent the UAV from being squeezed and damaged. The material of the movable support plates 5 is made of wood, which also has an elastic buffering effect and is convenient for timely replacement.

[0055] The above specific embodiments have further detailed the purpose, technical solution and beneficial effects of the present invention. It should be understood that the above is only the specific embodiment of the present invention and is not used to limit the protection scope of the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. A UAV fuselage section transport bracket, comprising a fuselage transport tray (1), a front support frame (2), a rear support frame (3) and a UAV fuselage section, characterized in that: A front support frame (2) and a rear support frame (3) are erected on the fuselage transport pallet (1) at intervals, and the front support frame (2) and the rear support frame (3) both include a movable support plate (5), and support frames (6) are respectively provided on both sides of the movable support plate (5), and a movable connecting head (7) is provided on the support frames (6); Four fuselage plug connectors (8) corresponding to the positions of the movable connector (7) are arranged below the fuselage section of the UAV. The fuselage section of the UAV is connected and installed on the movable connector (7) via the fuselage plug connectors (8). The belly of the fuselage section of the UAV is mounted on the movable support plate (5).

2. The UAV fuselage section transport bracket according to claim 1, characterized in that: The fuselage transport pallet (1) is provided with a plurality of lifting rings (9) around its periphery.

3. The UAV fuselage section transport bracket according to claim 1, characterized in that: The four corners of the bottom surface of the fuselage transport pallet (1) are respectively provided with sleeper mounting frames (10), and sleeper blocks (11) are installed in the sleeper mounting frames (10).

4. The UAV fuselage section transport bracket according to claim 3, characterized in that: The sleeper mounting frame (10) is provided with a hook (12) for connecting to the fuselage section of the drone.

5. The UAV fuselage section transport bracket according to claim 1, characterized in that: The movable joint (7) comprises a connecting base plate (13) and a concave joint pressure plate (14); the connecting base plate (13) is arranged on the top of the supporting stand (6); and the two sides of the concave joint pressure plate (14) are connected to the connecting base plate (13) by fastening bolts (15).

6. The UAV fuselage section transport bracket according to claim 5, characterized in that: One side of the end portion and the outer side of the connecting bottom plate (13) are respectively provided with connecting and adjusting side plates (16), and an adjusting screw rod (17) is provided on the connecting and adjusting side plates (16).

7. The UAV fuselage section transport bracket according to claim 5, characterized in that: The upper end supporting surface of the movable supporting plate (5) is a concave arc surface (18).

8. The UAV fuselage section transport bracket according to claim 6, characterized in that: The invention also comprises a stress test frame (4), wherein the stress test frame (4) comprises an I-shaped connecting frame (19), wherein the I-shaped connecting frame (19) comprises a transverse frame (20) and a longitudinal frame (21), wherein four corners of the I-shaped connecting frame (19) are respectively provided with L-shaped plug boards (22) movably connected to the movable connecting head (7), and one side of the transverse frame (20) is provided with a docking support plate (23) that matches and docks with the movable support plate (5).

9. The UAV fuselage section transport bracket according to claim 7, characterized in that: A positioning groove (24) is provided in the middle of the concave arc surface (18) of one of the movable support plates (5), and a positioning protrusion (25) is provided on the docking support plate (23) matched with the movable support plate (5).

10. The UAV fuselage section transport bracket according to claim 1, characterized in that: The fuselage transport trays (1) on both sides of the front support frame (2) and the rear support frame (3) are respectively provided with vertical plate joints (26) connected to the fuselage sections of the drone.

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