Quick docking device of replaceable module of unmanned aerial vehicle

Abstract

The utility model discloses a quick docking device for a replaceable module of an unmanned aerial vehicle, and particularly relates to the technical field of unmanned aerial vehicles, the quick docking device comprises an unmanned aerial vehicle body, two supporting legs are fixedly connected to the outer side of the unmanned aerial vehicle body, an interface slot is formed in the bottom end of the unmanned aerial vehicle body, and a plurality of clamping slots are formed in the bottom end of the unmanned aerial vehicle body; a mounting frame is fixedly connected to the bottom end of the unmanned aerial vehicle body, a mounting assembly is mounted in the mounting frame, and a protection mechanism is arranged below the mounting frame. By arranging the mounting assembly and the protection mechanism, the electrical component module and the unmanned aerial vehicle body can be quickly mounted, the mounting time is shortened, the mounting complexity is reduced, the electrical component module can be effectively limited, potential safety hazards in the flight process can be reduced, and the safety of the unmanned aerial vehicle is improved. Meanwhile, the two protective shells can protect the outer sides of the electrical component modules, the risk that the unmanned aerial vehicle collides with obstacles in the flying or landing process can be effectively reduced, and internal modules are protected against damage.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field more specifically, the utility model relates to a quick docking device of replaceable module of unmanned plane. BACKGROUND

[0002] The unmanned plane is a no -one pilot plane, is with wireless radio control equipment and self -provided program control device control's not load people plane, has no cockpit on the plane, but installs automatic pilot, program control device and equipment, ground, warship or mother machine remote control station personnel through radar and so on equipment, to its track, positioning, remote control, remote measurement and digital transmission.

[0003] The traditional unmanned plane electrical component connection mode usually is screw fixed or buckle type plug, although meet the demand of connection in a certain extent, but still have many deficiencies in practical application, for example, although the screw fixed is stable, but the installation and dismounting process is more tedious, need to use the tool, although the buckle type plug is convenient for quick installation, but after long -time use, easy to appear abrasion, influence the stability of connection, the contact of electrical connection is also one of common problems, this not only reduces the work efficiency of unmanned plane, also increases the maintenance cost.

[0004] Through the retrieval, the patent with the announcement number CN221783525U discloses a kind of quick docking mechanism for unmanned plane, while guaranteeing compact structure, electrical component and electrical external component can be quickly docked and disassembled, and connection stability can be ensured by multiple locking, reduce the contact of electrical connection is not good phenomenon, and it is convenient for unmanned plane integral modular design, easy to use, user learning cost is low.

[0005] The above-mentioned quick docking mechanism for unmanned plane is inconvenient to limit the module when connecting and installing the module during actual use, which causes the module to loosen or even fall off during flight due to vibration or air flow factors, resulting in unstable or interrupted data transmission. UTILITY MODEL CONTENTS

[0006] In order to overcome the above-mentioned defects of the prior art, the utility model provides a quick docking device of replaceable module of unmanned plane to solve the problems raised in the above background art.

[0007] To achieve the above-mentioned purpose, the utility model provides the following technical scheme:

[0008] The utility model provides a quick docking device of the replaceable module of unmanned plane, including unmanned plane body, two support legs are fixedly connected outside unmanned plane body, the bottom of unmanned plane body is equipped with the interface slot, the bottom of unmanned plane body is equipped with a plurality of clamping grooves, the bottom of unmanned plane body is fixedly connected with the mounting bracket, the mounting assembly is installed in mounting bracket, the protection mechanism is arranged below mounting bracket,

[0009] The installation assembly includes a first bevel gear, the first bevel gear is rotatably connected to the inside of the mounting bracket, a first rotating knob is fixedly connected to one end of the first bevel gear, a second bevel gear is engaged with one side of the first bevel gear, the second bevel gear is rotatably connected to the inside of the mounting bracket, a threaded rod is fixedly connected to the upper surface of the second bevel gear, the threaded rod is rotatably connected to the inside of the mounting bracket, a movable plate is threadedly connected to the outside of the threaded rod, the movable plate is slidably connected to the inside of the mounting bracket, two sliding rods are fixedly connected to the inside of the movable plate, a sliding block is slidably connected to the outside of the sliding rods, the cross section of the sliding block is adapted to the cross section of the inside of the movable plate, a telescopic spring is fixedly connected to one side of the sliding block, one end of the telescopic spring is fixedly connected to the inside of the mounting bracket, a connecting plate is fixedly connected to one side of the sliding block, two insertion rods are fixedly connected to one side of the connecting plate, an electrical component module is arranged on the inside of the mounting bracket, the insertion rods are clamped to one side of the electrical component module, a plurality of clamping blocks are fixedly connected to the upper surface of the electrical component module, the clamping blocks are clamped to the inside of the clamping grooves, an interface plate is installed at the top of the electrical component module, and the interface plate is inserted into the interface slot.

[0010] By adopting the above technical scheme, the electrical component module can be quickly installed on the unmanned plane body, and the electrical component module can be limited, so that the electrical component module can remain stable during the flight of the unmanned plane body.

[0011] As a further description of the above technical scheme, the protection assembly includes a guide rod, the guide rod is fixedly connected to the bottom of the mounting bracket, two protection shells are slidably connected to the outside of the guide rod, a sealing strip is fixedly connected to one side of the protection shell, a heat dissipation opening is formed in the lower surface of the protection shell, a supporting rod is fixedly connected to the inside of each of the two supporting legs, a two-way screw rod is threadedly connected to the inside of one of the supporting rods, one end of the two-way screw rod is rotatably connected to the inside of the other supporting rod, a second rotating knob is fixedly connected to one end of the two-way screw rod, and the two-way screw rod is threadedly connected to the inside of the two protection shells.

[0012] By adopting the above technical scheme, the two protection shells can protect the electrical component module outside, which can effectively reduce the risk of collision with obstacles during the flight or landing of the unmanned plane.

[0013] The technical effects and advantages of the utility model are as follows:

[0014] 1. By setting the installation assembly, compared with the prior art, the installation process of the electrical component module can be more convenient, the installation time and complexity are reduced, the electrical component module can be effectively limited, the loosening and falling of the electrical component module during flight are reduced, the firm connection between the electrical component module and the unmanned aerial vehicle body is ensured, and the safety hidden trouble during flight is reduced;

[0015] 2. By setting the protection mechanism, compared with the prior art, the risk of collision with obstacles during flight or landing of the unmanned aerial vehicle can be effectively reduced, the internal module is protected from damage, and direct impact or scratching physical damage in the external environment can be resisted to a certain extent, and the normal operation of the electrical component module is protected. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model.

[0017] Figure 2 It is a schematic diagram of the rear side structure of the mounting rack of the utility model.

[0018] Figure 3 It is a schematic diagram of the bottom structure of the unmanned aerial vehicle body of the utility model.

[0019] Figure 4 It is a schematic diagram of the mounting rack structure of the utility model.

[0020] Figure 5 It is a schematic diagram of the cross-section structure of the mounting rack of the utility model.

[0021] Figure 6 It is a schematic diagram of the structure of the plug-in rod and the electrical component module of the utility model.

[0022] Figure 7 It is a schematic diagram of the structure of the guide rod and the protection shell of the utility model.

[0023] The reference signs are: 1, unmanned aerial vehicle body; 2, support leg; 3, interface groove; 4, clamping groove; 5, mounting rack; 6, first bevel gear; 7, first rotating knob; 8, second bevel gear; 9, threaded rod; 10, movable plate; 11, sliding rod; 12, sliding block; 13, extension spring; 14, connecting plate; 15, plug-in rod; 16, electrical component module; 17, clamping block; 18, interface plate; 19, guide rod; 20, protection shell; 21, sealing strip; 22, support rod; 23, bidirectional screw; 24, second rotating knob; 25, heat dissipation port. DETAILED DESCRIPTION

[0024] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0025] The embodiments disclosed in this application are as follows: Figures 1-7 The device shown is a quick docking device for a replaceable module of a drone, including a drone body 1, two support legs 2 fixedly connected to the outside of the drone body 1, an interface groove 3 and multiple slots 4 at the bottom of the drone body 1, a mounting frame 5 fixedly connected to the bottom of the drone body 1, an installation component installed inside the mounting frame 5, and a protective mechanism provided below the mounting frame 5.

[0026] The mounting assembly comprises a first bevel gear 6 rotatably connected inside the mounting frame 5, one end of the first bevel gear 6 being fixedly connected with a first rotating lever 7, one side of the first bevel gear 6 being engaged with a second bevel gear 8, the second bevel gear 8 being rotatably connected inside the mounting frame 5, the upper surface of the second bevel gear 8 being fixedly connected with a threaded rod 9, the threaded rod 9 being rotatably connected inside the mounting frame 5, the outer side of the threaded rod 9 being threadedly connected with a movable plate 10, the movable plate 10 being slidably connected inside the mounting frame 5, the inner side of the movable plate 10 being fixedly connected with two slide rods 11, the outer side of the slide rod 11 being slidably connected with a sliding block 12, the cross section of the sliding block 12 being adapted to the inner side of the movable plate 10, one side of the sliding block 12 being fixedly connected with an extension spring 13, one end of the extension spring 13 being fixedly connected inside the mounting frame 5, one side of the sliding block 12 being fixedly connected with a connecting plate 14, one side of the connecting plate 14 being fixedly connected with two insertion rods 15, an electrical component module 16 being arranged inside the mounting frame 5, the insertion rods 15 being clamped with one side of the electrical component module 16, a plurality of clamping blocks 17 being fixedly connected to the upper surface of the electrical component module 16, the clamping blocks 17 being clamped with the inner side of the clamping groove 4, an interface plate 18 being arranged at the top end of the electrical component module 16, the interface plate 18 being inserted into the inner side of the interface groove 3, the first rotating lever 7 being aligned with the clamping groove 4, so as to facilitate positioning of the electrical component module 16 during installation, facilitating quick installation of the electrical component module 16, making the installation process of the electrical component module 16 more convenient, then the threaded rod 9 can drive the movable plate 10 to move upward through the thread, the inner side of the movable plate 10 being adapted to the cross section of one side of the sliding block 12, and the sliding block 12 being slidably connected with the outer side of the slide rod 11, so that when the movable plate 10 moves upward, the cross section of one side of the sliding block 12 can be squeezed and pushed, thereby driving the two connecting plates 14 to move relatively, the two insertion rods 15 being inserted into the inner side of the electrical component module 16 through the connecting plates 14, so as to limit the electrical component module 16, and at the same time, the two connecting plates 14 can support the bottom end of the electrical component module 16, reducing loosening and falling of the electrical component module 16 during flight, and ensuring firm connection between the electrical component module 16 and the unmanned aerial vehicle body 1.

[0027] Referring to Figure 1 and 7As shown, the protection assembly includes a guide rod 19 fixedly connected with the bottom end of the mounting frame 5, two protection shells 20 slidingly connected with the outer side of the guide rod 19, a sealing strip 21 fixedly connected with one side of the protection shell 20, a heat dissipation opening 25 formed in the lower surface of the protection shell 20, and two support rods 22 fixedly connected with the inner sides of the two support legs 2, wherein one of the support rods 22 is internally threadedly connected with a bidirectional screw rod 23, one end of the bidirectional screw rod 23 is rotatably connected with the inner side of the other support rod 22, the bidirectional screw rod 23 is fixedly connected with a second knob 24 at one end, and the outer side of the bidirectional screw rod 23 is threadedly connected with the inner sides of the two protection shells 20.

[0028] The utility model discloses a quick docking device of replaceable module of unmanned plane, and the specific structure is as follows: Figures 1-7 As shown, in the technical scheme, when the electrical component module 16 needs to be installed, first, the plurality of clamping blocks 17 is aligned with the clamping grooves 4, so that the electrical component module 16 drives the interface plate 18 to be inserted into the inner side of the interface groove 3 from bottom to top, thereby connecting the electrical component module 16 with the unmanned plane body 1, then the first knob 7 is rotated, the first bevel gear 6 is driven to rotate by the first knob 7, the first bevel gear 6 meshes with the second bevel gear 8 to drive the threaded rod 9 to rotate, the threaded rod 9 can drive the movable plate 10 to move upward by threads, the inner side "concave" surface of the movable plate 10 is adapted to the surface of one side of the sliding block 12, so that when the movable plate 10 moves upward, the two sliding blocks 12 can be relatively moved by being pressed and pushed by the surface, the sliding block 12 can drive the connecting plate 14 to move relatively, and the two connecting plates 14 can insert the two insertion rods 15 into the inner side of the electrical component module 16, so that the electrical component module 16 can be limited, and the two connecting plates 14 can support the bottom end of the electrical component module 16, so that the electrical component module 16 can be kept stable, after the electrical component module 16 is installed, the second knob 24 is rotated, the bidirectional screw rod 23 is driven to rotate by the second knob 24, the protection shell 20 is slidingly connected with the outer side of the guide rod 19, the guide rod 19 provides a guide function for the movement of the protection shell 20, the bidirectional screw rod 23 drives the two protection shells 20 to move relatively by the two threads with opposite screw directions, so that the two protection shells 20 drive the two sealing strips 21 to be attached, so that the two protection shells 20 can protect the electrical component module 16.

[0029] Among them, the utility model discloses the drawings in the embodiment, only relate to the structure with the embodiment of the present disclosure, other structures can refer to the usual design, under the condition of not conflict, the same embodiment and different embodiments of the utility model can be combined with each other;

[0030] The contents not described in detail in the specification all belong to the prior art known to those skilled in the art, and the model parameters of each electric appliance are not specifically limited, and conventional equipment can be used, in the technical solution, the electric appliance control elements not mentioned belong to the prior art, so they are not shown in the drawings, and will not be described here.

[0031] Finally: the above is only preferred embodiment of the utility model, and is not used for limiting the utility model, any modification, equivalent replacement, improvement etc. made within the spirit and principle of the utility model should be included in the protection scope of the utility model.

Claims

1. A quick docking device for replaceable modules of a UAV, comprising the UAV body (1), characterized in that: The drone body (1) has two support legs (2) fixedly connected to the outside. The drone body (1) has an interface groove (3) at the bottom end. The drone body (1) has multiple slots (4) at the bottom end. The drone body (1) has a mounting frame (5) fixedly connected to the bottom end. The mounting frame (5) has an installation component installed inside. The mounting frame (5) has a protective mechanism below it. The mounting assembly includes a first bevel gear (6), which is rotatably connected to the mounting bracket (5). A first torque (7) is fixedly connected to one end of the first bevel gear (6). A second bevel gear (8) meshes with one side of the first bevel gear (6). The second bevel gear (8) is rotatably connected to the mounting bracket (5). A threaded rod (9) is fixedly connected to the upper surface of the second bevel gear (8). The threaded rod (9) is rotatably connected to the mounting bracket (5).

2. The quick docking device for replaceable modules of a UAV according to claim 1, characterized in that: The threaded rod (9) is threadedly connected to a movable plate (10) on the outside. The movable plate (10) is slidably connected to the mounting bracket (5) inside. Two sliding rods (11) are fixedly connected to the inside of the movable plate (10). A sliding block (12) is slidably connected to the outside of the sliding rod (11). The cross-section of the sliding block (12) is adapted to the cross-section of the inside of the movable plate (10).

3. The quick docking device for replaceable modules of a UAV according to claim 2, characterized in that: A telescopic spring (13) is fixedly connected to one side of the sliding block (12), and one end of the telescopic spring (13) is fixedly connected to the inside of the mounting bracket (5).

4. The quick docking device for replaceable modules of a UAV according to claim 2, characterized in that: A connecting plate (14) is fixedly connected to one side of the sliding block (12), and two plug rods (15) are fixedly connected to one side of the connecting plate (14).

5. The quick docking device for replaceable modules of a UAV according to claim 4, characterized in that: An electrical component module (16) is provided on the inner side of the mounting bracket (5). The plug rod (15) is snapped into one side of the electrical component module (16). Multiple locking blocks (17) are fixedly connected to the upper surface of the electrical component module (16). The locking blocks (17) are snapped into the inner side of the slot (4).

6. The quick docking device for replaceable modules of a UAV according to claim 5, characterized in that: An interface board (18) is installed on the top of the electrical component module (16), and the interface board (18) is inserted into the inside of the interface slot (3).

7. The quick docking device for replaceable modules of a UAV according to claim 1, characterized in that: The protective mechanism includes a guide rod (19), which is fixedly connected to the bottom end of the mounting bracket (5), and two protective shells (20) are slidably connected to the outside of the guide rod (19).

8. The quick docking device for replaceable modules of a UAV according to claim 7, characterized in that: A sealing strip (21) is fixedly connected to one side of the protective shell (20), and a heat dissipation vent (25) is provided on the lower surface of the protective shell (20).

9. The quick docking device for replaceable modules of a UAV according to claim 1, characterized in that: Both of the support legs (2) are fixedly connected to the inner side of a support rod (22), and one of the support rods (22) is threadedly connected to a bidirectional screw (23), one end of which is rotatably connected to the other support rod (22).

10. The quick docking device for replaceable modules of a UAV according to claim 9, characterized in that: One end of the bidirectional screw (23) is fixedly connected to a second rotary knob (24), and the outer side of the bidirectional screw (23) is threadedly connected to the inside of the two protective shells (20).

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