Mounting and supporting device for unmanned aerial vehicle-mounted communication equipment

Abstract

The utility model discloses a mounting and supporting device for unmanned aerial vehicle-mounted communication equipment, which relates to the technical field of unmanned aerial vehicles, and comprises a shell, a communication equipment body, a flight component, a communication component, a communication component, a communication component, a power supply component and a communication component, and is characterized in that the flight component is arranged on the shell and is used for providing flight power for the unmanned aerial vehicle; the mounting assembly is arranged on the shell and is used for mounting a communication equipment body; the clamping assembly is arranged on the mounting assembly; the fixing assembly is arranged on the mounting assembly and is used for fixedly mounting a communication equipment body; the buffering assembly is arranged on the mounting assembly and used for buffering impact force generated when the unmanned aerial vehicle lands; the clamping plates are rapidly pulled open through magnetic force generated by the first electromagnets, so that communication equipment bodies of different sizes can be placed in the space between the clamping plates and other clamping plates, and then the clamping plates can tightly clamp the communication equipment bodies of different sizes through elastic force of the first springs. And therefore, the unmanned aerial vehicle can load communication equipment of different sizes, and the application range of the unmanned aerial vehicle is expanded.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to an installation support device for UAV-borne communication equipment. Background Technology

[0002] Unmanned aerial vehicle (UAV) onboard communication equipment refers to devices installed on UAVs to enable data transmission and communication with ground control stations or other UAVs. These devices play a crucial role in various UAV missions, ensuring that UAVs can successfully execute commands, transmit data, and interact with other systems.

[0003] The existing Chinese patent with authorization announcement number CN220281707U discloses a fixing device for a UAV-borne communication device, relating to the field of UAV technology. It includes a support frame, of which there are two. Connecting frames are provided at the front and rear ends of the upper surfaces of the two support frames. Connecting columns are provided on the left and right sides of the two connecting frames. Fixing seats are provided at the front and rear ends of the inner and outer surfaces of the two support frames. Shock-absorbing rubber balls are provided at the upper end of the fixing seats. Support plates are provided between the two front left and right shock-absorbing rubber balls and the two rear left and right shock-absorbing rubber balls, respectively. Vertical plates are provided at the left and right ends of the lower surfaces of the two support plates, and horizontal plates are provided at the front and rear ends of the lower surfaces of the two vertical plates. This design simplifies the installation structure, ensures efficient assembly and disassembly, and integrates the fixing device for the communication device with the UAV's support feet, avoiding excessive additional weight and reducing the impact on the UAV's range and maneuverability.

[0004] The above-mentioned device also has shortcomings. Although the installation device has a simple structure and can ensure efficient disassembly and assembly, it cannot meet the needs of installing communication equipment of different sizes. This means that different installation devices need to be designed when the drone is equipped with different types of communication equipment, which limits the applicability of the drone. Utility Model Content

[0005] In view of the shortcomings of the existing technology, the purpose of this utility model is to provide an installation support device for UAV-borne communication equipment, which aims to solve the technical problem that the above-mentioned devices cannot install communication equipment of different sizes, thus limiting the application range of UAVs.

[0006] To achieve the above objectives, the present invention adopts the following technical solution:

[0007] A mounting support device for an unmanned aerial vehicle (UAV)-borne communication device includes a housing, a communication device body, and further includes:

[0008] A flight component, mounted on the fuselage, is used to provide power for the drone's flight;

[0009] The mounting assembly is arranged on the shell and used for mounting the body of the communication device.

[0010] The clamping assembly is arranged on the mounting assembly.

[0011] The fixing assembly is arranged on the mounting assembly and used for fixing the body of the communication device.

[0012] The buffering assembly is arranged on the mounting assembly and used for buffering the impact force generated when the unmanned aerial vehicle lands.

[0013] Preferably, the flying assembly comprises:

[0014] The bracket is arranged on the shell and fixedly connected with the shell.

[0015] The driving motor is arranged on the bracket and fixedly connected with the bracket.

[0016] The fan blade is arranged on the output shaft of the driving motor and fixedly connected with the output shaft of the driving motor.

[0017] Preferably, the mounting assembly comprises:

[0018] The fixed frame is arranged on the shell and fixedly connected with the shell.

[0019] The square magnet is arranged on the shell and fixedly connected with the shell.

[0020] The fixed plate is arranged on the fixed frame and slidably connected with the fixed frame.

[0021] The iron plate is arranged on the fixed plate and fixedly connected with the fixed plate, and the iron plate is magnetically connected with the square magnet.

[0022] The second electromagnet is arranged on the fixed plate and fixedly connected with the fixed plate.

[0023] The second spring is arranged on the fixed plate and fixedly connected with the fixed plate.

[0024] The fixed groove is arranged on the fixed frame.

[0025] The clamping plate is arranged on the fixed plate and slidably connected with the fixed plate, the clamping plate is fixedly connected with the second spring, and the clamping plate is slidably connected with the fixed frame.

[0026] The connecting column is arranged on the fixed plate and fixedly connected with the fixed plate.

[0027] The mounting plate is arranged on the connecting column and fixedly connected with the connecting column.

[0028] Preferably, the clamping assembly comprises:

[0029] A sliding groove is arranged on the mounting plate.

[0030] A first electromagnet is arranged on the sliding groove and fixedly connected with the mounting plate.

[0031] A first spring is arranged on the first electromagnet and fixedly connected with the first electromagnet.

[0032] A clamping plate is arranged on the sliding groove and slidably connected with the mounting plate, and the clamping plate is fixedly connected with the first spring.

[0033] Preferably, the fixing assembly comprises:

[0034] A self-locking electric telescopic rod is arranged on the fixing plate and fixedly connected with the fixing plate.

[0035] A pressing plate is arranged on the self-locking electric telescopic rod and fixedly connected with the self-locking electric telescopic rod.

[0036] Preferably, the buffer assembly comprises:

[0037] A first telescopic cylinder is arranged on the fixing plate and fixedly connected with the mounting plate.

[0038] A second telescopic cylinder is arranged on the first telescopic cylinder and slidably connected with the first telescopic cylinder.

[0039] A third spring is arranged on the fixing plate and fixedly connected with the fixing plate, and the third spring is fixedly connected with the second telescopic cylinder.

[0040] A support frame is arranged on the second telescopic cylinder and fixedly connected with the second telescopic cylinder.

[0041] Preferably, the surface of the clamping plate is coated with multiple shielding coatings, and the side close to the communication equipment is provided with an anti-skid pad.

[0042] Preferably, the surface of the fixing plate is coated with multiple shielding coatings.

[0043] Preferably, the clamping plate is magnetically connected with the first electromagnet.

[0044] In summary, due to the adoption of the above technical solutions, the present application has the following advantages:

[0045] Through the setting of the first electromagnet, the first spring and the clamping plate, the magnetic force generated by the first electromagnet can quickly pull apart the clamping plate, so that the space between the clamping plate and other clamping plates can accommodate communication equipment bodies of different sizes, and then the elastic force of the first spring can tightly clamp the communication equipment bodies of different sizes, so that the unmanned aerial vehicle can load the communication equipment bodies of different sizes, and the application range is expanded. BRIEF DESCRIPTION OF DRAWINGS

[0046] In order to more clearly illustrate the technical scheme of the embodiments of the present application, the drawings needed in the embodiment description will be briefly introduced as follows. Obviously, the drawings described below are only some embodiments of the present application, and other drawings can also be obtained according to these drawings without creative labor for those skilled in the art.

[0047] Figure 1 A three-dimensional structural schematic view of the mounting support device of the unmanned aerial vehicle-mounted communication equipment is shown.

[0048] Figure 2 A sectional view of the mounting support device of the unmanned aerial vehicle-mounted communication equipment is shown.

[0049] Figure 3 A three-dimensional structural schematic view of the mounting support device of the unmanned aerial vehicle-mounted communication equipment is shown. Figure 2 A local enlarged schematic view of position A in FIG.

[0050] Figure 4 A three-dimensional structural schematic view of the mounting support device of the unmanned aerial vehicle-mounted communication equipment is shown. Figure 2 A local enlarged schematic view of position B in FIG.

[0051] Figure 5 Another sectional view of the mounting support device of the unmanned aerial vehicle-mounted communication equipment is shown.

[0052] Figure 6 A three-dimensional structural schematic view of the mounting support device of the unmanned aerial vehicle-mounted communication equipment is shown. Figure 5 A local enlarged schematic view of position C in FIG.

[0053] LEGEND:

[0054] 1, shell; 2, communication equipment body; 3, mounting plate; 4, sliding groove; 5, first electromagnet; 6, first spring; 7, clamping plate; 8, support; 9, driving motor; 10, fan blade; 11, fixed frame; 12, square magnet; 13, fixed plate; 14, iron plate; 15, second electromagnet; 16, second spring; 17, fixed groove; 18, clamping plate; 19, connecting column; 20, self-locking electric telescopic rod; 21, pressing plate; 22, first telescopic cylinder; 23, second telescopic cylinder; 24, third spring; 25, support frame. DETAILED DESCRIPTION

[0055] With reference to the accompanying drawings, the technical solutions in the embodiments of the present application will be clearly and completely described below, obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of the present application.

[0056] In the description of the present application, it should be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, and therefore cannot be understood as indicating or implying that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the present application.

[0057] It should be noted that when a component is referred to as "fixed to" another component, it can be directly on the other component or there can be a middle component. When a component is referred to as "connected to" another component, it can be directly connected to the other component or there can be a middle component. When a component is referred to as "disposed on" another component, it can be directly disposed on the other component or there can be a middle component. The terms "vertical", "horizontal", "left", "right" and the like used herein are for illustrative purposes only.

[0058] In addition, the terms "first", "second" are used only for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined with "first", "second" can explicitly or implicitly include one or more of the features. In the description of the present application, the meaning of "multiple" is two or more, unless otherwise specifically limited.

[0059] Referring to Figures 1 to 6 Further description is made to the mounting support device for the unmanned aerial vehicle communication equipment.

[0060] A mounting support device for unmanned aerial vehicle communication equipment, comprising a shell 1, a communication equipment body 2, further comprising:

[0061] A flight assembly is arranged on the shell 1 and is used to provide power for the flight of the unmanned aerial vehicle, and the flight assembly comprises:

[0062] A bracket 8 is arranged on the shell 1 and is fixedly connected with the shell 1.

[0063] A driving motor 9 is arranged on the support 8 and fixedly connected with the support 8.

[0064] A fan blade 10 is arranged on the output shaft of the driving motor 9 and fixedly connected with the output shaft of the driving motor 9.

[0065] The driving motor 9 is started, and the output shaft of the driving motor 9 rotates to drive the fan blade 10 fixedly connected with the output shaft of the driving motor 9 to rotate, so that the fan blade 10 rotates to stir air to generate upward airflow, and the unmanned aerial vehicle is enabled to fly and work.

[0066] A mounting assembly is arranged on the casing 1 and used for mounting the communication device body 2, and the mounting assembly comprises:

[0067] A fixed frame 11 is arranged on the casing 1 and fixedly connected with the casing 1.

[0068] A square magnet 12 is arranged on the casing 1 and fixedly connected with the casing 1.

[0069] A fixed plate 13 is arranged on the fixed frame 11 and slidably connected with the fixed frame 11, and a plurality of shielding coating layers are coated on the surface of the fixed plate 13.

[0070] An iron plate 14 is arranged on the fixed plate 13 and fixedly connected with the fixed plate 13, and the iron plate 14 is magnetically connected with the square magnet 12.

[0071] A second electromagnet 15 is arranged on the fixed plate 13 and fixedly connected with the fixed plate 13.

[0072] A second spring 16 is arranged on the fixed plate 13 and fixedly connected with the fixed plate 13.

[0073] A fixed groove 17 is arranged on the fixed frame 11.

[0074] A clamping plate 18 is arranged on the fixed plate 13 and slidably connected with the fixed plate 13, the clamping plate 18 is fixedly connected with the second spring 16, and the clamping plate 18 is slidably connected with the fixed frame 11.

[0075] A connecting column 19 is arranged on the fixed plate 13 and fixedly connected with the fixed plate 13.

[0076] A mounting plate 3 is arranged on the connecting column 19 and fixedly connected with the connecting column 19.

[0077] The second electromagnet 15 is started, and the magnetic force generated by the second electromagnet 15 pulls the clamping plate 18 to move in the direction of the second electromagnet 15 until the clamping plate 18 is separated from the fixed slot 17, and the iron plate 14 is slightly pulled to make the iron plate 14 magnetically connected with the square magnet 12 to be separated from the magnetic force generated by the square magnet 12, so that the installation assembly can be quickly replaced.

[0078] Referring to Figures 1 to 6 , the clamping assembly is arranged on the installation assembly, and the clamping assembly comprises:

[0079] The sliding slot 4 is arranged on the installation plate 3.

[0080] The first electromagnet 5 is arranged on the sliding slot 4 and fixedly connected with the installation plate 3.

[0081] The first spring 6 is arranged on the first electromagnet 5 and fixedly connected with the first electromagnet 5.

[0082] The clamping plate 7 is arranged on the sliding slot 4 and slidably connected with the installation plate 3, the clamping plate 7 is fixedly connected with the first spring 6, the surface of the clamping plate 7 is coated with a plurality of shielding coating layers, and the side close to the communication device is provided with an anti-skid pad, and the clamping plate 7 is magnetically connected with the first electromagnet 5.

[0083] The first electromagnet 5 is started, and the magnetic force generated by the first electromagnet 5 pulls the clamping plate 7 magnetically connected with the first electromagnet 5 to move in the direction of the first electromagnet 5, the communication device body 2 is placed on the installation plate 3, the first electromagnet 5 is turned off, the clamping plate 7 loses the magnetic force restraint and moves to the communication device body 2 under the elastic force of the fixedly connected first spring 6, and the clamping plate 7 is tightly close to the communication device body 2.

[0084] Through the arrangement of the first electromagnet 5, the first spring 6 and the clamping plate 7, the clamping plate 7 is quickly pulled apart by the magnetic force generated by the first electromagnet 5, so that the space between the clamping plate 7 and other clamping plates 7 can accommodate communication device bodies 2 of different sizes, and then the elastic force of the first spring 6 makes the clamping plate 7 tightly clamp the communication device bodies 2 of different sizes, so that the unmanned aerial vehicle can load communication devices of different sizes, and the application range is expanded.

[0085] The fixing assembly is arranged on the installation assembly and used for fixing the communication device body 2, and the fixing assembly comprises:

[0086] The self-locking electric telescopic rod 20 is arranged on the fixing plate 13 and fixedly connected with the fixing plate 13.

[0087] The pressing plate 21 is arranged on the self-locking electric telescopic rod 20 and fixedly connected with the self-locking electric telescopic rod 20.

[0088] The self-locking electric telescopic rod 20 is started, and the self-locking electric telescopic rod 20 is in elongation movement to drive the pressing plate 21 fixedly connected with the self-locking electric telescopic rod 20 to move downward until the pressing plate 21 is tightly attached to the communication device body 2, and the fixing effect is achieved.

[0089] With reference to Figures 1 to 6 The buffer assembly is arranged on the mounting assembly and is used for buffering the impact force generated when the unmanned aerial vehicle lands.

[0090] The first telescopic cylinder 22 is arranged on the fixed plate 13 and is fixedly connected with the mounting plate 3.

[0091] The second telescopic cylinder 23 is arranged on the first telescopic cylinder 22 and is slidingly connected with the first telescopic cylinder 22.

[0092] The third spring 24 is arranged on the fixed plate 13 and is fixedly connected with the fixed plate 13. The third spring 24 is fixedly connected with the second telescopic cylinder 23.

[0093] The support frame 25 is arranged on the second telescopic cylinder 23 and is fixedly connected with the second telescopic cylinder 23.

[0094] When the unmanned aerial vehicle returns and lands, the impact force generated when the support frame 25 contacts the ground is transmitted to the second telescopic cylinder 23 through the support frame 25, and then is transmitted to the third spring 24 fixedly connected with the second telescopic cylinder 23 through the second telescopic cylinder 23. The impact force is buffered by the elasticity of the third spring 24, and the effect of buffering and protecting the unmanned aerial vehicle is achieved.

[0095] Working principle: with reference to Figures 1 to 6 The first electromagnet 5 is started, the first electromagnet 5 generates a magnetic force to pull the clamping plate 7 magnetically connected with the first electromagnet 5 to move in the direction of the first electromagnet 5, and the communication device body 2 is placed on the mounting plate 3. The first electromagnet 5 is turned off, the clamping plate 7 loses the magnetic force constraint and moves towards the communication device body 2 under the elastic force of the fixedly connected first spring 6 until the clamping plate 7 is tightly attached to the communication device body 2. The self-locking electric telescopic rod 20 is started, and the self-locking electric telescopic rod 20 is in elongation movement to drive the pressing plate 21 fixedly connected with the self-locking electric telescopic rod 20 to move downward until the pressing plate 21 is tightly attached to the communication device body 2, and the fixing effect is achieved.

[0096] When the unmanned aerial vehicle needs to work, the driving motor 9 is started, the output shaft of the driving motor 9 rotates to drive the fan blade 10 fixedly connected with the output shaft of the driving motor 9 to rotate, the fan blade 10 rotates to stir air to generate upward airflow, so that the unmanned aerial vehicle performs flight work, when the unmanned aerial vehicle returns and lands, the impact force generated by the support frame 25 contacting the ground is transmitted to the second telescopic cylinder 23 through the support frame 25, and then transmitted to the third spring 24 fixedly connected with the second telescopic cylinder 23 through the second telescopic cylinder 23, the impact force is buffered by the elasticity of the third spring 24, so that the effect of buffering and protecting the unmanned aerial vehicle is achieved;

[0097] With reference to Figures 1 to 6 When the installation assembly needs to be replaced, the second electromagnet 15 is started, the magnetic force generated by the second electromagnet 15 pulls the clamping plate 18 to move towards the second electromagnet 15, until the clamping plate 18 is separated from the fixed groove 17, the iron plate 14 is slightly pulled to make the iron plate 14 magnetically connected with the square magnet 12 separated from the magnetic force generated by the square magnet 12, so that the installation assembly can be quickly replaced.

[0098] The above description of the embodiments enables those skilled in the art to implement or use the present application. Various modifications to these embodiments will be apparent to those skilled in the art, and the general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present application. Therefore, the present application will not be limited to these embodiments shown herein, but will conform to the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. An installation support device for unmanned airborne communication equipment, comprising a casing (1), a communication equipment body (2), characterized in that, Also include: Flight components, provided on the shell (1), for providing power unmanned aerial vehicle flight; Mounting components, provided on the shell (1), for installing the body of the communication device (2); Clamping components, provided on the mounting assembly; Mounting plate (3) for mounting clamping components; The clamping assembly comprises: Slide groove (4) provided on the mounting plate (3); The first electromagnet (5) is provided on the slide groove (4) and is fixedly connected with the mounting plate (3); The first spring (6) is provided on the first electromagnet (5) and is fixedly connected with the first electromagnet (5); The clamping plate (7) is provided on the slide groove (4) and is slidably connected with the mounting plate (3), and the clamping plate (7) is fixedly connected with the first spring (6); The fixed component is provided on the mounting assembly for fixing the body of the communication device (2); The buffer assembly is provided on the mounting assembly for buffering the impact force generated when the unmanned aerial vehicle lands.

2. The mounting support apparatus for unmanned airborne communication equipment according to claim 1, wherein The flight assembly comprises: Support (8) provided on the shell (1) and fixedly connected with the shell (1); Drive motor (9) provided on the support (8) and fixedly connected with the support (8); Fan blade (10) provided on the output shaft of the drive motor (9) and fixedly connected with the output shaft of the drive motor (9).

3. The mounting support apparatus for unmanned airborne communication equipment according to claim 2, wherein The mounting assembly comprises: Fixed frame (11) provided on the shell (1) and fixedly connected with the shell (1); Square magnet (12) provided on the shell (1) and fixedly connected with the shell (1); Fixed plate (13) provided on the fixed frame (11) and slidably connected with the fixed frame (11); Iron plate (14) provided on the fixed plate (13) and fixedly connected with the fixed plate (13), and the iron plate (14) is magnetically connected with the square magnet (12); Second electromagnet (15) provided on the fixed plate (13) and fixedly connected with the fixed plate (13); Second spring (16) provided on the fixed plate (13) and fixedly connected with the fixed plate (13); Fixed groove (17) provided on the fixed frame (11); Clamping plate (18) provided on the fixed plate (13) and slidably connected with the fixed plate (13), the clamping plate (18) is fixedly connected with the second spring (16), and the clamping plate (18) is slidably connected with the fixed frame (11); Connecting column (19) provided on the fixed plate (13) and fixedly connected with the fixed plate (13).

4. The mounting support apparatus for unmanned airborne communication equipment according to claim 3, wherein The mounting plate (3) is provided on the connecting column (19), and the mounting plate (3) is fixedly connected with the connecting column (19).

5. The mounting support apparatus for unmanned airborne communication equipment according to claim 4, wherein, The fixed component comprises: Self-locking electric telescopic rod (20) provided on the fixed plate (13) and fixedly connected with the fixed plate (13); Pressing plate (21) provided on the self-locking electric telescopic rod (20) and fixedly connected with the self-locking electric telescopic rod (20).

6. The mounting support apparatus for unmanned airborne communication equipment according to claim 5, wherein, The buffer assembly comprises: A first telescopic cylinder (22) is arranged on the fixed plate (13) and fixedly connected with the mounting plate (3); A second telescopic cylinder (23) is arranged on the first telescopic cylinder (22) and slidably connected with the first telescopic cylinder (22); A third spring (24) is arranged on the fixed plate (13) and fixedly connected with the fixed plate (13), and the third spring (24) is fixedly connected with the second telescopic cylinder (23); A support frame (25) is arranged on the second telescopic cylinder (23) and fixedly connected with the second telescopic cylinder (23).

7. The mounting support apparatus for unmanned airborne communication equipment according to claim 6, wherein The surface of the clamping plate (7) is coated with multiple shielding coating layers, and the side close to the communication equipment is provided with a non-slip pad.

8. The mounting support apparatus for unmanned airborne communication equipment according to claim 7, wherein The surface of the fixed plate (13) is coated with multiple shielding coating layers.

9. The mounting support apparatus for unmanned airborne communication equipment of claim 8, wherein, The clamping plate (7) is magnetically connected with the first electromagnet (5).

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