Small pod equipment for unmanned aerial vehicle-mounted radar

Abstract

The utility model relates to the technical field of communication protection, in particular to a small pod device for unmanned aerial vehicle-mounted radar, which comprises a pod outer shell structure, the pod outer shell structure comprises a pod body, a pod top cover, hatch covers and a pod door, the pod top cover is arranged at the top of the pod body, the hatch covers are arranged on two sides of the pod body, and the pod door is arranged in the pod body. The pod doors are arranged on the front face and the back face of the pod body, a round hole clamping groove is formed in the top of the pod top cover, outer heat dissipation holes are reserved in the two pod covers, the inner shell structure is arranged in the pod outer shell structure, and the inner shell structure comprises a battery storage cabin, a host storage cabin and an airborne radar storage cabin; compared with a small pod device of a traditional unmanned aerial vehicle-mounted radar, the small pod device of the unmanned aerial vehicle-mounted radar adopts high-performance light pure aluminum materials and a compact structural design, miniaturization and light weight of the pod device are achieved, the weight and resistance of the unmanned aerial vehicle are reduced, and the flight performance and the cruising ability are improved.

Description

Technical Field

[0001] The utility model belongs to the technical field of communication protection, and in particular relates to a small pod device for an unmanned aerial vehicle-borne radar. Background Art

[0002] With the continuous development of science and technology, drones are increasingly used in military and civilian fields. With the advantages of high flexibility and low risk, drones have become an important means of modern warfare and emergency rescue. The demand for radar systems is also increasing, especially in terms of high-precision detection and real-time information transmission in complex environments.

[0003] Traditional drone-mounted radar pods are usually large and heavy in design to achieve high detection performance. However, this design approach has many problems: large pods increase the weight and drag of drones, reducing their flight performance and endurance; large pods have high requirements for the structural strength of drones, increasing the difficulty of design and manufacturing; at the same time, traditional pods have poor heat dissipation performance, which can easily cause the equipment to overheat and affect the normal operation of the radar system. Utility Model Content

[0004] The purpose of the utility model is to provide a small pod device for unmanned aerial vehicle-borne radar, so as to solve the problems raised in the above-mentioned background technology.

[0005] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0006] A small pod device for unmanned aerial vehicle-mounted radar, comprising:

[0007] A pod shell structure, the pod shell structure comprising a pod body, a pod top cover, a hatch and a pod door, the pod top cover is arranged on the top of the pod body, the hatch cover is arranged on both sides of the pod body, the pod door is arranged on the front and back of the pod body, a round hole slot is arranged on the top of the pod top cover, and external heat dissipation holes are reserved on the two hatch covers;

[0008] The inner shell structure is arranged inside the outer shell structure of the pod, and the inner shell structure includes a battery storage compartment, a main engine storage compartment and an airborne radar storage compartment.

[0009] Preferably, the length, width and height of the cabin body are 370 mm, 258 mm and 350 mm respectively, and the cabin body is made of pure aluminum material as a whole.

[0010] Preferably, the diameter of the circular hole slot is 90 mm, and a partition is provided between the nacelle top cover and the two hatch covers.

[0011] Preferably, a sealing structure is provided between the cabin body and the two cabin covers, and a limiting structure is provided between the partition and the nacelle top cover.

[0012] Preferably, a GPS data receiving antenna is provided on the pod door.

[0013] Preferably, the length, width and height of the battery storage compartment are 195mm, 65mm and 165mm respectively; the front of the battery storage compartment is reserved with a battery operating indicator light port, a battery power display port and a battery switch port; the back of the battery storage compartment is reserved with a battery pack power supply port and a battery pack charging port.

[0014] Preferably, the length, width and height of the host storage compartment are 195mm, 65mm and 165mm respectively; the front of the host storage compartment is reserved with a host switch port, a host operation indicator light port, a host fault indicator light port and a host data receiving indicator light port; the back of the host storage compartment is reserved with a host power supply port, a host data transmission port, a radar power supply port and a radar data receiving port; the side of the host storage compartment is reserved with a lead groove; the back and one side of the host storage compartment are reserved with internal heat dissipation holes.

[0015] Preferably, a cooling fan is provided on the top of the airborne radar storage compartment, and data transmission interfaces are provided on all four sides of the airborne radar storage compartment.

[0016] Compared with the prior art, the beneficial effects of the utility model are:

[0017] (1) Compared with the small pod equipment of traditional UAV-mounted radar, this structure adopts high-performance lightweight pure aluminum material and compact structural design, which realizes the miniaturization and lightness of the pod equipment, reduces the weight and resistance of the UAV, and improves the flight performance and endurance.

[0018] (2) By optimizing the heat dissipation system, the heat dissipation performance of the pod equipment is improved, effectively preventing the equipment from overheating and ensuring the normal operation of the radar system. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 This is a schematic diagram of the pod outer shell structure of the utility model;

[0020] Figure 2 This is one of the exploded views of the pod outer shell of the utility model;

[0021] Figure 3 This is the second exploded view of the pod outer shell of the utility model;

[0022] Figure 4 This is one of the internal structure schematic diagrams of the utility model;

[0023] Figure 5This is the second schematic diagram of the internal structure of the utility model;

[0024] Figure 6 This is a schematic diagram of the airborne radar storage compartment of the utility model;

[0025] In the figure: 1. Cabin body; 2. Nacelle top cover; 3. Hatch cover; 4. Nacelle door; 5. Circular hole slot; 6. External heat dissipation hole; 7. Battery storage compartment; 8. Host storage compartment; 9. Airborne radar storage compartment; 10. Partition; 11. GPS data receiving antenna; 12. Battery working indicator port; 13. Battery power display port; 14. Battery switch port; 15. Battery pack power supply port; 16. Battery pack charging port; 17. Host switch port; 18. Host operation indicator port; 19. Host fault indicator port; 20. Host receiving data indicator port; 21. Host power supply port; 22. Host data transmission port; 23. Radar power supply port; 24. Radar data receiving port; 25. Data transmission interface; 26. Internal heat dissipation hole; 27. Cooling fan. DETAILED DESCRIPTION

[0026] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0027] Example:

[0028] See also Figure 1-Figure 6 As shown, a small pod device for unmanned aerial vehicle-mounted radar includes:

[0029] The pod shell structure includes a pod body 1, a pod top cover 2, a hatch 3 and a pod door 4. The pod top cover 2 is arranged on the top of the pod body 1, the hatch 3 is arranged on both sides of the pod body 1, and the pod door 4 is arranged on the front and back of the pod body 1. A circular hole slot 5 is arranged on the top of the pod top cover 2, and external heat dissipation holes 6 are reserved on the two hatch covers 3;

[0030] The inner shell structure is arranged inside the outer shell structure of the pod, and the inner shell structure includes a battery storage compartment 7, a host storage compartment 8 and an airborne radar storage compartment 9;

[0031] The battery storage compartment 7 is used to store the battery pack of the host; the host storage compartment 8 is used to store the host equipment for data storage control; and the airborne radar storage compartment 9 is used to store the unmanned aerial vehicle onboard radar equipment.

[0032] Depend on Figure 1-Figure 6It can be seen that the length, width and height of the cabin body 1 are 370mm, 258mm and 350mm respectively, and the whole is made of pure aluminum material;

[0033] The diameter of the circular hole slot 5 is 90 mm. A partition 10 is provided between the nacelle top cover 2 and the two hatch covers 3. A circular slot matching the circular hole slot 5 is provided on the partition 10. The partition 10 is used to isolate the space between the nacelle top cover 2 and the left and right hatch covers 3 to prevent dust and other debris from entering the interior of the nacelle and ensure the interior of the nacelle is clean.

[0034] A sealing structure is provided between the cabin body 1 and the two cabin covers 3. The sealing structure is used to ensure the stability of the internal environment of the pod, prevent moisture from entering the interior of the pod, and ensure the normal operation of equipment such as batteries. A limiting structure is provided between the partition 10 and the pod top cover 2. The limiting structure facilitates the opening and closing of the pod top cover 2 on the partition 10, and includes a sliding rod on the partition 10 and a socket on the pod top cover 2;

[0035] A GPS data receiving antenna 11 is provided on the pod door 4;

[0036] The length, width and height of the battery storage compartment 7 are 195 mm, 65 mm and 165 mm respectively. The front of the battery storage compartment 7 is provided with a battery working indicator port 12, a battery power display port 13 and a battery switch port 14. The back of the battery storage compartment 7 is provided with a battery pack power supply port 15 and a battery pack charging port 16.

[0037] The length, width and height of the host storage compartment 8 are 195mm, 65mm and 165mm respectively. The front of the host storage compartment 8 is reserved with a host switch port 17, a host operation indicator port 18, a host fault indicator port 19 and a host receiving data indicator port 20. The back of the host storage compartment 8 is reserved with a host power supply port 21, a host data transmission port 22, a radar power supply port 23 and a radar data receiving port 24. The side of the host storage compartment 8 is reserved with a lead groove. The back and one side of the host storage compartment 8 are reserved with internal heat dissipation holes 26 to ensure the internal temperature of the pod is stable, prevent the temperature from being too high, and ensure the normal operation of the battery, host and airborne radar and other equipment;

[0038] A cooling fan 27 is provided on the top of the airborne radar storage compartment 9 , and data transmission interfaces 25 are provided around the airborne radar storage compartment 9 .

[0039] Although the embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A small pod device for drone-mounted radar, characterized in that: include: A pod shell structure, the pod shell structure comprising a pod body (1), a pod top cover (2), a hatch cover (3) and a pod door (4), the pod top cover (2) being arranged on the top of the pod body (1), the hatch cover (3) being arranged on both sides of the pod body (1), the pod door (4) being arranged on the front and back sides of the pod body (1), the top of the pod top cover (2) being arranged with a circular hole slot (5), and two hatch covers (3) being reserved with external heat dissipation holes (6); The inner shell structure is arranged inside the outer shell structure of the pod, and the inner shell structure comprises a battery storage compartment (7), a main engine storage compartment (8) and an airborne radar storage compartment (9).

2. The small pod device for drone-mounted radar according to claim 1 is characterized in that: The length, width and height of the cabin body (1) are 370 mm, 258 mm and 350 mm respectively, and the cabin body (1) is made of pure aluminum material as a whole.

3. The small pod device for drone-mounted radar according to claim 1 is characterized in that: The diameter of the circular hole slot (5) is 90 mm, and a partition plate (10) is provided between the nacelle top cover (2) and the two hatch covers (3).

4. The small pod device for drone-mounted radar according to claim 3 is characterized in that: A sealing structure is provided between the cabin body (1) and the two cabin covers (3), and a limiting structure is provided between the partition plate (10) and the cabin top cover (2).

5. The small pod device for drone-mounted radar according to claim 1, characterized in that: The pod door (4) is provided with a GPS data receiving antenna (11).

6. The small pod device for drone-mounted radar according to claim 1, characterized in that: The length, width and height of the battery storage compartment (7) are 195 mm, 65 mm and 165 mm respectively. A battery operation indicator port (12), a battery power display port (13) and a battery switch port (14) are reserved on the front of the battery storage compartment (7). A battery pack power supply port (15) and a battery pack charging port (16) are reserved on the back of the battery storage compartment (7).

7. The small pod device for drone-mounted radar according to claim 1, characterized in that: The length, width and height of the host storage compartment (8) are 195 mm, 65 mm and 165 mm respectively. The front of the host storage compartment (8) is reserved with a host switch port (17), a host operation indicator port (18), a host fault indicator port (19) and a host data receiving indicator port (20). The back of the host storage compartment (8) is reserved with a host power supply port (21), a host data transmission port (22), a radar power supply port (23) and a radar data receiving port (24). The side of the host storage compartment (8) is reserved with a lead groove. The back and one side of the host storage compartment (8) are reserved with internal heat dissipation holes (26).

8. The small pod device for drone-mounted radar according to claim 1, characterized in that: A cooling fan (27) is provided on the top of the airborne radar storage compartment (9), and data transmission interfaces (25) are provided on all four sides of the airborne radar storage compartment (9).

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