Shell heat dissipation structure of unmanned aerial vehicle detection equipment
By designing heat dissipation plates and through-hole structures on the shell of the drone detection equipment, the problem of poor heat dissipation was solved, achieving efficient heat dissipation and ensuring stable operation of the equipment under high load conditions.
Patent Information
- Application Number
- CN202422882095.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-26
- Publication Date
- 2025-11-21
- Estimated Expiration
- 2034-11-26
AI Technical Summary
Existing drone detection equipment suffers from poor heat dissipation during operation, affecting equipment performance and reliability.
An outer shell structure including a support, a cover and a chassis is designed. The support is provided with heat dissipation plates and heat dissipation holes, and a heat dissipation gap is formed between the cover and the support. The heat dissipation plates and holes enable effective heat dissipation of internal components.
The heat dissipation effect of the UAV detection equipment has been improved, ensuring stable operation of the equipment under high-load working conditions.
Smart Images
Figure CN223584556U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the field of security products especially relates to a shell heat dissipation structure of unmanned aerial vehicle detection equipment. BACKGROUND
[0002] In recent years, the unmanned aerial vehicle technology field develops rapidly, and the cost of using unmanned aerial vehicle is also lower and lower, which brings a threat to various confidential units and important facilities, so the control and detection of unmanned aerial vehicle become very important, and therefore unmanned aerial vehicle detection equipment is needed. The internal elements of unmanned aerial vehicle detection equipment will heat when working, and therefore a shell heat dissipation structure of unmanned aerial vehicle detection equipment is provided. SUMMARY
[0003] The utility model discloses a shell heat dissipation structure of unmanned aerial vehicle detection equipment, has good heat dissipation effect.
[0004] Technical scheme: in order to realize the above-mentioned purpose, the utility model discloses a shell heat dissipation structure of unmanned aerial vehicle detection equipment, including the shell of unmanned aerial vehicle detection equipment, the shell includes support, cover shell and bottom disc, cover shell covers and is established on the support, and the bottom disc is connected below the support, cover shell and support form first element cavity between, be provided with first radiating plate group on the support, and first radiating plate group corresponds to be located the outer periphery side of first element cavity, still be provided with a plurality of heat dissipation through -hole on the support, and the inside communication of first element cavity is communicated with heat dissipation through -hole.
[0005] Further, the heat dissipation through -hole is located between the adjacent two radiating plates in the first radiating plate group.
[0006] Further, the support is provided with inner ring and outer ring, and the annular clamping groove is formed between the inner ring and the outer ring, the bottom of the cover shell is inserted into the annular clamping groove, and the heat dissipation gap is formed between the cover shell and the inner ring, and the heat dissipation through -hole is located in the annular clamping groove, and the heat dissipation through -hole is communicated with the first element cavity through the heat dissipation gap.
[0007] Further, the heat dissipation through -hole is located below the annular clamping groove, and the opening of the heat dissipation through -hole is downward, the bottom end of the heat dissipation gap is communicated with the heat dissipation through -hole, and the top end of the heat dissipation gap is communicated with the first element cavity.
[0008] Further, the bottom profile of the cover shell is rough.
[0009] Further, the second element cavity is formed between the bottom disc and the support, and the second radiating plate group is further provided on the support, and the second radiating plate group corresponds to be located the outer periphery side of second element cavity.
[0010] The shell heat dissipation structure of unmanned aerial vehicle detection equipment of the utility model, through radiating plate group and heat dissipation hole jointly heat dissipation unmanned aerial vehicle detection equipment, and the heat dissipation effect is good. BRIEF DESCRIPTION OF DRAWINGS
[0011] BRIEF DESCRIPTION OF DRAWINGS Fig. 1 It is an overall structure diagram of the shell of the unmanned aerial vehicle detection device.
[0012] BRIEF DESCRIPTION OF DRAWINGS Fig. 2 It is a schematic diagram of the heat dissipation through hole communicating with the inside of the first element cavity through the heat dissipation gap. DETAILED DESCRIPTION
[0013] The utility model will be described further in connection with the drawings.
[0014] As shown in the accompanying Figs. 1-2 The shell heat dissipation structure of the unmanned aerial vehicle detection device includes the shell of the unmanned aerial vehicle detection device, the shell includes support 1, cover 2 and bottom disc 3. As shown in the accompanying Fig. 1 Cover 2 is eggshell-shaped, cover 2 is covered on support 1, and bottom disc 3 is connected below support 1. As shown in the accompanying Fig. 2 First element cavity 4 is formed between cover 2 and support 1, and second element cavity 6 is formed between bottom disc 3 and support 1, and unmanned aerial vehicle spectrum detection assembly is arranged in first element cavity 4 and second element cavity 6, and the unmanned aerial vehicle spectrum detection assembly detects and identifies unmanned aerial vehicles by analyzing signals in radio spectrum. When the unmanned aerial vehicle detection device works, the unmanned aerial vehicle spectrum detection assembly will heat, so the corresponding heat dissipation structure is needed on the shell of the unmanned aerial vehicle detection device.
[0015] As shown in the accompanying Fig. 1 First heat dissipation plate group 5 is arranged on support 1, and second heat dissipation plate group 7 is also arranged on support 1. First heat dissipation plate group 5 corresponds to the outer peripheral side of first element cavity 4, and second heat dissipation plate group 7 corresponds to the outer peripheral side of second element cavity 6. In addition, a plurality of heat dissipation through holes 8 are formed on support 1, and the heat dissipation through holes 8 communicate with the inside of the first element cavity 4. Through the cooperation of the heat dissipation plate group and the heat dissipation through hole 8, the heat dissipation of the heating element in the shell can be effectively carried out.
[0016] As shown in the accompanying Fig. 1 First heat dissipation plate group 5 is divided into a plurality of sub-plate groups arranged at equal angles in a ring, and a plurality of heat dissipation plates are arranged in each sub-plate group. Second heat dissipation plate group 7 includes two sub-plate groups arranged on both sides of second element cavity 6.
[0017] As shown in the accompanying Fig. 2 Heat dissipation through hole 8 is located between adjacent two heat dissipation plates in first heat dissipation plate group 5, heat dissipation through hole 8 can generate heat dissipation airflow, and the heat dissipation airflow passes through the heat dissipation plate, which has better heat dissipation effect.
[0018] As shown in the accompanying Fig. 2As shown in the figure, the support 1 is provided with an inner ring 9 and an outer ring 10, and the inner ring 9 and the outer ring 10 form an annular clamping groove, the bottom of the cover 2 is inserted into the annular clamping groove, and a heat dissipation gap 11 is formed between the cover 2 and the inner ring 9. The heat dissipation through hole 8 is also located in the annular clamping groove, so that the heat dissipation through hole 8 can communicate with the first element cavity 4 through the heat dissipation gap 11.
[0019] Specifically, the heat dissipation through hole 8 is located below the annular clamping groove, and the opening of the heat dissipation through hole 8 is downward, so that dust or rainwater is not easy to enter the first element cavity 4 from the heat dissipation through hole 8. The bottom end of the heat dissipation gap 11 communicates with the heat dissipation through hole 8, and the top end of the heat dissipation gap 11 communicates with the first element cavity 4.
[0020] The bottom profile of the cover 2 is a rough surface, so that the bottom profile of the cover 2 and the groove bottom of the annular clamping groove can form an air gap for air flow, so that the bottom end of the heat dissipation gap 11 can communicate with the heat dissipation through hole 8.
[0021] In the utility model, the first element cavity 4 and the second element cavity 6 are cooled by the first heat dissipation plate group 5 and the second heat dissipation plate group 7 respectively, and a plurality of heat dissipation through holes 8 are further formed in the support 1, the heat dissipation through holes 8 communicate with the first element cavity 4 through the heat dissipation gap 11, and the heat dissipation effect of the first element cavity 4 is further improved, so that the unmanned aerial vehicle spectrum detection assembly in the first element cavity 4 and the second element cavity 6 can be effectively cooled when the unmanned aerial vehicle detection equipment works.
[0022] The above only describes the preferred embodiments of the utility model, and it should be pointed out that for ordinary skilled persons in the technical field, some improvements and decorations can be made without departing from the principles of the utility model, and these improvements and decorations should also be regarded as the protection scope of the utility model.
Claims
1. An unmanned aerial vehicle detection device shell heat dissipation structure, characterized in that: The shell of the unmanned aerial vehicle detection device comprises a support (1), a cover (2) and a bottom plate (3), the cover (2) is covered on the support (1), and the bottom plate (3) is connected below the support (1); a first element cavity (4) is formed between the cover (2) and the support (1); a first heat dissipation plate group (5) is arranged on the support (1), and the first heat dissipation plate group (5) is located at the outer circumferential side of the first element cavity (4); a plurality of heat dissipation through holes (8) are formed in the support (1) and communicate with the inside of the first element cavity (4).
2. The unmanned aerial vehicle detection device shell heat dissipation structure according to claim 1, characterized in that: The heat dissipation through holes (8) are located between adjacent two heat dissipation plates in the first heat dissipation plate group (5).
3. The unmanned aerial vehicle detection device shell heat dissipation structure of claim 2, wherein: An inner ring (9) and an outer ring (10) are arranged on the support (1), an annular clamping groove is formed between the inner ring (9) and the outer ring (10), the bottom of the cover (2) is inserted into the annular clamping groove, and a heat dissipation gap (11) is formed between the cover (2) and the inner ring (9); the heat dissipation through holes (8) are located in the annular clamping groove, and the heat dissipation through holes (8) communicate with the first element cavity (4) through the heat dissipation gap (11).
4. The unmanned aerial vehicle detection device shell heat dissipation structure of claim 3, wherein: The heat dissipation through holes (8) are located below the annular clamping groove, and the openings of the heat dissipation through holes (8) are downward; the bottom end of the heat dissipation gap (11) communicates with the heat dissipation through holes (8), and the top end of the heat dissipation gap (11) communicates with the first element cavity (4).
5. The unmanned aerial vehicle detection device shell heat dissipation structure of claim 4, wherein: The bottom profile surface of the cover (2) is a rough surface.
6. The unmanned aerial vehicle detection device shell heat dissipation structure of any one of claims 1-5, wherein: A second element cavity (6) is formed between the bottom plate (3) and the support (1), and a second heat dissipation plate group (7) is arranged on the support (1) and located at the outer circumferential side of the second element cavity (6).