A new light assembly for use in unmanned aerial vehicles
By using structures such as silicone pads, fixed frames, and stabilizing components in the optical components of unmanned aerial vehicles, the assembly gap problem of optical components under emergency stop and start conditions was solved, the stability of optical parameters and the detection accuracy were improved, and optical failures and data errors were avoided.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- 桂林艺研科技有限公司
- Filing Date
- 2026-02-10
- Publication Date
- 2026-06-02
AI Technical Summary
Existing unmanned aerial vehicles' optical components are prone to assembly gaps under conditions such as sudden stops and turns, leading to functional failures such as optical aiming deviations and blurred images.
The structure employs a design that includes silicone pads, a fixed frame, elastic elements, and stabilizing components. The silicone pads absorb vibration, the elastic elements buffer deformation, and the stabilizing components prevent the optical components from loosening. Combined with adaptive components and a heat dissipation system, it ensures stable connection and heat dissipation of the optical components.
It effectively prevents the optical components from loosening and shifting due to vibration and attitude changes, improves the stability of optical parameters and detection accuracy, avoids data fusion errors and image defects, and ensures the stable operation of the optical components under high load conditions.
Smart Images
Figure CN122126501A_ABST
Abstract
Description
Technical Field
[0001] This invention relates to the field of unmanned aerial vehicles, specifically a novel optical component used in unmanned aerial vehicles. Background Technology
[0002] The use of optical components in unmanned aerial vehicles is primarily to endow them with "vision" and "perception" capabilities. These components act as the "eyes" of the drone, enabling it to "see" its surroundings in real time, achieve autonomous obstacle avoidance, precise positioning, and stable hovering. More importantly, optical components transform drones from simple flight platforms into intelligent data acquisition terminals, enabling them to efficiently complete complex tasks such as surveying, inspection, agricultural analysis, and search and rescue reconnaissance.
[0003] The optical components of the aforementioned existing unmanned aerial vehicles are installed inside the unmanned aerial vehicle using hexagonal screws and countersunk screws. During sudden stops and turns, assembly gaps may occur, causing slight displacement of the optical components, which directly leads to functional failures such as optical aiming deviation and blurred imaging. Summary of the Invention
[0004] To address the shortcomings of existing technologies, this invention provides a novel optical component for use in unmanned aerial vehicles (UAVs). This invention solves the problem that existing UAV optical components experience assembly gaps during sudden stops and turns, leading to minute displacements of the optical components and resulting in functional failures such as optical aiming deviations and blurred images.
[0005] To achieve the above objectives, the present invention provides the following technical solution: a novel optical component for use in unmanned aerial vehicles (UAVs), comprising an optical component body, silicone pads at both ends of the optical component body, a UAV body fixedly connected to the top of the silicone pads, a fixed frame fixedly connected inside the optical component body, a first elastic element inside the fixed frame, the interior of the first elastic element being located outside a connecting rod, a rotating knob at the bottom of the first elastic element, a connecting rod fixedly connected to the top of the rotating knob, the exterior of the connecting rod being located inside the fixed frame, the exterior of the connecting rod being located inside the UAV body, a stabilizing component inside the connecting rod, and the exterior of the stabilizing component being located inside the UAV body.
[0006] The above solution involves the optical component body, which is the core functional component of the drone, having its upper and lower ends tightly fitted with silicone pads. The silicone pads can directly absorb the high-frequency, small-amplitude vibrations generated during the drone's flight, preventing the vibrations from being directly transmitted to the optical component body and causing the connection between the optical component body and the drone's flight equipment body to become loose.
[0007] Preferably, the stabilizing component includes a support rod, which is externally fixedly connected to the inside of a connecting rod. A second elastic element is provided inside the support rod, and a first locking rod is provided at one end of the second elastic element. A third elastic element is provided inside the support rod, and a top plate is provided at the top of the third elastic element. The top of the top plate is located inside the body of the unmanned aerial vehicle.
[0008] Preferably, the outer surfaces of the second and third elastic elements are disposed inside the support rod, the outer surface of the third elastic element is disposed inside the connecting rod, and the outer surface of the first locking rod is slidably connected to the connecting rod and the interior of the unmanned aerial vehicle body.
[0009] Preferably, a support frame is fixedly connected to the bottom outer side of the unmanned aerial vehicle body, and a driver is fixedly connected inside the unmanned aerial vehicle body.
[0010] Preferably, a hinge is fixedly connected to the bottom middle part of the unmanned aerial vehicle body, an opening and closing plate is fixedly connected to the outside of the hinge, a sealing strip is fixedly connected to the inside of the opening and closing plate, and the opening and closing plate and the sealing strip are disposed inside the unmanned aerial vehicle body.
[0011] Preferably, a guide rod is fixedly connected inside the opening and closing plate, and a locking block is slidably connected outside the guide rod. The locking block is slidably connected outside the unmanned aerial vehicle body and inside the opening and closing plate. A first support member is provided at the other end of the locking block. One end of the first support member is located inside the opening and closing plate, and the inside of the first support member is located outside the opening and closing plate. The top end of the opening and closing plate is fixedly connected to the bottom end of the silicone pad.
[0012] Preferably, a first connector is fixedly connected to the outside of the optical component body, a second connector is provided at one end of the first connector, one end of the second connector is fixedly connected to the inside of the unmanned aerial vehicle body, the outside of the first connector is located inside the unmanned aerial vehicle body, and adaptive components are provided inside the first connector and the second connector.
[0013] Preferably, the adaptive component includes a sliding magnet, the outer side of which is slidably connected to the inside of the first connector. One end of the sliding magnet is provided with a supporting magnet, the outer side of which is fixedly connected to the inside of the second connector. The inside of the first connector is provided with a sliding block, the top end of which is provided with a second locking rod. One end of the second locking rod is provided with a second support member, one end of which is located inside the first connector. The outer side of the sliding block and the second locking rod are slidably connected to the inside of the first connector, and one end of the second locking rod is slidably connected to the inside of the second connector.
[0014] Preferably, the unmanned aerial vehicle body has a hot air channel inside, the hot air channel is provided with an exhaust component inside, and the exhaust component is located outside the unmanned aerial vehicle body.
[0015] Preferably, the exhaust assembly comprises a carbon fiber reinforced composite material, the top end of which is disposed inside the hot air channel, a filter plate is fixedly connected to one end of the carbon fiber reinforced composite material, a baffle plate is fixedly connected to one end of the filter plate, and the carbon fiber reinforced composite material is slidably connected to the filter plate and the baffle plate inside the unmanned aerial vehicle body.
[0016] Working principle: First, the driver is activated to drive the unmanned aerial vehicle (UAV) body to fly in the air, and the support frame can keep the UAV body stable in the predetermined position. At the same time, the optical component body inside the UAV body can be quickly replaced through the fixed frame, the first elastic element, the rotating knob, the connecting rod, and the stabilizing component, thereby avoiding the problem of loosening and displacement of the optical component due to changes in flight attitude.
[0017] This invention provides a novel optical component for use in unmanned aerial vehicles. It offers the following advantages: 1. This invention enables the connecting rod, support rod, second elastic element, and first locking rod to rotate synchronously by rotating the rotating knob. When the support rod rotates, the first locking rod slides from inside the unmanned aerial vehicle body into the support rod. At the same time, the first locking rod presses against the second elastic element, thereby achieving the effect of quickly replacing the optical component body. This avoids the loosening and displacement of the optical component caused by changes in flight attitude, the drift of optical parameters caused by direct transmission of vibration, and the decrease in detection accuracy.
[0018] 2. The present invention connects the first connector and the second connector, and the sliding magnet and the supporting magnet attract each other, and the second support supports the second locking rod to be inserted into the second connector, thereby achieving an adaptive effect and avoiding serious problems such as data fusion errors, image stitching defects, and inaccurate target positioning.
[0019] 3. In this invention, the hot air generated by the operation of the optical component reacts with the carbon fiber reinforced composite material through the hot air channel. The carbon fiber reinforced composite material drives the filter plate and the baffle plate to slide outward, and the filter plate slides into the gap inside the unmanned aerial vehicle body, thereby achieving the effect of heat dissipation for the optical component body. This can efficiently conduct and dissipate the heat inside the optical component body, avoid heat accumulation under high load conditions, ensure that the optical components operate within a stable temperature range, and maintain the stability of the optical component's detection accuracy and response speed. Attached Figure Description
[0020] Figure 1 This is a three-dimensional structural diagram of the present invention; Figure 2 This is a partial structural diagram of the optical component body of the present invention; Figure 3 This is a partial structural diagram of the fixed frame of the present invention; Figure 4 This is a partial structural diagram of the opening and closing plate of the present invention; Figure 5 This is a partial structural diagram of the unmanned aerial vehicle body of the present invention; Figure 6 for Figure 5 Enlarged view of point A in the middle; Figure 7 This is a partial structural diagram of the second locking rod of the present invention; Figure 8 This is a partial structural diagram of the support frame of the present invention; Figure 9 for Figure 8 Enlarged diagram of point B in the middle.
[0021] The components include: 1. Optical component body; 2. Silicone pad; 3. Unmanned aerial vehicle body; 4. Fixed frame; 5. First elastic element; 6. Rotating knob; 7. Connecting rod; 8. Stabilizing component; 81. Support rod; 82. Second elastic element; 83. First locking rod; 84. Third elastic element; 85. Top plate; 9. Support frame; 10. Driver; 11. Hinge; 12. Opening and closing plate; 13. Sealing strip; 14. Guide rod; 15. First support component; 16. Locking block; 17. First connector; 18. Second connector; 19. Adaptive component; 191. Sliding magnet; 192. Supporting magnet; 193. Sliding block; 194. Second locking rod; 195. Second support component; 20. Hot air channel; 21. Exhaust component; 211. Carbon fiber reinforced composite material; 212. Filter plate; 213. Baffle plate. Detailed Implementation
[0022] The technical solution of the present invention will now be clearly and completely described with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.
[0023] Please see the appendix Figure 1 - Appendix Figure 3This invention provides a novel optical component for use in unmanned aerial vehicles (UAVs), comprising an optical component body 1, with silicone pads 2 at both ends of the optical component body 1, and an UAV body 3 fixedly connected to the top of the silicone pads 2. A fixed frame 4 is fixedly connected inside the optical component body 1, and a first elastic element 5 is disposed inside the fixed frame 4. The interior of the first elastic element 5 is disposed outside the connecting rod 7, and a rotating knob 6 is disposed at the bottom of the first elastic element 5. The top of the rotating knob 6 is fixedly connected to the connecting rod 7, and the exterior of the connecting rod 7 is disposed inside the fixed frame 4 and inside the UAV body 3. A stabilizing component 8 is disposed inside the connecting rod 7, and the exterior of the stabilizing component 8 is disposed inside the UAV body 3.
[0024] Specifically, the unmanned aerial vehicle body 3 is used to support and fix the silicone pad 2, and the silicone pad 2 is used to protect the optical component body 1. At the same time, the optical component body 1 is used to support and fix the fixing frame 4, and the fixing frame 4 is used to support the rotation knob 6 and the connecting rod 7 to rotate and slide. The rotation knob 6 and the connecting rod 7 are supported inside the fixing frame 4 by the first elastic element 5, and the first elastic element 5 can assist the rotation knob 6 to shake up and down, which can prevent the rotation knob 6 and the connecting rod 7 from sliding and being damaged inside the fixing frame 4 when the optical component body 1 is removed. Furthermore, the unmanned aerial vehicle body 3 has a hidden camera inside, which can be exposed by opening the cover when needed, so as to observe the external environment.
[0025] Please see the appendix Figure 1 - Appendix Figure 3 The stabilizing component 8 includes a support rod 81, which is externally fixedly connected to the inside of the connecting rod 7. A second elastic element 82 is provided inside the support rod 81. A first locking rod 83 is provided at one end of the second elastic element 82. A third elastic element 84 is provided inside the support rod 81. A top plate 85 is provided at the top of the third elastic element 84. The top of the top plate 85 is located inside the unmanned aerial vehicle body 3. The second elastic element 82 and the third elastic element 84 are externally located inside the support rod 81. The third elastic element 84 is externally located inside the connecting rod 7. The first locking rod 83 is externally slidably connected to the inside of the connecting rod 7 and the unmanned aerial vehicle body 3. Specifically, the connecting rod 7 is used to support and fix the support rod 81, and the support rod 81 is used to support the second elastic member 82 for compression. At the same time, the second elastic member 82 is used to support the first locking rod 83 to be inserted into the unmanned aerial vehicle body 3. The connecting rod 7 and the support rod 81 are used to support the third elastic member 84 for compression. The third elastic member 84 is used to support the top plate 85 to slide up and down. When the optical component body 1 shakes, the top plate 85 will press against the inside of the unmanned aerial vehicle body 3. There is a gap between the first locking rod 83 and the inside of the unmanned aerial vehicle body 3. The third elastic member 84 will avoid damage to the first locking rod 83 through its own characteristics.
[0026] Please see the appendix Figure 4 - Appendix Figure 6 A support frame 9 is fixedly connected to the bottom outer side of the unmanned aerial vehicle body 3. A driver 10 is fixedly connected inside the unmanned aerial vehicle body 3. A hinge 11 is fixedly connected to the bottom middle part of the unmanned aerial vehicle body 3. An opening and closing plate 12 is fixedly connected to the outside of the hinge 11. A sealing strip 13 is fixedly connected inside the opening and closing plate 12. The opening and closing plate 12 and the sealing strip 13 are located inside the unmanned aerial vehicle body 3. A guide rod 14 is fixedly connected inside the opening and closing plate 12. A locking block 16 is slidably connected to the outside of the guide rod 14. The locking block 16 is slidably connected to the inside of the unmanned aerial vehicle body 3 and the opening and closing plate 12. A first support member 15 is provided at the other end of the locking block 16. One end of the first support member 15 is located inside the opening and closing plate 12. The inside of the first support member 15 is located outside the opening and closing plate 12. The top end of the opening and closing plate 12 is fixedly connected to the bottom end of the silicone pad 2. Specifically, the unmanned aerial vehicle (UAV) body 3 is used to support and fix the support frame 9, and the support frame 9 allows the UAV body 3 to be steadily stopped in a predetermined position. At the same time, the UAV body 3 is used to support and fix the driver 10, and the driver 10 will cause the UAV body 3 to fly. Then, the UAV body 3 is used to support and fix the hinge 11, and the hinge 11 is used to assist the opening and closing plate 12 to rotate. Then, the opening and closing plate 12 is locked inside the UAV body 3 by the guide rod 14, the first support member 15, and the locking block 16. The opening and closing plate 12 is used to support and fix the sealing strip 13, and the sealing strip 13 can prevent dust and liquid from entering the UAV body 3.
[0027] Please see the appendix Figure 5 - Appendix Figure 7The optical component body 1 is externally fixedly connected to a first connector 17. A second connector 18 is provided at one end of the first connector 17. One end of the second connector 18 is fixedly connected to the inside of the unmanned aerial vehicle body 3. The outside of the first connector 17 is located inside the unmanned aerial vehicle body 3. An adaptive component 19 is provided inside the first connector 17 and the second connector 18. The adaptive component 19 includes a sliding magnet 191. The outside of the sliding magnet 191 is slidably connected to the inside of the first connector 17. A supporting magnet 192 is provided at one end of the sliding magnet 191. The outside of the supporting magnet 192 is fixedly connected to the inside of the second connector 18. A sliding block 193 is provided inside the first connector 17. A second locking rod 194 is provided at the top of the sliding block 193. A second support member 195 is provided at one end of the second locking rod 194. One end of the second support member 195 is located inside the first connector 17. The outside of the sliding block 193 and the second locking rod 194 are slidably connected to the inside of the first connector 17. One end of the second locking rod 194 is slidably connected to the inside of the second connector 18. Specifically, when the optical component body 1 is locked inside the unmanned aerial vehicle body 3, the first connector 17 is connected to the second connector 18, and the supporting magnet 192 attracts the sliding magnet 191 to slide, causing the sliding block 193 to lose its support force, and the second locking rod 194 slides into the second connector 18. Then, the first connector 17 is used to support the extension and retraction of the second support member 195, and the second support member 195 supports the second locking rod 194 to lock inside the second connector 18. When the sliding magnet 191 is pushed, the sliding block 193 slides upward and drives the second locking rod 194 to slide into the first connector 17 and squeeze the second support member 195, which can realize the function of quick connection and separation between the first connector 17 and the second connector 18. At the same time, the connection between the first connector 17 and the second connector 18 can realize the connection between the optical component body 1 and the hidden camera.
[0028] Please see the appendix Figure 7 - Appendix Figure 9 The unmanned aerial vehicle body 3 has a hot air channel 20 inside, and an exhaust component 21 is installed inside the hot air channel 20. The exhaust component 21 is installed outside the unmanned aerial vehicle body 3. The exhaust component 21 includes a carbon fiber reinforced composite material 211. The top of the carbon fiber reinforced composite material 211 is installed inside the hot air channel 20. A filter plate 212 is fixedly connected to one end of the carbon fiber reinforced composite material 211. A baffle plate 213 is fixedly connected to one end of the filter plate 212. The carbon fiber reinforced composite material 211 is slidably connected to the filter plate 212 and the baffle plate 213 inside the unmanned aerial vehicle body 3. Specifically, the unmanned aerial vehicle body 3 has a hot air channel 20 inside, which is used to transport hot air to come into contact with the carbon fiber reinforced composite material 211. The carbon fiber reinforced composite material 211 can expand when exposed to hot air, but its thermal expansion characteristics are significantly different from those of traditional metal materials. The collision direction can be precisely controlled through material design. At the same time, the carbon fiber reinforced composite material 211 is used to support and fix the filter plate 212, and the filter plate 212 is used to support and fix the baffle plate 213. Thus, the baffle plate 213 can completely block the gap in the unmanned aerial vehicle body 3, and the filter plate 212 can exhaust the hot air inside the unmanned aerial vehicle body 3 to the outside. In addition, the filter plate 212 can prevent dust and liquid from entering the interior of the unmanned aerial vehicle body 3.
[0029] Workflow: First, pulling the locking block 16 compresses the first support member 15, causing the opening and closing plate 12 and the sealing strip 13 to lose their locking force. The opening and closing plate 12 will then flip downwards via the hinge 11. Next, the optical component body 1 is inserted into the silicone pad 2, which prevents damage to the optical component body 1 during flight. Simultaneously, the connecting rod 7 and the stabilizing component 8 are also inserted into the unmanned aerial vehicle body 3. Then, rotating the rotary knob 6 causes the connecting rod 7, support rod 81, second elastic member 82, first locking rod 83, third elastic member 84, and top plate 85 to rotate, causing the first locking rod 83 to be squeezed into the notch inside the unmanned aerial vehicle body 3. The second elastic member 82 supports the first locking rod 83 and locks it inside the unmanned aerial vehicle body 3. Thus, a gap exists between the first locking rod 83 and the notch inside the unmanned aerial vehicle body 3. When the body 3 encounters strong currents or collides with a tree during flight, the optical component body 1 will shake inside the unmanned aerial vehicle body 3. The first elastic element 5 will support the rotating knob 6 and the connecting rod 7 to shake up and down. Then, the third elastic element 84 and the top plate 85 are used to support the support rod 81 and the first locking rod 83, effectively preventing them from being squeezed and damaged by the up and down shaking. When it is necessary to remove the optical component body 1, rotating the rotating knob 6 will drive the connecting rod 7, the support rod 81, the second elastic element 82, the first locking rod 83, the third elastic element 84, and the top plate 85 to rotate, and make them rotate from the locking groove to the sliding groove. This will cause the optical component body 1 to lose the locking force and slide down, thereby achieving the effect of quickly replacing the optical component body 1. This avoids the loosening and displacement of the optical component caused by changes in flight attitude, the drift of optical parameters caused by direct transmission of vibration, and the decrease in detection accuracy. Simultaneously, the optical component body 1 will drive the first connector 17 to dock with the second connector 18, and the supporting magnet 192 will attract the sliding magnet 191 to slide outward, and initially lock the first connector 17 and the second connector 18. Then, the second support member 195 will support the second locking rod 194 to be inserted into the second connector 18, and firmly lock the first connector 17 and the second connector 18. When it is necessary to remove the first connector 17 from the second connector 18, first push the sliding magnet 191, and the sliding magnet 191 will squeeze the sliding block 193 to slide upward, and drive the second locking rod 194 to slide into the first connector 17. Then, the second locking rod 194 will squeeze the second support member 195, and the locking force between the first connector 17 and the second connector 18 will be lost, and it will be removed with the optical component body 1. This can achieve an adaptive effect and avoid serious problems such as data fusion errors, image stitching defects, and inaccurate target positioning. When the optical component body 1 generates hot air, the hot air first enters the interior of the carbon fiber reinforced composite material 211 through the hot air channel 20. The carbon fiber reinforced composite material 211 reacts with the hot air and expands due to its own properties. The carbon fiber reinforced composite material 211 drives the filter plate 212 and the baffle plate 213 to slide. The opening inside the unmanned aerial vehicle body 3 changes from a closed state to a ventilated state, which allows the hot air inside the unmanned aerial vehicle body 3 to be discharged. This achieves the effect of heat dissipation for the optical component body 1, which can efficiently conduct and dissipate the heat inside the optical component body 1, avoid heat accumulation under high load working conditions, ensure that the optical components operate in a stable temperature range, and maintain the stability of the optical component's detection accuracy and response speed.
[0030] Although embodiments of the invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A novel optical component for use in unmanned aerial vehicles, comprising an optical component body (1), characterized in that, The optical component body (1) is provided with silicone pads (2) at both ends. The top of the silicone pads (2) is fixedly connected to the unmanned aerial vehicle body (3). The optical component body (1) is fixedly connected to a fixed frame (4). The fixed frame (4) is provided with a first elastic element (5). The first elastic element (5) is located outside the connecting rod (7). The bottom of the first elastic element (5) is provided with a rotating knob (6). The top of the rotating knob (6) is fixedly connected to a connecting rod (7). The outside of the connecting rod (7) is located inside the fixed frame (4). The outside of the connecting rod (7) is located inside the unmanned aerial vehicle body (3). The inside of the connecting rod (7) is provided with a stabilizing component (8). The outside of the stabilizing component (8) is located inside the unmanned aerial vehicle body (3).
2. The novel optical component for use in unmanned aerial vehicles according to claim 1, characterized in that, The stabilizing component (8) includes a support rod (81), which is externally fixedly connected to the inside of the connecting rod (7). A second elastic element (82) is provided inside the support rod (81), and a first locking rod (83) is provided at one end of the second elastic element (82). A third elastic element (84) is provided inside the support rod (81), and a top plate (85) is provided at the top of the third elastic element (84). The top of the top plate (85) is located inside the unmanned aerial vehicle body (3).
3. The novel optical component for use in unmanned aerial vehicles according to claim 2, characterized in that, The second elastic element (82) and the third elastic element (84) are externally disposed inside the support rod (81), the third elastic element (84) is externally disposed inside the connecting rod (7), and the first locking rod (83) is externally slidably connected to the connecting rod (7) and the unmanned aerial vehicle body (3) inside.
4. The novel optical component for use in unmanned aerial vehicles according to claim 1, characterized in that, A support frame (9) is fixedly connected to the bottom outer side of the unmanned aerial vehicle body (3), and a driver (10) is fixedly connected inside the unmanned aerial vehicle body (3).
5. A novel optical component for use in unmanned aerial vehicles according to claim 1, characterized in that, A hinge (11) is fixedly connected to the bottom middle part of the unmanned aerial vehicle body (3). An opening and closing plate (12) is fixedly connected to the outside of the hinge (11). A sealing strip (13) is fixedly connected to the inside of the opening and closing plate (12). The opening and closing plate (12) and the sealing strip (13) are located inside the unmanned aerial vehicle body (3).
6. A novel optical component for use in unmanned aerial vehicles according to claim 5, characterized in that, The opening and closing plate (12) is fixedly connected to a guide rod (14), and a locking block (16) is slidably connected to the outside of the guide rod (14). The locking block (16) is slidably connected to the inside of the unmanned aerial vehicle body (3) and the opening and closing plate (12). The other end of the locking block (16) is provided with a first support member (15). One end of the first support member (15) is located inside the opening and closing plate (12), and the inside of the first support member (15) is located outside the opening and closing plate (12). The top end of the opening and closing plate (12) is fixedly connected to the bottom end of the silicone pad (2).
7. A novel optical component for use in unmanned aerial vehicles according to claim 1, characterized in that, The optical component body (1) is fixedly connected to the outside of a first connector (17), and a second connector (18) is provided at one end of the first connector (17). One end of the second connector (18) is fixedly connected to the inside of the unmanned aerial vehicle body (3). The outside of the first connector (17) is provided inside the unmanned aerial vehicle body (3). Adaptive components (19) are provided inside the first connector (17) and the second connector (18).
8. A novel optical component for use in unmanned aerial vehicles according to claim 7, characterized in that, The adaptive component (19) includes a sliding magnet (191), the outside of which is slidably connected to the inside of the first connector (17). One end of the sliding magnet (191) is provided with a supporting magnet (192), the outside of which is fixedly connected to the inside of the second connector (18). The inside of the first connector (17) is provided with a sliding block (193), the top end of which is provided with a second locking rod (194). One end of the second locking rod (194) is provided with a second support member (195), one end of which is located inside the first connector (17). The outside of the sliding block (193) and the second locking rod (194) are slidably connected to the inside of the first connector (17), and one end of the second locking rod (194) is slidably connected to the inside of the second connector (18).
9. A novel optical component for use in unmanned aerial vehicles according to claim 1, characterized in that, The unmanned aerial vehicle body (3) has a hot air channel (20) inside, and an exhaust component (21) is provided inside the hot air channel (20). The exhaust component (21) is located outside the unmanned aerial vehicle body (3).
10. A novel optical component for use in unmanned aerial vehicles according to claim 9, characterized in that, The exhaust assembly (21) includes a carbon fiber reinforced composite material (211), the top of which is located inside the hot air channel (20). A filter plate (212) is fixedly connected to one end of the carbon fiber reinforced composite material (211), and a baffle plate (213) is fixedly connected to one end of the filter plate (212). The carbon fiber reinforced composite material (211), the filter plate (212), and the baffle plate (213) are slidably connected to the outside of the unmanned aerial vehicle body (3) inside.