A drone with a folding wing structure

Abstract

This invention discloses a drone with a folding wing structure, relating to the field of drone technology. It includes an outer shell mechanism, a camera mechanism mounted on the left side of the outer shell mechanism, a wing mechanism mounted on the top of the outer shell mechanism for gliding, and a horizontal wing mechanism mounted on the bottom of the outer shell mechanism. By mounting the wing mechanism at the top, the horizontal wing mechanism at the bottom, and tail rudder mechanisms at both ends of the outer shell mechanism, a complete flight control system is formed. The wing mechanism enables the outer shell mechanism to glide, the horizontal wing mechanism provides balance and guidance for the overall structure, and the tail rudder mechanism precisely controls the flight attitude. These three mechanisms work together to improve flight stability and maneuverability. The complementary functions and structural synergy between the mechanisms enhance the reliability and flexibility of the drone's flight, improve the overall durability and protective performance of the equipment, and significantly optimize the user experience of the drone.

Description

Technical Field

[0001] This invention relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a UAV with a folding wing structure. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and onboard program control devices. They have no cockpit, but are equipped with autopilots, program control devices, and other equipment. The wings of a UAV are an important component, used to lift and lower the UAV body. To make UAVs easy to carry and to reduce unnecessary damage to the wings, the wings of UAVs are usually designed to be foldable.

[0003] However, existing drones with folding wing structures have the following shortcomings: 1) Traditional UAVs have many limitations in their wing-folding structural design, and their flight control system is not perfect. They lack a stable structure that coordinates the wings, horizontal wings and tail rudder, resulting in insufficient balance and attitude control during flight. They are easily affected by airflow interference and become unstable, which seriously affects the accuracy and safety of flight control.

[0004] 2) Traditional drone camera protection modes have obvious shortcomings. They cannot provide effective protection while ensuring the field of view. External impurities can easily adhere to or impact the camera, causing scratches on the camera lens and damage to internal components. This not only results in blurred images and reduced image quality, but also shortens the camera's lifespan, increases the frequency and cost of equipment maintenance, and seriously restricts the drone's ability to operate continuously in complex environments.

[0005] 3) Traditional drones are not designed with a rear cover for protection, which cannot effectively isolate external impurities, causing the outer shell and internal components to be corroded by dust and moisture. This can easily cause scratches on the outer shell surface and loosening of internal components, which not only shortens the service life of the equipment but also increases the frequency and cost of equipment maintenance. It is also difficult to ensure the integrity of the core components when the drone is idle.

[0006] Therefore, we propose a drone with a folding wing structure to address the problems mentioned above. Summary of the Invention

[0007] The purpose of this invention is to provide a drone with a folding wing structure. By installing a wing mechanism at the top of the outer shell, a horizontal wing mechanism at the bottom, and tail rudder mechanisms at the front and rear ends, a complete flight control system is formed. The wing mechanism can drive the outer shell to achieve a gliding effect, the horizontal wing mechanism provides balance and guidance for the overall structure, and the tail rudder mechanism precisely controls the flight attitude. The three work together to improve flight stability and maneuverability. The functions of each mechanism are complementary and the structure is coordinated, which not only enhances the reliability and flexibility of the drone's flight, but also improves the overall durability and protection performance of the equipment, significantly optimizing the user experience of the drone, thereby solving the problems mentioned in the background art.

[0008] To achieve the above objectives, the present invention provides the following technical solution: a drone with a folding wing structure, including an outer shell mechanism; A camera mechanism is mounted on the left side of the outer casing mechanism; The top of the outer shell mechanism is equipped with a wing mechanism to drive the outer shell mechanism to achieve a gliding effect. The bottom of the outer shell mechanism is equipped with a flat wing mechanism to provide balance and guidance between the outer shell mechanism and the wing mechanism. The front and rear ends of the outer shell mechanism are equipped with tail rudder mechanisms to control the attitude of the outer shell mechanism in flight. The surface of the camera mechanism is provided with a protective mechanism to protect the camera mechanism. The right side of the outer shell mechanism is equipped with a rear cover mechanism to protect the outer shell mechanism when not in use.

[0009] Preferably, the outer shell mechanism includes an outer shell body, the top of which is provided with a battery compartment and an umbrella compartment, and an mounting plate is fixedly installed on the right side of the outer shell body.

[0010] Preferably, the camera mechanism includes a camera head, a controller is mounted on the top of the camera head, and a bracket and camera body are provided at the bottom of the camera head. The camera body rotates at the bottom of the camera head via the bracket.

[0011] Preferably, the wing body includes a wing limiting block, a wing mounting block, and a wing sleeve. A wing torsion spring A and a wing torsion spring B are disposed at the top of the wing mounting block. A wing plate A and a right wing are disposed at the top of the wing mounting block. The wing plate A is fixed to the top of the wing mounting block via a mounting groove A. The wing plate A rotates at the top of the wing mounting block via the wing torsion spring A. A wing plate B and a left wing are disposed at the top of the wing mounting block. The wing plate B is fixed to the top of the wing mounting block via a mounting groove B. The wing plate B rotates at the top of the wing mounting block via the wing torsion spring B. A wing fixing block is disposed at the top of the wing mounting block, and the wing fixing block is fixed to the top of the wing mounting block via wing bolts.

[0012] Preferably, the horizontal wing mechanism includes a horizontal wing limiting block, a horizontal wing mounting block, and a horizontal wing sleeve. A horizontal wing torsion spring A and a horizontal wing torsion spring B are provided at the top of the horizontal wing mounting block. A horizontal wing plate A, a right horizontal wing, and a steering plate A are also provided at the top of the horizontal wing mounting block. The horizontal wing plate A is fixed to the top of the horizontal wing mounting block via a groove A. The horizontal wing plate A rotates at the top of the horizontal wing mounting block via the horizontal wing torsion spring A. An adjuster A and a rotating arm A are mounted on the side of the horizontal wing plate A. The adjuster A drives the steering plate via the rotating arm A and the positioning block A. A rotates, and the top of the flat wing mounting block is provided with a flat wing plate B, a left flat wing, and a steering plate B. The flat wing plate B is fixed to the top of the flat wing mounting block through a groove B. The flat wing plate B rotates at the top of the flat wing mounting block through a flat wing torsion spring B. An adjuster B and a rotating arm B are installed on the side of the flat wing plate B. The adjuster B drives the steering plate B to rotate through the rotating arm B and the positioning block B. The top of the flat wing mounting block is provided with a flat wing fixing block, and the flat wing fixing block is fixed to the top of the flat wing mounting block by a flat wing bolt.

[0013] Preferably, the tail rudder mechanism includes a tail rudder limiting block, a tail rudder torsion spring, and a rotating block. The rotating block is mounted on the surface of the outer shell mechanism via a tail rudder bolt and a positioning groove. A tail rudder locking block is fixedly installed on the inner wall of the rotating block. A tail rudder body is provided on the surface of the rotating block. The tail rudder body is mounted on the surface of the rotating block via a threaded groove and a fixing groove.

[0014] Preferably, the protective mechanism includes a fixed ring, a rotating plate is provided inside the fixed ring, a fixed plate is fixedly installed on the surface of the rotating plate, and a transparent protective cover is fixedly installed on the surface of the fixed plate.

[0015] Preferably, the rotating plate rotates inside the fixed ring via spiral pattern A and spiral pattern B, and the rotating plate rotates inside the fixed ring via a rotating groove.

[0016] Preferably, the rear cover mechanism includes a protrusion and a protective cover, a protruding rod is fixedly installed on the inner wall of the protective cover, side plates are installed at the front and rear ends of the protective cover, and a soft pad is installed on the inner wall of the side plate.

[0017] Preferably, the protruding rod is slidably connected to the protrusion through a slot, the side plate is slidably connected to the outer shell mechanism, and the soft pad is slidably connected to the outer shell mechanism.

[0018] Compared with the prior art, the beneficial effects of the present invention are: 1. This invention comprises the following components: a wing limiting block, a wing mounting block, a wing sleeve, a wing torsion spring A, a wing torsion spring B, a wing plate A, a mounting groove A, a right wing, a wing plate B, a mounting groove B, a left wing, a wing fixing block, a wing bolt, a horizontal wing limiting block, a horizontal wing mounting block, a horizontal wing sleeve, a horizontal wing torsion spring A, a horizontal wing torsion spring B, a horizontal wing plate A, a groove A, a right horizontal wing, a steering plate A, an adjuster A, a rotating arm A, a positioning block A, a horizontal wing plate B, a groove B, a left horizontal wing, a steering plate B, an adjuster B, a rotating arm B, a positioning block B, a horizontal wing fixing block, a horizontal wing bolt, a tail rudder limiting block, a tail rudder torsion spring, a rotating block, and a tail rudder screw. The system comprises bolts, threaded grooves, tail rudder blocks, tail rudder bodies, positioning grooves, and fixing grooves. By installing a wing mechanism at the top of the outer shell, a horizontal wing mechanism at the bottom, and a tail rudder mechanism at both ends, a complete flight control system is formed. The wing mechanism drives the outer shell to achieve gliding, the horizontal wing mechanism provides balance and guidance for the overall structure, and the tail rudder mechanism precisely controls the flight attitude. The three work together to improve flight stability and maneuverability. The complementary functions and synergistic structure of each mechanism enhance the reliability and flexibility of the UAV flight, improve the overall durability and protection performance of the equipment, and significantly optimize the user experience of the UAV.

[0019] 2. This invention, by setting up a fixed ring, a rotating groove, a spiral pattern A, a rotating plate, a spiral pattern B, a fixed plate, and a transparent protective cover, utilizes the rotational adaptation structure of the spiral pattern and the rotating groove to allow the rotating plate to rotate smoothly within the fixed ring. This, in turn, causes the fixed plate and the transparent protective cover to flexibly adjust their states. While ensuring the normal shooting field of view of the camera, it constructs a stable physical protective barrier, effectively isolating external dust, moisture, and impacts, preventing direct damage to the camera, significantly improving the camera's protective reliability and service life, ensuring the continuous and stable operation of the shooting function in complex environments, and enhancing the overall environmental adaptability and operational reliability of the drone.

[0020] 3. This invention, by setting up protrusions, protective covers, protruding rods, slots, side plates, and soft pads, effectively isolates external dust, moisture, and impacts. During the sliding and fitting process, the soft pads on the inner wall of the side plates can buffer the direct action of external forces on the outer shell, avoiding wear on the outer shell surface or damage to internal components due to vibration. This not only improves the protective reliability of the outer shell but also enhances the overall durability of the equipment, ensuring that the core components of the drone are in a safe and stable storage state for a long time. Attached Figure Description

[0021] Figure 1 This is a perspective view of the main structure of a drone with a folding wing structure according to the present invention; Figure 2 This is a perspective view of a folding wing storage structure in a drone according to the present invention. Figure 3 This is an exploded front perspective view of the outer shell mechanism of a drone with a folding wing structure according to the present invention; Figure 4 This invention relates to a folding wing structure for a drone. Figure 3 Enlarged 3D view of the structure at point A in the middle; Figure 5 This is an exploded left perspective view of the outer shell mechanism of a drone with a folding wing structure according to the present invention; Figure 6 This invention relates to a folding wing structure for a drone. Figure 5 Enlarged 3D view of the structure at point B in the middle; Figure 7 This invention relates to a folding wing structure for a drone. Figure 5 Enlarged 3D view of the structure at point C; Figure 8 This is an exploded front perspective view of the wing mechanism in a drone with a folding wing structure according to the present invention. Figure 9 This is an exploded, bottom-view perspective view of the wing mechanism in a drone with a folding wing structure according to the present invention. Figure 10 This is an exploded front perspective view of the horizontal wing mechanism in a drone with a folding wing structure according to the present invention. Figure 11 This is an exploded, bottom-view perspective view of the flat-wing mechanism in a drone with a folding wing structure according to the present invention.

[0022] In the diagram: 1. Outer shell mechanism; 101. Outer shell body; 102. Battery compartment; 103. Parachute compartment; 104. Mounting plate; 2. Camera mechanism; 201. Nose; 202. Controller; 203. Bracket; 204. Camera body; 3. Wing mechanism; 301. Wing limiting block; 302. Wing mounting block; 303. Wing sleeve; 304. Wing torsion spring A; 305. Wing torsion spring B; 306. Wing plate A; 307. Mounting slot A; 308, Right wing; 309, Wing plate B; 310, Mounting slot B; 311, Left wing; 312, Wing fixing block; 313, Wing bolt; 4, wing mechanism; 401, Wing limiting block; 402, Wing mounting block; 403, Wing sleeve; 404, Wing torsion spring A; 405, Wing torsion spring B; 406, Wing plate A; 407, Groove A; 408, Right wing; 409, Direction plate A; 410, Adjustment... 411. Throttle A; 412. Rotating Arm A; 413. Positioning Block A; 414. Horizontal Wing Plate B; 415. Groove B; 416. Left Horizontal Wing; 417. Steering Plate B; 418. Adjuster B; 419. Rotating Arm B; 420. Positioning Block B; 421. Horizontal Wing Fixing Block; 5. Horizontal Wing Bolt; 5. Tail Rudder Mechanism; 501. Tail Rudder Limiting Block; 502. Tail Rudder Torsion Spring; 503. Rotating Block; 504. Tail Rudder Bolt; 505. Thread 506. Tail rudder locking block; 507. Tail rudder body; 508. Positioning groove; 509. Fixing groove; 6. Protective mechanism; 601. Fixing ring; 602. Rotating groove; 603. Spiral pattern A; 604. Rotating plate; 605. Spiral pattern B; 606. Fixing plate; 607. Transparent protective cover; 7. Rear cover mechanism; 701. Protrusion; 702. Protective cover; 703. Protruding rod; 704. Locking groove; 705. Side plate; 706. Soft pad. Detailed Implementation

[0023] The technical solutions of the embodiments of the present invention will be clearly and completely described below 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.

[0024] Please see the appendix Figure 1 - Appendix Figure 8 As shown, the present invention provides a technical solution: a drone with a folding wing structure, including an outer shell mechanism 1; A camera mechanism 2 is mounted on the left side of the outer casing mechanism 1; The top of the outer shell mechanism 1 is equipped with a wing mechanism 3, which is used to drive the outer shell mechanism 1 to achieve a gliding effect. The bottom of the outer shell mechanism 1 is equipped with a flat wing mechanism 4, which is used to balance and guide the outer shell mechanism 1 and the wing mechanism 3. The front and rear ends of the outer shell mechanism 1 are equipped with tail rudder mechanisms 5, which are used to control the attitude of the outer shell mechanism 1 in flight. The surface of the camera mechanism 2 is provided with a protective mechanism 6, which is used to protect the camera mechanism 2. The right side of the outer shell mechanism 1 is equipped with a rear cover mechanism 7, which is used to protect the outer shell mechanism 1 when it is not in use.

[0025] Example 1, according to Figures 1-5 , Figures 7-11As shown, the outer shell mechanism 1 includes an outer shell body 101, with a battery compartment 102 and a parachute compartment 103 at the top. A mounting plate 104 is fixedly installed on the right side of the outer shell body 101. The camera mechanism 2 includes a nose cone 201, with a controller 202 installed at the top. A bracket 203 and a camera body 204 are located at the bottom of the nose cone 201. The camera body 204 rotates at the bottom of the nose cone 201 via the bracket 203. The wing body includes a wing limiting block 301, a wing mounting block 302, and a wing sleeve 303. A wing torsion spring A304 and a wing torsion spring B305 are installed at the top of the wing mounting block 302. A wing plate A306 and a right wing 308 are also installed at the top of the wing mounting block 302. Wing plate A306 is fixed to the top of wing mounting block 302 via mounting groove A307. Wing plate A306 rotates on the top of wing mounting block 302 via wing torsion spring A304. Wing plate B309 and left wing 311 are mounted on the top of wing mounting block 302. Wing plate B309 is fixed to the top of wing mounting block 302 via mounting groove B310. Wing plate B309 rotates on the top of wing mounting block 302 via wing torsion spring B305. Wing fixing block 312 is mounted on the top of wing mounting block 302. Wing fixing block 312 is fixed to the top of wing mounting block 302 via wing bolt 313. The horizontal wing mechanism 4 includes horizontal wing limiting block 401, horizontal wing mounting block 402, and horizontal wing sleeve 403. The top of the horizontal wing mounting block 402 is provided with a horizontal wing torsion spring A404 and a horizontal wing torsion spring B405. The top of the horizontal wing mounting block 402 is provided with a horizontal wing plate A406, a right horizontal wing 408, and a steering plate A409. The horizontal wing plate A406 is fixed to the top of the horizontal wing mounting block 402 through a groove A407. The horizontal wing plate A406 rotates at the top of the horizontal wing mounting block 402 through the horizontal wing torsion spring A404. An adjuster A410 and a rotating arm A411 are installed on the side of the horizontal wing plate A406. The adjuster A410 drives the steering plate A409 to rotate through the rotating arm A411 and the positioning block A412. The top of the horizontal wing mounting block 402 is provided with a horizontal wing plate B413, a left horizontal wing 415, and a steering plate B416. The horizontal wing plate B41... 3. The wing plate B413 is fixed to the top of the wing mounting block 402 via the groove B414. The wing plate B413 rotates at the top of the wing mounting block 402 via the wing torsion spring B405. An adjuster B417 and a rotating arm B418 are installed on the side of the wing plate B413. The adjuster B417 drives the steering plate B416 to rotate via the rotating arm B418 and the positioning block B419. A wing fixing block 420 is provided at the top of the wing mounting block 402. The wing fixing block 420 is fixed to the top of the wing mounting block 402 via the wing bolt 421. The tail rudder mechanism 5 includes a tail rudder limiting block 501, a tail rudder torsion spring 502, and a rotating block 503. The rotating block 503 is installed on the surface of the outer shell mechanism 1 via the tail rudder bolt 504 and the positioning groove 508.A tail rudder locking block 506 is fixedly installed on the inner wall of the rotating block 503, and a tail rudder body 507 is provided on the surface of the rotating block 503. The tail rudder body 507 is installed on the surface of the rotating block 503 through a threaded groove 505 and a fixing groove 509.

[0026] The overall effect of Embodiment 1 is as follows: by modularly integrating and finely arranging the outer shell mechanism 1, camera mechanism 2, wing body, horizontal wing mechanism 4, and tail rudder mechanism 5, such as the reasonable arrangement of battery compartment 102 and parachute compartment 103 in the outer shell body 101, the camera body 204 achieving flexible rotation based on the bracket 203, the wing plate and horizontal wing plate achieving precise and controllable rotation with the help of torsion springs, and the tail rudder body 507 being conveniently installed through threaded groove 505 and fixing groove 509, the coordinated operation of each component not only greatly improves the overall integration of the equipment and the convenience of installation and maintenance, but also significantly enhances the stability and operational flexibility of the equipment, effectively making up for the defects of loose structure, insufficient control precision, and high maintenance cost in the prior art, and providing a solid guarantee for the efficient and stable operation of related equipment.

[0027] Example 2, according to Figures 1-3 , Figure 5 , Figure 6 As shown, the protective mechanism 6 includes a fixed ring 601, a rotating plate 604 is provided inside the fixed ring 601, a fixed plate 606 is fixedly installed on the surface of the rotating plate 604, and a transparent protective cover 607 is fixedly installed on the surface of the fixed plate 606. The rotating plate 604 rotates inside the fixed ring 601 through spiral patterns A603 and B605, and the rotating plate 604 rotates inside the fixed ring 601 through a rotating groove 602.

[0028] The overall effect of Embodiment 2 is as follows: By employing a structure in which a fixed ring 601, a rotating plate 604, a fixed plate 606, and a transparent protective cover 607 work together, and by utilizing the adaptation of the spiral patterns A603 and B605 on the rotating plate 604 with the fixed ring 601, as well as the assistance of the rotating groove 602, the rotating plate 604 can rotate smoothly and accurately within the fixed ring 601, thereby driving the transparent protective cover 607 to open and close flexibly. This not only greatly improves the ease of operation and flexibility of the protective mechanism 6, allowing for quick adjustment of the protective state as needed, but also provides a clear field of vision through the transparent protective cover 607, balancing protection and observation needs. This effectively solves the pain points of the existing protective mechanism 6, such as its bulky structure, cumbersome operation, and difficulty in balancing protection and observation, significantly enhancing the practicality and user experience of the equipment.

[0029] Example 3, according to Figures 1-3 , Figure 5As shown, the rear cover mechanism 7 includes a protrusion 701 and a cover 702. A protruding rod 703 is fixedly installed on the inner wall of the cover 702. Side plates 705 are installed at the front and rear ends of the cover 702. A soft pad 706 is installed on the inner wall of the side plate 705. The protruding rod 703 is slidably connected to the protrusion 701 through a slot 704. The side plate 705 is slidably connected to the outer shell mechanism 1. The soft pad 706 is slidably connected to the outer shell mechanism 1.

[0030] The overall effect of embodiment 3 is as follows: The rear cover mechanism 7 cleverly integrates core components such as protrusion 701, cover 702, protruding rod 703, side plate 705, and soft pad 706. The protruding rod 703 on the inner wall of the cover 702 and the protrusion 701 achieve precise sliding connection through the slot 704. The side plate 705 and soft pad 706 simultaneously slide and cooperate with the outer shell mechanism 1, constructing a stable and flexible assembly system. This not only greatly improves the efficiency of rear cover installation and disassembly, and makes the operation process smooth and convenient, but also the embedded soft pad 706 effectively buffers the friction between the cover 702 and the outer shell during sliding, avoids component wear, enhances the tightness and stability of the connection, and reduces the noise caused by hard contact. It effectively solves these technical pain points and provides a solid guarantee for the efficient assembly, stable operation and long-term use of the equipment, significantly improving the overall reliability of the equipment and the user experience.

[0031] The working principle of the entire device is as follows: Before use, place the outer shell mechanism 1 in the required position and install the battery inside the outer shell body 101 through the battery compartment 102. Then, install the wing mechanism 3, the horizontal wing mechanism 4, and the tail rudder mechanism 5 onto the outer shell body 101 in sequence. At this time, fix the wing mounting block 302 and the wing fixing block 312 to the top of the outer shell body 101 through the wing sleeve 303 and the wing bolt 313. At this time, the wing plate A306 and the wing plate B309 are fixed to the top of the outer shell body 101 through the mounting groove A307 and the mounting groove B310. Under the elastic force of the wing torsion spring A304 and the wing torsion spring B305, the wing plate A306 and the wing plate B309 are fixed to the top of the outer shell body 101. The right wing 308 and left wing 311 are opened via wing limiting block 301. Then, the horizontal wing mounting block 402 and horizontal wing fixing block 420 are fixed to the bottom of the outer shell via horizontal wing sleeve 403 and horizontal wing bolt 421. At this time, horizontal wing plate A406 and horizontal wing plate B413 are fixed to the bottom of the outer shell body 101 via groove A407 and groove B414. Under the elastic force of the horizontal wing torsion spring A404 and horizontal wing torsion spring B405, the horizontal wing plate A406 and horizontal wing plate B413 drive the right horizontal wing 408 and left horizontal wing 415 to open via horizontal wing limiting block 401. Finally, the tail rudder body 507 is installed on the surface of the rotating block 503 via threaded groove 505 and fixing groove 509. Then, the rotating block 50... 3. The tail rudder mechanism is installed at both ends of the outer shell 101 via the positioning groove 508 and the tail rudder bolt 504. Under the elastic force of the tail rudder torsion spring 502, the tail rudder limiting block 501 and the tail rudder locking block 506 can be engaged and opened. Once the wing mechanism 3, the horizontal wing mechanism 4, and the tail rudder mechanism 5 are installed, the rear cover mechanism 7 is pinched and pulled backward, causing the cover 702 to slide backward along with the soft pad 706 via the side plate 705. At the same time, the protruding rod 703 slides backward on the surface of the protrusion 701 via the slot 704. When the cover 702, along with the side plate 705, has completely slid into the right side of the outer shell 101, and the protruding rod 703 has completely slid out of the surface of the protrusion 701 via the slot 704, the installation is complete. Then... After the motor and propeller are fixed to the right side of the outer casing 101 via the mounting plate 104, the protective mechanism 6 is then lifted, and the rotating plate 604 is aligned with the rotating groove 602 and rotated. This causes the rotating plate 604 to rotate inwards through the spiral patterns A603 and B605 towards the fixing ring 601. Once the fixing plate 606 is attached to the surface of the fixing ring 601, the transparent protective cover 607 can be installed on the surface of the camera mechanism 2. When it needs to be folded and stored inside the launcher, first pinch the tail rudder body 507 and press it against the outer casing 101, causing the rotating block 503 to rotate via the tail rudder torsion spring 502. Then, the flat wing mechanism 4 and the wing mechanism 3 can be stored inside the launcher for launch.After transmission is complete, the controller 202 at the top of the nose cone 201 can control the camera body 204 to rotate and adjust at the bottom of the nose cone 201 via the bracket 203 to achieve its full functionality. The direction plates A409 and B416 can also be adjusted via adjusters A410 and B417. During adjustment, rotating arm A411 drives direction plate A409 via positioning block A412, and rotating arm B418 drives direction plate B416 via positioning block B419 to adjust the flight direction. After flight, the camera can be landed using a parachute inside the parachute compartment 103.

[0032] Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.

Claims

1. An unmanned plane of folding wing structure, comprising a shell mechanism (1); A camera mechanism (2) is installed on the left side of the shell mechanism (1); Characterized in that: A wing mechanism (3) is installed at the top end of the shell mechanism (1) for driving the shell mechanism (1) to complete the gliding effect, a flat wing mechanism (4) is installed at the bottom end of the shell mechanism (1) for balancing and guiding the shell mechanism (1) and the wing mechanism (3), rudders (5) are installed at the front and rear ends of the shell mechanism (1) for controlling the attitude of the shell mechanism (1) in flight, a protective mechanism (6) is arranged on the surface of the camera mechanism (2) for protecting the camera mechanism (2), and a rear cover mechanism (7) is installed on the right side of the shell mechanism (1) for protecting the shell mechanism (1) when not in use.

2. The foldable wing structure of claim 1, wherein: The shell mechanism (1) comprises a shell body (101), a battery compartment (102) and a parachute compartment (103) are arranged at the top end of the shell body (101), and a mounting plate (104) is fixedly installed on the right side of the shell body (101).

3. The foldable wing structure of claim 1, wherein: The camera mechanism (2) comprises a nose (201), a controller (202) is installed at the top end of the nose (201), a support (203) and a camera body (204) are arranged at the bottom end of the nose (201), and the camera body (204) rotates at the bottom end of the nose (201) through the support (203).

4. The foldable wing structure of claim 1, wherein: The wing body comprises wing limiting blocks (301), a wing mounting block (302) and a wing sleeve (303), wing torsion springs A (304) and B (305) are arranged at the top end of the wing mounting block (302), wing plates A (306) and a right wing (308) are arranged at the top end of the wing mounting block (302), the wing plate A (306) is fixed at the top end of the wing mounting block (302) through a mounting groove A (307), the wing plate A (306) rotates at the top end of the wing mounting block (302) through the wing torsion spring A (304), wing plates B (309) and a left wing (311) are arranged at the top end of the wing mounting block (302), the wing plate B (309) is fixed at the top end of the wing mounting block (302) through a mounting groove B (310), the wing plate B (309) rotates at the top end of the wing mounting block (302) through the wing torsion spring B (305), a wing fixing block (312) is arranged at the top end of the wing mounting block (302), and the wing fixing block (312) is fixed at the top end of the wing mounting block (302) through a wing bolt (313).

5. The foldable wing structure of claim 1, wherein: The horizontal wing mechanism (4) includes a horizontal wing limiting block (401), a horizontal wing mounting block (402), and a horizontal wing sleeve (403). The top of the horizontal wing mounting block (402) is provided with a horizontal wing torsion spring A (404) and a horizontal wing torsion spring B (405). The top of the horizontal wing mounting block (402) is also provided with a horizontal wing plate A (406), a right horizontal wing (408), and a direction plate A (409). The horizontal wing plate A (406) is open to... The plate A (406) is fixed to the top of the flat wing mounting block (402) via the groove A (407). The flat wing plate A (406) rotates at the top of the flat wing mounting block (402) via the flat wing torsion spring A (404). An adjuster A (410) and a rotating arm A (411) are installed on the side of the flat wing plate A (406). The adjuster A (410) drives the steering plate A (406) via the rotating arm A (411) and the positioning block A (412). 09) Rotation is performed. The top of the flat wing mounting block (402) is provided with a flat wing plate B (413), a left flat wing (415), and a direction plate B (416). The flat wing plate B (413) is fixed to the top of the flat wing mounting block (402) through a groove B (414). The flat wing plate B (413) rotates at the top of the flat wing mounting block (402) through a flat wing torsion spring B (405). An adjuster B (417) and a rotating arm B (418) are installed on the side of the flat wing plate B (413). The adjuster B (417) drives the direction plate B (416) to rotate through the rotating arm B (418) and the positioning block B (419). The top of the flat wing mounting block (402) is provided with a flat wing fixing block (420). The flat wing fixing block (420) is fixed to the top of the flat wing mounting block (402) through a flat wing bolt (421).

6. The foldable wing structure of claim 1, wherein: The tail rudder mechanism (5) includes a tail rudder limiting block (501), a tail rudder torsion spring (502), and a rotating block (503). The rotating block (503) is mounted on the surface of the outer shell mechanism (1) through a tail rudder bolt (504) and a positioning groove (508). A tail rudder locking block (506) is fixedly installed on the inner wall of the rotating block (503). A tail rudder body (507) is provided on the surface of the rotating block (503). The tail rudder body (507) is mounted on the surface of the rotating block (503) through a threaded groove (505) and a fixing groove (509).

7. The foldable wing structure of claim 1, wherein: The protective mechanism (6) includes a fixing ring (601), a rotating plate (604) is provided inside the fixing ring (601), a fixing plate (606) is fixedly installed on the surface of the rotating plate (604), and a transparent protective cover (607) is fixedly installed on the surface of the fixing plate (606).

8. The foldable wing structure of claim 7, wherein: The rotating plate (604) rotates inside the fixed ring (601) via spiral pattern A (603) and spiral pattern B (605), and the rotating plate (604) rotates inside the fixed ring (601) via the rotating groove (602).

9. The foldable wing structure of claim 1, wherein: The rear cover mechanism (7) includes a protrusion (701) and a cover (702). A protruding rod (703) is fixedly installed on the inner wall of the cover (702). Side plates (705) are installed at the front and rear ends of the cover (702). A soft pad (706) is installed on the inner wall of the side plate (705).

10. The foldable wing structure of claim 9, wherein: The protruding rod (703) is slidably connected to the protrusion (701) through the slot (704), the side plate (705) is slidably connected to the outer shell mechanism (1), and the soft pad (706) is slidably connected to the outer shell mechanism (1).

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