Unpowered wing-mounted sports equipment

Abstract

The utility model discloses unpowered wing-mounted sports equipment which comprises a wing-mounted body, a main parachute and an auxiliary wing system, the wing-mounted body comprises a trunk part, two arm parts, two leg parts and fin wings connected to the peripheral side of the trunk part, the main parachute is arranged on the rear portion of the wing-mounted body, and the auxiliary wing system comprises a trunk supporting plate and two main wings. The trunk supporting plate is arranged on the front side of the trunk part, and the two main wings are symmetrically arranged on the left side and the right side of the trunk supporting plate. In the flying process of the unpowered wing-mounted sports equipment, pressure difference is formed between the upper surface and the lower surface of the main wing, upward lifting force is generated, the main wing and the wing-mounted equipment jointly provide the lifting force in the flying process, the sliding-down ratio is increased, the sliding distance and the hang distance of flying of the unpowered wing-mounted equipment are increased, the athletic performance of athletes is improved, and the safety of the athletes is improved. And the flight safety is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of wing suit flying, in particular to a non-powered wing suit sports equipment. Background Art

[0002] Wingsuit flying can be divided into powered and unpowered. Unpowered wingsuit flying involves the athlete donning a flight suit and parachute equipment and leaping from a height. Using the lift provided by the wingsuit, the athlete uses body movements to control the glide direction while flying through the air. Once they reach a safe altitude, they deploy their parachute to land. Currently, the glide ratio for wingsuit flying is approximately 3:1, meaning that for every 1 meter of descent, the athlete simultaneously glides forward 3 meters. This limits the glide distance and time spent in the air, limiting the athlete's landing height and requiring quick adjustments to their stance and deploying their parachute. This makes wingsuit flying a highly challenging and risky sport, and unsafe. Summary of the Invention

[0003] The present invention aims to solve at least one of the technical problems existing in the prior art. To this end, the present invention provides a non-powered wingsuit sports equipment that can improve the safety of wingsuit flight.

[0004] The unpowered wingsuit sports equipment according to the embodiment of the present invention includes:

[0005] A wingsuit is used for athletes to wear, comprising a torso, two arms connected to the upper part of the torso, two legs connected to the lower part of the torso, and fins connected to the sides of the torso;

[0006] a main parachute, disposed at the rear of the wingsuit;

[0007] The auxiliary wing system includes a trunk support plate and two main wings. The trunk support plate is arranged on the front side of the trunk, and the two main wings are symmetrically arranged on the left and right sides of the trunk support plate.

[0008] The unpowered wingsuit sports equipment according to the embodiment of the present invention has at least the following beneficial effects:

[0009] During the flight of the unpowered wing suit sports equipment in the present invention, a pressure difference is formed between the upper and lower surfaces of the main wing, and an upward lift is generated. The main wing and the wing suit jointly provide lift during the flight to enhance the overall lift of the sports equipment, increase the glide ratio, and increase the gliding distance and hovering distance of the unpowered wing suit flight, reserving sufficient operating time for athletes to open the main parachute, thereby improving flight safety.

[0010] According to some embodiments of the present invention, the main wing includes a bending portion and a wing portion, one end of the bending portion is connected to the front side of the trunk support plate, and the other end is connected to the wing portion, and there is a gap between the rear side of the wing portion and the front side of the trunk support plate.

[0011] According to some embodiments of the present invention, the auxiliary wing system further includes an aileron, wherein the aileron is rotatably connected to the underside of the main wing;

[0012] The aileron system also includes a first drive unit and a control line. The non-powered wing suit sports equipment also includes a controller. The first drive unit is connected to the aileron and is used to drive the aileron to rotate. The end of each arm away from the torso is provided with the controller. One end of the control line is connected to the controller, and the other end is connected to the first drive unit. The controller can switch the working state of the first drive unit and be held by the athlete's hand.

[0013] According to some embodiments of the present invention, the control line is built into the main wing, the trunk support plate and the arm.

[0014] According to some embodiments of the present invention, the torso support plate is detachably connected to the torso portion, and the unpowered wing suit sports equipment further includes a second drive unit, which is capable of releasing the connection between the torso support plate and the torso portion to separate the auxiliary wing system from the wing suit.

[0015] According to some embodiments of the present invention, the non-powered wing suit sports equipment also includes a controller and a control line. The controller is provided at the end of each arm away from the torso. The control line includes a first wire and a second wire. One end of the first wire is connected to the controller, and the other end is plugged into the second wire. The other end of the second wire is connected to the second drive unit. The controller is used for the athlete to hold in his hand to send instructions to the second drive unit. The second wire can follow the auxiliary wing system to land and separate from the first wire after the auxiliary wing system is detached from the wing suit.

[0016] According to some embodiments of the present invention, the auxiliary wing system also includes a spoiler and a third driving unit, the spoiler is rotatably connected to the main wing, the third driving unit is connected to the spoiler, and the third driving unit is used to drive the spoiler to be supported relative to the main wing when the auxiliary wing system is separated from the wing suit.

[0017] According to some embodiments of the present invention, the non-powered wing suit sports equipment further includes a controller, wherein each end of the arm away from the torso is provided with the controller, the controller is electrically connected to the second drive unit, and the second drive unit is capable of releasing the connection between the torso support plate and the torso when the controller at each end of the arm is triggered; or, the second drive unit is capable of releasing the connection between the torso support plate and the torso when the controller at each end of the arm slips from the athlete's hand;

[0018] Alternatively, the non-powered wing suit sports equipment also includes a tilt sensor, which is used to detect the athlete's roll angle a. The tilt sensor is connected to the second drive unit, and the second drive unit can release the connection between the torso support plate and the torso when a>150°.

[0019] According to some embodiments of the present invention, the auxiliary wing system further comprises an auxiliary parachute, the auxiliary parachute being connected to the trunk support plate and / or the main wing, the auxiliary parachute being configured to be opened after the auxiliary wing system is separated from the wing suit;

[0020] Alternatively, the auxiliary wing system further comprises a positioning module, which is mounted on the trunk support plate and / or the main wing, and is used to mark the landing position of the auxiliary wing system after separation from the wing suit.

[0021] According to some embodiments of the present invention, the main wing is located in the lower middle portion of the trunk support plate;

[0022] And / or, the main wing is configured as a forward-swept wing.

[0023] Additional aspects and advantages of the present invention will be given in part in the following description and will become apparent from the following description or learned through practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] The present invention will be further described below with reference to the accompanying drawings and embodiments, wherein:

[0025] Figure 1 This is a schematic diagram of an embodiment of the non-powered wingsuit sports equipment of the present invention;

[0026] Figure 2 for Figure 1 Side view of the unpowered wingsuit sports equipment;

[0027] Figure 3 for Figure 1 The main view of the non-powered wingsuit sports equipment;

[0028] Figure 4 for Figure 2 Schematic diagram of the unpowered wing suit sports equipment after the auxiliary wing system is separated from the wing suit;

[0029] Figure 5 for Figure 3 Schematic diagram of the unpowered wing suit sports equipment after the auxiliary wing system is separated from the wing suit.

[0030] Reference numerals:

[0031] Wing suit 100, torso 110, arms 120, legs 130, fins 140; main parachute 200; auxiliary wing system 300, torso support plate 310, main wing 320, bending part 321, wing 322, aileron 330, control line 340, first wire 341, second wire 342, spoiler 350; controller 400. DETAILED DESCRIPTION

[0032] The following describes embodiments of the present invention in detail. Examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are intended only to explain the present invention and are not to be construed as limiting the present invention.

[0033] In the description of the present invention, it should be understood that descriptions involving orientations, such as up, down, front, back, left, right, etc., indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation. Therefore, they cannot be understood as limitations on the present invention.

[0034] In the description of this utility model, "several" means more than one, "plurality" means more than two, "greater than," "less than," and "exceed" are understood to exclude the number itself, while "above," "below," and "within" are understood to include the number itself. The use of the terms "first" and "second" is solely for the purpose of distinguishing technical features and is not to be construed as indicating or implying relative importance, implicitly specifying the number of the indicated technical features, or implicitly specifying the order of the indicated technical features.

[0035] In the description of the present invention, unless otherwise clearly defined, terms such as setting, installing, and connecting should be understood in a broad sense, and technicians in the relevant technical field can reasonably determine the specific meanings of the above terms in the present invention based on the specific content of the technical solution.

[0036] In the description of the present invention, reference to terms such as "one embodiment," "some embodiments," "illustrative embodiments," "examples," "specific examples," or "some examples" means that the specific features, structures, materials, or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present invention. In this specification, the exemplary expressions of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

[0037] For ease of description and understanding, the present invention uses the human body as a reference, where "up" refers to the direction toward the human head, "down" refers to the direction toward the human feet, "left" and "right" refer to the left and right sides of the human body respectively, "front" refers to the direction toward the front of the human body, and "back" refers to the direction toward the back of the human body.

[0038] Reference Figures 1 to 3 In an embodiment of the present invention, a non-powered wing suit sports equipment (hereinafter referred to as sports equipment) is provided. The sports equipment includes a wing suit 100, a main parachute 200 and an auxiliary wing system 300. The wing suit 100 is used for athletes to wear. The wing suit 100 can be made of nylon material with excellent toughness and tension. The wing suit 100 includes a torso 110, arms 120, legs 130 and fins 140. After the athlete wears the wing suit 100, the torso 110 wraps the back, chest and abdomen of the human body, the arms 120 wrap the upper arms and forearms of the human body, and the legs 130 wrap the human body. The thigh and calf positions of the body; there are two arms 120 and two legs 130, the two arms 120 are symmetrical and connected to the upper part of the torso 110, and the two legs 130 are symmetrical and connected to the lower part of the torso 110. The fins 140 are arranged on the circumference of the torso 110 and are connected to the legs 130 and the arms 120. Air inlets can be set on the inner sides of the arms 120 and / or legs 130. The interior of the wing suit 100 is hollow, and air can enter the wing suit 100 through the air inlets. The wing suit 100 is filled with gas and remains in an expanded state, providing flying lift for the athlete.

[0039] The wingsuit 100 may be provided with a zipper to make the wearing of the wingsuit 100 more convenient, and the zipper is not limited to being provided on the torso 110, the leg 130 or the arm 120. The wingsuit 100 may also include a helmet, which is used to be worn on the athlete's head.

[0040] The main parachute 200 is located at the rear of the wingsuit 100 and is designed to deploy after the wingsuit reaches a preset altitude, allowing the athlete to land safely. The main parachute 200 can be deployed in various ways, including by the athlete grasping the parachute cord and pulling down upon the glider to release the parachute from the parachute bag. Alternatively, the equipment can be equipped with an automatic deployment mechanism. If the athlete fails to deploy the main parachute 200 at a preset minimum altitude, the automatic deployment mechanism automatically activates and deploys the main parachute 200. Furthermore, the equipment may include a reserve parachute, which the athlete can use to land in the event of a malfunction in the main parachute 200.

[0041] The auxiliary wing system 300 includes a trunk support plate 310 and two main wings 320. The trunk support plate 310 is arranged on the front side of the trunk 110, and the two main wings 320 are symmetrically arranged on the left and right sides of the trunk support plate 310. During flight, a pressure difference is formed between the upper and lower surfaces of the main wings 320, and an upward lift is generated. The main wings 320 and the wing suit 100 jointly provide lift during flight, increase the glide ratio, and increase the gliding distance and hovering distance of the unpowered wing suit 100, thereby improving the athlete's athletic performance and improving safety.

[0042] The trunk support plate 310 is located in the middle of the trunk 110 and supports the athlete's chest and abdomen during flight. The trunk support plate 310 can be designed based on ergonomics to better fit the human body and improve comfort. In addition, by increasing the area and hardness of the trunk support plate 310, the pressure exerted by the trunk support plate 310 on the human body after wearing can be reduced, thereby improving wearing comfort. For example, after the sports equipment is put on, the trunk support plate 310 covers the front of the athlete's chest and abdomen, as well as the left and right sides of the chest and abdomen, to maximize the area of ​​the trunk support plate 310. The main wing 320 is located in the middle and lower part of the trunk support plate 310. After wearing, the main wing 320 is located near the waist and abdomen of the human body, so that the lift center of the main wing 320 matches the center of gravity of the athlete during flight, ensuring flight stability.

[0043] In one embodiment, the main wing 320 is configured as a forward-swept wing, that is, the main wing 320 is tilted upward relative to the trunk support plate 310. Since the main wing 320 is slightly swept forward, the main wing 320 can improve the low-speed performance to a certain extent, delay stall, and reduce wingtip vortex drag, thereby improving the athletic performance of wingsuit athletes with the assistance of the auxiliary wing system 300.

[0044] In addition, the main wing 320 includes a bending portion 321 and a wing portion 322. One end of the bending portion 321 is connected to the front side of the trunk support plate 310, and the other end is connected to the wing portion 322, so that there is a gap between the rear side of the wing portion 322 and the front side of the trunk support plate 310, so as to reduce the mutual interference between the flow fields of the wing suit 100 and the main wing 320; further, the bending portion 321 is arranged on the right side of the center of the trunk support plate 310 and on the left side of the center of the trunk support plate 310, so that the two main wings 320 are independent of each other and spaced apart.

[0045] A bending portion 321 may also be provided to bend toward the left or right side of the trunk support plate 310 away from the center of the trunk support plate 310 , and the bending portion 321 is integrally connected to the wing portion 322 to ensure that the shape of the main wing 320 is smooth to reduce air resistance.

[0046] In one embodiment, the aileron system 300 further includes ailerons 330, which are rotatably connected to the undersides of the main wings 320. Each main wing 320 is connected to an aileron 330. When the ailerons 330 rotate relative to the main wings 320, they can achieve roll control of the sports equipment. For example, when the ailerons 330 on the left main wing 320 rotate upward and the ailerons 330 on the right main wing 320 rotate downward, the lift of the left main wing 320 decreases and the lift of the right main wing 320 increases. The aileron system 300 generates a rolling torque around its longitudinal axis, assisting the athlete in completing a roll maneuver and making it easier for the athlete to adjust flight direction.

[0047] The aileron system 300 also includes a first drive unit and a control line 340. The first drive unit is configured as a power element such as a motor or a servo that can output rotational power. The first drive unit is connected to the aileron 330 and is used to drive the aileron 330 to rotate so that the aileron 330 rotates upward or downward relative to the main wing 320. The sports equipment also includes a controller 400. There are two controllers 400. Each arm 120 is provided with a controller 400 at the end away from the torso 110. The controller 400 is for the athlete to hold in his hand, making it convenient for the athlete to operate the controller 400. One end of the control line 340 is connected to the controller 400, and the other end is connected to the first drive unit. The controller 400 sends instructions to the first drive unit through the control line 340 to switch the working state of the first drive unit.

[0048] For example, the controller 400 is integrated with a control button. When the athlete presses the control button on the left controller 400, the aileron 330 on the left main wing 320 rotates upward, and the aileron 330 on the right main wing 320 rotates downward. In this case, a rolling moment to the left is generated to assist the athlete to turn left; when the athlete presses the control button on the right controller 400, the aileron 330 on the right main wing 320 rotates upward, and the aileron 330 on the left main wing 320 rotates downward. In this case, a rolling moment to the right is generated to assist the athlete to turn right.

[0049] In one embodiment, the athlete can adjust the rotation angle of the aileron 330 by controlling the depth of the control button's press, assisting the athlete in completing a roll. For example, when the control button is pressed, the first drive unit drives the aileron 330 to rotate. As the athlete presses the control button deeper, the rotation angle of the aileron 330 increases. As the athlete presses the control button less deeply, the rotation angle of the aileron 330 decreases. When the athlete stops pressing the control button and releases the control button, the aileron 330 returns to its initial position.

[0050] In another embodiment, the control button has a first position and a second position. When the athlete switches the control button to the first position, the first drive unit drives the aileron 330 to rotate to a preset angle to assist the athlete in completing a rolling maneuver. When the athlete switches the control button to the second position, the aileron 330 returns to its initial position. For example, the athlete can press the control button to switch it to the first position. For example, when the athlete presses the control button to switch it to the first position, the first drive unit drives the aileron 330 to rotate to a preset angle. When the athlete presses the control button again or stops pressing and releases the control button, the control button switches to the second position, and the aileron 330 returns to its initial position. The rotation angle of the aileron 330 in the first position can be preset according to the flight requirements of the sports equipment.

[0051] The control line 340 is made of a flexible material and is built into the main wing 320, the torso 110 and the arm 120. The control line 340 is routed from the inside of the wing suit 100 and the torso support plate 310 to prevent the control line 340 from shaking or getting entangled due to the influence of external airflow, thereby ensuring an effective connection between the controller 400 and the first drive unit, and the athlete can open the main parachute 200 normally without abandoning the auxiliary wing system 300.

[0052] In one embodiment, if Figure 4 and Figure 5The trunk support plate 310 is detachably connected to the trunk portion 110. The sports equipment also includes a second drive unit that can disconnect the trunk support plate 310 from the trunk portion 110, thereby separating the flap system 300 from the wing suit 100. In the event of a dive or other emergency, the flap system 300 can be quickly jettisoned through the second drive unit, making flight more flexible and safer.

[0053] For example, one of the trunk support plate 310 and the trunk portion 110 is provided with a latch, and the other is provided with a latch hole. The latch is inserted into the latch hole. When the wing system 300 needs to be discarded, the second drive unit drives the latch to move, causing the latch to withdraw from the latch hole. At this time, the connection between the trunk portion 110 and the trunk support plate 310 is released, and the wing system 300 can be separated from the wing suit 100 under the action of gravity. In this case, the second drive unit can be configured as a motor capable of outputting linear power. Alternatively, the trunk support plate 310 and the trunk portion 110 are provided with engaging hooks. When the wing system 300 needs to be discarded, the second drive unit drives one of the hooks to rotate, causing the two hooks to separate. At this time, the connection between the trunk portion 110 and the trunk support plate 310 is released, and the wing system 300 can be separated from the wing suit 100.

[0054] Furthermore, the athlete can manually operate the controller 400 to trigger the separation of the auxiliary wing system 300 and the wing suit 100. In this case, a controller 400 is provided at the end of each arm 120 away from the torso 110. The controller 400 is for the athlete to hold in the hand. The controller 400 is electrically connected to the second drive unit. When the controller 400 at the end of each arm 120 is triggered, that is, when the athlete operates the controllers 400 on the left and right sides with both hands at the same time, the second drive unit receives the command of the controller 400 and releases the connection between the torso support plate 310 and the torso 110, so that the auxiliary wing system 300 is separated from the wing suit 100.

[0055] It should be noted that the roll control of the sports equipment and the disengagement control of the aileron system 300 can share the same controller 400. Roll control only requires the athlete to operate a single controller 400, while disengagement of the aileron system 300 requires the athlete to simultaneously operate both controllers 400. Different manipulations of the controllers 400 can change the sports equipment to different flight states. Furthermore, roll control can be achieved by the athlete pressing a control button on one of the controllers 400, while disengagement of the aileron system 300 can be achieved by the athlete simultaneously pressing control buttons on both controllers 400 with both hands.

[0056] In another embodiment, if both controllers 400 located at the ends of each arm 120 slip from the athlete's hand, the second actuator automatically disconnects the trunk support plate 310 from the torso 110. Specifically, if the athlete accidentally drops both controllers 400, the athlete loses control of the flap system 300. The second actuator can directly disconnect the trunk support plate 310 from the torso 110, separating the flap system 300 from the wingsuit 100. In this scenario, a tactile sensor, such as a microswitch or conductive rubber, can be integrated into the controller 400 to detect whether the controller 400 is in contact with or separated from the human hand. When the tactile sensor detects that the controller 400 has separated from the human hand, the second actuator is triggered to disconnect the trunk support plate 310 from the torso 110.

[0057] Alternatively, in another embodiment, the sports equipment also includes a tilt sensor, which is used to detect the athlete's roll angle a. When the athlete is in a level flight state, his face is facing downward, and at this time a=0°. When the athlete rolls to the left or right and his face is facing downward, 0°<a<90°, and the athlete is tilted. When the athlete tilts to a>150°, the athlete's face is facing upward. In this case, it is assumed that a flight accident has occurred, and the second drive unit is directly triggered to release the connection between the torso support plate 310 and the torso 110, so that the auxiliary wing system 300 is separated from the wing suit 100 to avoid secondary injury.

[0058] When the controller 400 is manipulated to send a command to the second drive unit to disconnect the trunk support plate 310 from the trunk portion 110, the controller 400 and the second drive unit are connected via a control line 340, enabling signal transmission between the controller 400 and the second drive unit. The control line 340 includes a first wire 341 and a second wire 342. One end of the first wire 341 is connected to the controller 400 and the other end plugs into the second wire 342. The other end of the second wire 342 is connected to the second drive unit. In other words, the controller 400 and the second drive unit are electrically connected by plugging the first wire 341 and the second wire 342. When the connection between the trunk support plate 310 and the trunk portion 110 is disconnected, the aileron system 300 gradually descends under the action of gravity. The second wire 342 follows the aileron system 300 and descends synchronously with it. Under the action of gravity on the aileron system 300, it separates from the first wire 341, completely separating the aileron system 300 from the wing suit 100.

[0059] In one embodiment, the auxiliary wing system 300 also includes a spoiler 350 and a third driving unit. The spoiler 350 is rotatably connected to the main wing 320. The third driving unit is connected to the spoiler 350 and can drive the spoiler 350 to rotate. When the athlete is flying normally, the spoiler 350 is in contact with the upper surface of the main wing 320 to reduce flight resistance. After the auxiliary wing system 300 is separated from the wing suit 100, the third driving unit drives the spoiler 350 to prop up relative to the main wing 320 to increase the flight resistance of the auxiliary wing system 300, so that the auxiliary wing system 300 falls backward and downward relative to the athlete without interfering with the athlete's subsequent flight path.

[0060] The third drive unit can be connected to the controller 400 through the control line 340. When the athlete sends an instruction to the second drive unit to release the connection between the torso support plate 310 and the torso 110 by operating the controller 400, the third drive unit simultaneously receives the instruction from the controller 400 and drives the spoiler 350 to prop up, so that the auxiliary wing system 300 reduces the flight speed while separating from the wing suit 100, ensuring that the auxiliary wing system 300 falls backward and downward relative to the athlete.

[0061] The auxiliary wing system 300 also includes an auxiliary parachute, which is connected to the trunk support plate 310 and / or the main wing 320. The auxiliary parachute is used to open after the auxiliary wing system 300 is separated from the wing suit 100 to reduce the landing speed of the auxiliary wing system 300 and avoid accidental injuries caused by falling objects from high altitude.

[0062] The aileron system 300 also includes a positioning module, which is mounted on the trunk support plate 310 and / or the main wing 320. The positioning module is used to mark the landing position of the aileron system 300 after separation from the wingsuit 100, facilitating recovery. The positioning module is not limited to an infrared positioning module capable of emitting infrared light, an ultrasonic positioning module capable of emitting ultrasonic waves, a radar, a liquid smoke device capable of emitting colored smoke, a GPS locator, etc.

[0063] The embodiments of the present invention have been described in detail above with reference to the accompanying drawings. However, the present invention is not limited to the above embodiments. Various modifications can be made within the scope of knowledge possessed by a person skilled in the art without departing from the spirit of the present invention. In addition, the embodiments of the present invention and the features of the embodiments can be combined with each other unless there is a conflict.

Claims

1. Unpowered wingsuit sports equipment, characterized in that: include: A wingsuit is used for athletes to wear, comprising a torso, two arms connected to the upper part of the torso, two legs connected to the lower part of the torso, and fins connected to the sides of the torso; a main parachute, disposed at the rear of the wing suit; The auxiliary wing system includes a trunk support plate and two main wings. The trunk support plate is arranged on the front side of the trunk, and the two main wings are symmetrically arranged on the left and right sides of the trunk support plate.

2. The non-powered wingsuit sports equipment according to claim 1, characterized in that: The main wing includes a bending portion and a wing portion, one end of the bending portion is connected to the front side of the trunk support plate, and the other end is connected to the wing portion, and there is a gap between the rear side of the wing portion and the front side of the trunk support plate.

3. The non-powered wingsuit sports equipment according to claim 1, characterized in that: The auxiliary wing system further comprises an aileron, wherein the aileron is rotatably connected to the lower side of the main wing; The aileron system also includes a first drive unit and a control line. The non-powered wing suit sports equipment also includes a controller. The first drive unit is connected to the aileron and is used to drive the aileron to rotate. The end of each arm away from the torso is provided with the controller. One end of the control line is connected to the controller, and the other end is connected to the first drive unit. The controller can switch the working state of the first drive unit and be held by the athlete's hand.

4. The non-powered wingsuit sports equipment according to claim 3, characterized in that: The control line is built into the main wing, the trunk support plate and the arm.

5. The unpowered wingsuit sports equipment according to any one of claims 1 to 4, characterized in that: The torso support plate is detachably connected to the torso portion, and the non-powered wing suit sports equipment further includes a second driving unit, which is capable of releasing the connection between the torso support plate and the torso portion to separate the auxiliary wing system from the wing suit.

6. The non-powered wing suit sports equipment according to claim 5, characterized in that: The non-powered wing suit sports equipment also includes a controller and a control line. The controller is provided at the end of each arm away from the torso. The control line includes a first wire and a second wire. One end of the first wire is connected to the controller, and the other end is plugged into the second wire. The other end of the second wire is connected to the second drive unit. The controller is used for the athlete to hold in his hand to send instructions to the second drive unit. The second wire can follow the auxiliary wing system to land and separate from the first wire after the auxiliary wing system is detached from the wing suit.

7. The non-powered wingsuit sports equipment according to claim 5, characterized in that: The auxiliary wing system also includes a spoiler and a third driving unit. The spoiler is rotatably connected to the main wing. The third driving unit is connected to the spoiler. The third driving unit is used to drive the spoiler to be supported relative to the main wing when the auxiliary wing system is separated from the wing suit.

8. The non-powered wingsuit sports equipment according to claim 5, characterized in that: The unpowered wingsuit sports equipment further comprises a controller, wherein each arm portion is provided with the controller at an end away from the torso portion, the controller being electrically connected to the second drive unit, and the second drive unit being capable of releasing the connection between the torso support plate and the torso portion when the controller at each arm portion is triggered; or, the second drive unit being capable of releasing the connection between the torso support plate and the torso portion when the controller at each arm portion slips from the athlete's hand; Alternatively, the non-powered wing suit sports equipment also includes a tilt sensor, which is used to detect the athlete's roll angle a. The tilt sensor is connected to the second drive unit, and the second drive unit can release the connection between the torso support plate and the torso when a>150°.

9. The non-powered wingsuit sports equipment according to claim 5, characterized in that: The auxiliary wing system further comprises an auxiliary parachute, the auxiliary parachute being connected to the trunk support plate and / or the main wing, and the auxiliary parachute being configured to be opened after the auxiliary wing system is separated from the wing suit; Alternatively, the auxiliary wing system further comprises a positioning module, which is mounted on the trunk support plate and / or the main wing, and is used to mark the landing position of the auxiliary wing system after separation from the wing suit.

10. The non-powered wingsuit sports equipment according to claim 1, characterized in that: The main wing is located at the middle and lower part of the trunk support plate; And / or, the main wing is configured as a forward-swept wing.

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