Unmanned aerial vehicle wind-resistant material stable throwing frame

Abstract

The utility model discloses an unmanned aerial vehicle wind-load-resistant material stable throwing frame, and relates to the technical field of material throwing frames. The throwing device comprises a throwing frame, a shielding assembly is arranged on the front face of the throwing frame, a plurality of elastic supporting assemblies are arranged in the throwing frame, locking assemblies are arranged at the supporting ends, corresponding to the elastic supporting assemblies, of the throwing frame, a traction assembly is arranged at the top of the throwing frame, and the traction end of the traction assembly is connected with the locking assemblies. When the throwing frame is placed on the ground through an unmanned aerial vehicle, the supporting ends of the elastic supporting assemblies can make contact with the ground in sequence, then the locking assembly is pulled through the traction assembly, and the supporting ends can be locked through the locking assembly; by means of the arrangement, when the throwing frame is placed on the uneven ground, the throwing frame is not prone to inclining, and the risks that when an unmanned aerial vehicle lands, the gravity center shifts, and even a vehicle body shakes and turns on one side are effectively avoided.

Description

TECHNICAL FIELD

[0001] The utility model belongs to material delivery frame technical field, concretely, especially relate to a unmanned aerial vehicle wind load resistance material stable delivery frame. BACKGROUND

[0002] When unmanned aerial vehicle executes material transportation task, usually needs to realize goods bearing and transportation by the help of special delivery frame. In order to ensure the stability and safety of structure in the transportation process, the delivery frame of current most unmanned aerial vehicle adopts rigid connection design, is fixed with unmanned aerial vehicle main body through integrated structure or high-strength fastener, thereby effectively avoids the risk of connection loosening or load deviation caused by mechanical vibration, airflow disturbance and other factors when air operation.

[0003] The bottom of delivery frame is mostly set relatively flat, when unmanned aerial vehicle needs to execute task on uneven, soft or inclined ground (such as mountain, ruins, farmland and other scenes), flat base is difficult to completely adhere to ground;Because the force of each contact point of base is uneven, delivery frame is easy to unilateral tilt or partially suspended, resulting in gravity center deviation when unmanned aerial vehicle lands, even appears body shaking, rollover and other risks, seriously affects landing stability. UTILITY MODEL CONTENT

[0004] In view of the problem that the base of delivery frame is not easy to completely adhere to uneven ground, the utility model provides a unmanned aerial vehicle wind load resistance material stable delivery frame to overcome the above technical problems existing in prior art.

[0005] To solve the above technical problems, the utility model is realized by the following technical schemes:

[0006] The utility model discloses a unmanned aerial vehicle wind load resistance material stable delivery frame, including delivery frame, the front of delivery frame is provided with the sheltering subassembly, the inside of delivery frame is provided with a plurality of elastic support subassembly, the support end of elastic support subassembly extends to the bottom of delivery frame, the support end of corresponding elastic support subassembly of delivery frame is provided with locking assembly, the top of delivery frame is provided with traction assembly, the traction end of traction assembly is connected together with locking assembly;

[0007] The support end of a plurality of elastic support subassembly moves under the gravity of delivery frame and internal substance, so that a plurality of support ends are in contact with ground together, the traction assembly is used for pulling locking assembly, so that locking assembly locks the support end of adjustment.

[0008] Further, the shielding assembly comprises a shielding frame, one side of the shielding frame is rotationally connected with the throwing frame, the other side of the shielding frame movably connects with an L-shaped moving plate, the inner wall of the shielding frame fixedly connects with a guide rod, the outer surface of the guide rod movably connects with a connecting plate, one side of the L-shaped moving plate movably connects with the connecting plate, the outer side of the throwing frame is provided with a fixed groove, the inner part of the fixed groove movably connects with a fixed plate, and the fixed plate is fixedly connected with the L-shaped moving plate.

[0009] Further, the connecting plate is fixedly connected with the inner wall of the throwing frame through a fixed spring, and the other side of the L-shaped moving plate is fixedly connected with a pulling frame.

[0010] Further, the elastic supporting assembly comprises a receiving cavity, a plurality of receiving cavities are formed in the inside of the throwing frame, the inside of the receiving cavity is fixedly connected with a supporting pipe movably connected with a supporting pipe, the bottom end of the supporting pipe extends to the outside of the throwing frame, the inner wall top of the receiving cavity is fixedly connected with a fixed rod, the fixed rod is movably connected with the supporting pipe, the top end of the supporting pipe is fixedly connected with a pushing disc, and the pushing disc is fixedly connected with the inner wall top of the receiving cavity through a pushing spring.

[0011] Further, the locking assembly comprises a mounting cavity, the mounting cavity is formed in the inner wall of the receiving cavity, the inside of the mounting cavity movably connects with a locking piece, the inner wall of the locking piece is fixedly connected with a pulling plate, one side of the pulling plate penetrates through the fixed rod and extends to the outside of the throwing frame, the outer surface of the supporting pipe is provided with a through groove corresponding to the pulling plate, one side of the pulling plate is fixedly connected with a pulling disc, the pulling disc is fixedly connected with the throwing frame through a locking spring, and the inner wall of the locking piece and the outer surface of the supporting pipe are both provided with a friction groove.

[0012] Further, the traction assembly comprises two T-shaped traction ropes, the two ends of the two T-shaped traction ropes are fixedly connected with corresponding pulling discs, the top of the throwing frame is fixedly provided with a winding frame, the inside of the winding frame is rotationally connected with a winding disc, the top end of the T-shaped traction rope penetrates through the throwing frame and is fixedly connected with the winding disc, the top of the winding frame is fixedly connected with a motor, the output end of the motor is fixedly connected with the winding disc, and the top and the inner wall of the throwing frame are rotationally connected with a plurality of guide wheels corresponding to the T-shaped traction rope.

[0013] Further, the top of the throwing frame is fixedly provided with a plurality of mounting frames.

[0014] The utility model has the following beneficial effects:

[0015] 1. The utility model discloses a placing frame is placed on the ground through unmanned plane, with the unmanned plane is constantly lowered, the support end on the elastic support component that first contacts the ground can constantly move upwards, thereby making the support end of other elastic support components can be in turn contacted together with the ground, then through the traction component to the locking component is pulled, and the locking component can lock the support end, the above -mentioned setting makes when placing the frame on the uneven ground, the frame is not easy to appear the phenomenon of inclination, effectively avoid the gravity center deviation when the unmanned plane lands, even the fuselage shakes, rolls over and other risks, thereby the stability of unmanned plane when landing can be guaranteed.

[0016] 2. The utility model discloses through motor drive winding disc, and the winding disc can be wound two T type traction ropes simultaneously, and two constantly wound T type traction ropes are pulled to all pull -on disc simultaneously, and the pull -on disc is pulled to the locking piece through the pull -on plate, thereby making the locking piece contact the outer surface of support pipe and locking it, the above -mentioned setting when locking several support tubes, only need to drive motor, and the operation is relatively convenient, simultaneously, adopt T type traction rope as transmission medium, compared with traditional rigid link structure, effectively alleviate the overall weight of the frame, realizes the lightweight design goal under the premise of guaranteeing the structural strength.

[0017] Of course, any product implementing the utility model does not necessarily need to achieve all the advantages described above at the same time. BRIEF DESCRIPTION OF DRAWINGS

[0018] In order to more clearly illustrate the technical scheme of the utility model embodiment, the following will be needed to use the drawings described in the embodiment briefly introduced, obviously, the drawings in the following description only some embodiments of the utility model, for those skilled in the art, under the premise of not paying creative labor, other drawings can also be obtained according to these drawings.

[0019] Figure 1 It is the external contour structure schematic diagram of the utility model;

[0020] Figure 2 It is the shielding assembly structure schematic diagram of the utility model;

[0021] Figure 3 It is the Figure 2 Amplification structure schematic diagram in place B of the utility model;

[0022] Figure 4 It is the frame structure schematic diagram of the utility model;

[0023] Figure 5 It is the Figure 4 Amplification structure schematic diagram in place B of the utility model;

[0024] Figure 6 For the utility model Figure 4 Amplification structure schematic view at C;

[0025] Figure 7 For the utility model Figure 4 Amplification structure schematic view at D;

[0026] Figure 8 For the utility model elastic support assembly structure schematic view;

[0027] Figure 9 For the utility model locking assembly structure schematic view.

[0028] In the drawings, the component list represented by each sign is as follows:

[0029] 1, the delivery frame;2, the shielding assembly;201, the shielding frame;202, the L-shaped moving plate;203, the guide rod;204, the connecting plate;205, the fixed groove;206, the fixed plate;207, the fixed spring;208, the pulling frame;3, the elastic support assembly;301, the storage cavity;302, the support tube;303, the fixed rod;304, the push disc;305, the push spring;4, the locking assembly;401, the installation cavity;402, the locking piece;403, the pulling plate;404, the through slot;405, the pulling disc;406, the locking spring;407, the friction slot;5, the traction assembly;501, the T-shaped traction rope;502, the winding frame;503, the winding disc;504, the motor;505, the guide wheel;6, the mounting frame. Specific implementation

[0030] The technical solutions in the utility model embodiments will be clearly and completely described below with reference to the drawings in the utility model embodiments. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of the utility model protection.

[0031] In the description of the utility model, it is understood that the terms "opening", "upper", "lower", "top", "middle", "inner" and the like indicate the orientation or positional relationship, which is only for the convenience of describing the utility model and simplifying the description, and does not indicate or imply that the indicated components or elements must have a particular orientation, be constructed and operated in a particular orientation, therefore it cannot be understood as a limitation on the utility model.

[0032] Please refer to Figures 1-9The utility model discloses a kind of unmanned aerial vehicle wind load material stable release frame, including release frame 1, the front of release frame 1 is provided with shielding assembly 2, the inside of release frame 1 is provided with several elastic support assemblies 3, the support end of elastic support assembly 3 extends to the bottom of release frame 1, the support end of release frame 1 is provided with locking assembly 4 corresponding elastic support assembly 3, the top of release frame 1 is provided with traction assembly 5, the traction end of traction assembly 5 is connected together with locking assembly 4.

[0033] The support end of several elastic support assemblies 3 moves under the action of the gravity of release frame 1 and internal substance, so that the support end is in contact with the ground, and the traction assembly 5 is used to pull the locking assembly 4, so that the locking assembly 4 locks the support end adjusted.

[0034] When the release frame 1 is installed at the bottom of the unmanned aerial vehicle, the support end of the elastic support assembly 3 can be in contact with the ground when the unmanned aerial vehicle drives the release frame 1 to land, and as the unmanned aerial vehicle continuously descends, the support end of the elastic support assembly 3 first in contact with the ground can continuously move upward under the action of the gravity of the release frame 1 and the material, and the support end of the other elastic support assembly 3 is in contact with the ground in turn, and when all the support ends are in contact with the ground, the traction assembly 5 pulls the locking assembly 4, so that the locking assembly 4 can lock the corresponding support end.

[0035] When the release frame 1 is placed on the ground by the unmanned aerial vehicle, as the unmanned aerial vehicle continuously descends, the support end of the elastic support assembly 3 first in contact with the ground can continuously move upward, so that the support end of the other elastic support assembly 3 is in contact with the ground in turn, and then the traction assembly 5 pulls the locking assembly 4, and the locking assembly 4 can lock the support end, and the above-mentioned arrangement makes the release frame 1 not easy to tilt when placed on the uneven ground, effectively avoids the center of gravity from deviating when the unmanned aerial vehicle lands, and even the risk of body shaking, rollover, etc., so that the stability of the unmanned aerial vehicle when landing can be guaranteed.

[0036] In one embodiment, for the above-mentioned shielding assembly 2, the shielding assembly 2 comprises a shielding frame 201, one side of the shielding frame 201 is rotatably connected with the delivery frame 1, the other side of the shielding frame 201 movably connects with an L-shaped moving plate 202, the inner wall of the shielding frame 201 fixedly connects with a guide rod 203, the outer surface of the guide rod 203 movably connects with a connecting plate 204, one side of the L-shaped moving plate 202 movably connects with the connecting plate 204, the outer side of the delivery frame 1 is provided with a fixed groove 205, the inside of the fixed groove 205 movably connects with a fixed plate 206, and the fixed plate 206 is fixedly connected with the L-shaped moving plate 202.

[0037] After the goods are placed in the inside of the delivery frame 1, the shielding frame 201 is rotated to the front of the delivery frame 1, and the L-shaped moving plate 202 is pushed, so that the fixed plate 206 can be moved into the inside of the fixed groove 205 under the pushing of the L-shaped moving plate 202, at this time the L-shaped moving plate 202 can limit the shielding frame 201 through the fixed plate 206 and the fixed groove 205, so that the shielding frame 201 will not be randomly rotated when shielding the front of the delivery frame 1; the L-shaped moving plate 202 can drive the connecting plate 204 to slide on the guide rod 203 when moving, and the connecting plate 204 is arranged so that the L-shaped moving plate 202 will not be randomly separated from the shielding frame 201.

[0038] In one embodiment, for the above-mentioned connecting plate 204, one side of the connecting plate 204 is fixedly connected with the inner wall of the delivery frame 1 through a fixed spring 207, and the other side of the L-shaped moving plate 202 is fixedly connected with a pulling frame 208.

[0039] The fixed spring 207 pushes the L-shaped moving plate 202 through the connecting plate 204, so that when the L-shaped moving plate 202 drives the fixed plate 206 to move into the inside of the fixed groove 205, the fixed plate 206 will not be randomly separated from the inside of the fixed groove 205; and when the shielding frame 201 is rotated, the fixed plate 206 can be moved out of the inside of the fixed groove 205 by directly pulling the L-shaped moving plate 202 through the pulling frame 208, and the whole operation is also relatively convenient.

[0040] In one embodiment, for the above-mentioned elastic support assembly 3, the elastic support assembly 3 comprises a receiving cavity 301, a plurality of which are opened in the inside of the delivery frame 1, the inside of the receiving cavity 301 is fixedly connected with a movable connection with a support pipe 302, the bottom end of the support pipe 302 extends to the outside of the delivery frame 1, the inner wall top of the receiving cavity 301 is fixedly connected with a fixed rod 303, the fixed rod 303 is movably connected with the support pipe 302, the top end of the support pipe 302 is fixedly connected with a push disc 304, and the push disc 304 is fixedly connected with the inner wall top of the receiving cavity 301. A push spring 305 is fixedly connected between the push disc 304 and the inner wall top of the receiving cavity 301.

[0041] The push spring 305 pushes the support pipe 302 downward through the push disc 304, so that the support pipe 302 is mostly outside the delivery frame 1; when the delivery frame 1 lands under the driving of the unmanned aerial vehicle, if the landing ground is uneven, at this time one of the support pipes 302 can first contact the upwardly protruding ground, and as the delivery frame 1 continuously moves to the ground, the support pipe 302 in contact with the ground continuously extrudes the push spring 305 upward through the push disc 304, and the support pipe 302 continuously slides in the inside of the receiving cavity 301, so that the other support pipes 302 can be in contact with the ground in turn; in the above-mentioned arrangement, the fixed rod 303 can guide the push spring 305, so that the push spring 305 can maintain straightness as a whole when being compressed.

[0042] In one embodiment, for the above-mentioned locking assembly 4, the locking assembly 4 comprises a mounting cavity 401, which is opened in the inner wall of the receiving cavity 301, the inside of the mounting cavity 401 is movably connected with a locking piece 402, the inner wall of the locking piece 402 is fixedly connected with a pulling plate 403, one side of the pulling plate 403 penetrates through the fixed rod 303 and extends to the outside of the delivery frame 1, the outer surface of the support pipe 302 is provided with a through slot 404 corresponding to the pulling plate 403, one side of the pulling plate 403 is fixedly connected with a pulling disc 405, the pulling disc 405 is fixedly connected with the delivery frame 1 through a locking spring 406, and the inner wall of the locking piece 402 and the outer surface of the support pipe 302 are both provided with a friction groove 407.

[0043] The locking spring 406 pushes the locking sheet 402 to the inside of the mounting cavity 401 through the pulling disc 405 and the pulling plate 403, so that the locking sheet 402 is in a separated state with the support pipe 302 when the support pipe 302 moves; when the support pipe 302 moves in the inside of the storage cavity 301, the support pipe 302 can slide outside the pulling plate 403 through the through slot 404, and the through slot 404 is arranged so that the pulling plate 403 does not hinder the movement of the support pipe 302; after all the support pipes 302 are in contact with the ground, all the pulling discs 405 are pulled, so that the pulling disc 405 can pull the locking sheet 402 through the corresponding pulling plate 403, and the locking sheet 402 is in contact with the outer surface of the support pipe 302, and since the inner wall of the locking sheet 402 and the outer surface of the support pipe 302 are both provided with friction grooves 407, the friction between the locking sheet 402 and the support pipe 302 is large after they are in contact, and this arrangement can ensure the firmness of the locking sheet 402 when locking the support pipe 302.

[0044] In one embodiment, for the above-mentioned traction assembly 5, the traction assembly 5 comprises two T-shaped traction ropes 501, both ends of the two T-shaped traction ropes 501 are fixedly connected with the corresponding pulling disc 405, the top of the delivery frame 1 is fixedly installed with a winding frame 502, the inside of the winding frame 502 is rotatably connected with a winding disc 503, the top end of the T-shaped traction rope 501 penetrates through the delivery frame 1 and is fixedly connected with the winding disc 503, the top of the winding frame 502 is fixedly connected with a motor 504, the output end of the motor 504 is fixedly connected with the winding disc 503, and the top of the delivery frame 1 is rotatably connected with a plurality of guide wheels 505 corresponding to the T-shaped traction rope 501.

[0045] The winding disc 503 is driven by the motor 504, the rotating winding disc 503 can wind the two T-shaped traction ropes 501, the two T-shaped traction ropes 501 being continuously wound can simultaneously pull all the pulling discs 405, the pulling discs 405 pull the locking pieces 402 through the pulling plates 403, and the locking pieces 402 are in contact with the outer surface of the supporting pipe 302; since the guide wheels 505 are arranged at positions where the T-shaped traction ropes 501 need to be turned, the T-shaped traction ropes 501 have high stability when moving under the guidance of the guide wheels 505; when the locking of the supporting pipe 302 needs to be released, the winding disc 503 is reversely rotated under the driving of the motor 504, the T-shaped traction ropes 501 wound on the outer surface of the winding disc 503 continuously move out, and the traction force of the T-shaped traction ropes 501 on the pulling discs 405 continuously decreases, at this time, the locking spring 406 can pull the pulling disc 405, so that the pulling disc 405 pushes the locking piece 402 through the pulling plate 403, and the locking piece 402 is separated from the outer surface of the supporting pipe 302.

[0046] In one embodiment, for the above-mentioned delivery frame 1, a plurality of mounting frames 6 are fixedly installed on the top of the delivery frame 1.

[0047] The fixing bolt can install the mounting frame 6 on the support at the bottom of the unmanned aerial vehicle through the fixing hole arranged on the mounting frame 6, since the unmanned aerial vehicle and the mounting frame 6 are rigidly connected together, the stability of the unmanned aerial vehicle when moving in flight through the mounting frame 6 driving the delivery frame 1 can be guaranteed.

[0048] By the above technical scheme, 1, when the delivery frame 1 is placed on the ground by the unmanned aerial vehicle, the support end on the elastic support assembly 3 that first contacts the ground can continuously move upward, so that the support end of the other elastic support assembly 3 can be in contact with the ground in turn, then the locking assembly 4 is pulled by the traction assembly 5, and the locking assembly 4 can lock the support end. The above arrangement makes it not easy for the delivery frame to tilt when it is placed on the uneven ground, effectively avoids the risk of center of gravity deviation when the unmanned aerial vehicle lands, even the risk of body shaking, rollover and the like, so that the stability of the unmanned aerial vehicle during landing can be ensured; 2, the motor 504 drives the winding disc 503, the rotating winding disc 503 can wind the two T-shaped traction ropes 501 at the same time, and the two continuously wound T-shaped traction ropes 501 pull all the pulling discs 405 at the same time, so that the pulling disc 405 pulls the locking piece 402 through the pulling plate 403, so that the locking piece 402 contacts and locks the outer surface of the support pipe 302; the above arrangement only needs to drive the motor 504 when locking the plurality of support pipes 302, which is relatively convenient to operate, and the T-shaped traction rope 501 is used as a transmission medium, which effectively reduces the overall weight of the delivery frame 1 compared with the traditional rigid connecting rod structure, and realizes the lightweight design goal under the premise of ensuring the structural strength.

[0049] In the description of the present specification, the description of the terms "one embodiment", "example", "specific example" and the like means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are contained in at least one embodiment or example of the utility model. In the present specification, the illustrative description of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner.

[0050] The above disclosed utility model preferred embodiment is only used to help explain the utility model. The preferred embodiment does not describe all the details and limit the utility model to the specific implementation described. Obviously, according to the content of the specification, many modifications and changes can be made. The specification selects and describes these embodiments in order to better explain the principles and practical application of the utility model, so that the person skilled in the art can well understand and use the utility model. The utility model is limited by the claims and the whole scope and equivalents thereof.

Claims

1. An unmanned aerial vehicle wind load resistant cargo stabilizing delivery rack, comprising a delivery rack (1), characterized in that, The front of the delivery frame (1) is provided with a shielding assembly (2), the inside of the delivery frame (1) is provided with a plurality of elastic support assemblies (3), the support end of the elastic support assembly (3) extends to the bottom of the delivery frame (1), the support end of the corresponding elastic support assembly (3) of the delivery frame (1) is provided with a locking assembly (4), the top of the delivery frame (1) is provided with a traction assembly (5), the traction end of the traction assembly (5) is connected with the locking assembly (4). The support end of the plurality of elastic support assemblies (3) moves under the action of the gravity of the delivery frame (1) and the internal substance, so that the plurality of support ends are in contact with the ground, and the traction assembly (5) is used for pulling the locking assembly (4), so that the locking assembly (4) locks the completed support end.

2. The wind-resistant payload stabilizing delivery rack of claim 1, wherein, The shielding assembly (2) comprises a shielding frame (201), one side of the shielding frame (201) is rotatably connected with the delivery frame (1), the other side of the shielding frame (201) movably connects with an L-shaped moving plate (202), the inner wall of the shielding frame (201) is fixedly connected with a guide rod (203), the outer surface of the guide rod (203) movably connects with a connecting plate (204), one side of the L-shaped moving plate (202) movably connects with the connecting plate (204), the outer side of the delivery frame (1) is provided with a fixed groove (205), the inside of the fixed groove (205) movably connects with a fixed plate (206), and the fixed plate (206) is fixedly connected with the L-shaped moving plate (202).

3. The wind-resistant payload stabilizing delivery rack of claim 2, wherein, The connecting plate (204) is fixedly connected with the inner wall of the delivery frame (1) on one side, and the other side of the L-shaped moving plate (202) is fixedly connected with a pulling frame (208).

4. The wind-resistant payload stabilizing delivery rack of claim 1, wherein, The elastic support assembly (3) comprises a receiving cavity (301), a plurality of receiving cavities (301) are formed in the inside of the delivery frame (1), the inside of the receiving cavity (301) is fixedly connected with a movable support pipe (302), the bottom end of the support pipe (302) extends to the outside of the delivery frame (1), the inner wall top of the receiving cavity (301) is fixedly connected with a fixed rod (303), the fixed rod (303) is movably connected with the support pipe (302), the top end of the support pipe (302) is fixedly connected with a pushing disc (304), and the pushing disc (304) is fixedly connected with the inner wall top of the receiving cavity (301) through a pushing spring (305).

5. The wind-resistant payload stabilizing delivery rack of claim 4, wherein, The locking assembly (4) comprises a mounting cavity (401) which is opened in the inner wall of the receiving cavity (301), the inside of the mounting cavity (401) is movably connected with a locking sheet (402), the inner wall of the locking sheet (402) is fixedly connected with a pulling plate (403), one side of the pulling plate (403) penetrates through the fixed rod (303) and extends to the outside of the release frame (1), the outer surface of the supporting pipe (302) is provided with a through slot (404) corresponding to the pulling plate (403), one side of the pulling plate (403) is fixedly connected with a pulling disc (405), the pulling disc (405) and the release frame (1) are fixedly connected with a locking spring (406), the inner wall of the locking sheet (402) and the outer surface of the supporting pipe (302) are both provided with a friction groove (407).

6. The wind-resistant payload stabilizing delivery rack of claim 5, wherein, The traction assembly (5) comprises two T-shaped traction ropes (501), both ends of the two T-shaped traction ropes (501) are fixedly connected with the corresponding pulling disc (405), the top of the release frame (1) is fixedly installed with a winding frame (502), the inside of the winding frame (502) is rotatably connected with a winding disc (503), the top end of the T-shaped traction rope (501) penetrates through the release frame (1) and is fixedly connected with the winding disc (503), the top of the winding frame (502) is fixedly connected with a motor (504), the output end of the motor (504) is fixedly connected with the winding disc (503), the top of the release frame (1) and the inner wall are rotatably connected with a plurality of guide wheels (505) corresponding to the T-shaped traction rope (501).

7. The wind-resistant payload stabilizing delivery rack of claim 1, wherein, The top of the release frame (1) is fixedly installed with a plurality of mounting frames (6).

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