Automatic cargo delivery system and method in unmanned aerial vehicle cabin
The automatic cargo delivery system for UAVs addresses the safety risks in human-operated missions by automating material delivery and storage, ensuring safe and efficient airdrop operations.
Patent Information
- Application Number
- CN202211311813.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-10-25
- Publication Date
- 2024-12-13
- Estimated Expiration
- 2042-10-25
AI Technical Summary
Current long-distance firefighting and rescue, airdrop, and air delivery missions rely on human crews, posing risks to their life safety under harsh conditions.
An automatic cargo delivery system for unmanned aerial vehicles (UAVs) comprising a material delivery structure and storage structure, utilizing a delivery platform, double-row module, propulsion limit locks, and guide rails to automate the delivery and storage of materials within the UAV cabin.
Ensures the safety of pilots and crew by enabling automated cargo delivery and storage, enhancing mission success rates and standardizing delivery operations.
Smart Images

Figure CN115447778B_ABST
Abstract
Description
Technical Field
[0001] The present invention belongs to the field of aviation and airborne equipment, and in particular relates to a system and method for automatically delivering cargo in an unmanned aircraft cabin. Background Art
[0002] Long-distance firefighting and rescue, airdrop and air delivery missions under severe conditions are very important mission objectives in the aviation field. They are not only related to the emergency response speed and implementation of response plans at the critical moment of disaster prevention and control, but also related to the national defense security guarantee under special circumstances. Traditionally, long-distance firefighting and rescue, airdrop and air delivery missions under severe conditions are carried out by the pilot driving the aircraft and the crew to the designated location, and then the crew will carry out the firefighting and rescue and the targeted delivery of materials.
[0003] The current way of executing this task relies on the driver and crew to deliver materials, which often poses a certain risk to the life safety of the driver and crew during material delivery under harsh conditions. Summary of the invention
[0004] The purpose of the present invention is to provide a system and method for automatically delivering cargo in an unmanned aircraft cabin, so as to solve the problem that the prior art relies on the driver and crew to deliver materials, and the life safety of the driver and crew cannot be guaranteed.
[0005] In order to achieve the above object, the present invention adopts the following technical solution:
[0006] According to a first aspect of the present invention, there is provided a system for automatically delivering cargo to an unmanned aerial vehicle cabin, comprising: a material delivery structure and a material storage structure; the material delivery structure is located inside the cabin of the unmanned aerial vehicle and directly faces the cabin door of the unmanned aerial vehicle, and is used for delivering materials to be delivered; the material storage structure is located inside the cabin of the unmanned aerial vehicle along the heading direction, and is used for storing materials in a storage area, and after the material delivery structure delivers the materials to be delivered, the materials in the storage area are transported to the material delivery structure.
[0007] As an optional solution of the present invention, the material delivery structure includes a delivery platform and a double-row module;
[0008] The surface of the delivery platform is used to place materials to be delivered;
[0009] The double-row module is installed at the lower position of the delivery platform, and a delivery push rod assembly is provided at one end of the double-row module away from the drone cabin door. A slide groove is provided on the delivery platform, and the middle part of the delivery push rod assembly is arranged in the slide groove; the upper part of the delivery push rod assembly is located above the delivery platform, and is used for pushing the materials to be delivered toward the drone cabin door to achieve delivery under the drive of the double-row module.
[0010] As an optional solution of the present invention, a propulsion limit lock and a long guide rail of the delivery area are arranged on both sides of the delivery platform. The propulsion limit lock is used to advance or retract in the direction of the long guide rail of the delivery area, thereby limiting or releasing the materials to be delivered; the long guide rail of the delivery area is used to limit the movement direction of the materials to be delivered.
[0011] As an optional solution of the present invention, a delivery limit lock is provided at one end of the delivery platform close to the UAV cabin door, which is used to limit the position of the materials to be delivered before the delivery begins.
[0012] As an optional solution of the present invention, the double-row module includes a belt transmission module, a slide and a drive assembly;
[0013] The slide is mounted on the belt transmission module, and the drive assembly is used to drive the belt transmission module to achieve linear reciprocating motion of the slide on the belt transmission module.
[0014] As an optional solution of the present invention, a double-row module connecting base is connected to the bottom of the belt transmission module, and the double-row module connecting base is used to fix the position of the belt transmission module.
[0015] As an optional solution of the present invention, the material storage structure includes a side rail assembly, a bottom rail and a power output unit;
[0016] The side guide rail assembly includes two side guide rails that are arranged opposite to each other, and the outlet of the side guide rail assembly is opposite to the position of the delivery platform; the bottom guide rail is arranged between the two side guide rails and parallel to the side guide rails, and is used to carry and transport materials in the storage area; the power output unit is arranged between the two side guide rails, and is used to drive the materials in the storage area to move along the bottom guide rail toward the delivery platform.
[0017] As an optional solution of the present invention, the propulsion limit lock includes an electric limit lock, a linear module and a stepping motor;
[0018] The electric limit lock includes a lock seat and a lock tongue. The lock seat is provided with a lock tongue mounting groove along the top downward. The first end of the lock tongue is mounted in the lock tongue mounting groove in a manner that it can be driven to rotate by a motor, and the lock tongue can be received in the lock tongue mounting groove and extend out of the lock tongue mounting groove in the vertical direction when rotating. The lock seat is slidably mounted on the linear module and is connected to the output end of the stepper motor.
[0019] As an optional solution of the present invention, the delivery push rod assembly includes a delivery push plate and a push plate column; the delivery push plate is installed on the first end of the push plate column for pushing the materials to be delivered, and the second end of the push plate column is fixed on the slide.
[0020] A second aspect of the present invention provides a method for automatically placing cargo in an unmanned aircraft cabin, based on the above-mentioned automatic cargo placing system in an unmanned aircraft cabin, comprising the following steps:
[0021] The stepper motor that pushes the limit lock is retracted, and the lock tongue is released to allow materials to be released;
[0022] The driving assembly drives the belt transmission module to move, and the slide moves on the belt transmission module along a straight line toward the door of the UAV cabin; then the slide drives the delivery push rod assembly to move, and the delivery push rod assembly pushes the materials to be delivered to move toward the door of the UAV cabin;
[0023] After the materials are successfully delivered, the power output unit drives the materials in the storage area to move along the direction of the side guide rail combination on the bottom guide rail to the push limit lock. At this time, the lock tongue of the push limit lock rotates and retracts into the lock tongue mounting groove of the lock seat, and then the power output unit continues to drive the materials in the storage area until the materials in the storage area are transported to the delivery platform; at this time, the lock tongue of the push limit lock rotates and extends out of the lock tongue mounting groove of the lock seat, and the stepper motor of the push limit lock extends out, driving the lock tongue to press the storage area materials on the delivery platform, waiting for the next material delivery.
[0024] Compared with the prior art, the present invention has the following beneficial effects:
[0025] 1) The automatic cargo delivery system provided by the present invention includes a material delivery structure and a material storage structure arranged in an unmanned aerial vehicle. By carrying materials on the unmanned aerial vehicle and automatically delivering the materials using the material delivery structure, and storing materials in the material storage structure, a large unmanned aerial vehicle can automatically perform an airdrop mission on the onboard materials, replacing the pilot flying the aircraft to perform a long-distance airdrop mission, thereby ensuring the life safety of the pilot and crew members.
[0026] 2) The automatic cargo delivery system provided by the present invention, wherein the material delivery structure is connected to the material storage structure. After the material delivery structure successfully delivers the materials, the material storage structure can automatically transport the stored materials to the material delivery structure, thereby realizing continuous delivery of the materials. BRIEF DESCRIPTION OF THE DRAWINGS
[0027] The drawings constituting a part of the present application are used to provide a further understanding of the present invention. The exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an improper limitation of the present invention. In the drawings:
[0028] Figure 1 1 is a schematic diagram of the installation state of the automatic cargo delivery system according to an embodiment of the present invention;
[0029] Figure 2 It is a schematic diagram of the material storage structure and the material delivery structure in an embodiment of the present invention;
[0030] Figure 3 This is a schematic diagram of the material delivery structure in an embodiment of the present invention;
[0031] Figure 4 is a top view of the material delivery structure in an embodiment of the present invention;
[0032] Figure 5 This is a schematic diagram of material delivery in an embodiment of the present invention;
[0033] Figure 6 It is a structural diagram of a double-row module in an embodiment of the present invention;
[0034] Figure 7 This is a schematic diagram of a double-row module belt transmission in an embodiment of the present invention;
[0035] Figure 8 1 is a structural diagram of a delivery push rod assembly in an embodiment of the present invention;
[0036] Fig. 9 It is a schematic diagram of the thrust limit lock in an embodiment of the present invention.
[0037] Among them: 1-UAV cabin; 2-automatic cargo delivery system; 3-UAV cabin door; 4-material storage structure; 5-material delivery structure; 6-materials to be delivered; 7-short guide rail in delivery area; 8-side guide rail combination; 9-bottom guide rail; 10-power output unit; 11-advance limit lock; 12-delivery push rod assembly; 13-delivery platform; 14-double-row module; 15-long guide rail in delivery area; 16-delivery limit lock; 17-materials in storage area; 18-belt drive module; 19-double-row module connecting base; 20-slide; 21-servo motor; 22-reducer; 23-module connecting shaft; 24-driving pulley; 25-driven pulley; 26-synchronous belt; 27-delivery push plate; 28-push plate reinforcement rib; 29-push plate column; 30-electric limit lock; 31-linear module; 32-stepping motor; 301-lock tongue; 302-lock seat. DETAILED DESCRIPTION
[0038] The present invention will be described in detail below with reference to the accompanying drawings and in combination with embodiments. It should be noted that the embodiments and features in the embodiments of the present application can be combined with each other without conflict.
[0039] The following detailed description is an exemplary description, which is intended to provide further detailed description of the present invention. Unless otherwise specified, all technical terms used in the present invention have the same meaning as those generally understood by those skilled in the art to which the present application belongs. The terms used in the present invention are only for describing specific embodiments, and are not intended to limit exemplary embodiments according to the present invention.
[0040] The embodiment of the present invention aims at the defects and deficiencies in the execution of long-distance airdrop and air delivery tasks under the current harsh conditions, and provides a cargo automatic delivery system in the cabin of an unmanned aircraft. The cargo automatic delivery system is installed in the cabin of an unmanned aircraft to realize the automatic delivery of cargo in the cabin of an unmanned aircraft. The life safety problem of the pilot and crew members when the aircraft performs an airdrop mission under harsh conditions is solved, and the intelligent implementation of the airdrop mission is realized, so that the implementation of the delivery mission can be standardized, thereby improving the delivery success rate.
[0041] like Figure 1 and Figure 2 As shown, a cargo automatic delivery system in an unmanned aerial vehicle cabin, the cargo automatic delivery system 2 is installed on the cabin floor inside the unmanned aerial vehicle cabin 1, and the cargo automatic delivery system 2 includes: a material delivery structure 5 and a material storage structure 4; the material delivery structure 5 is located inside the unmanned aerial vehicle cabin 1 and directly faces the unmanned aerial vehicle cabin door 3, and is used to deliver materials 6 to be delivered; the material storage structure 4 is located inside the unmanned aerial vehicle cabin 1 along the heading direction, and is used to store materials 17 in the storage area, and after the material delivery structure 5 delivers the materials 6 to be delivered, the storage area materials 17 are transported to the material delivery structure 5.
[0042] like Figure 3 and Figure 4 As shown, the material delivery structure 5 includes a delivery platform 13 and a double-row module 14; the surface of the delivery platform 13 is used to place the materials 6 to be delivered; the double-row module 14 is installed at the lower position of the delivery platform 13, and the two may not be in contact. When the double-row module 14 moves, it will not drive the delivery platform 13 to move together. A delivery push rod assembly 12 is provided at one end of the double-row module 14 away from the unmanned aerial vehicle cabin door 3; a slide groove is provided on the delivery platform 13, and the slide groove penetrates the upper and lower surfaces of the delivery platform 13, and is arranged on the delivery platform 13 along a straight line toward the direction of the unmanned aerial vehicle cabin door, and the middle part of the delivery push rod assembly 12 is vertically arranged in the slide groove; the upper part of the delivery push rod assembly 12 is located above the delivery platform 13, and is used to push the materials 6 to be delivered on the delivery platform 13 toward the direction of the unmanned aerial vehicle cabin door 3 under the drive of the double-row module 14 to achieve delivery. The two sides of the delivery platform 13 are provided with a push limit lock 11 and a delivery zone long guide rail 15. The push limit lock 11 is used to push or retract in the direction of the delivery zone long guide rail 15, thereby limiting or releasing the materials to be delivered 6; the delivery zone long guide rail 15 is used to limit the movement direction of the materials to be delivered 6, so that the delivery push rod assembly 12 pushes the materials in the direction of the drone cabin door. A delivery limit lock 16 is provided at one end of the delivery platform 13 close to the drone cabin door 3, which is used to limit the materials to be delivered 6 before delivery begins.
[0043] Through the above-mentioned arrangement, the propulsion limit lock 11, the delivery push rod assembly 12, the delivery area long guide rail 15, and the delivery limit lock 16 can limit and lock the posture of the material 6 to be delivered before delivery, and can also correct the material. In this way, it can be ensured that each time the material is delivered, it can be delivered in a fixed preset posture and position, thereby ensuring the delivery success rate.
[0044] In a preferred embodiment, a short guide rail 7 is also provided in the delivery area. The short guide rail 7 is arranged opposite to the long guide rail 15 in the delivery area. The short guide rail 7 in the delivery area is located on a side close to the cabin door of the drone and is used for the delivery of auxiliary materials.
[0045] like Figure 6 and Figure 7 As shown, the double-row module 14 includes a belt drive module 18, a slide 20 and a drive assembly; the slide 20 is mounted on the belt drive module 18, and the drive assembly is used to drive the belt drive module 18 so as to realize the slide 20 to reciprocate along a straight line on the belt drive module 18. The bottom of the belt drive module 18 is connected to a double-row module connecting base 19, and the double-row module connecting base 19 is used to fix the position of the belt drive module 18.
[0046] As a specific example of the above embodiment, the driving assembly includes a servo motor 21, a reducer 22, a module connecting shaft 23, a driving pulley 24, a driven pulley 25 and a synchronous belt 26. The servo motor 21 inputs power into the driving pulley 24 through the reducer 22 and the module connecting shaft 23. The driving pulley 24 drives the synchronous belt 26 to move, and the synchronous belt 26 then transmits the motion to the slide 20 and the driven pulley 25.
[0047] Through the above arrangement, the reducer 22 can increase the torque input into the driving pulley 24, and the belt transmission can increase the lead of the module, thereby increasing the running speed of the slide. Therefore, the reducer 22 and the belt transmission module 18 are used in combination to increase the weight of a single material delivery and the speed of the material delivery out of the cabin. The two belt transmission modules 18 are directly connected through the module connection shaft 23, thereby ensuring the synchronization of the movement of the two belt transmission modules 18.
[0048] As a specific example, the servo motor 21 can be a DC motor. By setting the power output mode to a DC motor acceleration and reduction gear, a large torque output can be achieved under the onboard power supply condition (DC28V). This can increase the thrust of the cargo delivery device and can adapt to a larger single delivery weight of materials.
[0049] At the same time, the delivery execution functional component is belt-driven (the power is output from the servo motor and the reducer to the synchronous pulley at the drive end, the driving pulley transmits the motion to the synchronous belt, and the synchronous belt drives the driven pulley to rotate, forming the structure of the entire delivery execution functional component). This can achieve the large lead operation of the delivery execution functional component, thereby achieving low speed of the input drive pulley, and the module slide can output high linear speed. In addition, the delivery method adopts a double-row module structure. The two-row modules are connected in parallel through the transmission shaft to realize a power input to the double-row modules. The double-row modules can move synchronously, which can improve the stability of the cargo when it needs to be delivered at a short distance and high speed when exiting the hatch.
[0050] As a preferred embodiment of the above embodiment, three double-row module connecting bases 19 are respectively connected to the front, middle and rear positions of the two belt drive modules 18, so as to ensure the parallelism of the two belt drive modules 18 along the movement direction. The two belt drive modules 18 can be used in parallel to ensure stability during high-speed delivery.
[0051] When materials are delivered, the delivery limit lock 16 is unlocked, the servo motor 21 drives the double-row module 14 to work, and the delivery push rod assembly 12 installed on the slide 20 pushes the materials 6 to be delivered out of the cabin from the drone cabin door 3 to complete the delivery task.
[0052] like Figure 3 to Figure 5 As shown, the material storage structure 4 includes a side guide rail assembly 8, a bottom guide rail 9 and a power output unit 10; the side guide rail assembly 8 includes two oppositely arranged side guide rails, and the outlet of the side guide rail assembly 8 is opposite to the position of the delivery platform 13; the bottom guide rail 9 is arranged between the two side guide rails and parallel to the side guide rails, and is used to carry and transport the storage area materials 17; the power output unit 10 is arranged between the two side guide rails, and is used to drive the storage area materials 17 to move along the bottom guide rail 9 toward the delivery platform 13.
[0053] It should be noted that the power output unit 10 mentioned in this solution can also be configured as a structure similar to a double-row module, or adopt other types of transmission structures in the field, which will not be described in detail here.
[0054] After the materials to be delivered 6 are delivered out of the cabin, the propulsion limit lock 11 cooperates with the power output unit 10 to provide transfer power for the storage area materials 17 of the material storage structure 4, and the side guide rail assembly 8 and the bottom guide rail 9 can ensure that the storage area materials 17 are transferred according to the planned route, so that the storage area materials 17 can be smoothly transferred to the delivery platform 13. At this time, the delivery limit lock 16 is locked, and the posture of the storage area materials 17 transferred to the delivery platform 13 can be locked in cooperation with the propulsion limit lock 11, the delivery push rod assembly 12, and the delivery area long guide rail 15. At this time, the storage area materials 17 enter the waiting delivery state. Repeating the above actions can realize the fixed-point airdrop and air delivery task of all materials inside the automatic cargo delivery system 2.
[0055] like Figure 8 As shown, the delivery push rod assembly 12 includes a delivery push plate 27 and a push plate column 29; the delivery push plate 27 is installed on the first end of the push plate column 29 by bolts, and is used to push the materials to be delivered 6, and the second end of the push plate column 29 is fixed to the slide 20 by bolts. In the preferred embodiment, a push plate reinforcement rib 28 is also provided, and the push plate reinforcement rib 28 is connected to the delivery push plate 27 and the push plate column 29 by bolts, and is locked with the delivery push plate 27 and the push plate column 29 through its own "concave" shape structure, so as to realize structural force and ensure the strength of the delivery push rod assembly 12. The delivery push rod assembly 12 realizes the separation of the delivery execution function component and the delivery materials through a simple and compact structure.
[0056] like Fig. 9 As shown, the push limit lock 11 includes an electric limit lock 30, a linear module 31 and a stepper motor 32; the electric limit lock 30 includes a lock seat 302 and a lock tongue 301, the lock seat 302 is provided with a lock tongue mounting groove along the top downward, the first end of the lock tongue 301 is installed in the lock tongue mounting groove in a manner that it can be driven to rotate by a motor, and the lock tongue 301 can be received in the lock tongue mounting groove and extend out of the lock tongue mounting groove in the vertical direction when rotating; the lock seat 302 is slidably installed on the linear module 31 and connected to the output end of the stepper motor 32; by controlling the stepper motor 32, the forward and backward movement of the electric limit lock 30 in the stroke direction of the linear module 31 can be controlled, thereby realizing the function of the push limit lock 11 to push and lock the position of the materials 17 in the storage area.
[0057] Example 2
[0058] A method for automatically delivering cargo in an unmanned aircraft cabin, based on the above-mentioned automatic delivery system for cargo in an unmanned aircraft cabin, comprises the following steps:
[0059] Before the materials are released, the propulsion limit lock 11, the release push rod assembly 12, the release zone long guide rail 15, and the release limit lock 16 are used to limit and lock the posture of the materials 6 to be released before release.
[0060] When delivering, the stepping motor 32 that pushes the limit lock 11 is retracted, and the lock tongue 301 releases the material 6 to be delivered; and the delivery limit lock 16 releases the lock on the material 6 to be delivered.
[0061] The driving assembly drives the belt transmission module 18 to move, and the slide 20 moves on the belt transmission module 18 along a straight line toward the drone cabin door 3; then the slide 20 drives the delivery push rod assembly 12 to move, and the delivery push rod assembly 12 pushes the material to be delivered 6 to move toward the drone cabin door 3, pushing the material to be delivered 6 out of the drone cabin to achieve delivery.
[0062] After the delivery of the to-be-delivered material 6 is successful, the power output unit 10 drives the storage area material 17 to move on the bottom guide rail 9 along the direction of the side guide rail assembly 8 to the push-limit lock 11. At this time, the lock tongue 301 of the push-limit lock 11 rotates and retracts into the lock tongue mounting groove of the lock seat 302, and then the power output unit 10 continues to drive the storage area material 17 until the storage area material 17 is transported to the delivery platform 13; at this time, the lock tongue 301 of the push-limit lock 11 rotates and extends out of the lock tongue mounting groove of the lock seat 302, and the stepper motor 32 of the push-limit lock 11 extends out, driving the lock tongue 301 to press the storage area material 17 on the delivery platform 13, waiting for the next delivery of materials.
[0063] It is known from common technical knowledge that the present invention can be implemented by other embodiments that do not deviate from its spirit or essential features. Therefore, the above disclosed embodiments are only illustrative in all respects and are not exclusive. All changes within the scope of the present invention or within the scope equivalent to the present invention are included in the present invention.
Claims
1. An automatic cargo delivery system in an unmanned aircraft cabin, characterized in that: include: A material delivery structure (5) and a material storage structure (4); the material delivery structure (5) is located inside the cabin of the unmanned aerial vehicle (1) and directly facing the cabin door (3) of the unmanned aerial vehicle, and is used to deliver materials to be delivered (6); the material storage structure (4) is located inside the cabin of the unmanned aerial vehicle (1) along the heading direction, and is used to store materials in the storage area (17); and after the material delivery structure (5) delivers the materials to be delivered (6), the materials in the storage area (17) are transported to the material delivery structure (5); The material delivery structure (5) comprises a delivery platform (13) and a double-row module (14); The surface of the delivery platform (13) is used for placing materials (6) to be delivered; The double-row module (14) is installed at a position below the delivery platform (13); a delivery push rod assembly (12) is provided at one end of the double-row module (14) away from the drone cabin door (3); a slide groove is provided on the delivery platform (13); the middle part of the delivery push rod assembly (12) is arranged in the slide groove; the upper part of the delivery push rod assembly (12) is located above the delivery platform (13) and is used for pushing the materials (6) to be delivered toward the drone cabin door (3) to achieve delivery under the drive of the double-row module (14); A propulsion limit lock (11) and a long guide rail (15) for the delivery area are arranged on both sides of the delivery platform (13) in a relative manner. The propulsion limit lock (11) is used to be pushed or retracted in the direction of the long guide rail (15) for the delivery area, thereby limiting or releasing the material (6) to be delivered; the long guide rail (15) for the delivery area is used to limit the movement direction of the material (6) to be delivered; The double-row module (14) comprises a belt transmission module (18), a slide table (20) and a drive assembly; The slide table (20) is mounted on the belt transmission module (18), and the drive assembly is used to drive the belt transmission module (18) to thereby realize linear reciprocating motion of the slide table (20) on the belt transmission module (18); The material storage structure (4) comprises a side guide rail assembly (8), a bottom guide rail (9) and a power output unit (10); The side guide rail assembly (8) comprises two side guide rails arranged opposite to each other, and an outlet of the side guide rail assembly (8) is directly opposite to the position of the delivery platform (13); the bottom guide rail (9) is arranged between the two side guide rails and is arranged parallel to the side guide rails, and is used to carry and transport the storage area materials (17); the power output unit (10) is arranged between the two side guide rails, and is used to drive the storage area materials (17) to move along the bottom guide rail (9) toward the delivery platform (13); The propulsion limit lock (11) comprises an electric limit lock (30), a linear module (31) and a stepping motor (32); The electric limit lock (30) comprises a lock seat (302) and a lock tongue (301); the lock seat (302) is provided with a lock tongue installation groove along the top downward; the first end of the lock tongue (301) is installed in the lock tongue installation groove in a manner that it can be driven to rotate by a motor, and the lock tongue (301) can be received in the lock tongue installation groove and extend out of the lock tongue installation groove in a vertical direction when rotating; the lock seat (302) is slidably installed on the linear module (31) and is connected to the output end of the stepping motor (32); A delivery limiting lock (16) is provided at one end of the delivery platform (13) close to the unmanned aerial vehicle cabin door (3), and is used to limit the position of the material (6) to be delivered before delivery begins.
2. The automatic cargo delivery system in the unmanned aircraft cabin according to claim 1, characterized in that: A double-row module connection base (19) is connected to the bottom of the belt transmission module (18), and the double-row module connection base (19) is used to fix the position of the belt transmission module (18).
3. The automatic cargo delivery system in the unmanned aircraft cabin according to claim 1, characterized in that: The delivery push rod assembly (12) comprises a delivery push plate (27) and a push plate column (29); the delivery push plate (27) is mounted on a first end of the push plate column (29) for pushing materials (6) to be delivered, and a second end of the push plate column (29) is fixed on the slide (20).
4. A method for automatically delivering cargo in an unmanned aircraft cabin, based on the automatic delivery system for cargo in an unmanned aircraft cabin according to claim 3, characterized in that: The steps include: The stepping motor (32) for advancing the limit lock (11) is retracted, and the lock tongue (301) releases the material to be released (6); The driving assembly drives the belt transmission module (18) to move, and the slide (20) moves on the belt transmission module (18) along a straight line toward the direction of the unmanned aerial vehicle cabin door (3); the slide (20) then drives the delivery push rod assembly (12) to move, and the delivery push rod assembly (12) pushes the material to be delivered (6) to move toward the direction of the unmanned aerial vehicle cabin door (3); After the delivery of the delivered material (6) is successful, the power output unit (10) drives the storage area material (17) to move along the direction of the side guide rail assembly (8) on the bottom guide rail (9) to the push limit lock (11), at which time the lock tongue (301) of the push limit lock (11) rotates and retracts into the lock tongue installation groove of the lock seat (302), and then the power output unit (10) continues to drive the storage area material (17) until the storage area material (17) is transported to the delivery platform (13); at this time, the lock tongue (301) of the push limit lock (11) rotates and extends out of the lock tongue installation groove of the lock seat (302), and the stepping motor (32) of the push limit lock (11) extends, driving the lock tongue (301) to press the storage area material (17) on the delivery platform (13), waiting for the next delivery of materials.
