Airplane toy with container

Abstract

The utility model discloses an aircraft toy with a container. The aircraft toy comprises an aircraft body and the container. A concave cavity is formed in the bottom of the aircraft main body, a winding mechanism is arranged on the aircraft main body, the winding mechanism comprises a rotating part and a flexible part, and one end of the flexible part is wound on the rotating part. The container is connected to the other end of the flexible piece. The rotating part rotates to wind or release the flexible part, so that the container is close to or far away from the aircraft main body, and at least part of the container is contained in the concave cavity in the state that the container is in contact with the aircraft main body. According to the aircraft toy with the container, through the structural design that the aircraft body is integrated with the winding mechanism and the bottom concave cavity and the flexible part is connected with the container, the flexible part can be driven by the rotating part to be wound or released to achieve dynamic retracting and releasing of the container, a real transportation scene is restored, and the container can be contained in the concave cavity; interaction interestingness, structural stability and use convenience are all considered.

Description

Technical Field

[0001] This utility model relates to the field of toy technology, specifically to an airplane toy with a container. Background Technology

[0002] Against the backdrop of the children's toy industry's ever-increasing demands for interactivity and scene recreation, airplane toys simulating cargo transportation scenarios are increasingly becoming a market focus due to their combination of fun and educational value. These toys typically require additional components such as shipping containers to fully recreate the core processes of air transport, thereby satisfying children's curiosity about transportation and their need for immersive play.

[0003] However, existing airplane toys with container carrying functions still have many prominent defects: most products adopt a static carrying or storage design, with the container and the main body of the aircraft connected by fixed structures such as buckles and slots, which can only achieve static assembly and display, and cannot simulate dynamic actions such as cargo hoisting and dropping in the real transportation process; some other designs are separate, with the container and the main body of the aircraft completely independent, and can only be stored together in a storage box, without an integrated carrying structure of the fuselage. Not only is the interactive form limited, but there are also problems with the container being easy to lose or be damaged, making it difficult to meet children's needs for dynamic play scenarios.

[0004] Even among the few products that achieve dynamic connections, the connection mechanisms also have significant shortcomings. For example, some products use a rope hook structure, with the connecting parts directly exposed without any protection or storage design. During play, the rope is prone to tangling and jamming, and the connection stability is poor, making it easy for the container to fall off during transport or hoisting. At the same time, this type of structure is cumbersome to operate, requiring a high level of skill from children, reducing the ease of use of the toy. Furthermore, the exposed connecting parts are easily damaged by collisions and pulling, thus shortening the toy's lifespan.

[0005] In summary, existing airplane-shaped toys carrying containers generally suffer from core problems such as a lack of dynamic interaction and exposed, easily damaged structures, failing to meet users' comprehensive needs for practicality and fun. Therefore, there is an urgent need for an airplane toy with a reasonable structural design, convenient operation, and the ability to specifically address these shortcomings, thus filling the current technological gap.

[0006] In view of the above, this utility model is hereby proposed. Utility Model Content

[0007] To solve one of the above-mentioned technical problems, this utility model provides an airplane toy with a container.

[0008] This application provides the following technical solution:

[0009] An airplane toy with a shipping container, comprising:

[0010] An aircraft body, the bottom of which is provided with a cavity, and a winding mechanism is provided on the aircraft body. The winding mechanism includes a rotating component and a flexible component, one end of which is wound around the rotating component.

[0011] A container, which is connected to the other end of the flexible member;

[0012] The rotating component can rotate to wind or release the flexible component, causing the container to move closer to or away from the aircraft body. When the container is in contact with the aircraft body, the container is at least partially accommodated within the cavity.

[0013] Optionally, the main body of the aircraft includes a fuselage, a front structure, and a rear structure;

[0014] Both the front structure and the rear structure are connected to the fuselage. The front structure and the rear structure are arranged at intervals along the length of the fuselage, and the cavity is formed between the front structure and the rear structure.

[0015] When the winding mechanism lifts the container to its limit position, the container is confined between the front structure and the rear structure.

[0016] Optionally, the aircraft body includes a front wheel and a rear wheel;

[0017] The front wheel is disposed on the front structure, and the rear wheel is disposed on the rear structure.

[0018] Optionally, the aircraft body has a cavity and an operating port, the operating port is connected to the cavity, the operating port is located on the side of the aircraft body away from the concave cavity, the rotating component is located in the cavity and partially extends out of the operating port;

[0019] Alternatively, a drive mechanism may be provided within the main body of the aircraft, and the drive mechanism and the rotating component may be in a transmission cooperation to drive the rotating component to rotate.

[0020] Optionally, two support frames are provided inside the cavity of the aircraft body, and the support frames are provided with rotation holes;

[0021] The rotating component includes a winding body and rotating shafts located at both ends of the winding body;

[0022] The rotating shaft is rotatably supported by the rotating hole;

[0023] The flexible element is wound around the wound body.

[0024] Optionally, the winding body is provided with an outer flange, and the outer flange extends out of the operating port;

[0025] Multiple protruding teeth are provided on the peripheral end face of the outer flange;

[0026] A spring is installed inside the cavity of the aircraft body, and the spring can extend into the groove between adjacent protrusions to restrict the rotation of the winding body.

[0027] Optionally, the bottom wall of the cavity is provided with a wire-passing hole;

[0028] The flexible element is disposed through the wire hole.

[0029] Optionally, the container includes a container shell and connecting fittings;

[0030] The container shell surface is provided with a buckle seat;

[0031] The connecting fitting is connected to the flexible member, and the connecting fitting is detachably connected to the buckle seat.

[0032] Optionally, the connecting component has a connecting hole in the middle, and multiple snap-fit ​​pieces are provided on the peripheral edge of the connecting component;

[0033] The container shell surface is provided with multiple fastening seats, and the fastening seats have fastening slots;

[0034] When the connecting parts are rotated in the forward direction, each of the snap-fit ​​pieces can be snapped into its corresponding slot.

[0035] When the connecting parts are rotated in the opposite direction, each of the snap-fit ​​pieces disengages from its corresponding slot.

[0036] Optionally, the container shell includes a bottom plate, a three-fold panel assembly, and two side plates;

[0037] The two side plates are respectively disposed on both sides of the base plate, and the two side plates are rotatably connected to the two length sides of the base plate;

[0038] The three-fold plate assembly includes three plates that are rotatably connected in sequence. One end of the plate is hinged to a width side of the base plate, and the other end of the plate is detachably inserted into a slot on another width side of the base plate.

[0039] The buckle seat is provided on the middle plate of the three-fold plate assembly;

[0040] A catapult mechanism is provided on the base plate;

[0041] The container shell has an unfolded state, in which the plates in the three-fold panel assembly and the bottom plate are arranged in sequence to form a slide.

[0042] By adopting the above technical solution, this application has the following beneficial effects:

[0043] The airplane toy with a container in this application has a structural design that integrates a winding mechanism with a bottom cavity and flexible parts to connect the container. This design allows the container to be dynamically wound and unfolded by rotating parts driving the flexible parts to wind or release, thus recreating a real transportation scenario. It also allows the container to be stored in the cavity, thus balancing interactive fun, structural stability and ease of use. Attached Figure Description

[0044] The accompanying drawings, which form part of this application, are used to provide a further understanding of the present invention. The illustrative embodiments and descriptions of the present invention are used to explain the present invention, but do not constitute an undue limitation of the present invention. Obviously, the drawings described below are merely some embodiments, and those skilled in the art can obtain other drawings based on these drawings without any creative effort.

[0045] Figure 1 This is a schematic diagram of the structure of a containerized airplane toy provided in an embodiment of this application;

[0046] Figure 2 A schematic diagram of the main body of the containerized airplane toy provided in this application embodiment;

[0047] Figure 3 A schematic diagram of the internal structure of the fuselage of the containerized airplane toy provided in this application embodiment;

[0048] Figure 4 A schematic diagram of the internal structure of the fuselage of a containerized toy airplane with rotating parts removed, provided in an embodiment of this application.

[0049] Figure 5 A schematic diagram of the rotating component of the containerized airplane toy provided in this embodiment of the application;

[0050] Figure 6 This is a schematic diagram of the structure of the container for the toy airplane provided in the embodiments of this application;

[0051] Figure 7 A schematic diagram of the container shell of the toy airplane provided in this application embodiment;

[0052] Figure 8 A schematic diagram of the connecting and mating parts of the containerized airplane toy provided in this application embodiment;

[0053] Figure 9 A schematic diagram of the container shell of the toy airplane provided in this application in its unfolded state;

[0054] Figure 10This is a schematic diagram of the ejector detaching from the chuck in the unfolded state of the container shell of the toy airplane provided in this application embodiment.

[0055] In the diagram: Aircraft body 1, fuselage 11, front structure 12, rear structure 13, cavity 14, wire hole 141, front wheel 15, rear wheel 16, operating port 17, support frame 18, rotating hole 181, spring 19, container 2, container shell 21, bottom plate 211, slide 2111, slot 2112, three-fold plate assembly 212, buckle seat 2121, slot 2121a, side plate 213, connecting mating part 22, connecting hole 221, snap-fit ​​mating piece 222, winding mechanism 3, rotating part 31, winding body 311, outer flange 3111, tooth 3111a, rotating shaft 312, ejection mechanism 4, pressing key 41, claw 411, ejection part 42, slider 421, push block 422, mating claw 4221. Detailed Implementation

[0056] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions in the embodiments will be clearly and completely described below with reference to the accompanying drawings. The following embodiments are used to illustrate this utility model, but are not intended to limit the scope of this utility model.

[0057] In the description of this utility model, it should be noted that the terms "upper", "lower", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0058] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation" and "connection" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0059] See Figures 1 to 10As shown in the illustration, this application provides an airplane toy with a container 2, comprising: an airplane body 1 and a container 2. A cavity 14 is provided at the bottom of the airplane body 1, and a winding mechanism 3 is provided on the airplane body 1. The winding mechanism 3 includes a rotating component 31 and a flexible component (not shown), one end of which is wound around the rotating component 31. The container 2 is connected to the other end of the flexible component. The rotating component 31 can rotate to wind or release the flexible component, causing the container 2 to move closer to or away from the airplane body 1. When the container 2 is in contact with the airplane body 1, the container 2 is at least partially contained within the cavity 14. The flexible component can be any one of flexible rope, nylon rope, polyester rope, braided rope, steel wire rope, flexible strip, or flexible cable. One end of the flexible component is fixedly connected to the winding body 311 of the rotating component 31, and the other end is connected to the connecting fitting 22 of the container 2 to realize the suspension and retraction of the container 2. The airplane toy with container 2 in this application has a structural design that integrates a winding mechanism 3 with a bottom cavity 14 and a flexible component to connect the container 2. This design allows the container 2 to be dynamically wound and unfolded by driving the flexible component to wind or release through the rotating component 31, thus recreating a real transportation scenario. It also allows the container 2 to be stored in the cavity 14, thus taking into account the interactive fun, structural stability and ease of use.

[0060] like Figure 1 and Figure 2 As shown, the aircraft body 1 includes a fuselage 11, a front structure 12, and a rear structure 13. The front structure 12 and the rear structure 13 are both connected to the fuselage 11. The front structure 12 and the rear structure 13 are arranged sequentially at intervals along the length direction of the fuselage 11. The cavity 14 is formed between the front structure 12 and the rear structure 13. When the winding mechanism 3 lifts the container 2 to the limit position, the container 2 is confined between the front structure 12 and the rear structure 13, which further improves the stability of the container 2 during the carrying process, avoids displacement or collision with the fuselage 11, and enhances the synergistic effect of storage and dynamic functions.

[0061] In one possible implementation, such as Figure 2 As shown, the aircraft body 1 includes a front wheel 15 and a rear wheel 16. The front wheel 15 is disposed on the front structure 12, and the rear wheel 16 is disposed on the rear structure 13. This provides a stable and reliable mounting position for the front wheel 15 and the rear wheel 16, and also makes the mounting position of the front wheel 15 and the rear wheel 16 closer to the ground, thereby lowering the overall center of gravity of the aircraft body 1 and improving the stability of the toy when placed and driven.

[0062] like Figure 1 and Figure 3As shown, the aircraft body 1 has a cavity and an operating port 17. The operating port 17 communicates with the cavity and is located on the side of the aircraft body 1 opposite to the recessed cavity 14. The rotating component 31 is located inside the cavity and partially extends out of the operating port 17. The rotating component 31 is completely housed within the cavity of the aircraft body 1 and is manually operated by the user only through the operating port 17. This effectively avoids the problems of entanglement and collision damage caused by the exposed rotating component 31 and connecting ropes, improving the safety and durability of the overall toy structure. Alternatively, a drive mechanism (not shown) is provided inside the aircraft body 1. The drive mechanism and the rotating component 31 are driven together to drive the rotating component 31 to rotate. The drive mechanism may include a drive motor and a transmission gear system. The output shaft of the drive motor is connected to the input gear of the transmission gear system, and the output of the transmission gear system is driven together with the rotating component 31 to drive the rotating component 31 to rotate in the forward or reverse direction. When the rotating component 31 rotates in the forward direction, it winds the flexible component, causing the container 2 to move closer to the aircraft body 1 and be stored in the cavity 14. When the rotating component 31 rotates in the reverse direction, it releases the flexible component, causing the container 2 to move away from the aircraft body 1, thereby realizing the dynamic opening and closing of the container 2.

[0063] In one possible implementation, such as Figure 3 and Figure 4 As shown, two support frames 18 are provided inside the cavity of the aircraft body 1. Each support frame 18 has a rotating hole 181. The rotating component 31 includes a winding body 311 and rotating shafts 312 located at both ends of the winding body 311. The rotating shafts 312 are rotatably supported by the rotating holes 181, and the flexible component is wound around the winding body 311. The support frames 18 and the rotating holes 181 provide rotational support for the rotating shafts 312, making the rotation of the winding body 311 more stable and reliable, effectively ensuring the smooth winding and unwinding of the flexible component.

[0064] like Figure 3 , Figure 4 and Figure 5As shown, the winding body 311 is provided with an outer flange 3111, a portion of which extends out of the operating opening 17. Multiple protruding teeth 3111a are provided on the peripheral end face of the outer flange 3111. A spring piece 19 is provided within the cavity of the aircraft body 1. The spring piece 19 can extend into the groove between adjacent protruding teeth 3111a to restrict the rotation of the winding body 311. The outer flange 3111 extending out of the operating opening 17 facilitates manual operation by children. The convex tooth 3111a cooperates with the spring piece 19 to form a stop positioning, which can restrict the free rotation of the winding body 311. When no external force is applied, the spring piece 19 abuts against the tooth groove between the convex teeth 3111a, restricting the rotation of the winding body 311 and keeping the container 2 in the current position. When an external force drives the winding body 3111 to rotate, the convex tooth 3111a overcomes the limiting effect of the spring piece 19, realizing the winding or releasing of the flexible part, so that the container 2 can be stably suspended at different heights, thereby significantly improving the controllability and stability of the toy operation.

[0065] like Figure 2 As shown, the bottom wall of the cavity 14 is provided with a wire hole 141, and the flexible component is provided through the wire hole 141, so that the wire of the flexible component is neat and the guidance is clear, effectively avoiding tangling and jamming, and improving the smoothness and reliability of winding and unwinding.

[0066] In one possible implementation, such as Figure 6 As shown, the container 2 includes a container shell 21 and a connecting fitting 22. The surface of the container shell 21 is provided with a buckle seat 2121. The connecting fitting 22 is connected to the flexible component. The connecting fitting 22 is detachably connected to the buckle seat 2121, which makes it convenient to assemble and disassemble the container 2 and the flexible component, and facilitates the replacement or separate storage of the container 2, thereby improving the versatility and flexibility of the toy.

[0067] like Figure 6 , Figure 7 and Figure 8As shown, the connecting fitting 22 has a connecting hole 221 in the middle, and multiple snap-fit ​​pieces 222 are provided on the peripheral edge of the connecting fitting 22. Multiple buckle seats 2121 are provided on the surface of the container shell 21. Each buckle seat 2121 has a buckle groove 2121a. When the connecting fitting 22 is rotated in the forward direction, each snap-fit ​​piece 222 can be snapped into the corresponding buckle groove 2121a. When the connecting fitting 22 is rotated in the reverse direction, each snap-fit ​​piece 222 disengages from the corresponding buckle groove 2121a. This not only makes the disassembly and assembly operation intuitive and effortless, suitable for children's hands-on abilities, but also makes the connection more stable due to the corresponding design of multiple snap-fit ​​pieces 222 and buckle seats 2121. This effectively prevents the container 2 from accidentally falling off during dynamic operation, while retaining the flexibility of replacing and storing the container 2 individually, thus balancing connection reliability and ease of use.

[0068] In one possible implementation, such as Figure 7 , Figure 9 and Figure 10 As shown, the container shell 21 includes a bottom plate 211, a three-fold panel assembly 212, and two side plates 213. The two side plates 213 are respectively disposed on both sides of the bottom plate 211, and the two side plates 213 are rotatably connected to the two length sides of the bottom plate 211. The three-fold panel assembly 212 includes three plates that are rotatably connected in sequence. One end of the plate is hinged to a width side of the bottom plate 211, and the other end of the plate is detachably inserted into a slot 2112 on another width side of the bottom plate 211. A buckle seat 2121 is provided on the middle plate of the three-fold panel assembly 212, and an ejection mechanism 4 is provided on the bottom plate 211. The container shell 21 has an unfolded state. In the unfolded state, the plates in the three-fold panel assembly 212 and the bottom plate 211 are arranged in sequence to form a slide. This structure allows the container 2 to be assembled in a forward-facing, closed storage state, and when unfolded, each panel and the base plate 211 form a sliding track. Combined with the ejection mechanism 4 on the base plate 211, it enables the toy to slide and launch, enriching the play scenarios. Meanwhile, the latch 2121 is located in the middle panel of the three-fold panel assembly 212, ensuring stable connection with the flexible components without affecting the folding and unfolding of the shell. The rotating latch structure balances ease of assembly and disassembly with reliable connection. The overall design allows the toy to perform multiple functions, including transportation simulation and sliding / launching, enhancing interactive fun and flexibility, and catering to diverse play needs of children.

[0069] like Figure 9 and Figure 10As shown, a groove 2111 is provided on the base plate 211, and the groove 2111 extends along the length direction of the base plate 211. The ejection mechanism 4 includes a pressing key 41, an ejector 42, and a spring (not shown). The pressing key 41 is connected to the base plate 211 and is located at one end of the groove 2111. The pressing key 41 is provided with a claw 411. The ejector 42 is slidably disposed in the groove 2111. The ejector 42 includes a slider 421 and a pusher 422. The slider 421 slides in engagement with the groove 2111. The pusher 422 is connected to the end of the slider 421 near the pressing key 41. The pusher 422 is provided with a cooperating claw 4221. One end of the spring is connected to the ejector 42, and the other end is connected to the base plate 211. When the claw 411 engages with the mating claw 4221, the spring is in a stretched and deformed state. Pressing the button 41 under external force disengages the claw 411 from the mating claw 4221, the spring returns to its original shape, and the ejector 42 slides along the groove 2111 under the spring's elastic force, ejecting the toy car located on the track via the pusher block 422.

[0070] The preferred embodiments disclosed above are merely illustrative of this application. These preferred embodiments do not exhaustively describe all details, nor do they limit the application to the specific implementations described. Clearly, many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of this application, thereby enabling those skilled in the art to better understand and utilize this application. This application is limited only by the claims and their full scope and equivalents.

Claims

1. An airplane toy with a container, characterized in that, include: An aircraft body, the bottom of which is provided with a cavity, and a winding mechanism is provided on the aircraft body. The winding mechanism includes a rotating component and a flexible component, one end of which is wound around the rotating component. A container, which is connected to the other end of the flexible member; The rotating component can rotate to wind or release the flexible component, causing the container to move closer to or away from the aircraft body. When the container is in contact with the aircraft body, the container is at least partially accommodated within the cavity.

2. The airplane toy with a container according to claim 1, characterized in that, The main body of the aircraft includes the fuselage, the front structure, and the rear structure; Both the front structure and the rear structure are connected to the fuselage. The front structure and the rear structure are arranged at intervals along the length of the fuselage, and the cavity is formed between the front structure and the rear structure. When the winding mechanism lifts the container to its limit position, the container is confined between the front structure and the rear structure.

3. The airplane toy with a container according to claim 2, characterized in that, The aircraft body includes a front wheel and a rear wheel; The front wheel is disposed on the front structure, and the rear wheel is disposed on the rear structure.

4. The airplane toy with a container according to claim 1, characterized in that, The aircraft body has a cavity and an operating port. The operating port communicates with the cavity and is located on the side of the aircraft body away from the concave cavity. The rotating component is located inside the cavity and partially extends out of the operating port. Alternatively, a drive mechanism may be provided within the main body of the aircraft, and the drive mechanism and the rotating component may be in a transmission cooperation to drive the rotating component to rotate.

5. The airplane toy with a container according to claim 4, characterized in that, Two support frames are installed inside the cavity of the aircraft body, and the support frames are provided with rotation holes; The rotating component includes a winding body and rotating shafts located at both ends of the winding body; The rotating shaft is rotatably supported by the rotating hole; The flexible element is wound around the wound body.

6. The airplane toy with a container according to claim 5, characterized in that, The winding body is provided with an outer flange, and the outer flange extends out of the operating port; Multiple protruding teeth are provided on the peripheral end face of the outer flange; A spring is installed inside the cavity of the aircraft body, and the spring can extend into the groove between adjacent protrusions to restrict the rotation of the winding body.

7. The airplane toy with a container according to claim 1, characterized in that, The bottom wall of the cavity is provided with a wire-passing hole; The flexible element is disposed through the wire hole.

8. The airplane toy with a container according to claim 1, characterized in that, The container includes a container shell and connecting fittings; The container shell surface is provided with a buckle seat; The connecting fitting is connected to the flexible member, and the connecting fitting is detachably connected to the buckle seat.

9. The toy airplane with a container according to claim 8, characterized in that, The connecting component has a connecting hole in the middle, and multiple snap-fit ​​pieces are provided on the peripheral edge of the connecting component; The container shell surface is provided with multiple fastening seats, and the fastening seats have fastening slots; When the connecting parts are rotated in the forward direction, each of the snap-fit ​​pieces can be snapped into its corresponding slot. When the connecting parts are rotated in the opposite direction, each of the snap-fit ​​pieces disengages from its corresponding slot.

10. The airplane toy with a container according to claim 9, characterized in that, The container shell includes a bottom plate, a three-fold panel assembly, and two side plates; The two side plates are respectively disposed on both sides of the base plate, and the two side plates are rotatably connected to the two length sides of the base plate; The three-fold plate assembly includes three plates that are rotatably connected in sequence. One end of the plate is hinged to a width side of the base plate, and the other end of the plate is detachably inserted into a slot on another width side of the base plate. The buckle seat is provided on the middle plate of the three-fold plate assembly; A catapult mechanism is provided on the base plate; The container shell has an unfolded state, in which the plates in the three-fold panel assembly and the bottom plate are arranged in sequence to form a slide.

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