Lightning fighter model
By designing a twin-structured lightning fighter model, using mortise and tenon structure and slot connection, the existing wooden toys are difficult to provide challenging problems for children in middle and upper grades in primary schools, and the enhancement of children's hands-on ability and cognitive development is achieved. Combined with STEM education, it provides a challenging assembly experience.
Patent Information
- Application Number
- CN202422961448.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-03
- Publication Date
- 2025-08-26
- Estimated Expiration
- 2034-12-03
AI Technical Summary
Existing wooden toys are difficult for middle and senior primary school children to provide challenging activities that are neither simple nor complex, and the drone model lacks a catamaran structure.
A Blitzfighter model was designed, adopting a two-body structure, including components such as the flight main wing plate, the head plate, the tail wing, the side fuselage plate and the propeller. It is connected through the mortise and tenon structure and the slot to achieve stable and easy assembly.
It provides a challenging assembly experience suitable for middle and upper grades of primary schools, combines drone models to enhance children's hands-on ability and cognitive development, integrates STEM education elements to meet children's sense of accomplishment needs.
Smart Images
Figure CN223263406U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of unmanned aerial vehicle (UAV) culture, education and technology, and in particular to a lightning fighter model. Background Art
[0002] In terms of child development, children in the middle and upper grades of elementary school are experiencing rapid development in their cognitive and hands-on abilities. Modern educational theory emphasizes the importance of hands-on activities for a child's overall development. Child psychology suggests that children of this age group are particularly interested in challenging and fulfilling activities. In the toy market, environmentally friendly and educational toys are increasingly popular among parents and children. Wooden toys, due to their natural materials, are gradually gaining market share. However, existing wooden toys are either too simple or too challenging for children of this age. Furthermore, with the increasing popularity of STEM education concepts, toys are also beginning to incorporate elements of related disciplines.
[0003] Drones are currently a hot topic, but the structures of drone models are all traditional, and there are no models of catamaran drones. Utility Model Content
[0004] Purpose of the utility model: To provide a better lightning fighter model. The specific purpose can be seen in the multiple substantial technical effects in the specific implementation part.
[0005] In order to achieve the above purpose, the present invention adopts the following technical solutions:
[0006] Lightning fighter model, characterized by,
[0007] The model includes a main flight wing panel A1. The middle of the flight wing panel A1 has an open hole for mounting an aircraft nose panel A4. The aircraft nose panel A4 includes a groove that can be inserted into the open hole of the flight wing panel A1.
[0008] An outer nose reinforcement plate A2 and an inner flight reinforcement plate A3 are arranged on both sides of the aircraft nose panel A4. The outer nose reinforcement plate A2 and the inner flight reinforcement plate A3 also include grooves that can be inserted into the open holes of the flight main wing panel A1.
[0009] Side panels A7 are arranged on both sides of the main flight wing panel A1. Side panels A5 and A6 are arranged on both sides of the side panels A7. The side panels A5 and A6 pass through the side panels A1 on both sides of the main flight wing panel A1 through a hole.
[0010] The aircraft nose panel A4 and the two side fuselage panels A7 include circular wheel components below.
[0011] A further technical solution of the present invention is that a groove is arranged at the end of the side body plate A7 for mounting the aircraft propeller B2 and the propeller fixing member B3.
[0012] A further technical solution of the present invention is that the side fuselage outer fixing member A8 and the side fuselage inner fixing member A9 fix the side fuselage outer reinforcement plate A5, the side fuselage inner reinforcement plate A6 and the side fuselage plate A7 from both sides of the protrusion of the flight main wing panel A1 respectively.
[0013] A further technical solution of the present invention is that grooves are arranged at the rear of the two side fuselage panels A7 to be used for installing the aircraft tail fixing parts B1.
[0014] A further technical solution of the present invention is that the aircraft propeller B2 includes a downward groove, which can be inserted into the front end of the side body plate A7.
[0015] A further technical solution of the present invention is that two groups of side fuselage outer reinforcement panels A5 and side fuselage inner reinforcement panels A6 and side fuselage panels A7 are symmetrically arranged around the flight main wing panel A1.
[0016] The utility model adopting the above technical solution has the following beneficial effects compared with the prior art: the outer nose reinforcement plate A2, the inner flight reinforcement plate A3, the aircraft nose plate A4, the inner flight reinforcement plate A3, and the outer nose reinforcement plate A2 are combined in sequence and the combined parts are inserted into the aircraft main wing panel A1 and the middle socket and fixed; the side body outer reinforcement plate A5, the side body inner reinforcement plate A6, the side body panel A7, the side body inner reinforcement plate A6, and the side body outer reinforcement plate A5 are combined in sequence and the holes are aligned; the holes are inserted into the right side of the flight main wing panel A1 and the corresponding grooves; and the side body outer fixing member A8 and the side body inner fixing member A9 are inserted into the grooves and fixed.
[0017] Assemble the side fuselage outer reinforcement plate A5, the side fuselage inner reinforcement plate A6, the right fuselage plate A7, the side fuselage inner reinforcement plate A6, and the side fuselage outer reinforcement plate A5 in sequence and align the holes, insert the holes into the left side of the flight main wing panel A1 and the corresponding grooves, and insert the side fuselage outer fixing piece A8 and the side fuselage inner fixing piece A9 into the grooves and fix them.
[0018] Insert the tail wing fixture B1 into the tail groove of the main wing panel A1. Insert the propeller B2 and propeller fixture B3 into the groove of the left fuselage panel A7. Insert the propeller B2 and propeller fixture B3 into the groove of the side fuselage panel A7. The assembly is complete. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] In order to further illustrate the present invention, the following is a further description with reference to the accompanying drawings:
[0020] Figure 1 A structural diagram of one of the utility model assembly processes;
[0021] Figure 2 This is a structural diagram of the second assembly process of the utility model;
[0022] Figure 3 This is a structural diagram of the third assembly process of the utility model;
[0023] Figure 4 This is a structural diagram of the fourth assembly process of the utility model;
[0024] Figure 5 A structural diagram of a utility model;
[0025] Among them: A1 flight main wing panel, A2 outer nose reinforcement plate, A3 inner flight reinforcement plate, A4 aircraft nose panel, A5 side fuselage outer reinforcement plate, A6 side fuselage inner reinforcement plate, A7 side fuselage panel, A8 side fuselage outer fixings, A9 side fuselage inner fixings, B1 aircraft tail fixings, B2 aircraft propeller, B3 propeller fixings. DETAILED DESCRIPTION
[0026] The present invention is further explained below in conjunction with the accompanying drawings and specific embodiments. It should be understood that the following specific embodiments are only used to illustrate the present invention and are not used to limit the scope of the present invention. In the description of the present invention, it should be noted that the terms "center", "up", "down", "left", "right", "vertical", "horizontal", "inside", "outside", "top", "bottom" and the like indicate directions or positional relationships based on the directions or positional relationships shown in the accompanying drawings. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction. Therefore, they cannot be understood as limitations on the present invention. In addition, unless otherwise clearly specified and limited, the terms "installed", "connected" and "connected" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or an indirect connection through an intermediate medium, or it can be a communication between the internal parts of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to the specific circumstances.
[0027] It should be noted that, in this document, relational terms such as first and second, etc., are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that includes a list of elements includes not only those elements but also other elements not explicitly listed, or elements inherent to such process, method, article, or apparatus.
[0028] This patent provides multiple parallel solutions. The differences in descriptions are improvements or parallel solutions based on the basic solution. Each solution has its own unique characteristics. In addition, the technical features involved in the different embodiments of the utility model described below can be combined with each other as long as they do not conflict with each other. Fixing methods not described in this article can be any fixing method such as threaded fixing, bolt fixing, or gluing.
[0029] Embodiment 1: With reference to all the accompanying drawings; A Lightning fighter model, characterized in that:
[0030] The model includes a main flight wing panel A1. The middle of the flight wing panel A1 has an open hole for mounting an aircraft nose panel A4. The aircraft nose panel A4 includes a groove that can be inserted into the open hole of the flight wing panel A1.
[0031] An outer nose reinforcement plate A2 and an inner flight reinforcement plate A3 are arranged on both sides of the aircraft nose panel A4. The outer nose reinforcement plate A2 and the inner flight reinforcement plate A3 also include grooves that can be inserted into the open holes of the flight main wing panel A1.
[0032] Side panels A7 are arranged on both sides of the main flight wing panel A1. Side panels A5 and A6 are arranged on both sides of the side panels A7. The side panels A5 and A6 pass through the side panels A1 on both sides of the main flight wing panel A1 through a hole.
[0033] The aircraft nose panel A4 and the two side fuselage panels A7 include circular wheel components below.
[0034] The substantial technical effects and implementation process of this technical solution, i.e., the basic functions, are as follows:
[0035] Assemble the outer nose reinforcement plate A2, the inner flight reinforcement plate A3, the aircraft nose plate A4, the inner flight reinforcement plate A3, and the outer nose reinforcement plate A2 in sequence and insert the assembled parts into the aircraft main wing panel A1, the middle socket and secure them. Assemble the side body outer reinforcement plate A5, the side body inner reinforcement plate A6, the side body panel A7, the side body inner reinforcement plate A6, and the side body outer reinforcement plate A5 in sequence and align the holes. Insert the holes into the right side of the flight main wing panel A1 and the corresponding grooves and insert the side body outer fixing piece A8 and the side body inner fixing piece A9 into the grooves and secure them.
[0036] Assemble the side fuselage outer reinforcement plate A5, the side fuselage inner reinforcement plate A6, the right fuselage plate A7, the side fuselage inner reinforcement plate A6, and the side fuselage outer reinforcement plate A5 in sequence and align the holes, insert the holes into the left side of the flight main wing panel A1 and the corresponding grooves, and insert the side fuselage outer fixing piece A8 and the side fuselage inner fixing piece A9 into the grooves and fix them.
[0037] Insert the tail wing fixture B1 into the tail groove of the main wing panel A1. Insert the propeller B2 and propeller fixture B3 into the groove of the left fuselage panel A7. Insert the propeller B2 and propeller fixture B3 into the groove of the side fuselage panel A7. The assembly is complete.
[0038] This wooden assembly toy falls into the category of educational toys. In modern educational concepts, toys are no longer just entertainment tools, but also auxiliary products with educational significance. For children, this toy can integrate knowledge learning and skill development into the process of playing.
[0039] It involves handmade educational technology, allowing children to get in touch with basic handmade crafts through wooden assembly. At the same time, it is also related to children's cognitive development technology. During the assembly process, children's shape cognition, spatial cognition and color cognition abilities can be exercised.
[0040] This wooden assembly toy conforms to this trend, allowing children to apply knowledge and skills such as spatial thinking, shape and quantity judgment, and understanding of materials and structures during the assembly process, learn and practice STEM knowledge in games, meet children's development needs, fill market gaps, and help cultivate children's comprehensive literacy and innovation capabilities.
[0041] This utility model focuses on a wooden assembly toy airplane designed specifically for children. The main body of the airplane is made of high-quality wood and has undergone meticulous craftsmanship. It has a soft texture and is odorless. Numerous slots and mortise and tenon structures facilitate precise splicing. The front simulates a cockpit with rich details, which can greatly enhance children's sense of immersion. The wings and tail are independent wooden components. The wings have smooth lines and simulate engine textures. The unique interface at the connection with the fuselage is both stable and easy to install. The tail conforms to the principles of aerodynamics, making the toy both scientific and practical. The wooden landing gear has a stable structure, and the struts fit tightly with the holes at the bottom of the fuselage. It has a certain elasticity to cushion collisions and ensure the toy is placed stably. The whole uses advanced wooden slots and mortise and tenon splicing technology. The component interfaces are strictly designed and tested. No auxiliary tools are required. The difficulty level is suitable for 9-year-old children, which can stimulate their enthusiasm for independent exploration and hands-on experience. After assembly, the structure is sturdy and can be played with and appreciated for a long time.
[0042] Example 2: As a further improved, parallel, or independent solution, the end of side panel A7 is provided with a groove for mounting aircraft propeller B2 and propeller mounting member B3. The substantial technical effect of this solution and its implementation process are as follows: Thus, a unique dual-propeller mounting structure is achieved.
[0043] Example 3: As a further improved solution, a parallel solution, or an optional independent solution, side fuselage outer side fasteners A8 and side fuselage inner side fasteners A9 secure the side fuselage outer side reinforcement panel A5, side fuselage inner side reinforcement panel A6, and side fuselage panel A7, respectively, from either side of the protrusion of the flight main wing panel A1. The substantial technical effect of this technical solution and its implementation process are as follows: Similar fastening methods are all within the scope of protection of this patent.
[0044] Example 4: As a further improved solution, a parallel solution, or an optional independent solution, grooves are arranged on the rear of the two side panels A7 for mounting the aircraft tail fixing member B1. The substantial technical effect and implementation process of this technical solution are as follows: Thus, the aircraft tail can be fixed.
[0045] Example 5: As a further improved, parallel, or independent solution, aircraft propeller B2 includes a downwardly facing groove that can be inserted into the front end of side panel A7. The substantial technical effect of this technical solution and its implementation process are as follows: Similar fixing methods are within the scope of protection of this patent.
[0046] Example 6: As a further improved solution, a parallel solution, or an optional independent solution, two sets of side fuselage outer reinforcement panels A5, side fuselage inner reinforcement panels A6, and side fuselage panels A7 are symmetrically arranged around the flight main wing panel A1. The substantial technical effect of this technical solution and its implementation process are as follows: a unique dual-plane structure is achieved to simulate a real fighter jet.
[0047] Innovatively, each of the above effects exists independently, and a set of structures can be used to combine the above results.
[0048] It should be noted that the multiple solutions provided by this patent include the basic solutions themselves, are independent of each other, and do not restrict each other, but they can also be combined with each other without conflict to achieve multiple effects together.
[0049] The above shows and describes the basic principles, main features, and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely illustrative of the principles of the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention, and such changes and improvements fall within the scope of the claimed invention.
Claims
1. Lightning fighter model, characterized by, The model includes a main flight wing panel (A1), wherein the middle portion of the flight wing panel (A1) has an open hole for mounting an aircraft nose panel (A4), and the aircraft nose panel (A4) includes a groove capable of being inserted into the open hole of the flight wing panel (A1); An outer nose reinforcement plate (A2) and an inner flight reinforcement plate (A3) are arranged on both sides of the aircraft nose plate (A4), and the outer nose reinforcement plate (A2) and the inner flight reinforcement plate (A3) also include grooves capable of being inserted into the open holes of the flight main wing plate (A1); Side fuselage panels (A7) are arranged on both sides of the main flight wing panel (A1), and side fuselage outer reinforcement panels (A5) and side fuselage inner reinforcement panels (A6) are arranged on both sides of the side fuselage panel (A7), and the side fuselage outer reinforcement panels (A5), the side fuselage inner reinforcement panels (A6) and the side fuselage panel (A7) pass through the side wings on both sides of the main flight wing panel (A1) through a hole; The aircraft nose plate (A4) and the two side fuselage plates (A7) contain circular wheel parts below.
2. The Lightning fighter model according to claim 1, characterized in that: The end of the side fuselage plate (A7) is provided with a groove for installing an aircraft propeller (B2) and a propeller fixing member (B3).
3. The Lightning fighter model according to claim 1, characterized in that: The side fuselage outer fixing member (A8) and the side fuselage inner fixing member (A9) respectively fix the side fuselage outer reinforcement plate (A5), the side fuselage inner reinforcement plate (A6) and the side fuselage plate (A7) from both sides of the protrusion of the flight main wing panel (A1).
4. The Lightning fighter model according to claim 1, characterized in that: The rear of the two side fuselage panels (A7) is provided with grooves for installing the aircraft tail fixing parts (B1).
5. The Lightning fighter model according to claim 2, characterized in that: The aircraft propeller (B2) includes a downward-facing groove that can be inserted into the front end of the side fuselage panel (A7).
6. The Lightning fighter model according to claim 1, characterized in that: The two groups of side fuselage outer reinforcement plates (A5), side fuselage inner reinforcement plates (A6), and side fuselage plates (A7) are symmetrically arranged around the flight main wing plate (A1).