Airplane model device

Abstract

The utility model provides an airplane model device, and relates to the technical field of airplane models.The airplane model device comprises a supporting assembly and a driving assembly, the supporting assembly comprises an undercarriage, a fuselage bottom plate and a fuselage top plate, a butt joint groove is formed in the bottom of the fuselage bottom plate, and the undercarriage is clamped in the butt joint groove; the driving assembly comprises a connecting frame, a motor and a propeller, the connecting frame is connected to the fuselage top plate in a sleeving mode, the undercarriage, the fuselage bottom plate and the fuselage top plate are arranged, a butt joint groove is formed in the bottom of the fuselage bottom plate, the undercarriage can be conveniently in butt joint with the fuselage bottom plate to find the designated position of the fuselage bottom plate through the formed butt joint groove, and a tail groove and a positioning groove are formed; the fuselage top plate can be conveniently inserted and connected, then the motor and the propeller are installed on the connecting frame in advance and then inserted into the fuselage top plate together through the connecting frame, and therefore assembling is greatly facilitated, the assembling efficiency is improved, the thin plate design is adopted, and the weight is light.

Description

Technical Field

[0001] This application relates to the field of aircraft models, and more particularly, to an aircraft model device. Background Art

[0002] A model is an object for expressing a purpose that constitutes an objective elaboration of a morphological structure by means of subjective consciousness with the help of an entity or virtual representation (an object is not equal to an object, not limited to entities and virtualities, not limited to planes and solids). Generally speaking: If one thing can change with the change of another thing, then this thing is a model of the other thing. The role of a model is to express the properties of different concepts. A concept can cause different degrees of changes in many models, but only a few models can express the properties of a concept. Therefore, a concept can change the expression form of its properties by referring to different models. Of course, an aircraft model is just one of them and is also relatively common and has collection value.

[0003] Currently, there are various aircraft models. An aircraft model is different from a model aircraft. An aircraft model is generally only used for decoration and display and cannot fly. However, most aircraft models are troublesome to assemble. Non-professional personnel have low assembly efficiency, and the overall weight is relatively high, which is not conducive to use. Summary of the Invention

[0004] In order to overcome the existing deficiencies, the embodiments of this application provide an aircraft model device, which can solve the problems that most aircraft models are troublesome to assemble, non-professional personnel have low assembly efficiency, and the overall weight is relatively high and not conducive to use.

[0005] The technical solution adopted by the embodiments of this application to solve its technical problems is:

[0006] An aircraft model device includes a support assembly and a drive assembly.

[0007] The support assembly includes landing gears, a fuselage bottom plate, and a fuselage top plate. A docking groove is formed at the bottom of the fuselage bottom plate, and the landing gears are snap-fitted into the docking groove. A tail groove is provided at one end of the fuselage bottom plate, and a positioning groove is formed at the other end of the fuselage bottom plate. One end of the fuselage top plate is inserted into the tail groove, and the other end of the fuselage top plate is snap-fitted into the positioning groove.

[0008] The drive assembly includes a connecting frame, a motor, and a propeller. The connecting frame is sleeved on the fuselage top plate, the motor is fixedly connected to the connecting frame, and the propeller is installed at the output end of the motor.

[0009] In a specific implementation, the landing gear includes a bracket and a walking wheel. The top of the bracket is adapted to the docking groove, and the walking wheel is rotatably provided on the side of the bracket.

[0010] In a specific embodiment, the fuselage top plate includes a wing part, a nose part, and a tail part, and the wing part is located between the nose part and the tail part.

[0011] In a specific embodiment, a positioning block is slidably and penetratively arranged in the nose part, and the positioning block is adaptively inserted into the positioning groove.

[0012] In a specific embodiment, the connecting frame includes a fixed frame and a U-shaped clamping plate. The U-shaped clamping plate is arranged on the top of the fixed frame. The U-shaped clamping plate is clamped to the wing part, and the motor is fixedly connected to the fixed frame.

[0013] In a specific embodiment, a connecting groove is formed in the wing part, and the U-shaped clamping plate is adapted to the connecting groove.

[0014] In a specific embodiment, the fuselage bottom plate is arc-shaped, and the fuselage top plate is also arc-shaped.

[0015] In a specific embodiment, both the fuselage bottom plate and the fuselage top plate are thin plates.

[0016] The advantages of the embodiments of the present application are as follows: By providing a landing gear, a fuselage bottom plate, and a fuselage top plate, a docking groove is formed at the bottom of the fuselage bottom plate. The formation of the docking groove can facilitate the docking of the landing gear to a specified position on the fuselage bottom plate. The formed tail groove and positioning groove can facilitate the insertion and connection of the fuselage top plate. Then, the motor and the propeller are pre-installed on the connecting frame, and then the connecting frame is inserted into the fuselage top plate together, which greatly facilitates the assembly, improves the assembly efficiency, and adopts a thin plate design, making it light in weight. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 is a schematic structural diagram of the aircraft model device provided by the embodiment of the present application;

[0018] Figure 2 is a schematic structural diagram of the fuselage bottom plate provided by the embodiment of the present application;

[0019] Figure 3 is a schematic structural diagram of the landing gear provided by the embodiment of the present application;

[0020] Figure 4 is a schematic structural diagram of the fuselage top plate provided by the embodiment of the present application;

[0021] Figure 5 is a schematic structural diagram of the connecting frame provided by the embodiment of the present application.

[0022] In the figure: 100 - support component; 110 - landing gear; 111 - bracket; 112 - walking wheel; 120 - fuselage bottom plate; 121 - docking groove; 122 - tail groove; 123 - positioning groove; 130 - fuselage top plate; 131 - wing part; 1311 - connection groove; 132 - nose part; 1321 - positioning block; 133 - tail part; 200 - drive component; 210 - connecting frame; 211 - fixed frame; 212 - U-shaped clamping plate; 220 - motor; 240 - propeller. Detailed implementation manners

[0023] In order to make the objectives, technical solutions and advantages of the present application clearer and more understandable, the following further details the present application in conjunction with embodiments.

[0024] It should be understood that the specific embodiments described herein are only used to explain the present application and are not used to limit the present application.

[0025] In the embodiments, unless otherwise specified, the means used are all conventional means in the art.

[0026] Please refer to Figures 1 - 5 , the aircraft model device includes a support component 100 and a drive component 200.

[0027] Please refer to Figure 1 , 2 , 3 and 4. The support component 100 includes a landing gear 110, a fuselage bottom plate 120 and a fuselage top plate 130. A docking groove 121 is opened at the bottom of the fuselage bottom plate 120. The landing gear 110 is clamped in the docking groove 121. A tail groove 122 is provided at one end of the fuselage bottom plate 120. A positioning groove 123 is opened at the other end of the fuselage bottom plate 120. One end of the fuselage top plate 130 is inserted into the tail groove 122, and the other end of the fuselage top plate 130 is clamped in the positioning groove 123.

[0028] The landing gear 110 includes a bracket 111 and a walking wheel 112. The top end of the bracket 111 is adapted to the docking groove 121. The walking wheel 112 is rotatably arranged on the side of the bracket 111. Through the trumpet-shaped bracket 111, a good symmetric connection and support effect of the walking wheel 112 can be achieved. The top end is adapted and inserted into the docking groove 121 to facilitate disassembly and assembly.

[0029] In a specific implementation manner, the fuselage top plate 130 includes a wing part 131, a nose part 132 and a tail part 133. The wing part 131 is located between the nose part 132 and the tail part 133.

[0030] Specifically, a positioning block 1321 is slidably penetrated through the nose portion 132. The positioning block 1321 is adaptively inserted into the positioning groove 123. By providing the positioning block 1321, the nose portion 132 of the fuselage top plate 130 is connected to the fuselage bottom plate 120.

[0031] It should be noted that the fuselage bottom plate 120 is arc-shaped, and the fuselage top plate 130 is also arc-shaped. The arc design ensures the accuracy of the model.

[0032] In a specific implementation, both the fuselage bottom plate 120 and the fuselage top plate 130 are thin plates. The thin plate design makes the weight light and easier to use.

[0033] Please refer to Figure 1 、 3 Figures 4,

[0034] and 5, the drive assembly 200 includes a connecting frame 210, a motor 220, and a propeller 240. The connecting frame 210 is sleeved on the fuselage top plate 130. The motor 220 is fixedly connected to the connecting frame 210. The propeller 240 is installed at the output end of the motor 220.

[0035] Among them, the connecting frame 210 includes a fixed frame 211 and a U-shaped clamping plate 212. The U-shaped clamping plate 212 is arranged at the top of the fixed frame 211. The U-shaped clamping plate 212 is clamped to the wing portion 131. The motor 220 is fixedly connected to the fixed frame 211. A connecting groove 1311 is formed in the wing portion 131. The U-shaped clamping plate 212 is adapted to the connecting groove 1311. By providing the docking connection method in which the U-shaped clamping plate 212 is adapted to the connecting groove 1311, it is not only convenient for insertion, but also ensures the accurate installation position.

[0036] It should be noted that the specific model specifications of the motor 220 need to be selected and determined according to the actual specifications of the device. The specific selection calculation method adopts the existing technology in this field, so it will not be elaborated in detail.

[0037] The power supply of the motor 220 and its principle are clear to those skilled in the art, and will not be described in detail herein.

[0038] Finally, it should be noted that: Obviously, the above embodiments are merely examples for clearly illustrating the present invention, rather than limitations on the implementation manners. For those of ordinary skill in the art, other different forms of changes or variations can be made based on the above description. It is not necessary and impossible to enumerate all the implementation manners here. And the obvious changes or variations derived therefrom still fall within the protection scope of the present invention.

Claims

1. An aircraft model device, characterized in that, including a support assembly (100), the support assembly (100) includes a landing gear (110), a fuselage bottom plate (120) and a fuselage top plate (130), a docking groove (121) is formed at the bottom of the fuselage bottom plate (120), the landing gear (110) is clamped in the docking groove (121), a tail groove (122) is arranged at one end of the fuselage bottom plate (120), a positioning groove (123) is formed at the other end of the fuselage bottom plate (120), one end of the fuselage top plate (130) is inserted into the tail groove (122), and the other end of the fuselage top plate (130) is clamped in the positioning groove (123); a drive assembly (200), the drive assembly (200) includes a connecting frame (210), a motor (220) and a propeller (240), the connecting frame (210) is sleeved on the fuselage top plate (130), the motor (220) is fixedly connected to the connecting frame (210), and the propeller (240) is installed at the output end of the motor (220).

2. The aircraft model device according to claim 1, characterized in that, The landing gear (110) includes a bracket (111) and a traveling wheel (112), the top end of the bracket (111) is adapted to the docking groove (121), and the traveling wheel (112) is rotatably arranged on the side of the bracket (111).

3. The aircraft model device according to claim 1, wherein, The fuselage top plate (130) includes a wing portion (131), a fuselage head portion (132) and a fuselage tail portion (133), and the wing portion (131) is located between the fuselage head portion (132) and the fuselage tail portion (133).

4. The aircraft model device according to claim 3, characterized in that, A positioning block (1321) is arranged through the fuselage head portion (132), and the positioning block (1321) is inserted into the positioning groove (123) in an adapted manner.

5. The aircraft model device according to claim 4, characterized in that, The connecting frame (210) includes a fixed frame (211) and a U-shaped clamping plate (212), the U-shaped clamping plate (212) is arranged at the top of the fixed frame (211), the U-shaped clamping plate (212) is clamped to the wing portion (131), and the motor (220) is fixedly connected to the fixed frame (211).

6. The aircraft model device according to claim 5, characterized in that A connecting groove (1311) is formed in the wing portion (131), and the U-shaped clamping plate (212) is adapted to the connecting groove (1311).

7. The aircraft model device according to claim 1, characterized in that, The fuselage bottom plate (120) is arc-shaped, and the fuselage top plate (130) is also arc-shaped.

8. The aircraft model device according to claim 1, wherein Both the fuselage bottom plate (120) and the fuselage top plate (130) are thin and light plates.

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