CN214808423U

CN214808423U - Novel aeromodelling assembling and connecting structure

Info

Publication number: CN214808423U
Application number: CN202121260015.3U
Authority: CN
Inventors: 孙延波; 李汉东; 陈颖聪
Original assignee: Shenzhen Boer Creative Culture Development Co ltd
Current assignee: Shenzhen Boer Creative Culture Development Co ltd
Priority date: 2021-06-07
Filing date: 2021-06-07
Publication date: 2021-11-23
Anticipated expiration: 2031-06-07

Abstract

The utility model discloses a novel aeromodel equipment connection structure, including base and fuselage, the equal fixedly connected with wing in both sides of fuselage, tip fixedly connected with support behind the fuselage lower extreme, support and base are triangle-shaped all to be equipped with the gyro wheel through first assembly devices fixed connection in the middle of winding, the fuselage lower extreme, and the gyro wheel passes through second assembly devices fixed connection with the fuselage, and the department is provided with the guided missile in the middle of the fuselage lower extreme, and the guided missile passes through third assembly devices fixed connection with the fuselage. The utility model discloses an use magnet as the assembly intermediary, with two magnet settings in assembly body inside, use magnet magnetic force as the medium, with both sides assembly body mounted together to realize the effect of show model behind the whole assembly, let the model outward appearance more scientific, also let the assembly of each spare part more reasonable, both kept the advantage of the easy dismouting that original tenon fourth of the twelve earthly branches structure assembly exists, also avoided at the installation or the damage risk that dismantles the in-process and exist.

Description

Novel aeromodelling assembling and connecting structure

Technical Field

The utility model relates to an aeromodelling technical field especially relates to a novel aeromodelling equipment connection structure.

Background

At present, most of toys and models on the market are assembled by adopting a mortise and tenon structure, namely a male connector is arranged on one assembly part, and a female connector is arranged on the other assembly part.

This kind of connected mode is for general product relatively easy dismouting, but has great damage risk in installation or dismantlement process simultaneously. Therefore, a new model airplane assembly connection structure is needed.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the novel aeromodelling equipment connection structure that proposes can solve the aesthetic property of aeromodelling handicraft to and add the convenience in man-hour, let the model outward appearance more scientific, also let the assembly of each spare part more reasonable, simultaneously, the magnetism of magnet is in steerable within range, and it is also more convenient when needing to dismantle.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides a novel aeromodel equipment connection structure, includes base and fuselage, the equal fixedly connected with wing in both sides of fuselage, tip fixedly connected with support behind the fuselage lower extreme, the support with the base is through first assembly devices fixed connection, the fuselage lower extreme is triangle-shaped around the centre and all is equipped with the gyro wheel, the gyro wheel with the fuselage passes through second assembly devices fixed connection, department is provided with the guided missile in the middle of the fuselage lower extreme, the guided missile with the fuselage passes through third assembly devices fixed connection.

Preferably, the first assembling mechanism comprises a bottom fixing groove and a bottom assembling part, the bottom fixing groove is formed in the upper end of the base, the bottom assembling part is fixedly connected to the lower end of the support, the bottom assembling part is embedded in the bottom fixing groove, and magnets are fixedly mounted on the bottom of the bottom fixing groove and the bottom assembling part.

Preferably, the second assembly devices comprise roller fixing grooves and roller assembly parts, the roller fixing grooves are triangular and are formed in the lower end of the machine body, the roller assembly parts are embedded in the roller fixing grooves, the rollers are movably mounted on the side walls of the roller assembly parts, and magnets are fixedly mounted on the top portions of the roller fixing grooves and the roller assembly parts.

Preferably, the third assembling mechanism comprises a missile fixing groove and a missile assembling part, the missile fixing groove is formed in the middle of the lower end of the machine body, the missile assembling part is embedded in the missile fixing groove, the missile is fixedly installed on the missile assembling part, and magnets are fixedly installed on the top in the missile fixing groove and the missile assembling part.

The utility model discloses following beneficial effect has:

through using magnet as the assembly intermediary, with two magnet settings inside assembly body, regard as the medium with magnet magnetic force, with both sides assembly body erection together to realize the effect of whole assembly back show model, let the model outward appearance more scientific, also let the assembly of each spare part more reasonable, both kept the advantage of the easy dismouting that original tenon fourth of twelve earthly branches structure assembly exists, also avoided the damage risk that exists at installation or dismantlement in-process.

Drawings

Fig. 1 is a schematic structural view of a novel aeromodelling assembly connection structure provided by the present invention;

fig. 2 is a bottom view of a novel aeromodelling assembly connection structure provided by the present invention;

fig. 3 is a side view of the novel aeromodelling assembly connection structure provided by the utility model.

In the figure: 1. a base; 2. a body; 3. an airfoil; 4. a bottom fixing groove; 5. a bottom assembly member; 6. a support; 7. a roller fixing groove; 8. a roller assembly member; 9. a roller; 10. a missile fixing groove; 11. missile fittings; 12. and (4) guided missiles.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

Referring to fig. 1-3, a novel aeromodel assembly connection structure comprises a base 1 and a fuselage 2, wherein wings 3 are fixedly connected to both sides of the fuselage 2, and a support 6 is fixedly connected to the rear end of the lower end of the fuselage 2.

Support 6 and base 1 are through first assembly devices fixed connection, and first assembly devices includes bottom fixed slot 4 and bottom assembly part 5, and bottom fixed slot 4 is seted up in base 1 upper end, and bottom assembly part 5 fixed connection is at 6 lower extremes of support, and bottom assembly part 5 inlays and establishes in bottom fixed slot 4, and equal fixed mounting has magnet on bottom and the bottom assembly part 5 in the bottom fixed slot 4.

2 lower extremes of fuselage all are the triangle-shaped around the centre and all are equipped with gyro wheel 9, and gyro wheel 9 passes through second assembly devices fixed connection with fuselage 2, and second assembly devices includes gyro wheel fixed slot 7 and gyro wheel assembly spare 8, and three gyro wheel fixed slot 7 is triangle-shaped and all establishes at 2 lower extremes of fuselage, and gyro wheel assembly spare 8 inlays and establishes in gyro wheel fixed slot 7, and gyro wheel 9 movable mounting is on gyro wheel assembly spare 8 lateral wall, and equal fixed mounting has magnet on top portion and the gyro wheel assembly spare 8 in the gyro wheel fixed slot 7.

The guided missile assembly installation structure comprises a body 2, a guided missile 12, a third assembly mechanism, a guided missile assembly part 11, a guided missile fixing groove 10, a guided missile assembly part 11 and a guided missile assembly part 11, wherein the guided missile assembly part 11 is fixedly arranged on the body 2, the guided missile assembly part 11 is fixedly arranged on the top of the guided missile assembly part 11, and magnets are fixedly arranged on the top of the guided missile assembly part 11 in the guided missile fixing groove 10.

The utility model discloses in, during the assembly model, install magnet earlier in bottom assembly part 5, gyro wheel assembly part 8, guided missile assembly part 11 and bottom fixed slot 4, gyro wheel fixed slot 7, guided missile fixed slot 10 to utilize assembly part self and notch self to hide magnet, during the unit mount, magnet on each assembly part and rather than the intraoral magnet of corresponding notch adsorb each other together, form a whole, make the pattern of exhibition frame, thereby reach the effect of showpiece.

The appearance of the model is more scientific and the assembly of each part is more reasonable; meanwhile, the magnetism of the magnet is within a controllable range, and the magnet is convenient to disassemble.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The utility model provides a novel aeromodel equipment connection structure, includes base (1) and fuselage (2), its characterized in that, the equal fixedly connected with wing (3) in both sides of fuselage (2), tip fixedly connected with support (6) behind fuselage (2) lower extreme, support (6) with base (1) is through first assembly devices fixed connection, fuselage (2) lower extreme is triangle-shaped around the centre and all is equipped with gyro wheel (9), gyro wheel (9) with fuselage (2) are through second assembly devices fixed connection, department is provided with guided missile (12) in the middle of fuselage (2) lower extreme, guided missile (12) with fuselage (2) are through third assembly devices fixed connection.

2. The novel aeromodel assembly-connection structure of claim 1, wherein the first assembly mechanism comprises a bottom fixing groove (4) and a bottom assembly member (5), the bottom fixing groove (4) is opened at the upper end of the base (1), the bottom assembly member (5) is fixedly connected at the lower end of the bracket (6), the bottom assembly member (5) is embedded in the bottom fixing groove (4), and magnets are fixedly mounted on the bottom of the bottom fixing groove (4) and the bottom assembly member (5).

3. The novel aeromodel assembly connection structure of claim 1, wherein the second assembly mechanism comprises roller fixing grooves (7) and roller assemblies (8), three roller fixing grooves (7) are triangular and are formed in the lower end of the fuselage (2), the roller assemblies (8) are embedded in the roller fixing grooves (7), the rollers (9) are movably mounted on the side walls of the roller assemblies (8), and magnets are fixedly mounted on the top portions of the roller fixing grooves (7) and the roller assemblies (8).

4. The novel aeromodel assembly connection structure of claim 1, wherein the third assembly mechanism comprises a missile fixing groove (10) and a missile assembly part (11), the missile fixing groove (10) is arranged in the middle of the lower end of the machine body (2), the missile assembly part (11) is embedded in the missile fixing groove (10), the missile (12) is fixedly installed on the missile assembly part (11), and magnets are fixedly installed on the top in the missile fixing groove (10) and the missile assembly part (11).