Combined type aerial aircraft

Abstract

The utility model discloses a combined type aerial airplane, and relates to the field of simulation models. The combined aerial aircraft comprises a simulation aircraft unit, the simulation aircraft unit comprises a first mounting plate, a second mounting plate and an airflow channel, and a first connecting plate and a second connecting plate are clamped between the first mounting plate and the second mounting plate; an airflow channel is formed among the first mounting plate, the second mounting plate, the first connecting plate and the second connecting plate; and the second mounting plate is connected with an airflow driving unit. According to the combined type aerial aircraft, an aerial aircraft model can be formed by simply splicing and combining the first mounting plate, the second mounting plate, the first connecting plate and the second connecting plate, meanwhile, an airflow driving unit can be mounted on the second mounting plate, and an airflow channel can be formed among the first mounting plate, the second mounting plate, the first connecting plate and the second connecting plate; the airflow driving unit accelerates airflow flowing in the airflow channel, and the effect of aircraft flight simulation is achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of simulation models, in particular to a combined aerial aircraft. Background Art

[0002] Airplane models are scaled-down and simulated versions of real airplanes. They can be used as children's toys, as collections for aviation enthusiasts, and even as teaching or display props in some situations.

[0003] There are many types of airplane models. Common children's assembled airplane models are usually simple in design, easy for children to operate, and often have a certain degree of entertainment and educational value. However, existing children's airplane models are fixed and mainly used to display the appearance of the aircraft. Generally, other entertainment operations cannot be performed, which makes them less interesting. Therefore, this application proposes a modular airplane. Utility Model Content

[0004] In view of the shortcomings of the existing technology, the utility model provides a combined aerial airplane, which solves the problem that the existing children's airplane models are fixed and mainly used to display the appearance of the airplane, generally cannot perform other entertainment operations, and are less interesting.

[0005] To achieve the above objectives, the present invention is implemented through the following technical solutions: A modular aerial aircraft includes a simulated aircraft unit, wherein the simulated aircraft unit includes:

[0006] a first mounting plate and a second mounting plate, wherein a first connecting plate and a second connecting plate are clamped between the first mounting plate and the second mounting plate;

[0007] An air flow channel is formed between the first mounting plate, the second mounting plate, the first connecting plate and the second connecting plate;

[0008] The second mounting plate is connected to an airflow driving unit.

[0009] Preferably, an air inlet is provided on the outer side of the first mounting plate, and the air inlet is connected to the air flow channel.

[0010] Preferably, a simulated tail wing is clamped between the first mounting plate and the second mounting plate.

[0011] Preferably, the airflow driving unit includes:

[0012] A support plate, the support plate being clamped to the ends of the plurality of second connecting plates;

[0013] A drive motor is installed between the second mounting plate and the support plate;

[0014] The driving member is rotatably arranged in the air flow channel and is fixedly sleeved on the outer side of the output end of the driving motor.

[0015] Preferably, the driving member includes:

[0016] A fixed ring, with multiple toggle plates fixedly connected to the outer side of the fixed ring;

[0017] A connecting ring is fixedly connected to the outer sides of the plurality of toggle plates.

[0018] Preferably, a mounting shaft is fixedly connected to the outer side of the fixing ring, and a mounting groove is provided at the end of the mounting shaft.

[0019] The utility model discloses a modular aerial airplane, which has the following beneficial effects: during use, the modular aerial airplane can form an aerial airplane model by simply splicing and assembling a first mounting plate, a second mounting plate, a first connecting plate, and a second connecting plate; at the same time, an airflow driving unit can be installed on the second mounting plate; an airflow channel can be formed between the first mounting plate, the second mounting plate, the first connecting plate, and the second connecting plate; the airflow driving unit accelerates the flow of air in the airflow channel, thereby achieving an effect of aircraft flight simulation and improving the operability and fun of the aerial airplane. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0021] Figure 1 This is one of the schematic diagrams of the structure of the utility model;

[0022] Figure 2 This is the second schematic diagram of the structure of the utility model

[0023] Figure 3 It is a partial structural diagram of the utility model;

[0024] Figure 4 This is a schematic structural diagram of the driving component of the utility model.

[0025] In the figure: 1. Simulated aircraft unit; 11. First mounting plate; 12. Second mounting plate; 13. First connecting plate; 14. Second connecting plate; 15. Airflow channel; 16. Air inlet; 17. Simulated tail wing; 2. Airflow drive unit; 21. Support plate; 22. Drive motor; 23. Drive member; 231. Fixed ring; 232. Toggle plate; 233. Connecting ring; 234. Mounting shaft. DETAILED DESCRIPTION

[0026] In order to better understand the above technical solution, the above technical solution will be described in detail below with reference to the accompanying drawings and specific implementation methods.

[0027] The utility model discloses a combined aerial aircraft according to the attached Figure 1-4 As shown, it includes a simulated aircraft unit 1, which includes:

[0028] A first mounting plate 11 and a second mounting plate 12, with a first connecting plate 13 and a second connecting plate 14 clamped between the first mounting plate 11 and the second mounting plate 12;

[0029] An air flow channel 15 is formed between the first mounting plate 11, the second mounting plate 12, the first connecting plate 13 and the second connecting plate 14;

[0030] The second mounting plate 12 is connected to the airflow driving unit 2 .

[0031] During use, an aerial aircraft model can be formed by simply splicing and combining the first mounting plate 11, the second mounting plate 12, the first connecting plate 13 and the second connecting plate 14. At the same time, the airflow driving unit 2 can be installed on the second mounting plate 12. An airflow channel 15 can be formed between the first mounting plate 11, the second mounting plate 12, the first connecting plate 13 and the second connecting plate 14. The airflow driving unit 2 accelerates the flow of air in the airflow channel 15 to achieve the effect of aircraft flight simulation, thereby improving the operability and fun of the aerial aircraft.

[0032] Furthermore, an air inlet hole 16 is formed on the outer side of the first mounting plate 11 , and the air inlet hole 16 is connected to the air flow channel 15 .

[0033] The air inlet holes 16 are provided to facilitate the entry of air from the outside into the air flow channel 15 to form air circulation.

[0034] Furthermore, a simulated tail wing 17 is clamped between the first mounting plate 11 and the second mounting plate 12 .

[0035] Specifically disclosed, the airflow driving unit 2 includes:

[0036] A support plate 21, the support plate 21 is clamped with the ends of the plurality of second connecting plates 14;

[0037] A drive motor 22 is installed between the second mounting plate 12 and the support plate 21;

[0038] The driving member 23 is rotatably disposed in the air flow channel 15 and is fixedly sleeved on the outer side of the output end of the driving motor 22 .

[0039] The support plate 21 provided can effectively support the driving motor 22 . When the driving motor 22 is working, its output end can drive the driving member 23 to rotate, thereby driving the airflow to flow in the airflow channel 15 .

[0040] Furthermore, the driving member 23 includes:

[0041] A fixed ring 231, with multiple toggle plates 232 fixedly connected to the outer side of the fixed ring 231;

[0042] The connecting ring 233 is fixedly connected to the outer sides of the plurality of toggle plates 232 .

[0043] When the driving motor 22 is working, its output end can drive the multiple toggle plates 232 to rotate via the fixed ring 231, thereby accelerating the flow of air.

[0044] Furthermore, a mounting shaft 234 is fixedly connected to the outer side of the fixing ring 231 , and a mounting groove is formed at the end of the mounting shaft 234 .

[0045] The installation shaft 234 and the installation groove are provided to facilitate connecting external parts thereto, thereby enhancing its operability.

[0046] During use, an aerial aircraft model can be formed by simply splicing and combining the first mounting plate 11, the second mounting plate 12, the first connecting plate 13 and the second connecting plate 14. At the same time, the airflow driving unit 2 can be installed on the second mounting plate 12. An airflow channel 15 can be formed between the first mounting plate 11, the second mounting plate 12, the first connecting plate 13 and the second connecting plate 14. The airflow driving unit 2 accelerates the flow of air in the airflow channel 15 to achieve the effect of aircraft flight simulation, thereby improving the operability and fun of the aerial aircraft.

[0047] The support plate 21 provided can effectively support the driving motor 22. When the driving motor 22 is working, its output end can drive the driving member 23 to rotate, thereby driving the airflow to flow in the airflow channel 15. When the driving motor 22 is working, its output end can drive multiple toggle plates 232 to rotate through the provided fixing ring 231, thereby accelerating the flow of air. Through the provided mounting shaft 234 and mounting groove, it is convenient to connect external parts to it, thereby enhancing its operability.

[0048] 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. Such changes and improvements are intended to fall within the scope of the present invention. The scope of protection claimed in this invention is defined by the appended claims and their equivalents.

Claims

1. A modular aerial aircraft comprising a simulated aircraft unit (1), characterized in that: The simulated aircraft unit (1) comprises: A first mounting plate (11) and a second mounting plate (12), wherein a first connecting plate (13) and a second connecting plate (14) are clamped between the first mounting plate (11) and the second mounting plate (12); An air flow channel (15), wherein the air flow channel (15) is formed between the first mounting plate (11), the second mounting plate (12), the first connecting plate (13) and the second connecting plate (14); The second mounting plate (12) is connected to an airflow drive unit (2).

2. A modular aerial aircraft according to claim 1, characterized in that: An air inlet hole (16) is provided on the outer side of the first mounting plate (11), and the air inlet hole (16) is connected to the air flow channel (15).

3. The modular aerial aircraft according to claim 1, characterized in that: A simulated tail wing (17) is clamped between the first mounting plate (11) and the second mounting plate (12).

4. The modular aerial aircraft according to claim 1, characterized in that: The airflow driving unit (2) comprises: A support plate (21), wherein the support plate (21) is clamped with ends of the plurality of second connecting plates (14); a drive motor (22), wherein the drive motor (22) is installed between the second mounting plate (12) and the support plate (21); A driving member (23) is rotatably disposed in the air flow channel (15), and the driving member (23) is fixedly sleeved on the outside of the output end of the driving motor (22).

5. The modular aerial aircraft according to claim 4, characterized in that: The driving member (23) comprises: A fixed ring (231), the outer side of which is fixedly connected to a plurality of toggle plates (232); A connecting ring (233) is fixedly connected to the outer sides of the plurality of toggle plates (232).

6. The modular aerial aircraft according to claim 5, characterized in that: The outer side of the fixing ring (231) is fixedly connected to a mounting shaft (234), and a mounting groove is provided at the end of the mounting shaft (234).

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