Teaching rocket boosting airplane model with rotatable and foldable wings

By designing the rotatable folding rocket booster aircraft model for teaching wings with structures such as rotating shafts, folding plates and fixed plates, the difficulties in placement, folding and rotation of the existing aircraft model are solved, and the flexible rotation and folding of the aircraft model is achieved, which is convenient for teaching and display.

CN222562157UActive Publication Date: 2025-03-04NANCHANG QIYANG TECH CO LTD
View PDF 1 Cites 0 Cited by

Patent Information

Application Number
CN202420465721.9
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-03-11
Publication Date
2025-03-04
Estimated Expiration
2034-03-11

AI Technical Summary

Technical Problem

Existing aircraft models have difficulties in placement, folding and rotating, and cannot meet the needs of teaching and display.

Method used

A rotatable folding rocket booster aircraft model for teaching wings was designed, using structures such as rotating shaft, folding plate and fixed plate to achieve 360° rotation and partial folding. Supporting equipment is installed at the bottom for easy placement and disassembly.

Benefits of technology

It realizes flexible rotation and folding of the aircraft model, simplifies the teaching and display process, and the overall structure is simple and easy to operate and maintain.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN222562157U_ABST
    Figure CN222562157U_ABST
Patent Text Reader

Abstract

The utility model relates to the technical field of aerodynamics, in particular to a teaching rocket boosting airplane model with rotatable and foldable wings, which comprises an airplane model mechanism, and the airplane model mechanism comprises an airplane body, a cockpit, an airplane bottom end fixing plate, a rotating shaft, a first wing, a first rocket booster and a first folding plate. When the equipment is operated, the airplane model can be held on a hand for teaching, the airplane model can be placed on the supporting column through the assembling and disassembling screws when being used up or not used temporarily, and the equipment has the advantages that the equipment is simple in overall structure and can be more conveniently used for teaching display, the wings can rotate by 360 degrees due to the rotating shaft, and the teaching effect is better. A first folding plate and a second folding plate are arranged to enable the device to be partially folded, supporting equipment is arranged at the bottom to facilitate placement, and a first rocket booster and a second rocket booster are provided with internal structures to further perform teaching work.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The utility model relates to the technical field of aerodynamics, in particular to a teaching rocket-propelled aircraft model with rotatable and foldable wings. Background Art

[0002] "The wisdom of a child lies in his fingers." This sentence is the most appropriate to summarize the significance of youth science and technology model making. The traditional "book education" is important, but it is far from enough to develop the intelligence of young people and cultivate their innovative ability. Young people are eager to realize their dreams with their own hands.

[0003] For example, an aircraft model disclosed in the authorization announcement number CN 205516486 U can achieve a more ultra-light and strong aircraft model, thereby ensuring fast, stable and flexible flight of the aircraft model, but it does not solve the problems of model placement, folding and rotation of the aircraft model. Utility Model Content

[0004] The utility model aims to provide a teaching rocket-assisted aircraft model with rotatable and foldable wings, so as to solve the problems raised in the above-mentioned background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a teaching wing rotatable foldable rocket booster aircraft model, comprising an aircraft model mechanism, the aircraft model mechanism comprising an aircraft body, a cockpit, a fixed plate at the bottom of the aircraft, a rotating shaft, a first wing, a first rocket booster and a first folding plate, a cockpit is fixedly arranged on one side of the aircraft body, a fixed plate at the bottom of the cockpit is fixedly arranged, a rotating shaft is fixedly arranged on the other side of the aircraft body, a first wing is fixedly arranged on one side of the rotating shaft, a first rocket booster is fixedly arranged at the bottom of the first wing, and a first folding plate is fixedly arranged on one side of the first wing;

[0006] A second wing is fixedly provided on the other side of the first wing, a second rocket booster is fixedly provided on the bottom end of the second wing, a second folding plate is fixedly provided on the top end of the second rocket booster, and a tail wing is fixedly provided on the top end of the fixed plate at the bottom end of the aircraft.

[0007] Preferably, a first aileron is fixedly provided on one side of the tail wing, and a second aileron is fixedly provided on one side of the first aileron, which has the beneficial effect of assisting the first wing and the second wing to help them stabilize or glide.

[0008] Preferably, a mounting and disassembly screw is fixedly provided at the bottom end of the fixing plate at the bottom end of the aircraft, which has the beneficial effect of selecting whether to fix the aircraft model in place or to disassemble it.

[0009] Preferably, a support column is fixedly provided on one side of the loading and unloading screw, and a support base is fixedly provided on the bottom end of the support column. The beneficial effect is that the aircraft model can be placed on the support column and fixed in conjunction with the loading and unloading screw.

[0010] Preferably, a fuel tank is fixedly provided on one side of the first rocket booster, which has the beneficial effect of storing fuel therein and providing a source of injection energy for the first rocket booster and the second rocket booster.

[0011] Preferably, an injection device is fixedly provided on one side of the fuel tank, which has the beneficial effect of allowing the fuel to be converted into energy and injected.

[0012] Compared with the prior art, the beneficial effects of the utility model are:

[0013] 1. When operating the device, the aircraft model can be held in the hand to perform the teaching function. When it is used up or temporarily not needed, it can be placed on the support column by installing and removing screws.

[0014] 2. The device is advantageous in that the overall structure is simple and can be more conveniently used for teaching demonstrations; a rotating shaft is provided to enable the wing to rotate at degrees; a first folding plate and a second folding plate are provided to enable partial folding; a supporting device is provided at the bottom to facilitate placement; and the first rocket booster and the second rocket booster are provided with internal structures to further facilitate teaching work. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0016] Figure 2 It is a schematic diagram of the top structure of the utility model;

[0017] Figure 3 It is a schematic diagram of the structure of one side of the utility model;

[0018] Figure 4 This is a schematic diagram of the structure of a rocket booster of the utility model.

[0019] In the figure: 1. Aircraft body; 2. Cockpit; 3. Fixed panel at the bottom of the aircraft; 4. Rotation axis; 5. First wing; 6. First rocket booster; 7. First folding panel; 8. Second wing; 9. Second rocket booster; 10. Second folding panel; 11. Tail; 12. First aileron; 13. Second aileron; 14. Loading and unloading screws; 15. Support column; 16. Support base; 17. Fuel tank; 18. Injection equipment. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0021] See also Figure 1-Figure 4 As shown, a technical solution provided by the utility model:

[0022] A teaching rocket-boosted aircraft model with rotatable and foldable wings, comprising an aircraft model mechanism, wherein the aircraft model mechanism comprises an aircraft body 1, a cockpit 2, an aircraft bottom fixed plate 3, a rotating shaft 4, a first wing 5, a first rocket booster 6 and a first folding plate 7, wherein the cockpit 2 is fixedly arranged on one side of the aircraft body 1, the aircraft bottom fixed plate 3 is fixedly arranged on the bottom end of the cockpit 2, the rotating shaft 4 is fixedly arranged on the other side of the aircraft body 1, the first wing 5 is fixedly arranged on one side of the rotating shaft 4, the first rocket booster 6 is fixedly arranged on the bottom end of the first wing 5, and the first folding plate 7 is fixedly arranged on one side of the first wing 5;

[0023] A second wing 8 is fixedly provided on the other side of the first wing 5, a second rocket booster 9 is fixedly provided on the bottom end of the second wing 8, a second folding panel 10 is fixedly provided on the top end of the second rocket booster 9, and a tail 11 is fixedly provided on the top end of the fixed panel 3 at the bottom end of the aircraft.

[0024] In this embodiment, preferably, a first aileron 12 is fixedly provided on one side of the tail wing 11, and a second aileron 13 is fixedly provided on one side of the first aileron 12, which has the beneficial effect of assisting the first wing 5 and the second wing 8 to help them stabilize or glide.

[0025] In this embodiment, preferably, a mounting screw 14 is fixedly provided at the bottom end of the aircraft bottom fixing plate 3, which has the beneficial effect of selecting whether to fix the aircraft model in place or to disassemble it.

[0026] In this embodiment, preferably, a support column 15 is fixedly provided on one side of the loading and unloading screw 14, and a support base 16 is fixedly provided on the bottom end of the support column 15. The beneficial effect is that the aircraft model can be placed on the support column 15 and fixed in conjunction with the loading and unloading screw 14.

[0027] In this embodiment, preferably, a fuel tank 17 is fixedly provided on one side of the first rocket booster 6, which has the beneficial effect of storing fuel therein and providing a source of injection energy for the first rocket booster 6 and the second rocket booster 9.

[0028] In this embodiment, preferably, a spray device 18 is fixedly provided on one side of the fuel tank 17, which has the beneficial effect of allowing the fuel to be converted into energy and sprayed out.

[0029] When using the rocket-boosted aircraft model with rotatable and foldable wings for teaching in this embodiment, the teaching function can be carried out by holding the aircraft model in the hand during operation of the device. When it is used up or temporarily not needed, it can be placed on the support column 15 by installing and removing the screws 14. The advantage of this device is that the overall structure is simple and can be more conveniently used for teaching demonstrations. The rotating shaft 4 can make the wing rotate 360°, and the first folding plate 7 and the second folding plate 10 can make it partially foldable. The bottom is equipped with a supporting device for easy placement, and the first rocket booster 6 and the second rocket booster 9 are provided with an internal structure to further carry out teaching work.

[0030] The above shows and describes the basic principle, main features and advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and descriptions are only preferred examples of the utility model and are not used to limit the utility model. Without departing from the spirit and scope of the utility model, the utility model may have various changes and improvements, which fall within the scope of the utility model to be protected. The scope of protection of the utility model is defined by the attached claims and their equivalents.

Claims

1. A rocket-assisted aircraft model with rotatable and foldable wings for teaching, characterized in that: The invention comprises an aircraft model mechanism, wherein the aircraft model mechanism comprises an aircraft body (1), a cockpit (2), a fixed plate (3) at the bottom of the aircraft, a rotating shaft (4), a first wing (5), a first rocket booster (6) and a first folding plate (7); the cockpit (2) is fixedly arranged on one side of the aircraft body (1); the fixed plate (3) at the bottom of the aircraft is fixedly arranged at the bottom of the cockpit (2); the rotating shaft (4) is fixedly arranged on the other side of the aircraft body (1); the first wing (5) is fixedly arranged on one side of the rotating shaft (4); the first rocket booster (6) is fixedly arranged at the bottom of the first wing (5); and the first folding plate (7) is fixedly arranged on one side of the first wing (5); A second wing (8) is fixedly arranged on the other side of the first wing (5), a second rocket booster (9) is fixedly arranged at the bottom end of the second wing (8), a second folding plate (10) is fixedly arranged at the top end of the second rocket booster (9), and a tail wing (11) is fixedly arranged at the top end of the fixed plate (3) at the bottom end of the aircraft.

2. A rocket-assisted aircraft model with rotatable and foldable wings for teaching use according to claim 1, characterized in that: A first aileron (12) is fixedly arranged on one side of the tail wing (11), and a second aileron (13) is fixedly arranged on one side of the first aileron (12).

3. A rocket-assisted aircraft model with rotatable and foldable wings for teaching use according to claim 1, characterized in that: A mounting and dismounting screw (14) is fixedly arranged at the bottom end of the aircraft bottom fixing plate (3).

4. A rocket-assisted aircraft model with rotatable and foldable wings for teaching use according to claim 3, characterized in that: A support column (15) is fixedly arranged on one side of the mounting and disassembly screw (14), and a support base (16) is fixedly arranged on the bottom end of the support column (15).

5. The teaching rocket-assisted aircraft model with rotatable and foldable wings according to claim 1, characterized in that: A fuel tank (17) is fixedly arranged on one side of the first rocket booster (6).

6. A rocket-assisted aircraft model with rotatable and foldable wings for teaching use according to claim 5, characterized in that: An injection device (18) is fixedly arranged on one side of the fuel tank (17).

Citation Information

Patent Citations

  • Airplane model

    CN205516486U