A self-generating helicopter simulation device
By introducing self-generating devices and automatic control systems into the aircraft model, the problem of single use experience of existing aircraft models is solved, children are able to play more enthusiastic and service life, and provide real aircraft simulation experience and environmentally friendly use effects .
Patent Information
- Application Number
- CN201911366540.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2019-12-26
- Publication Date
- 2024-12-31
- Estimated Expiration
- 2039-12-26
AI Technical Summary
Existing aircraft models lack fun after long use, reducing children's enthusiasm for use because they rely on external power supply and fixed tracks, resulting in a single user experience.
A self-generating helicopter simulation device is designed to generate power-powered propellers and rotating components through the rotation of the foot pedal, and to achieve lifting and circular motions through the adjustment rod and counterweight block, allowing children to control the helicopter's height and movement by themselves without external power supply.
It increases the enthusiasm and fun of children to play. Through self-generating power and automatic control functions, the toys last longer, providing a more realistic aircraft simulation experience, and at the same time, it has the effects of fitness and energy conservation and emission reduction.
Smart Images
Figure HDA0002338581660000011 
Figure HDA0002338581660000021
Abstract
Description
Technical Field
[0001] The invention belongs to the technical field of amusement equipment, and in particular relates to a self-generating helicopter simulation device. Background Art
[0002] Currently, most children like airplanes and yearn for the fun of sitting in an airplane and moving up and down in the air. However, existing airplane models are all powered by external power and controlled by programs, and move up and down on fixed tracks. After long-term use, they will lack fun and reduce children's enthusiasm for use. Summary of the invention
[0003] The purpose of the invention is to provide a self-generating helicopter simulation device which has a stable structure, can automatically control the height and has a long service life.
[0004] The object of the present invention is achieved in this way: a self-generating helicopter simulation device comprises a column, a rotating assembly rotatably arranged on the column, and a support rod penetrated in the rotating assembly, a first counterweight is arranged at one end of the support rod, an aircraft model is arranged at the other end of the support rod, a first seat and a second seat are arranged on the aircraft model, a mounting seat is arranged on one side of the first seat and the second seat, pedals are arranged on both sides of the mounting seat, and the pedals are connected to the self-generating device arranged in the mounting seat; an adjusting rod is arranged on one side of the second seat, the adjusting rod is rotatably arranged in the aircraft model, the other end of the adjusting rod is connected to the inner wall of the aircraft model, a first pulley is sleeved on the adjusting rod, a second pulley is connected to one side of the first pulley through a first belt, a third pulley is arranged on one side of the second pulley through a transmission assembly, a fourth pulley is connected to the upper part of the third pulley through a second belt, a fifth pulley is arranged on one side of the fourth pulley, the fifth pulley is connected to a sixth pulley through a third belt, a second counterweight is connected to the third belt, the second counterweight is slidably arranged on the support rod, and the second counterweight is moved to achieve the tilting of the support rod.
[0005] Preferably, the rotating assembly comprises a support frame rotatably arranged on a column, and a support ring for mounting a support rod is rotatably arranged in the support frame.
[0006] Preferably, the self-generating device supplies power to the propeller disposed at the upper end of the aircraft model and the rotating assembly on the column respectively.
[0007] Preferably, an anti-slip sleeve is provided on the adjusting rod.
[0008] Preferably, both the first seat and the second seat are provided with anti-slip stripes.
[0009] Preferably, armrests are provided on both sides of the first seat and the second seat.
[0010] Preferably, a protective cover is provided on the fourth pulley.
[0011] Compared with the prior art, the present invention has the following outstanding and beneficial technical effects: the self-generating helicopter simulation device of the present invention is provided with a rotating pedal on the first seat, and when the operator steps on the pedal to rotate it, the self-generating device arranged inside the mounting seat will generate electricity to supply power to the propeller of the helicopter and the rotating component on the column, and an adjusting rod is provided on one side of the second seat to control the lifting and lowering of the helicopter, and the lifting and lowering is achieved by moving the second counterweight block left and right. The entire toy does not require external power supply during use, and the height of the helicopter can be automatically controlled by the driver, and the helicopter can be made to perform a circular motion around the column by stepping on the pedal. The whole process is full of fun and can arouse children's interest to the greatest extent, increasing their enthusiasm for playing. BRIEF DESCRIPTION OF THE DRAWINGS
[0012] Figure 1 It is a structural diagram of the present invention;
[0013] Figure 2 It is a structural diagram of the interior of the aircraft model of the present invention. DETAILED DESCRIPTION
[0014] The present invention is further described below with reference to specific embodiments.
[0015] like Figure 1-2 As shown, a self-generating helicopter simulation device comprises a column 1, a rotating assembly 2 rotatably arranged on the column 1, and a support rod 3 inserted into the rotating assembly 2, wherein one end of the support rod 3 is provided with a first counterweight 4, and the other end of the support rod 3 is provided with an aircraft model 5, and the aircraft model 5 is provided with a first seat 6 and a second seat 7, and one side of the first seat 6 and the second seat 7 is provided with a mounting seat 8, and both sides of the mounting seat 8 are provided with foot pedals 9, and the foot pedals 9 are connected to the self-generating device arranged in the mounting seat 8; one side of the second seat 7 is provided with an adjusting rod 10, and the adjusting rod 10 is rotatably inserted into the aircraft model 5, and the other end of the adjusting rod 10 is connected to the self-generating device arranged in the mounting seat 8. The inner wall of the aircraft model 5 is connected, and a first pulley 11 is sleeved on the adjusting rod 10. One side of the first pulley 11 is connected to a second pulley 13 through a first belt 12, and one side of the second pulley 13 is provided with a third pulley 15 connected through a transmission assembly 14, and the third pulley 15 is connected to a fourth pulley 17 through a second belt 16, and one side of the fourth pulley 17 is provided with a fifth pulley 18, and the fifth pulley 18 is connected to a sixth pulley 20 through a third belt 19, and a second counterweight block 21 is connected to the third belt 19, and the second counterweight block 21 is slidably set on the support rod 3, and the second counterweight block 21 is moved to realize the tilting of the support rod 3.
[0016] The self-generating helicopter simulation device of the present technical solution is provided with a foot pedal 9 on the first seat 6. When the operator steps on the foot pedal 9 to rotate the foot pedal 9, the self-generating device arranged inside the mounting seat 8 will generate electricity to supply power to the propeller 24 of the helicopter and the rotating component 2 on the column 1. An adjusting rod 10 is provided on one side of the second seat 7 to control the lifting and lowering of the helicopter. The lifting and lowering is achieved by moving the second counterweight block 21 left and right. The entire toy does not require external power supply during use, and the height of the helicopter can be automatically controlled by the driver. By stepping on the foot pedal 9, the helicopter moves in a circle around the column 1. The whole process is interesting and can arouse children's interest to the greatest extent and increase their enthusiasm for playing.
[0017] The self-generating device comprises a fixed frame and a magnetic flux line cutting wheel rotatably mounted in the fixed frame, wherein the magnetic flux line cutting wheel cuts the magnetic flux lines when rotating, thereby achieving the effect of self-generating electricity and supplying the generated electricity to various components.
[0018] The transmission assembly 14 includes a first bevel gear coaxially arranged with the second pulley 13 , a second bevel gear is meshed with the first bevel gear, and a transmission rod connected to the third pulley 15 is penetrated through the second bevel gear.
[0019] Preferably, the rotating assembly 2 includes a support frame 22 rotatably disposed on the column 1, and a support ring 23 for mounting the support rod 3 is rotatably disposed in the support frame 22. The support frame 22 can rotate on the column 1 so that the aircraft model 5 can perform a circular motion around the column 1, and the support ring 23 can rotate on the support frame 22 so that the aircraft model 5 can be raised or lowered.
[0020] Preferably, the self-generating device supplies power to the propeller 24 disposed on the upper end of the aircraft model 5 and the rotating assembly 2 on the column 1. The propeller 24 disposed on the aircraft model 5 rotates to arouse the interest of children in hitting the aircraft model 5, simulating the real state of the aircraft to a greater extent, and the self-generating device not only helps the operator to exercise, but also achieves the purpose of energy saving and emission reduction.
[0021] Preferably, an anti-slip cover 25 is provided on the adjusting rod 10. The anti-slip cover 25 can allow the operator to better control the adjusting rod 10, thereby increasing its practical performance.
[0022] Preferably, the first seat 6 and the second seat 7 are both provided with anti-skid stripes 26. The anti-skid stripes 26 can make it safer for the user to sit on the first seat 6 and the second seat 7, and increase the friction between the first seat 6 and the second seat 7.
[0023] Preferably, armrests 27 are provided on both sides of the first seat 6 and the second seat 7. The armrests 27 are provided to make the user safer and prevent dangerous accidents from occurring when the aircraft model 5 is raised, lowered or rotated.
[0024] Preferably, a protective cover 28 is provided on the fourth pulley 17. The protective cover 28 can prevent the fourth pulley 17 from being corroded by dust in the outside air, which may affect the transmission effect of the fourth pulley 17.
[0025] The above embodiments are only preferred embodiments of the present invention and are not intended to limit the protection scope of the present invention. Therefore, any equivalent changes made based on the structure, shape, and principle of the present invention should be included in the protection scope of the present invention.
Claims
1. A self-generating helicopter simulation device, characterized in that: The invention comprises a column (1), a rotating assembly (2) rotatably arranged on the column (1), and a support rod (3) inserted into the rotating assembly (2); a first counterweight (4) is arranged at one end of the support rod (3); an aircraft model (5) is arranged at the other end of the support rod (3); a first seat (6) and a second seat (7) are arranged on the aircraft model (5); a mounting seat (8) is arranged on one side of the first seat (6) and the second seat (7); pedals (9) are arranged on both sides of the mounting seat (8); the pedals (9) are connected to a self-generating device arranged in the mounting seat (8); an adjusting rod (10) is arranged on one side of the second seat (7); the adjusting rod (10) is rotatably inserted into the aircraft model (5); the other end of the adjusting rod (10) is connected to the inner wall of the aircraft model (5); the adjusting rod (10) The upper sleeve is provided with a first pulley (11), one side of the first pulley (11) is connected to a second pulley (13) via a first belt (12), one side of the second pulley (13) is provided with a third pulley (15) connected to the second pulley via a transmission assembly (14), the third pulley (15) is connected to a fourth pulley (17) via a second belt (16), one side of the fourth pulley (17) is provided with a fifth pulley (18), the fifth pulley (18) is connected to a sixth pulley (20) via a third belt (19), and the third belt (19) is connected to a second counterweight (21). The second counterweight (21) is slidably arranged on the support rod (3), and the support rod (3) is tilted by moving the second counterweight (21). The rotating assembly (2) comprises a support frame (22) rotatably arranged on the column (1), and a support ring (23) for mounting the support rod (3) is rotatably arranged in the support frame (22). The self-generating device supplies power to a propeller (24) arranged at the upper end of the aircraft model (5) and the rotating assembly (2) on the column (1), respectively. The adjusting rod (10) is provided with an anti-slip sleeve (25).
2. The self-generating helicopter simulation device according to claim 1, characterized in that: The first seat (6) and the second seat (7) are both provided with anti-slip stripes (26).
3. The self-generating helicopter simulation device according to claim 1, characterized in that: Armrests (27) are provided on both sides of the first seat (6) and the second seat (7).
4. The self-generating helicopter simulation device according to claim 1, characterized in that: The fourth pulley (17) is provided with a protective cover (28).