Amusement equipment self-control aircraft cockpit structure
By introducing structures such as cockpit brackets, swing components, and limit plates into the self-controlled aircraft cockpit of amusement equipment, the problems of limited movement modes and insufficient safety have been solved, realizing an entertainment experience and improved safety of tilting and gliding aircraft.
Patent Information
- Application Number
- CN202421408871.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-20
- Publication Date
- 2026-01-02
- Estimated Expiration
- 2034-06-20
AI Technical Summary
Existing amusement rides with self-controlled airplanes have a single movement mode and lack the ability to swing and glide from side to side, resulting in poor safety and failing to provide a comfortable and safe experience.
An autonomous aircraft cockpit structure was designed, comprising a cockpit bracket, a cockpit, a swing assembly, a limiting plate, and a fixing assembly. The swing assembly enables the cockpit to swing left and right, while the limiting plate and fixing assembly enhance safety and improve passenger stability.
This allows tourists to experience the sensation of an airplane tilting and gliding, enhancing the entertainment experience while also improving the safety of the equipment and preventing unnecessary movement of tourists in the cabin.
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Figure CN223746955U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the technical field of recreation equipment, specifically relates to a recreation equipment self -control airplane cabin structure. BACKGROUND
[0002] The common self -control airplane type amusement machine in the recreation ground is old -fashioned structure, and the movement mode only has two movement modes of the revolution of the cabin around the central column and the up and down swing of the supporting arm, specifically, people control the equipment large arm to lift the passenger cabin to ascend or descend, and slowly rotate around the center, so that the tourists experience the feeling of flying.
[0003] The existing recreation equipment self -control airplane cabin structure movement structure is single, does not have the function of the left and right swing gliding of the cabin, and the safety is poor, there is certain high altitude danger, and can not bring the comfortable and safe experience to the tourists, to solve the problems proposed above, the utility model provides a recreation equipment self -control airplane cabin structure. UTILITY MODEL CONTENTS
[0004] The utility model is aimed at: to solve the problems proposed in the background art, the utility model provides a recreation equipment self -control airplane cabin structure.
[0005] The utility model discloses a kind of recreation equipment self -control airplane cabin structures, including: cabin bracket;Cabin, the cabin is installed at the top of the cabin bracket, seat is fixedly installed on the cabin;Swing component, the swing component is installed on the cabin bracket, it is used to drive the left and right swing of the cabin, the swing component includes rotationally installed in the top of the cabin bracket rotating frame, the cabin is fixedly installed in the top of the rotating frame, one side of the cabin bracket is fixedly installed with mounting plate, one side of the mounting plate is rotationally installed with pneumatic cylinder, and the telescopic end of the pneumatic cylinder is rotationally connected between the rotating frame;Limiting plate, the number is two, two The limiting plate is symmetrically distributed and is rotationally installed on the seat by damping pivot, it is used to limit the protection of end sitting tourist, the limiting plate is installed with the fixed component for connecting and fixing two The limiting plate.
[0006] Further, one side of the mounting plate is rotationally installed with first rotating block, the telescopic end of the pneumatic cylinder is fixedly installed with second rotating block, one end of the second rotating block is rotationally installed between the two sides of the inner wall of the rotating frame.
[0007] Further, the fixed component includes two half cylinders fixedly installed on one side of two The limiting plate, one side of two The half cylinder is fixedly installed with baffle, fixed plate is tightly sleeved between two The half cylinder, one side of the fixed plate is fixedly installed with short rod, one end of the short rod is inserted and passes through the baffle and the half cylinder.
[0008] Further, the top of the cabin bracket is rotatably provided with two telescopic rods, one end of the two telescopic rods is fixedly connected with the bottom of the cabin.
[0009] Further, the top of the cabin is fixedly provided with a sun shield.
[0010] Further, the outer surface of the seat and the outer surface of the limiting plate are both fixedly provided with rubber pads.
[0011] The beneficial effects of the present application are as follows:
[0012] The swing assembly can drive the cabin to swing, and the lifting and rotating functions of the self-controlled airplane are combined, so that the tourists can experience the feeling of airplane tilting and gliding, the entertainment experience effect of the tourists is greatly improved, and the safety of the equipment is improved compared with the existing safety rope, so that the tourists are not easy to move when sitting on the seat, and the use of people is facilitated. BRIEF DESCRIPTION OF DRAWINGS
[0013] Figure 1 is a perspective view of the present application;
[0014] Figure 2 is a perspective view of the present application Figure 1 ;
[0015] Figure 3 is a partial structure sectional view of the present application Figure 1 ;
[0016] Figure 4 is a structure explosion view of the fixing assembly in the present application Figure 1 .
[0017] Significant: 1, cabin bracket; 2, cabin; 3, seat; 4, swing assembly; 41, rotating frame; 42, mounting plate; 43, air cylinder; 5, limiting plate; 6, fixing assembly; 61, semicircular column; 62, baffle; 63, fixed plate; 64, short rod; 7, first rotating block; 8, second rotating block; 9, telescopic rod; 10, sun shield; 11, rubber pad. DETAILED DESCRIPTION
[0018] In order to make the purpose, technical scheme and advantages of the embodiments of the present application more clear, the technical scheme in the embodiments of the present application will be described clearly and completely with reference to the drawings in the embodiments of the present application.
[0019] As Figures 1-4The utility model discloses an amusement equipment self -control aircraft cockpit structure, including: cockpit bracket 1, cockpit bracket 1 is connected with the supporting arm of this kind of self -control aircraft equipment.
[0020] The cockpit 2 is installed on the top of the cockpit bracket 1, and the seat 3 is fixedly installed on the cockpit 2.
[0021] The swing assembly 4 is installed on the cockpit bracket 1, which is used to drive the cockpit 2 to swing left and right, and the swing assembly 4 includes a rotating frame 41 rotatably installed on the top of the cockpit bracket 1, the cockpit 2 is fixedly installed on the top of the rotating frame 41, one side of the cockpit bracket 1 is fixedly installed with a mounting plate 42, one side of the mounting plate 42 is rotatably installed with a pneumatic cylinder 43, and the telescopic end of the pneumatic cylinder 43 is rotatably connected with the rotating frame 41.
[0022] The first rotating block 7 and the second rotating block 8 are arranged, which facilitates the movement of the two ends of the pneumatic cylinder 43, so that the pneumatic cylinder 43 can drive the rotating frame 41 to swing when it is telescopic.
[0023] The limiting plate 5 is symmetrically distributed on the seat 3 through a damping rotating shaft, which is used for limiting and protecting the tourists sitting on the seat, and the limiting plate 5 is installed with a fixing assembly 6 for connecting and fixing the two limiting plates 5.
[0024] When the tourists need to experience this entertainment project, first, sit on the seat 3, then rotate the limiting plate 5, so that the two sides of the limiting plate 5 are close to each other, then use the fixing assembly 6 to connect and fix them, and two semicircular grooves are arranged below the limiting plate 5 for placing the legs of the tourists, at this time, the limiting plate 5 can be used for limiting and fixing the body of the tourists, avoiding the tourists moving randomly, causing the equipment to fall when moving, after the body of the tourists is fixed, the telescopic end of the pneumatic cylinder 43 can be telescopic, so as to push or pull the rotating frame 41, and then realize the swing of the rotating frame 41, and drive the cockpit 2 on the top of the rotating frame 41 to swing, cooperate with the lifting and rotating functions of the self -control aircraft, so that the tourists can experience the feeling of aircraft inclined gliding, greatly improve the entertainment experience effect of the tourists, and the limiting plate 5 is relative to the existing safety rope, which improves the safety of the equipment, so that the tourists are not easy to move on the seat 3.
[0025] Therefore, compared with the prior art, the cabin can be swung by the swinging assembly, the lifting and rotating functions of the self-controlled airplane are matched, tourists can experience the feeling of airplane inclined gliding, the entertainment experience effect of the tourists is greatly improved, the safety of the equipment is improved compared with the existing safety rope, the tourists are not easy to move when sitting on the seat, and use of people is facilitated
[0026] As Figure 1 and Figure 4 As shown in some embodiments, the fixing assembly 6 comprises two semicylinders 61 fixedly installed on one side of the two limiting plates 5 respectively, the semicylinders 61 are fixedly installed with baffles 62 on one side, the semicylinders 61 are tightly sleeved with a fixed plate 63, the fixed plate 63 is fixedly installed with a short rod 64 on one side, and the short rod 64 is inserted through the baffles 62 and the semicylinders 61. The fixed plate 63 is provided with a slot, which has the same shape as the combined shape of the two baffles 62, and the shape of the slot is a circle with symmetrically cut off two ends. The short rod 64 can limit the random movement of the fixed plate 63, avoiding loosening of the limiting structure.
[0027] The side of the fixed plate 63 adjacent to the baffle 62 is tightly fitted, when the two limiting plates 5 need to be fixed, the slot on the fixed plate 63 is aligned with the shape formed when the two baffles 62 are fitted, then the short rod 64 is inserted into the baffle 62, the fixed plate 63 is pushed through the baffle 62 to be located in the same plane as the semicylinder 61, the fixed plate 63 is rotated to 90°, so that the baffle 62 can limit the fixed plate 63, thereby limiting and fixing the limiting plate 5.
[0028] As Figure 1 shown, in some embodiments, the top of the cabin bracket 1 is rotatably installed with two telescopic rods 9, and one end of the telescopic rod 9 is fixedly connected with the bottom of the cabin 2.
[0029] The telescopic rod 9 increases the connection support stability between the cabin bracket 1 and the telescopic rod 9, so that the cabin 2 can be stably swung and is not easy to be damaged.
[0030] As Figure 2 shown, in some embodiments, the top of the cabin 2 is fixedly installed with a sun visor 10.
[0031] When the weather is hot, the sun visor 10 can block strong sunlight, avoiding tourists being directly exposed to the sun and hot, and improving the comfortable experience effect of tourists playing.
[0032] As Figure 1 shown, in some embodiments, the outer surface of the seat 3 and the outer surface of the limiting plate 5 are fixedly installed with rubber protective pads 11.
[0033] The existing cockpit seat is a plastic hard shell, and the tourist experiences poor in sitting, and the rubber pad 11 can increase the softness, and improve the comfort.
[0034] The above description of disclosed embodiments enables one of ordinary skill in the art to make or use the application. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein can be applied to other embodiments without departing from the spirit or scope of the application. Thus, the present application is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims
1. An amusement ride self-pilot aircraft cockpit structure, characterized by, The utility model relates to a cockpit bracket (1) for a sightseeing vehicle, comprising: a cockpit (2) mounted on the top of the cockpit bracket (1), the cockpit (2) being fixedly installed with a seat (3); a swing assembly (4) mounted on the cockpit bracket (1) for swinging the cockpit (2) left and right, the swing assembly (4) comprising a rotating frame (41) rotatably mounted on the top of the cockpit bracket (1), the cockpit (2) being fixedly installed on the top of the rotating frame (41), one side of the cockpit bracket (1) being fixedly installed with a mounting plate (42), one side of the mounting plate (42) being rotatably installed with a pneumatic cylinder (43), the pneumatic cylinder (43) being rotatably connected between the telescopic end and the rotating frame (41); two limiting plates (5) symmetrically distributed and rotatably mounted on the seat (3) through a damping rotating shaft, the limiting plates (5) being used for limiting and protecting the end sitting tourists, the limiting plates (5) being installed with a fixing assembly (6) for connecting and fixing the two limiting plates (5). One side of the mounting plate (42) is rotatably installed with a first rotating block (7), the telescopic end of the pneumatic cylinder (43) is fixedly installed with a second rotating block (8), one end of the second rotating block (8) being rotatably installed between the inner walls of the rotating frame (41).
2. The amusement ride self-control cockpit structure according to claim 1, characterized in that, The fixing assembly (6) comprises two semicylinders (61) fixedly installed on one side of the two limiting plates (5), the semicylinders (61) being fixedly installed with baffles (62) on one side, the semicylinders (61) being tightly sleeved with a fixing plate (63) between them, the fixing plate (63) being fixedly installed with a short rod (64) on one side, one end of the short rod (64) being inserted through the baffle (62) and the semicylinder (61).
3. The amusement ride self-control cockpit structure according to claim 1, characterized in that, The top of the cockpit bracket (1) is rotatably installed with two telescopic rods (9), one end of the telescopic rods (9) being fixedly connected with the bottom of the cockpit (2).
4. The amusement ride self-control cockpit structure according to claim 1, characterized in that, The top of the cockpit (2) is fixedly installed with a sun visor (10).
5. The amusement ride self-control cockpit structure according to claim 1, characterized in that, The outer surfaces of the seat (3) and the limiting plates (5) are fixedly installed with rubber protective pads (11).
6. The amusement ride self-control cockpit structure according to claim 1, characterized in that,