Aircraft cabin with high safety

Abstract

The utility model provides an aircraft cabin with high safety, which relates to the field of amusement park equipment and comprises an integral frame and a riding unit, the integral frame comprises an airship track for bearing the riding unit, and the riding unit comprises an airship rear sensing module arranged on the right side of the airship track. The airship front sensing module is arranged on the left side of the airship track; the airship driving vehicle, the airship driven vehicle, the airship rear sensing module and the airship front sensing module are arranged to be matched with the travel switch, so that the airship cabin can form a closed loop in the movement process from starting, acceleration, constant speed to deceleration and stopping, and in the braking stage, when the airship cabin passes through the airship rear sensing module and the airship front sensing module, the airship cabin can be driven to move to the airship rear sensing module and the airship front sensing module. The travel switch controls braking, and when the travel switch cannot complete braking due to faults, the proximity switch serving as a standby proximity switch can play a role in secondary protection, and normal braking of equipment is guaranteed.

Description

Technical Field

[0001] The utility model belongs to the field of amusement park equipment, in particular to an aircraft cockpit with high safety. Background Art

[0002] A rotating track spaceship is a track-type amusement device in a theme park. It is usually designed to simulate the appearance of a spaceship. It runs along a rotating track to simulate the feeling of flight or space travel. The passenger cabin usually has a certain tilt angle to enhance the flight experience. The track design usually includes up and down or rotating movements to increase the sense of excitement. Overall, it combines the characteristics of rotation and orbital motion to provide a unique entertainment experience.

[0003] Since the Paradise Orbital Spacecraft has no secondary braking protection during operation, if there is an electrical fault in the control system or a signal transmission problem, the Paradise Orbital Spacecraft may become stuck or stop during operation, posing a huge safety hazard.

[0004] In summary, the present invention provides a highly safe aircraft cockpit to solve the above problems. Utility Model Content

[0005] In order to solve the above technical problems, the present invention provides the following technical solutions:

[0006] A highly safe aircraft cockpit, comprising an integral frame and a seating unit.

[0007] The overall frame includes spacecraft tracks for carrying the ride units;

[0008] The riding unit includes a spacecraft cabin arranged on the spacecraft track, a spacecraft cabin hanging shaft arranged on both sides of the top of the spacecraft cabin, a spacecraft driving vehicle arranged on the top of the left spacecraft cabin hanging shaft, a spacecraft driven vehicle arranged on the top of the right spacecraft cabin hanging shaft, a spacecraft rear sensing module arranged on the right side of the spacecraft track, and a spacecraft front sensing module arranged on the left side of the spacecraft track;

[0009] The vehicle also includes a travel switch and a proximity switch which are arranged on both sides of the spacecraft driving vehicle.

[0010] Furthermore, in the present invention, the spacecraft driving vehicle and the spacecraft driven vehicle are both slidably connected to the spacecraft track.

[0011] Furthermore, in the present invention, traffic lights are provided on the overall frame, with one on each side, and the spacecraft rear sensing module and the spacecraft front sensing module are located between the two traffic lights.

[0012] Furthermore, in the present invention, the overall frame also includes a console and a safety door arranged on one side.

[0013] Furthermore, in the present invention, the spacecraft track is composed of steel structure washers, steel structure nuts and steel structure bolts.

[0014] Beneficial effects: The utility model has the following beneficial effects:

[0015] The utility model arranges a spacecraft driving vehicle, a spacecraft driven vehicle, a spacecraft rear sensing module and a spacecraft front sensing module in cooperation with a travel switch, so that the movement process of the spacecraft cabin from starting, acceleration, constant speed to deceleration and stopping can form a closed loop. In the braking stage, when the spacecraft cabin passes through the spacecraft rear sensing module and the spacecraft front sensing module, the travel switch controls the braking. When the travel switch cannot complete the braking due to a fault, the proximity switch as a backup can play a secondary protection role to ensure normal braking of the equipment. Through the setting of the secondary protection system, if any one system has a problem, the other one can play a secondary protection role to ensure normal braking of the equipment. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 This is a schematic diagram of the main structure of the riding unit of the utility model;

[0017] Figure 2 This is a schematic diagram of the structure of the riding unit of the utility model from a top view;

[0018] Figure 3 This is a side structural diagram of the riding unit of the utility model;

[0019] Figure 4 This is a schematic diagram of the overall frame structure of the utility model;

[0020] Figure 5 It is an enlarged schematic diagram of the local structure of A1 of the utility model;

[0021] Figure 6 It is an enlarged schematic diagram of the local structure of A2 of the present utility model.

[0022] In the picture:

[0023] 1. Overall frame; 101. Spacecraft track; 102. Traffic light; 2. Passenger unit; 201. Spacecraft cabin; 202. Spacecraft cabin suspension shaft; 203. Spacecraft drive vehicle; 204. Spacecraft driven vehicle; 205. Spacecraft rear sensing module; 206. Spacecraft front sensing module. DETAILED DESCRIPTION

[0024] In order to better understand the technical content of the present invention, specific embodiments are given and described as follows in conjunction with the accompanying drawings. Various aspects of the present invention are described in this disclosure with reference to the accompanying drawings, in which many illustrative embodiments are shown. The embodiments of the present disclosure are not necessarily defined to include all aspects of the present invention. It should be understood that the various concepts and embodiments introduced above, as well as those described in more detail below, can be implemented in any of many ways, because the concepts and embodiments disclosed in the present invention are not limited to any implementation method. In addition, some aspects disclosed in the present invention can be used alone or in any appropriate combination with other aspects disclosed in the present invention.

[0025] Example 1

[0026] like Figure 1-4 FIG. 1 is a first embodiment of the present invention, which provides a highly safe aircraft cabin, including an overall frame 1 and a seating unit 2.

[0027] The overall frame 1 includes a spacecraft track 101 for carrying the ride unit 2;

[0028] The riding unit 2 includes a spaceship cabin 201 disposed on the spaceship track 101, spaceship cabin suspension shafts 202 disposed on both sides of the top of the spaceship cabin 201, a spaceship driving vehicle 203 disposed on the top of the left spaceship cabin suspension shaft 202, a spaceship driven vehicle 204 disposed on the top of the right spaceship cabin suspension shaft 202, a spaceship rear sensing module 205 disposed on the right side of the spaceship track 101, and a spaceship front sensing module 206 disposed on the left side of the spaceship track 101;

[0029] The vehicle also includes a travel switch 203a and a proximity switch 203b disposed on both sides of the vehicle.

[0030] like Figure 1-4As shown, the overall frame 1 is fixed to the spacecraft track 101 by steel washers, steel nuts and steel bolts. The spacecraft cabin hanging shaft 202 is used to connect the spacecraft cabin 201. The spacecraft driving vehicle 203 and the spacecraft driven vehicle 204 are used to drive the spacecraft cabin 201 to run on the spacecraft track 101. By arranging the spacecraft driving vehicle 203, the spacecraft driven vehicle 204, the spacecraft rear sensing module 205 and the spacecraft front sensing module 206 to cooperate with the limit switch 203a, the movement process of the spacecraft cabin 201 from starting, acceleration, constant speed to deceleration and stopping can form a closed loop. During the braking phase, when the spacecraft cabin 201 passes through the spacecraft rear sensing module 205 and the spacecraft front sensing module 206, the limit switch 203a controls the braking. If the limit switch 203a fails to complete the braking due to a fault, the backup proximity switch 203b can serve as a secondary protection to ensure normal braking of the equipment. By setting up the secondary protection system, if any system fails, the other system can serve as a secondary protection to ensure normal braking of the equipment.

[0031] Example 2

[0032] Reference Figure 4-6 , which is the second embodiment of the present utility model, and this embodiment is based on the previous embodiment.

[0033] In this embodiment, the spacecraft driving vehicle 203 and the spacecraft driven vehicle 204 are both slidably connected to the spacecraft track 101 .

[0034] Traffic lights 102 are provided on the overall frame 1 , with one on each side. The spacecraft rear sensing module 205 and the spacecraft front sensing module 206 are located between the two traffic lights 102 .

[0035] The overall frame 1 further includes a console and a safety door arranged on one side.

[0036] The spacecraft track 101 is composed of steel structure washers, steel structure nuts and steel structure bolts.

[0037] like Figure 4-6 As shown, the traffic lights 102 are fixed to the overall frame 1 by fasteners. The traffic lights 102 are set to remind passengers, that is, when the spacecraft cabin 201 enters between the two traffic lights 102, the spacecraft rear sensing module 205 and the spacecraft front sensing module 206 successively trigger the two spacecraft cabin hanging shafts 202 to make red and green light prompts respectively. The green light indicates that the equipment has completed braking and passengers can enter the spacecraft cabin 201 from the safety door on one side. The red light indicates that the equipment has completed braking and is waiting for passengers to board. The spacecraft track 101 is composed of steel structure washers, steel structure nuts and steel structure bolts. The connection between the spacecraft track 101 and the overall frame 1 is also composed of steel structure washers, steel structure nuts and steel structure bolts, which improves the stability of the main load-bearing components of the equipment.

[0038] In use, when the spacecraft cabin 201 enters between the two traffic lights 102, the spacecraft rear sensing module 205 and the spacecraft front sensing module 206 trigger the two traffic lights 102 to make red light and green light prompts in turn, respectively, and the green light indicates that the device has completed braking, and the passengers can enter the spacecraft cabin 201 from the side safety door, and the red light indicates that the device has completed braking and is waiting for passengers, and in the braking stage, when the spacecraft cabin 201 passes through the spacecraft rear sensing module 205 and the spacecraft front sensing module 206, the travel switch 203a controls braking, and when the travel switch 203a fails to complete braking, the proximity switch 203b as a backup can play a secondary protection role, to ensure normal braking of the device, and through the setting of the secondary protection system, it is ensured that if any one system fails, the other can play a secondary protection role, to ensure normal braking of the device.

[0039] The standard parts used in the present application file can be purchased from the market, and can be ordered according to the description and the drawings, and the specific connection mode of each part adopts the conventional means such as bolts, rivets and welding in the prior art, the mechanical parts and equipment adopt conventional models in the prior art, the control mode is automatically controlled through a controller, and the control circuit of the controller can be realized by simple programming of the person skilled in the art, which belongs to the common knowledge in the art, and the present application is mainly used to protect the mechanical device, so the control mode and circuit connection will not be explained in detail.

[0040] Although the present application has been disclosed as above with preferred embodiments, it is not intended to limit the present application. Those skilled in the art can make various modifications and decorations without departing from the spirit and scope of the present application. Therefore, the protection scope of the present application shall be subject to the definition of the claims.

Claims

1. A highly safe aircraft cockpit, characterized by: It comprises an overall frame (1) and a riding unit (2), The overall frame (1) includes a spacecraft track (101) for carrying the riding unit (2); The riding unit (2) comprises a spacecraft cabin (201) arranged on the spacecraft track (101), spacecraft cabin hanging shafts (202) arranged on both sides of the top of the spacecraft cabin (201), a spacecraft driving vehicle (203) arranged on the top of the spacecraft cabin hanging shaft (202) on the left side, a spacecraft driven vehicle (204) arranged on the top of the spacecraft cabin hanging shaft (202) on the right side, a spacecraft rear sensing module (205) arranged on the right side of the spacecraft track (101), and a spacecraft front sensing module (206) arranged on the left side of the spacecraft track (101); The vehicle also includes a travel switch (203a) and a proximity switch (203b) arranged on both sides of the spacecraft driving vehicle (203).

2. The high-safety aircraft cockpit according to claim 1, characterized in that: The spacecraft driving vehicle (203) and the spacecraft driven vehicle (204) are both slidably connected to the spacecraft track (101).

3. The high-safety aircraft cockpit according to claim 1, characterized in that: Traffic lights (102) are provided on the overall frame (1), with one traffic light (102) on each side. The spacecraft rear sensing module (205) and the spacecraft front sensing module (206) are located between the two traffic lights (102).

4. The high-safety aircraft cockpit according to claim 1, characterized in that: The overall frame (1) also includes a control console and a safety door arranged on one side.

5. The highly safe aircraft cockpit according to claim 1, characterized in that: The spacecraft track (101) is composed of a steel structure washer, a steel structure nut and a steel structure bolt.

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