Aerial bicycle track and aerial bicycle system

Abstract

The present invention relates to the technical field of sports equipment, and specifically to an aerial bicycle track and an aerial bicycle system, comprising a plurality of installation piles distributed at intervals, wherein the installation piles include installation columns and installation beams across the installation columns fixed on the tops of the installation columns, wherein one end of all the installation beams is connected to a first guide rail, and the other end of all the installation beams is connected to a second guide rail, wherein the first guide rail and the second guide rail are both formed with guide channels for the suspension and movement of a driving wheel assembly, and the system has two guide rails.

Claims

1. An in-flight entertainment system, It is characterized in that The invention comprises an aerial bicycle track and an aerial bicycle capable of hanging and walking on the aerial bicycle track; The aerial bicycle track comprises a plurality of installation piles distributed at intervals, wherein the installation piles comprise installation columns (d1) and installation beams (d2) fixed on the tops of the installation columns (d1) and spanning the installation columns (d1); one end of all the installation beams (d2) is connected to a first guide rail (e1), and the other end of all the installation beams (d2) is connected to a second guide rail (e2); a guide channel (e0) for the driving wheel assembly to be suspended and travel is formed in the first guide rail (e1) and the second guide rail (e2); a travel opening (g) is formed at the bottoms of the first guide rail (e1) and the second guide rail (e2) and is opened along the travel direction for the front support column (a) and the rear support column (b) of the aerial bicycle to extend upward and pass forward and backward; The aerial bicycle comprises a cabin (1) for passengers to ride in and a counterweight balancing mounting beam seat (2) extending forward and backward arranged above the cabin (1); a front support column (a) extending upward and a rear support column (b) extending upward are fixed to the counterweight balancing mounting beam seat (2); a driving wheel assembly is installed on the top of the front support column (a); an auxiliary wheel assembly is installed on the top of the rear support column (b); a human pedal assembly for providing power to the driving wheel assembly is also installed on the cabin (1); a front suspension column (3) and a rear suspension column (4) extending upward from the cabin (1) are fixed to the cabin (1); the front suspension column (3) and the rear suspension column (4) are both suspended on the counterweight balancing mounting beam seat (2) and can swing left and right; the counterweight balancing mounting beam seat (2) comprises a bottom plate (21) and a left inclined plate (22) extending upward and leftward and a right inclined plate (22) respectively fixedly connected to the left and right sides of the bottom plate (21). The bottom plate (21), the left inclined plate (22) and the right inclined plate (23) surround a mounting groove (20) with an opening facing upward and in the shape of an inverted trapezoid. The head of the front suspension column (3) extends into the mounting groove (20). The head of the rear suspension column (4) also extends into the mounting groove (20). The counterweight balancing mounting beam seat (2) is provided with a front swing limit hole (201) which passes through the front suspension column (3) up and down. The left-right length dimension of the front swing limit hole (201) is greater than the left-right length dimension of the portion of the front suspension column (3) passing through the front swing limit hole (201); the counterweight balance mounting beam seat (2) is also provided with a rear swing limit hole (202) which is vertically through-through and for the rear suspension column (4) to pass through vertically; the left-right length dimension of the rear swing limit hole (202) is greater than the left-right length dimension of the portion of the rear suspension column (4) passing through the rear swing limit hole (202).

2. An in-flight entertainment system according to claim 1, It is characterized in that Two side mounting reinforcement plates (d20) extending downward and spaced apart are fixed at the bottom of both ends of the mounting crossbeam (d2); an inverted U-shaped positioning groove (dd) for inserting and installing a first guide rail (e1) or a second guide rail (e2) is formed between the two side mounting reinforcement plates (d20) at the same end of the mounting crossbeam (d2) and the bottom of the mounting crossbeam (d2); the first guide rail (e1) or the second guide rail (e2) is installed and fixed in the inverted U-shaped positioning groove (dd).

3. An in-flight entertainment system according to claim 1, It is characterized in that The first guide rail (e1) and the second guide rail (e2) are both formed by splicing a plurality of guide rail segments (e01).

4. An in-flight entertainment system according to claim 3, It is characterized in that The guide rail segment (e01) is fixed with a splicing plate (f) at the splicing position.

5. An in-flight entertainment system according to claim 1, It is characterized in that The first guide rail (e1) and the second guide rail (e2) are both formed with a curved portion and a straight portion.

6. An in-flight entertainment system according to claim 1, It is characterized in that The first guide rail (e1) and the second guide rail (e2) are formed with vertically staggered sections.

7. An in-flight entertainment system according to claim 1, It is characterized in that The first guide rail (e1) and the second guide rail (e2) are formed with left-right staggered sections.

8. An in-flight entertainment system according to claim 1, It is characterized in that The guide channel (e0) is in communication with the travel opening (g), and the guide channel (e0) is in a U-shaped channel structure with the opening facing upward.

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