Aerospace vacuum environment simulation cabin

Abstract

The utility model relates to the technical field of aviation flight, in particular to an aerospace vacuum environment simulation cabin which comprises a cabin body. The bearing bottom cover is fixedly welded to one side of the cabin body and used for blocking one side of the cabin body; the cabin cover is hinged to the other side of the cabin body and used for opening and closing the simulation empty cabin; the two bearing bases are arranged at the lower end of the cabin body in a spaced mode; the number of the bearing lantern rings is two, the two bearing lantern rings are arranged on the cabin body in a sleeving mode at intervals, and the lower ends of the bearing lantern rings are connected with the two bearing bases correspondingly; the load-bearing cross beam is transversely arranged at the upper end of the cabin body, and the two ends of the load-bearing cross beam are connected with the two load-bearing lantern rings respectively; the number of the lifting rings is two, and the lifting rings are arranged at the upper end of the bearing cross beam at intervals, so that the problems that when the aerospace vacuum environment simulation bin is lifted and carried, time and labor are wasted, the outer wall of the aerospace vacuum environment simulation bin is easily damaged, and normal use of the aerospace vacuum environment simulation bin is affected are solved.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation flight, in particular to an aerospace vacuum environment simulation chamber. Background Art

[0002] The aerospace vacuum environment simulation chamber is a kind of simulated flight, which can be used as a device for the initial training of professional pilots. At the same time, it can also be used as a device for ordinary users to experience real flight. The flight experience has become a popular entertainment project.

[0003] When the aerospace vacuum environment simulation chamber is used for teaching or exhibition, it is inevitable to move the aerospace vacuum environment simulation chamber. However, because the aerospace vacuum environment simulation chamber is heavy as a whole, it is often lifted to transport the aerospace vacuum environment simulation chamber to the transportation equipment. However, the conventional lifting device needs to wrap the lifting rope around the aerospace vacuum environment simulation chamber. This process is time-consuming and labor-intensive, and the lifting rope is easy to cause marks on the outer wall of the aerospace vacuum environment simulation chamber, affecting the normal service life of the aerospace vacuum environment simulation chamber, causing the aerospace vacuum environment simulation chamber to be time-consuming and labor-intensive to lift and transport, and easily causing damage to the outer wall of the aerospace vacuum environment simulation chamber, affecting the normal use of the aerospace vacuum environment simulation chamber. Utility Model Content

[0004] The purpose of the utility model is to provide an aerospace vacuum environment simulation chamber to solve the problem that the aerospace vacuum environment simulation chamber is time-consuming and labor-intensive to lift and transport, and the outer wall of the aerospace vacuum environment simulation chamber is easily damaged, thus affecting the normal use of the aerospace vacuum environment simulation chamber.

[0005] In order to solve the above technical problems, the utility model adopts the following technical solutions:

[0006] An aerospace vacuum environment simulation chamber, comprising: a cabin body, which is a laterally arranged cylindrical structure, and a laterally transparent simulated empty chamber is provided in the cabin body; a load-bearing bottom cover, which is fixedly welded to one side of the cabin body and is used to seal one side of the cabin body; a cabin cover, which is hingedly arranged on the other side of the cabin body and is used to open and close the simulated empty chamber; a load-bearing base, two of which are provided and are spaced apart at the lower end of the cabin body; a load-bearing ring, two of which are provided and are spaced apart on the cabin body, and the lower ends of the load-bearing rings are respectively connected to the two load-bearing bases; a load-bearing crossbeam, which is laterally arranged at the upper end of the cabin body, and the two ends of the load-bearing crossbeam are respectively connected to the two load-bearing rings; and a lifting ring, two of which are provided and are spaced apart at the upper end of the load-bearing crossbeam.

[0007] A further technical solution is that the load-bearing base includes: a first support plate, an upper end of which is provided with an arc groove, and the lower end of the load-bearing ring is fitted in the arc groove; a second support plate, an upper end of which is provided with a connecting ring that is sleeved on the cabin body, and the second support plate is connected to the load-bearing ring at one end facing the first support plate; and a connecting plate, two connecting plates are arranged at intervals, and the two ends of the connecting plate are respectively connected to the lower ends of the first support plate and the second support plate.

[0008] A further technical solution is that the cabin body is provided with two first hinged plates and a first rotating shaft rotatably arranged between the first hinged plates, the cabin cover is provided with two second hinged plates and a second rotating shaft rotatably arranged between the two second hinged plates, two connecting rotating plates spaced apart from each other up and down are provided between the first rotating shaft and the second rotating shaft, and the two ends of the connecting rotating plates are respectively rotatably mounted on the first rotating shaft and the second rotating shaft, and the two connecting rotating plates are connected by a reinforcing plate.

[0009] Compared with the prior art, the beneficial effects of the utility model are:

[0010] When lifting and transporting the entire equipment, it is only necessary to connect the lifting device and the lifting ring. The lifting ring is respectively connected to the cabin and the load-bearing ring. The load-bearing ring is mounted on the cabin and contacts the cabin through the two load-bearing rings, thereby avoiding direct contact between the starting device and the cabin, thereby avoiding marks on the cabin during the lifting process. The entire transportation process is quick and efficient, while ensuring the safety of the cabin. BRIEF DESCRIPTION OF THE DRAWINGS

[0011] Figure 1 The utility model is a structural schematic diagram of an aerospace vacuum environment simulation chamber.

[0012] Figure 2 It is a structural schematic diagram of the load-bearing base in the utility model.

[0013] Figure 3 for Figure 2 A partial enlarged schematic diagram in the middle. DETAILED DESCRIPTION

[0014] In order to make the purpose, technical solution and advantages of the utility model more clear, the utility model is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the utility model and are not used to limit the utility model.

[0015] Embodiment 1:

[0016] refer to Figures 1 to 3 , discloses an aerospace vacuum environment simulation chamber, comprising:

[0017] The cabin 1 is a transversely arranged cylindrical structure, and a transversely transparent simulated empty chamber is provided in the cabin 1;

[0018] A load-bearing bottom cover 2, wherein the load-bearing bottom cover 2 is fixedly welded to one side of the cabin body 1 and is used to block one side of the cabin body 1;

[0019] A hatch cover 3 is hingedly arranged on the other side of the cabin body 1 and is used for opening and closing the simulated empty cabin;

[0020] A load-bearing base 4, wherein two load-bearing bases 4 are provided and are spaced apart at the lower end of the cabin 1;

[0021] A load-bearing collar 5, wherein two load-bearing collars 5 are provided and are sleeved on the cabin body 1 at intervals, and the lower ends of the load-bearing collars 5 are respectively connected to two load-bearing bases 4;

[0022] A load-bearing crossbeam 6 is transversely arranged at the upper end of the cabin 1, and both ends of the load-bearing crossbeam 6 are respectively connected to the two load-bearing collars 5; and

[0023] The lifting rings 7 are provided with two and are spaced apart at the upper end of the load-bearing beam 6 .

[0024] In the utility model, when lifting and transporting the entire equipment, it is only necessary to connect the lifting equipment and the lifting ring 7, and the lifting ring 7 is respectively connected to the cabin 1 and the load-bearing ring 5, and the load-bearing ring 5 is sleeved on the cabin 1. The two load-bearing rings 5 ​​are in contact with the cabin 1, thereby avoiding direct contact between the starting device and the cabin 1, thereby avoiding the cabin 1 from having stranglehold marks during the lifting process. The entire transportation process is quick and efficient, and the safety of the cabin 1 is ensured at the same time.

[0025] Example 2

[0026] The load-bearing base 4 comprises:

[0027] A first support plate 8, wherein an arc-shaped groove 9 is provided at the upper end of the first support plate 8, and the lower end of the load-bearing ring 5 is fitted in the arc-shaped groove 9;

[0028] A second support plate 10, wherein the upper end of the second support plate 10 is provided with a connecting ring 11 sleeved on the cabin body 1, and one end of the second support plate 10 facing the first support plate 8 is connected to the load-bearing sleeve ring 5; and

[0029] The connecting plates 12 are provided with two connecting plates 12 at intervals, and both ends of the connecting plates 12 are connected to the lower ends of the first supporting plate 8 and the second supporting plate 10 respectively.

[0030] The load-bearing ring 5 is supported by the first support plate 8, and the cabin 1 is supported by the second support plate 10 to prevent the cabin 1 from contacting the ground when the cabin 1 is stationary. At the same time, by providing a load-bearing bottom cover 2, it is convenient to place the cabin 1 vertically to simulate the cabin 1 in different environments.

[0031] Two connecting plates 12 are arranged at intervals, and the two ends of the connecting plates 12 are respectively connected to the lower ends of the first support plate 8 and the second support plate 10. The first support plate 8 and the second support plate 10 are connected by the connecting plates 12 to increase the stability of the first support plate 8 and the second support plate 10. The connection method is to weld the two ends of the connecting plate 12 to the first support plate 8 and the second support plate 10 respectively.

[0032] Example 3

[0033] The cabin body 1 is provided with two first hinged plates 13 and a first rotating shaft 14 rotatably arranged between the first hinged plates 13, and the hatch cover 3 is provided with two second hinged plates 15 and a second rotating shaft 16 rotatably arranged between the two second hinged plates 15, and two connecting rotating plates 17 spaced apart from each other are provided between the first rotating shaft 14 and the second rotating shaft 16, and the two ends of the connecting rotating plates 17 are rotatably sleeved on the first rotating shaft 14 and the second rotating shaft 16 respectively, and the two connecting rotating plates 17 are connected by a reinforcing plate 18. By pushing the hatch cover 3, the hatch cover 3 drives the second hinged plates 15 to rotate along the second rotating shaft 16, so as to facilitate opening or closing the hatch cover 3.

[0034] Although the utility model is described herein with reference to a plurality of illustrative embodiments of the utility model, it should be understood that those skilled in the art may devise many other modifications and implementations that fall within the scope and spirit of the principles disclosed herein. More specifically, within the scope of the disclosure, drawings, and claims of the present application, various modifications and improvements may be made to the components and / or layout of the subject combination layout. In addition to the modifications and improvements made to the components and / or layout, other uses will also be apparent to those skilled in the art.

Claims

1. An aerospace vacuum environment simulation chamber, characterized in that: include: A cabin body, which is a laterally arranged cylindrical structure, and a laterally transparent simulated empty chamber is provided in the cabin body; a load-bearing bottom cover, which is fixedly welded to one side of the cabin body and used for sealing one side of the cabin body; a hatch cover, which is hingedly arranged on the other side of the cabin body and used for opening and closing the simulated empty chamber; a load-bearing base, two of which are arranged at intervals at the lower end of the cabin body; a load-bearing ring, two of which are arranged at intervals on the cabin body, and the lower ends of the load-bearing rings are respectively connected to the two load-bearing bases; a load-bearing crossbeam, which is laterally arranged at the upper end of the cabin body, and the two ends of the load-bearing crossbeam are respectively connected to the two load-bearing rings; and a lifting ring, two of which are arranged at intervals at the upper end of the load-bearing crossbeam.

2. The aerospace vacuum environment simulation chamber according to claim 1, characterized in that: The load-bearing base includes: a first support plate, an upper end of which is provided with an arc-shaped groove, and the lower end of the load-bearing ring is fitted in the arc-shaped groove; a second support plate, an upper end of which is provided with a connecting ring that is sleeved on the cabin body, and one end of the second support plate facing the first support plate is connected to the load-bearing ring; and a connecting plate, two connecting plates are arranged at intervals, and the two ends of the connecting plate are respectively connected to the lower ends of the first support plate and the second support plate.

3. The aerospace vacuum environment simulation chamber according to claim 1, characterized in that: The cabin body is provided with two first hinge plates and a first rotating shaft rotatably arranged between the first hinge plates, the cabin cover is provided with two second hinge plates and a second rotating shaft rotatably arranged between the two second hinge plates, two connecting rotating plates spaced apart up and down are provided between the first rotating shaft and the second rotating shaft, and the two ends of the connecting rotating plates are rotatably mounted on the first rotating shaft and the second rotating shaft respectively, and the two connecting rotating plates are connected by a reinforcing plate.

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