CN220411335U - Storage and transportation box for aerospace equipment - Google Patents
Storage and transportation box for aerospace equipment Download PDFInfo
- Publication number
- CN220411335U CN220411335U CN202322083271.5U CN202322083271U CN220411335U CN 220411335 U CN220411335 U CN 220411335U CN 202322083271 U CN202322083271 U CN 202322083271U CN 220411335 U CN220411335 U CN 220411335U
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- Prior art keywords
- box body
- frame
- transportation
- aerospace equipment
- box
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Links
- 239000003292 glue Substances 0.000 claims abstract description 6
- 238000007789 sealing Methods 0.000 claims description 29
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 239000002313 adhesive film Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 239000010410 layer Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 230000008707 rearrangement Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Packaging Of Machine Parts And Wound Products (AREA)
Abstract
The application provides a space equipment storage and transportation case, its specific structure includes: a case; the cover plate is arranged at the top end of the box body, and one end of the cover plate is rotationally connected with the box body so as to close or open the interior of the box body; the limiting fixing frame is positioned in the box body and comprises a frame body with an opening in the middle and a glue film which is supported by the frame body, and the glue film is arranged to cover the opening; the first structure is arranged at the connection position of the inner side wall and the bottom end of the box body, and the first structure is rotationally connected with a frame of the frame body of the limit fixing frame, so that the limit fixing frame can rotate to a horizontal position contacted with the bottom end of the box body or to a vertical position contacted with the side wall of the box body. The aerospace equipment storage and transportation box can flexibly fix aerospace equipment, and the transportation safety of the aerospace equipment is improved.
Description
Technical Field
The utility model relates to the field of transportation and storage equipment, in particular to a storage and transportation box for aerospace equipment.
Background
The space equipment refers to equipment, tools, instruments, accessories, materials and the like for developing, designing, manufacturing, testing and operating the spacecraft, which cover all aspects of the space exploration field, from rocket engines and propellants to satellites, detectors and electronic equipment of the spacecraft, control systems, communication equipment, attitude controllers, supporting structures, parachutes, insulating materials, protective materials and the like, and the equipment needs to be protected by a transport case with higher quality so as to ensure the normal use of the equipment.
Some aerospace equipment is fragile, and in the process of transportation, the aerospace equipment can be damaged due to jolt of a road surface, the follow-up influence caused by the damage of the precision of the aerospace equipment is high, and meanwhile, when the aerospace equipment is stored, water vapor can enter the storage and transportation box due to the change of external environment, so that the aerospace equipment cannot be normally used.
Disclosure of Invention
In view of this, this application provides a space equipment stores up fortune seal structure, can carry out flexible fixation to space equipment, and its specific structure includes: a case; the cover plate is arranged at the top end of the box body, and one end of the cover plate is rotationally connected with the box body so as to close or open the interior of the box body; the limiting fixing frame is positioned in the box body and comprises a frame body with an opening in the middle and a glue film which is supported by the frame body, and the glue film is arranged to cover the opening; the first structure is arranged at the connection position of the inner side wall and the bottom end of the box body, and the first structure is rotationally connected with a frame of the frame body of the limit fixing frame, so that the limit fixing frame can rotate to a horizontal position contacted with the bottom end of the box body or to a vertical position contacted with the side wall of the box body.
By adopting the specific structure, the space equipment is placed into the opening of the limiting and fixing frame in the box body, and one end of the space equipment is contacted with the fixing adhesive film and glued. The first structure can drive the spacing fixed frame to rotate, makes fixed glued membrane parcel live space equipment, realizes the flexible fixation to space equipment.
As one possible implementation manner, the first structure includes: the part of the rotating shaft extending into the box body is connected with a frame of the frame body of the limit fixing frame; the driving motor is arranged outside the box body and is coupled with the part of the rotating shaft positioned outside the box body so as to drive the rotating shaft to rotate.
With the above possible implementation, the rotation shaft driven by the driving motor can be used as power for driving the first structure to rotate.
As a possible implementation manner, a mounting frame is arranged at the bottom end of one side surface outside the box body, and is a frame structure with a space inside; the driving motor is arranged in the mounting frame.
As one possible implementation manner, soft rubber protection plates are arranged on the inner walls of the two sides of the box body.
By adopting the possible implementation mode, the soft rubber protection plate can avoid collision with the side wall of the box body in the transportation process of the aerospace equipment, so that damage is generated.
As one possible implementation manner, a sealing groove is formed in the top end of the box body, and a sealing gasket is arranged at the bottom end of the sealing cover plate in cooperation with the sealing groove.
By adopting the possible implementation manner, the sealing groove and the sealing gasket are matched, so that the space in the box body has certain tightness when the cover sealing plate covers the box body.
As one possible implementation manner, the inner walls of the two sides of the box body are fixedly connected with a plurality of magnetic attraction table posts, and a plurality of magnetic attraction iron sheets are arranged at the bottom end of the cover plate in a matching manner with the magnetic attraction table posts.
By adopting the possible implementation manner, the magnetic attraction table column is matched with the magnetic attraction patch, so that the stability of the sealing cover plate matched with the box body can be improved.
As a possible implementation manner, the box body includes a sealing sleeve, and the rotating shaft is arranged at a position where the rotating shaft extends into the box body, and is rotatably connected with the sealing sleeve.
By adopting the possible implementation manner, the sealing sleeve can seal the hole of the rotating shaft extending into the box body, so that the tightness of the inside of the box body in a closed state is ensured.
As a possible implementation manner, the inner frame of the limit fixing frame is provided with anti-collision protection strips.
By adopting the possible implementation manner, the anti-collision protection layer can prevent the space equipment from colliding with the limiting fixed frame when the box body collides, thereby causing damage to the space equipment.
As a possible implementation manner, the bottom of the box body is uniformly and fixedly connected with a plurality of universal wheels.
By adopting the possible implementation manner, the plurality of universal wheels facilitate the transportation and movement of the box body.
As a possible implementation manner, one end of the cover plate is provided with a buckling plate, and the box body is provided with a buckling groove matched with the buckling plate.
With the adoption of the possible implementation manner, the clamping plate and the clamping groove are matched, so that the sealing cover plate can be locked on the upper side of the box body.
Drawings
The individual technical features of the present application and their relationships are further described below with reference to the accompanying drawings. The drawings are exemplary, some technical features are not shown in actual proportion, and some drawings may omit technical features that are conventional in the art to which the present application pertains and are not essential to understanding and realizing the present application, or additionally show technical features that are not essential to understanding and realizing the present application, that is, combinations of the technical features shown in the drawings are not limiting the present application. In addition, throughout this application, like reference numerals refer to like elements. The specific drawings are as follows:
FIG. 1 is a schematic view of an aerospace equipment storage and transportation box according to an embodiment of the present application;
FIG. 2 is a schematic diagram II of a storage and transportation box for aerospace equipment according to an embodiment of the application;
FIG. 3 is a schematic view of a container body of an aerospace equipment storage and transportation container according to an embodiment of the present application;
FIG. 4 is a schematic view of a closure plate of an aerospace equipment storage and transportation case according to an embodiment of the present application;
fig. 5 is a schematic view of a limiting and fixing frame of a storage and transportation box for aerospace equipment according to an embodiment of the application.
Reference numerals illustrate: 10-a box body; 11-limiting fixed frames; 111-opening; 112-fixing the adhesive film; 113-an anti-collision protective layer; 12-mounting a frame; 13-a drive motor; 14-a rotation axis; 15-a soft rubber protection plate; 16-sealing the groove; 17-sealing sleeve; 18-a magnetic attraction table column; 19-universal wheels; 20-sealing cover plates; 21-a gasket; 22-magnet pieces; 23-buckling plates; 24-snap groove.
Detailed Description
Hereinafter, specific embodiments of the present application will be described in detail with reference to the accompanying drawings.
As shown in fig. 1, the storage and transportation box for aerospace equipment according to the embodiment of the application specifically includes: a rectangular cylindrical case 10; the cover plate 20 covered on the top of the box body 10 has one end rotatably connected with the box body 10 and the other end clamped and fixed with the clamping groove 24 on the box body 10 through the clamping plate 23. As shown in fig. 3, a limiting fixing frame 11 is disposed at the bottom end of the inside of the case 10, and an opening 111 with a fixing adhesive film 112 is disposed in the middle. The first structure is arranged at the connection position of the inner side wall and the bottom end of the box body 10, and the first structure is rotationally connected with a frame body of the limit fixing frame 11, so that the limit fixing frame 11 can rotate to a horizontal position contacted with the bottom end of the box body 10 or to a vertical position contacted with the side wall of the box body 10. The bottom end of one side surface outside the box body 10 is provided with a mounting frame 12 which is a frame structure with a space inside.
The first structure includes a rotation shaft 14, and a portion of the rotation shaft extending into the case 10 is connected to a frame of the frame body of the limit fixing frame 11.
As shown in fig. 3, inner walls of two sides of the case 10 are provided with soft rubber protection plates 15 for providing buffer protection for the aircraft.
As shown in fig. 3, a seal groove 16 is provided at the top end of the case 10. The seal groove 16 extends through the top end of the entire tank 10.
Wherein the shape of the cover plate 20 is designed to match the shape of the case 10. And as shown in fig. 4, the bottom end of the cover plate 20 is provided with a gasket 21 in cooperation with the seal groove 16. The seal groove 16 cooperates with the gasket 21 to provide a certain tightness to the space inside the case 10 when the cover plate 20 covers the case 10.
As shown in fig. 2, a driving motor 13 is installed in the installation frame 12; the driving motor 13 is coupled with a part of the rotating shaft 14 positioned outside the box body so as to drive the rotating shaft to rotate; the rotation shaft 14 extends into the case 10; a sealing sleeve 17 slidably connected to the rotary shaft 14 is provided between the rotary shaft 14 and the case 10.
As shown in fig. 3-4, two magnetic attraction table posts 18 are fixedly connected to the inner walls of two sides of the box body 10, and four magnetic attraction table posts 18 are provided at the bottom end of the cover plate 20 in cooperation with a total of four magnetic attraction table posts 18. When the cover plate 20 is covered on the case 10, the magnet piece 22 is attracted by the magnet post 18, so that the stability of the fitting of the cover plate 20 with the case 10 can be increased and the sealability can be increased.
As shown in fig. 5, an anti-collision protection layer 113 is disposed at the inner frame of the opening 111 of the limit fixing frame 11. The buffer device is used for buffering the space equipment and the limiting fixed frame 11, and damage caused by collision between the space equipment and the limiting fixed frame 11 is avoided.
As shown in fig. 1, four universal wheels 19 are uniformly and fixedly connected to the bottom of the box body 10, so as to facilitate transportation of the storage and transportation box. In addition, in other embodiments, other numbers of universal wheels 19 may be used, such as 6.
The embodiment of the application relates to a specific operation flow of a storage and transportation box for aerospace equipment, which comprises the following steps:
s1, opening the cover plate 20, and placing the aerospace equipment into the middle of the opening 111 of the limiting and fixing frame 11 in the storage and transportation box body 10.
S2, starting the driving motor 13 to drive the rotating shaft 14 to rotate, and driving the limiting fixed frame 11 to rotate by taking the rotating shaft 14 as an axis through the rotating shaft 14.
S3, along with the rotation of the limiting fixed frame 11, the outer part of the limiting fixed frame 11 is completely attached to the rear wall of the box body 10, and the fixed adhesive film 112 wraps the space equipment.
S4, closing the cover plate 20, clamping the sealing gasket 21 in the sealing groove 16, respectively and correspondingly adsorbing the magnetic iron sheets 22 on the top ends of the magnetic attraction table columns 18, and fixedly connecting the clamping plate 23 with the clamping groove 24, thereby completing the fixation.
In summary, embodiments of the present application relate to a storage and transportation box for aerospace devices, which can flexibly wrap and fix the aerospace devices with a fixing adhesive film 112. And the fixed adhesive film 112 can be changed along with the external shape of the aerospace equipment, so as to adapt to more special-shaped aerospace equipment. And the protection of the aerospace equipment by the soft rubber protection plate 15 and the anti-collision protection layer 113 is matched, so that the damage to the aerospace equipment caused by bumping on the road surface in the transportation process is avoided, and the precision of the aerospace equipment is affected. The storage and transportation box is matched with the sealing groove 16 through the sealing gasket 21, the sealing sleeve 17 and the rotating shaft 14 and the magnetic attraction table column 18 and the magnetic attraction sheet 22, so that the inside of the storage and transportation box can be kept in a sealing state in the transportation process, and moisture is prevented from entering the storage and transportation box to make the aerospace equipment wet, and the storage and transportation box cannot be used normally.
The term "comprising" as used throughout this application should not be construed as limited to what is listed thereafter; it does not exclude other elements or steps.
It will be appreciated that those skilled in the art may implement the application in any suitable manner combining features of one or more embodiments mentioned throughout the application with features of other embodiments.
Note that the above is only the preferred embodiments of the present application and the technical principles applied. Those skilled in the art will appreciate that the present application is not limited to the particular embodiments described herein, but is capable of numerous obvious changes, rearrangements and substitutions as will now become apparent to those skilled in the art without departing from the scope of the present application. Therefore, although the present application has been described in more detail through the above embodiments, the present application is not limited to the above embodiments, and may include many other equivalent embodiments without departing from the technical concept of the present application, which falls within the protection scope of the present application.
Claims (10)
1. A storage and transportation box for aerospace equipment, comprising:
a case;
the cover plate is arranged at the top end of the box body, and one end of the cover plate is rotationally connected with the box body so as to close or open the interior of the box body;
the limiting fixing frame is positioned in the box body and comprises a frame body with an opening in the middle and a glue film which is supported by the frame body, and the glue film is arranged to cover the opening;
the first structure is arranged at the connection position of the inner side wall and the bottom end of the box body, and the first structure is rotationally connected with a frame of the frame body of the limit fixing frame, so that the limit fixing frame can rotate to a horizontal position contacted with the bottom end of the box body or to a vertical position contacted with the side wall of the box body.
2. The aerospace equipment storage and transportation tank of claim 1, wherein the first structure comprises: the part of the rotating shaft extending into the box body is connected with a frame of the frame body of the limit fixing frame;
the driving motor is arranged outside the box body and is coupled with the part of the rotating shaft positioned outside the box body so as to drive the rotating shaft to rotate.
3. A storage and transportation container for space vehicles according to claim 2, wherein,
the bottom end of one side surface outside the box body is provided with a mounting frame which is a frame structure with a space inside;
the driving motor is arranged in the mounting frame.
4. The aerospace equipment storage and transportation box according to claim 1, wherein soft rubber protection plates are arranged on inner walls of two sides of the box body.
5. The aerospace equipment storage and transportation box according to claim 2, wherein a sealing groove is formed in the top end of the box body, and a sealing gasket is arranged at the bottom end of the sealing cover plate in cooperation with the sealing groove.
6. The aerospace equipment storage and transportation box according to claim 3, wherein a plurality of magnetic attraction table posts are fixedly connected to inner walls of two sides of the box body, and a plurality of magnetic attraction iron sheets are arranged at the bottom end of the cover plate in a matched mode with the magnetic attraction table posts.
7. The aerospace equipment storage and transportation box of claim 6, wherein the box body comprises a sealing sleeve, the sealing sleeve is arranged at a position where the rotating shaft extends into the box body, and the rotating shaft is rotatably connected with the sealing sleeve.
8. The aerospace equipment storage and transportation box according to claim 1, wherein the inner frame of the limit fixing frame is provided with anti-collision protection strips.
9. The aerospace equipment storage and transportation box of claim 1, wherein a plurality of universal wheels are uniformly and fixedly connected to the bottom of the box body.
10. The aerospace equipment storage and transportation box according to claim 1, wherein the cover plate is provided with a buckling plate at one end, and the box body is provided with a buckling groove matched with the buckling plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322083271.5U CN220411335U (en) | 2023-08-03 | 2023-08-03 | Storage and transportation box for aerospace equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322083271.5U CN220411335U (en) | 2023-08-03 | 2023-08-03 | Storage and transportation box for aerospace equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220411335U true CN220411335U (en) | 2024-01-30 |
Family
ID=89650630
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322083271.5U Active CN220411335U (en) | 2023-08-03 | 2023-08-03 | Storage and transportation box for aerospace equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220411335U (en) |
-
2023
- 2023-08-03 CN CN202322083271.5U patent/CN220411335U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |