CN216332870U - Transfer bracket - Google Patents
Transfer bracket Download PDFInfo
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- CN216332870U CN216332870U CN202123132878.5U CN202123132878U CN216332870U CN 216332870 U CN216332870 U CN 216332870U CN 202123132878 U CN202123132878 U CN 202123132878U CN 216332870 U CN216332870 U CN 216332870U
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- support
- supporting
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- plate
- transfer carriage
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Abstract
The application provides a transfer bracket, which comprises a base and at least two supporting components arranged on the base along a first direction; the support assembly includes: one end of the first supporting piece is connected to the base, and the other end of the first supporting piece is provided with a first supporting surface for supporting the rocket cabin body; at least one second support member selectively connectable with the first support member; one end of the second supporting piece is detachably connected with the first supporting surface, and the other end of the second supporting piece is provided with a second supporting surface; the first supporting surface and the second supporting surface can be used for supporting rocket cabin bodies with different diameters respectively. Through the detachable arrangement of the first supporting piece and the second supporting piece, the transfer bracket can support rocket cabin bodies with different diameters.
Description
Technical Field
The application relates to the technical field of ground equipment of rocket launching support systems, in particular to a transfer bracket.
Background
Need ground equipment to support the protection to the arrow body among the full arrow transportation process, when being used for the rocket to transport, current support equipment has full arrow transportation bracket, is the support protection to each cabin section of rocket, but the support is transported to the full arrow only satisfies the support and the parking of a model arrow body cabin section, and the commonality of equipment is single, need be equipped with multiple corresponding support equipment when the arrow body of different models.
Disclosure of Invention
The present application aims to address the above problems by providing a transfer carriage.
The technical scheme of the application provides a transfer bracket, which comprises a base and at least two supporting components arranged on the base along a first direction;
the support assembly includes:
one end of the first supporting piece is connected to the base, and the other end of the first supporting piece is provided with a first supporting surface for supporting the rocket cabin body;
at least one second support member selectively connectable with the first support member; one end of the second supporting piece is detachably connected with the first supporting surface, and the other end of the second supporting piece is provided with a second supporting surface;
the first supporting surface and the second supporting surface can be used for supporting rocket cabin bodies with different diameters respectively.
According to the technical solution provided by some embodiments of the present application, the second support has a second bottom plate connected with the first support; the second bottom plate is provided with a bearing surface completely attached to the first supporting surface.
According to the technical solution provided by some embodiments of the present application, the second supporting member includes a second receiving plate, and the second supporting surface is located on a top surface of the second receiving plate; the second bottom plate is connected with the second bearing plate through at least two reinforcing rib plates.
According to the technical scheme that some embodiments of this application provided, first holding surface with the second holding surface is the arc surface, the diameter of first holding surface with the diameter of second holding surface is different each other.
According to the technical scheme provided by some embodiments of the application, the range of the central angle corresponding to the first supporting surface and the range of the central angle corresponding to the second supporting surface are both larger than or equal to 100 degrees.
According to the technical scheme provided by some embodiments of the application, a plurality of fixing plates are distributed on the base along the first direction, and the distance between every two adjacent fixing plates is equal.
According to the technical scheme provided by some embodiments of the application, the first supporting piece is detachably installed on the base through the fixing plate.
According to the technical scheme provided by some embodiments of the application, the first supporting piece is provided with a first bottom plate connected with the fixing plate, and the first bottom plate is provided with a height-adjusting bolt for adjusting the flatness of the supporting component on the base.
According to the technical scheme provided by some embodiments of the present application, the first supporting surface and the second supporting surface are both provided with a buffer layer.
According to the technical scheme provided by some embodiments of the application, the two ends of the first supporting piece are respectively provided with universal lifting rings.
Compared with the prior art, the beneficial effect of this application: a transfer carriage, the support assembly comprising, by way of a support assembly disposed on a base: the first support part and the second support part are detachably connected with the first support part; the first supporting piece is provided with a first supporting surface for supporting the rocket cabin body, the second supporting piece is provided with a second supporting surface for supporting the rocket cabin body, and the first supporting surface and the second supporting surface can be used for supporting the rocket cabin bodies with different diameters respectively.
When the rocket cabin body supporting device is used, the second supporting piece can be detached from the first supporting piece, the rocket cabin body of one type can be supported through the first supporting face, and the first supporting piece can also be arranged on the second supporting room in a rotating mode, and the rocket cabin body of the other type can be supported through the second supporting face. This transport bracket can provide the demand of support to the arrow body of different models, consequently, this transport holds in the palm support has certain commonality.
Drawings
Fig. 1 is a schematic structural diagram of a transfer carriage according to an embodiment of the present disclosure;
FIG. 2 is a schematic view of a base structure;
FIG. 3 is a schematic view of a first support member;
fig. 4 is a schematic structural view of a second supporting member.
The text labels in the figures are represented as:
10. a first support member; 11. a first support surface; 12. a universal hoisting ring; 13. a first base plate; 14. a first bearing plate; 15. heightening the bolt; 20. a second support member; 21. a second support surface; 22. a first lifting lug; 23. a second base plate; 24. a second bearing plate; 30. a base; 31. a fixing plate; 32. and the second lifting lug.
Detailed Description
The following detailed description of the present application is given for the purpose of enabling those skilled in the art to better understand the technical solutions of the present application, and the description in this section is only exemplary and explanatory, and should not be taken as limiting the scope of the present application in any way.
Referring to fig. 1, the present embodiment provides a transfer carriage, which includes a base 30 and at least two supporting components arranged on the base 30 along a first direction, wherein the base 30 is a fixing seat of the supporting components.
The support assembly includes: a first support 10 and a second support 20;
as shown in fig. 2, one end of the first supporting member 10 is connected to the base 30, and the other end thereof has a first supporting surface 11 for supporting the rocket cabin; the size of the first support 10 is 1360 mm × 380 mm × 424 mm, a first bearing plate 14 is arranged on one side of the first support 10 away from the base 30, and a top surface of the first bearing plate 14 is provided with the first support surface 11 for supporting the rocket cabin body;
as shown in fig. 3, one end of the second supporting member 20 is detachably connected to the first supporting surface 11, and the other end has a second supporting surface 21 for supporting the rocket cabin; the dimensions of the second support 20 are 1062 mm × 200 mm × 444 mm.
The first support 10 is a fixed seat of the second support 20, the first support 10 has a first receiving plate 14 connected with the second support 20, and the first receiving plate 14 is provided with a connecting hole; a second bottom plate 23 is arranged at a position of the second supporting piece 20 corresponding to the first bearing plate 14, and the second bottom plate 23 is fixedly connected with the first bearing plate 14 through bolts; the side of the second supporting member 20 away from the second bottom plate 23 is provided with a second bearing plate 24, and the top surface of the second bearing plate 24 is provided with a second supporting surface 21 for supporting the rocket cabin.
It should be noted that the support assembly includes a first support 10 and a second support 20, but when the first support 10 or the second support 20 is selected according to the size of the rocket cabin, the support assembly only includes the first support 10 when the first support 10 is selected, and the support assembly includes the first support 10 and the second support 20 when the second support 20 is selected.
The first supporting surface 11 and the second supporting surface 21 can be used for supporting rocket cabin bodies with different diameters respectively, and the detachable arrangement of the first supporting piece 10 and the second supporting piece 20 ensures that the transfer bracket can support rocket cabin bodies with different diameters; when the first support 10 can support the rocket cabin, the second support 20 does not need to be mounted on the first support 10, and when the first support 10 does not meet the size of supporting the rocket cabin, the second support 20 is mounted on the first support 10 to support the rocket cabin.
In a preferred embodiment, the second bottom plate 23 has a bearing surface completely attached to the first supporting surface 11, and the second bottom plate 23 is connected to the second bearing plate 24 through at least two reinforcing rib plates. The stability of the second support member 20 during the supporting process is ensured.
In a preferred embodiment, the first supporting surface 11 and the second supporting surface 21 are both arc surfaces, and the diameter of the first supporting surface 11 is different from the diameter of the second supporting surface 21. The diameter of the first supporting surface 11 is 600 mm, and the rocket cabin body with the diameter of 600 mm can be parked and transported. The diameter of the second supporting surface 21 is 1000 mm, and the rocket cabin body with the diameter of 1000 mm can be parked and transported.
The width ranges of the first supporting surface 11 and the second supporting surface 21 herein are both greater than or equal to 200 mm.
In a preferred embodiment, the range of the central angle corresponding to the first supporting surface 11 and the central angle corresponding to the second supporting surface 21 is greater than or equal to 100 °.
In a preferred embodiment, the number of the second supporting members 20 is several, all the second supporting members 20 can be used alternatively, the diameters of the second supporting surfaces 21 of the second supporting members 20 are different, the second supporting surfaces 21 with different diameters can be used for supporting rocket cabins with corresponding diameters, and therefore, the first supporting member 10 can be detachably connected with any one of the second supporting members 20, so that the transfer tray support can support rocket cabins with different diameters.
In a preferred embodiment, as shown in fig. 4, the base 30 extends along a first direction, a plurality of fixing plates 31 are distributed on the base 30 along the first direction, and the supporting component is detachably connected to any one of the fixing plates 31.
What transport the whole adoption of bracket is the Q235 material, base 30 constitutes the support body that the size is 4362 mm x 1460 mm x 152 mm by square pipe, base 30 is provided with a plurality of being used for fixing in length direction the fixed plate 30 of supporting component, each be provided with multiunit screw thread hole group on the fixed plate 30, can be used to the ann change not unidimensional supporting component makes again the supporting component can the length direction of base is adjusted.
The first direction here refers to a length direction of the base 30.
In a preferred embodiment, the interval between two adjacent fixing plates 31 on the base 30 is equal.
In a preferred embodiment, the first supporting member 10 has a first bottom plate 13 connected to the fixing plate 31, the first bottom plate 13 is provided with an elevation bolt 15 for adjusting the flatness of the supporting member on the base 30, and one end of the elevation bolt 15 penetrates through the first bottom plate 13 and abuts against the fixing plate 31. The distance between the first bottom plate 13 and the fixing plate 31 is adjusted by rotating the height-adjusting bolt 15, that is, the height of the supporting assembly on the fixing plate 31 is finely adjusted.
A through hole is formed in the first bottom plate 13, and a bolt penetrates through the through hole and is in threaded connection with the fixing plate 31, so that the first supporting piece 10 is fixedly connected with the fixing plate 31.
In a preferred embodiment, both the first 11 and the second 21 support surfaces are provided with a damping layer. The buffer layer is made of wool felt and is mainly used for protecting the outer surface of the arrow body from being damaged in the supporting process.
In a preferred embodiment, the two ends of the first supporting member 10 are respectively provided with a universal hanging ring 12, the universal hanging rings 12 are used for lifting and moving the whole transfer bracket, and the two ends of the second supporting member 20 are respectively provided with a second lifting lug 22 for assembling the transfer bracket. The two sides of the base 30 are respectively provided with a first lifting lug 32 for assembling the transfer bracket.
In a preferred embodiment, it should be noted that, according to the length of the rocket cabin body and the diameter of each cabin section, the number of the transfer brackets can be selected and used according to needs in transferring or supporting, so that the stability in the transferring process can be increased.
The embodiment of the present application provides a transfer carriage, and the support assembly is disposed on the base 30, and includes a first support 10 and a second support 20. The diameters of the first supporting surface 11 on the first supporting member 10 and the second supporting surface 21 on the second supporting member 20 are different from each other, the plurality of fixing plates 31 are arranged on the base 30 at equal intervals, the number of the supporting components is set on the base 30 according to the requirement of supporting the rocket cabin body, and when the rocket cabin bodies with different diameters are supported, the rocket cabin body is supported by detaching or installing the second supporting member 20 on the first supporting member 10.
Here, the second supporting members 20 are detachably connected to the first supporting members 10, the number of the second supporting members 20 is several, and each of the second supporting members 20 can support rocket cabins of different diameters.
Therefore, the transfer bracket can meet the requirements of providing parking and transfer support for arrow bodies with different lengths or diameters under different working conditions.
The principles and embodiments of the present application are explained herein using specific examples, which are provided only to help understand the method and the core idea of the present application. The foregoing is only a preferred embodiment of the present application, and it should be noted that there are no specific structures which are objectively limitless due to the limited character expressions, and it will be apparent to those skilled in the art that a plurality of modifications, decorations or changes can be made without departing from the principle of the present invention, and the technical features mentioned above can be combined in a suitable manner; such modifications, variations, combinations, or adaptations of the invention in other instances, which may or may not be practiced, are intended to be within the scope of the present application.
Claims (10)
1. A transfer carriage, comprising:
the device comprises a base (30) and at least two supporting components arranged on the base (30) along a first direction;
the support assembly includes:
a first support (10) having one end connected to the base (30) and the other end having a first support surface (11) for supporting a rocket cabin;
at least one second support (20) selectively connectable with the first support (10); one end of the second supporting piece (20) is detachably connected with the first supporting surface (11), and the other end of the second supporting piece is provided with a second supporting surface (21);
the first supporting surface (11) and the second supporting surface (21) can be used for supporting rocket cabins with different diameters respectively.
2. A transfer carriage in accordance with claim 1, characterized in that the second support (20) has a second bottom plate (23) connected to the first support (10); the second bottom plate (23) is provided with a bearing surface completely attached to the first supporting surface (11).
3. A transfer carriage according to claim 2, characterised in that the second support member (20) comprises a second adaptor plate (24), the second support surface (21) being located on a top surface of the second adaptor plate (24); the second bottom plate (23) is connected with the second bearing plate (24) through at least two reinforcing rib plates.
4. A transfer carriage according to any of claims 1-3, wherein the first support surface (11) and the second support surface (21) are both circular arc surfaces, the diameter of the first support surface (11) and the diameter of the second support surface (21) being different from each other.
5. A transport carriage as claimed in claim 4, characterized in that the range of the central angle corresponding to the first support surface (11) and the central angle corresponding to the second support surface (21) is greater than or equal to 100 °.
6. A carrier frame according to claim 1, wherein a plurality of fixing plates (31) are distributed on the base (30) along the first direction, and the distance between two adjacent fixing plates (31) is equal.
7. A transfer carriage in accordance with claim 6, characterized in that the first support (10) is detachably mounted on the base (30) by means of the fixing plate (31).
8. A transfer carriage in accordance with claim 6, characterized in that the first support (10) has a first base plate (13) connected to the fixed plate (31), the first base plate (13) being provided with elevation bolts (15) for adjusting the flatness of the support assembly on the base (30).
9. A transfer carriage in accordance with claim 1, characterized in that the first support surface (11) and the second support surface (21) are provided with a buffer layer.
10. A transfer carriage in accordance with claim 1, characterized in that said first support member (10) is provided with universal lifting eyes (12) at each end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123132878.5U CN216332870U (en) | 2021-12-14 | 2021-12-14 | Transfer bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123132878.5U CN216332870U (en) | 2021-12-14 | 2021-12-14 | Transfer bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216332870U true CN216332870U (en) | 2022-04-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123132878.5U Active CN216332870U (en) | 2021-12-14 | 2021-12-14 | Transfer bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216332870U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115900438A (en) * | 2022-12-16 | 2023-04-04 | 北京凌空天行科技有限责任公司 | Loading device of box type launch rocket |
-
2021
- 2021-12-14 CN CN202123132878.5U patent/CN216332870U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115900438A (en) * | 2022-12-16 | 2023-04-04 | 北京凌空天行科技有限责任公司 | Loading device of box type launch rocket |
| CN115900438B (en) * | 2022-12-16 | 2024-05-28 | 北京凌空天行科技有限责任公司 | Filling device for box-type rocket launcher |
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