CN220435327U - Forging balance ring for rocket convenient to installation - Google Patents
Forging balance ring for rocket convenient to installation Download PDFInfo
- Publication number
- CN220435327U CN220435327U CN202322167024.3U CN202322167024U CN220435327U CN 220435327 U CN220435327 U CN 220435327U CN 202322167024 U CN202322167024 U CN 202322167024U CN 220435327 U CN220435327 U CN 220435327U
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- CN
- China
- Prior art keywords
- wall
- rocket
- ring
- forging
- guide
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- 238000005242 forging Methods 0.000 title claims abstract description 32
- 238000009434 installation Methods 0.000 title claims abstract description 31
- 230000000149 penetrating effect Effects 0.000 claims abstract description 6
- 239000002156 adsorbate Substances 0.000 description 7
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The utility model discloses a forged piece balance ring for a rocket, which comprises a ring body, wherein adjusting components are symmetrically arranged on the inner wall of the ring body, each adjusting component comprises a limit groove, a support shaft, a thread cylinder, a threaded rod and a support ring, the inner wall of each adjusting component is provided with the limit groove, one end of each support shaft is arranged in the limit groove in a penetrating mode, the thread cylinder is arranged on the inner wall of each support shaft, the threaded rod is arranged on the inner wall of each thread cylinder in a penetrating mode, and the support ring is arranged on the inner wall of each limit groove. According to the utility model, the adjusting assembly is arranged to facilitate the installation of the rocket forging balance ring, after the rocket forging balance ring is placed at the installation site, the threaded rod is rotated to enable the position of the threaded cylinder to move, the position of the supporting shaft is driven to move, when the position of the supporting shaft moves, the guide plate guides the position of the supporting shaft through the guide groove, and after one end of the supporting shaft moves into the groove body preset at the installation site, the installation of the rocket forging balance ring is facilitated.
Description
Technical Field
The utility model relates to the technical field of balance rings, in particular to a forged piece balance ring for a rocket, which is convenient to install.
Background
The balance ring or balance gyroscope is the basis of a modern gyroscope, the modern balance ring becomes an indispensable instrument during the rocket running, and can also be called a gyroscope, the balance ring or balance gyroscope is an indispensable device for automatic navigation in the modern rocket running, and the modern rocket can recognize the direction through the gyroscope no matter how rapidly moves in the air or at sea;
patent document CN210290601U discloses a dynamic balance ring, "comprising an eccentric ring a and an eccentric ring B sleeved on the outer side of the eccentric ring a, wherein the outer side wall of the eccentric ring a is matched with the inner wall of the eccentric ring B in a fitting manner, the inner side wall of the eccentric ring a is concentric with the outer side wall of the eccentric ring B, the eccentric ring a is a hollow ring, and the eccentric ring B is a solid ring. As can be seen from the above structure, according to the dynamic balance ring of the present utility model, by the structural arrangement of the eccentric ring a and the eccentric ring B, the mass center of the dynamic balance ring is offset by the maximum amount of the geometric center on the premise of ensuring the concentricity of the innermost side wall and the outermost side wall of the dynamic balance ring, so as to improve the adjustment capability of the dynamic balance ring.
Disclosure of Invention
The utility model aims to provide a forging balance ring for a rocket, which is convenient to install, so as to solve the technical problem that the forging balance ring for the rocket, which is proposed in the background art, is inconvenient to install quickly.
In order to achieve the above purpose, the present utility model provides the following technical solutions: a rocket forging gimbal for easy installation, comprising:
the device comprises a ring body, wherein the inner wall of the ring body is symmetrically provided with an adjusting assembly, and the adjusting assembly comprises a limit groove, a supporting shaft, a threaded cylinder, a threaded rod and a supporting ring;
the inner wall of the adjusting component is provided with a limit groove, one end of the supporting shaft penetrates through the limit groove, the inner wall of the supporting shaft is provided with a thread cylinder, the inner wall of the thread cylinder is provided with a threaded rod in a penetrating manner, the inner wall of the limit groove is provided with a supporting ring, and one end of the threaded rod is provided with the supporting ring in a penetrating manner;
the inner wall of the limiting groove is provided with a guide component, and the guide component is used for assisting the sliding position of the support shaft.
Preferably, the guide assembly comprises a guide groove and a guide plate, wherein the guide groove is symmetrically arranged in the support shaft, the guide groove is positioned on one side of the threaded cylinder, the guide plate corresponding to the guide groove is symmetrically arranged on the inner wall of the limit groove, and one end of the guide plate is arranged in the guide groove in a penetrating mode.
Preferably, the inner wall of the limit groove is provided with a bearing plate, and the bearing plate is circular and is attached to the outer wall of the support shaft.
Preferably, the inner wall of the ring body is provided with mounting boxes in sequence.
Preferably, the inner wall of the installation box is provided with a fan, and the outer wall of the installation box is provided with a filter screen.
Preferably, the outer wall of the mounting box is provided with a connector, the output end of the fan is connected with the input end of the connector, and the output end of the connector is provided with an exhaust hole.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the utility model, the adjusting component is arranged to facilitate the installation of the rocket forging balance ring, when the rocket forging balance ring is installed, after the rocket forging balance ring is placed at an installation site, the threaded rod is rotated to enable the position of the threaded cylinder to move, the position of the supporting shaft is driven to move when the position of the threaded cylinder moves, when the position of the supporting shaft moves, the guide plate guides the position of the supporting shaft through the guide groove, so that the position of the supporting shaft can be adjusted, and after one end of the supporting shaft moves into a groove body preset at the installation site, the rocket forging balance ring is conveniently installed, thereby achieving the purpose of improving the installation efficiency of the rocket forging balance ring;
2. according to the utility model, the fan and the exhaust hole are arranged to facilitate the removal of the adsorbate on the outer wall of the gyroscope assembly arranged in the forging balance ring for the rocket, when the adsorbate on the outer wall of the device arranged in the interior is cleaned during the use period of the forging balance ring for the rocket, which is convenient to install, the fan is enabled to work to extract the air in the installation box, and after the extracted air flows into the connector, the extracted air flows to the outer wall of the gyroscope assembly arranged in the interior through the exhaust hole, so that the adsorbate on the outer wall of the gyroscope assembly is conveniently removed.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic diagram of the front structure of the present utility model;
FIG. 3 is a schematic view of a portion of a lubrication ring according to the present utility model;
fig. 4 is a schematic view of a portion of a connecting pipe according to the present utility model.
In the figure: 1. a ring body; 2. an adjustment assembly; 3. a limit groove; 4. a support shaft; 5. a bearing plate; 6. a guide groove; 7. a guide plate; 8. a thread cylinder; 9. a threaded rod; 10. a support ring; 11. a mounting box; 12. a filter screen; 13. a blower; 14. a connector; 15. and an exhaust hole.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In the description of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
Please refer to fig. 1 and 2, a forging balance ring for rocket convenient to installation, including ring body 1, the inner wall symmetry of ring body 1 is provided with adjusting part 2, and ring body 1 is forging balance ring for rocket, and both the basic supporting part of gyroscope is, when the rocket launches, need use the gyroscope to guarantee that these flying equipment can go work according to appointed mode, and the inner wall of spacing groove 3 is provided with bearing plate 5, and bearing plate 5 appearance is the ring form, laminating with the outer wall of back shaft 4, bearing plate 5 pairs.
Referring to fig. 2 and 3, the adjusting component 2 includes a limit groove 3, a support shaft 4, a thread cylinder 8, a threaded rod 9 and a support ring 10, the inner wall of the adjusting component 2 is provided with the limit groove 3, one end of the support shaft 4 is penetrated and arranged in the limit groove 3, the inner wall of the support shaft 4 is provided with the thread cylinder 8, the threaded rod 9 is penetrated and arranged in the inner wall of the thread cylinder 8, the inner wall of the limit groove 3 is provided with the support ring 10, one end of the threaded rod 9 is penetrated and arranged in the support ring 10, the inner wall of the limit groove 3 is provided with the guide component, and the guide component is used for assisting the sliding position of the support shaft 4, the guide component comprises a guide groove 6 and a guide plate 7, the guide groove 6 is symmetrically arranged in the support shaft 4, the guide groove 6 is positioned on one side of the thread cylinder 8, the guide plate 7 corresponding to the guide groove 6 is symmetrically arranged on the inner wall of the limit groove 3, one end of the guide plate 7 is penetrated and arranged in the guide groove 6, when the forging balance ring for rocket is installed, the forging balance ring for rocket is placed at the installation place, the position of the screw rod 9 can enable the position of the thread cylinder 8 to move, when the position of the thread cylinder 8 moves, the support shaft 4 can drive the support shaft 4 to move to the guide shaft 4, and then the rocket can move to the guide shaft 4 can reach the installation position of the preset position, and reach the purpose of the installation position of the forging body, and the guide plate can reach the installation position of the balance position when the rocket is adjusted by the guide plate 4.
Referring to fig. 2 and 4, the inner wall of the ring body 1 is sequentially provided with a mounting box 11, a fan 13 is arranged on the inner wall of the mounting box 11, a filter screen 12 is arranged on the outer wall of the mounting box 11, a connector 14 is arranged on the outer wall of the mounting box 11, the output end of the fan 13 is connected with the input end of the connector 14, an exhaust hole 15 is arranged at the output end of the connector 14, when the device outer wall adsorbate of the internal mounting device is cleaned during the use period of the rocket forging balance ring, the fan 13 is enabled to work to extract air in the mounting box 11, and after the extracted air flows into the connector 14, the extracted air flows to the outer wall of the internally arranged gyroscope assembly through the exhaust hole 15, so that the adsorbate of the outer wall of the gyroscope assembly is conveniently removed.
When the rocket forging balance ring is installed, the threaded rod 9 is rotated to enable the position of the threaded cylinder 8 to move after the rocket forging balance ring is placed at an installation site, the position of the threaded cylinder 8 can be driven to move when moving, the position of the support shaft 4 can be guided by the guide plate 7 through the guide groove 6 when moving, the position of the support shaft 4 can be adjusted, one end of the support shaft 4 moves into a groove body preset at the installation site, the rocket forging balance ring is convenient to install, when the rocket forging balance ring convenient to install is used after the rocket forging balance ring is used, air inside the installation box 11 is extracted when an adsorbate on the outer wall of an internally installed device is cleaned, the extracted air flows to the outer wall of a gyroscope assembly arranged inside after entering the connector 14 through the exhaust hole 15, and the adsorbate on the outer wall of the gyroscope assembly is convenient to clean.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides a forging balance ring for rocket convenient to installation which characterized in that includes:
the device comprises a ring body (1), wherein adjusting components (2) are symmetrically arranged on the inner wall of the ring body (1), and each adjusting component (2) comprises a limiting groove (3), a supporting shaft (4), a thread cylinder (8), a threaded rod (9) and a supporting ring (10);
the inner wall of the adjusting component (2) is provided with a limit groove (3), one end of the supporting shaft (4) is penetrated into the limit groove (3), the inner wall of the supporting shaft (4) is provided with a thread cylinder (8), the inner wall of the thread cylinder (8) is penetrated with a threaded rod (9), the inner wall of the limit groove (3) is provided with a supporting ring (10), and one end of the threaded rod (9) is penetrated into the supporting ring (10);
the inner wall of the limit groove (3) is provided with a guide component, and the guide component is used for assisting the sliding position of the support shaft (4).
2. The rocket forging gimbal for facilitating installation according to claim 1, wherein: the guide assembly comprises a guide groove (6) and a guide plate (7), wherein the guide groove (6) is symmetrically arranged in the support shaft (4), the guide groove (6) is located on one side of the threaded cylinder (8), the guide plate (7) corresponding to the guide groove (6) is symmetrically arranged on the inner wall of the limit groove (3), and one end of the guide plate (7) is arranged in the guide groove (6) in a penetrating mode.
3. The rocket forging gimbal for facilitating installation according to claim 2, wherein: the inner wall of the limit groove (3) is provided with a bearing plate (5), and the bearing plate (5) is in a ring shape and is attached to the outer wall of the support shaft (4).
4. A rocket forging gimbal for facilitating installation according to claim 3, wherein: the inner wall of the ring body (1) is sequentially provided with a mounting box (11).
5. The rocket forging gimbal for facilitating installation according to claim 4, wherein: the inner wall of the installation box (11) is provided with a fan (13), and the outer wall of the installation box (11) is provided with a filter screen (12).
6. The rocket forging gimbal for facilitating installation according to claim 5, wherein: the outer wall of installation case (11) is provided with connector (14), and the output of fan (13) is connected with the input of connector (14), and the output of connector (14) is provided with exhaust hole (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322167024.3U CN220435327U (en) | 2023-08-14 | 2023-08-14 | Forging balance ring for rocket convenient to installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322167024.3U CN220435327U (en) | 2023-08-14 | 2023-08-14 | Forging balance ring for rocket convenient to installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220435327U true CN220435327U (en) | 2024-02-02 |
Family
ID=89693994
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322167024.3U Active CN220435327U (en) | 2023-08-14 | 2023-08-14 | Forging balance ring for rocket convenient to installation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220435327U (en) |
-
2023
- 2023-08-14 CN CN202322167024.3U patent/CN220435327U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |