CN116294806A - Large-scale modularized rocket launching pad - Google Patents
Large-scale modularized rocket launching pad Download PDFInfo
- Publication number
- CN116294806A CN116294806A CN202310418615.5A CN202310418615A CN116294806A CN 116294806 A CN116294806 A CN 116294806A CN 202310418615 A CN202310418615 A CN 202310418615A CN 116294806 A CN116294806 A CN 116294806A
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- China
- Prior art keywords
- leveling
- side beam
- platform
- main body
- rocket
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- 230000003247 decreasing effect Effects 0.000 abstract description 3
- 238000009434 installation Methods 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
Abstract
The invention provides a large modularized rocket launching table, which comprises a leveling table main body, wherein the bottom of the leveling table main body is supported by leveling supporting legs, leveling table cover plates are arranged around the leveling table main body and are connected into a plane, the leveling table cover plates are arranged on a beam body at the bottom through bolts, the beam body is arranged on a foundation connecting piece through bolts, and the foundation connecting piece is welded and connected with a launching site foundation; the platform main body has various specifications according to the rocket interface form. According to the invention, the supporting force and the supporting position of the leveling supporting leg can be improved by replacing the local module of the lower table body of the launching table; the positions of the leveling support legs can be increased or decreased and replaced, so that the rocket can meet different rocket requirements; the adjustable platform main body can be replaced to adapt to the requirements of rocket launching with various diameters or boosting; the accessories are concentrated in the lower table body, so that the protection work of the vulnerable parts is simplified; has the characteristics of strong adaptability, simple operation, convenience, quickness and the like.
Description
Technical Field
The invention relates to a large modularized rocket launching pad.
Background
With the development of rocket launching technology, launching modes of three-flat-one-vertical (horizontal assembly, horizontal test, horizontal transfer and vertical launching schemes) are widely used. The launching pad is mainly used for supporting and fixing the rocket in a vertical state and accessories thereof before shooting, the launching pad is customized according to the characteristics of each model rocket at present, and in order to ensure the position alignment precision of the rocket and the launching pad after erection, the installation precision of an erection support and the launching pad needs to be ensured, and the installation, debugging and production work are complicated.
In the prior art, a small rocket launching pad is disclosed in Chinese patent application No. CN201910266614, but the invention is not suitable for large rocket launching with foundation diversion trenches; there is also a simple launch system for a carrier rocket disclosed in chinese patent application No. CN201410167798, which is difficult to adapt to rocket launch in more structural states.
Disclosure of Invention
In order to solve the technical problems, the invention provides a large-sized modularized rocket launching pad, which integrates the functions of a launching pad and a standing support, adopts a modularized design, and can be used for replacing local modules according to requirements so as to adapt to different rocket working conditions.
The invention is realized by the following technical scheme.
The invention provides a large modularized rocket launching table, which comprises a leveling table main body, wherein the bottom of the leveling table main body is supported by leveling supporting legs, leveling table cover plates are arranged around the leveling table main body and are connected into a plane, the leveling table cover plates are arranged on a beam body at the bottom through bolts, the beam body is arranged on a foundation connecting piece through bolts, and the foundation connecting piece is welded and connected with a launching site foundation; the platform main body has various specifications according to the rocket interface form.
The leveling table main body is covered with a leveling table cover plate.
The middle part of the leveling platform main body is provided with a diversion trench cover plate, and the diversion trench cover plate has various specifications according to the rocket interface form.
The position slewing bearing and the limiting seat which are positioned on the leveling table cover plate and at the edge of the leveling table main body are connected with the beam body through bolts.
The beam body comprises a platform west side beam, a platform north side beam, a platform east side beam and a platform south side beam, and the platform west side beam, the platform north side beam, the platform east side beam and the platform south side beam form a frame and form a closed space inside.
The rotary support and the limiting seat are both arranged on the north side beam of the table body.
The leveling support legs are arranged on the beam body.
The movable step ladder is arranged on the outer side wall of any one of the western side beam, the north side beam, the east side beam and the south side beam of the table body through bolts.
The invention has the beneficial effects that: the supporting force and the supporting position of the supporting leg can be lifted and leveled by replacing a local module of the lower table body of the launching table; the positions of the leveling support legs can be increased or decreased and replaced, so that the rocket can meet different rocket requirements; the adjustable platform main body can be replaced to adapt to the requirements of rocket launching with various diameters or boosting; the accessories are concentrated in the lower table body, so that the protection work of the vulnerable parts is simplified; has the characteristics of strong adaptability, simple operation, convenience, quickness and the like.
Drawings
FIG. 1 is an oblique side view of the present invention;
FIG. 2 is a front view of the present invention;
FIG. 3 is a top view of the present invention;
FIG. 4 is a schematic view of the structure of FIG. 1 after the leveling table body, cover plate and diversion trench cover plate are hidden;
FIG. 5 is a top view of FIG. 4;
FIG. 6 is a schematic view of the internal structure of FIG. 4;
fig. 7 is a schematic structural view of another embodiment of the present invention.
In the figure: the leveling device comprises a 1-leveling supporting leg, a 2-diversion trench cover plate, a 3-leveling platform body, a 4-leveling platform cover plate, a 5-platform body west side beam, a 6-platform body north side beam, a 7-slewing bearing, an 8-limiting seat, a 9-basic connecting piece, a 10-moving step, a 11-platform body east side beam and a 12-platform body south side beam.
Detailed Description
The technical solution of the present invention is further described below, but the scope of the claimed invention is not limited to the above.
Example 1
The large-scale modularized rocket launching pad as shown in fig. 1-6 comprises a leveling platform main body (3), wherein the bottom of the leveling platform main body 3 is supported by leveling supporting legs 1, leveling platform cover plates 4 are connected to form a plane around the leveling platform main body 3, the leveling platform cover plates 4 are arranged on a beam body at the bottom through bolts, the beam body is arranged on a foundation connecting piece 9 through bolts, and the foundation connecting piece 9 is welded and connected to a launching site foundation; the platform body 3 has various specifications according to the rocket interface form.
Example 2
Based on embodiment 1, the leveling table body 3 is capped with a leveling table cover plate 4.
Example 3
Based on embodiment 1, the middle part of the leveling platform main body 3 is provided with a diversion trench cover plate 2, and the diversion trench cover plate 2 has various specifications according to the rocket interface form.
Example 4
Based on embodiment 1, the position swivel support 7 and the limit seat 8 on the leveling platform cover plate 4 at the edge of the leveling platform main body 3 are connected to the beam body through bolts.
Example 5
Based on embodiment 1, the beam body includes a table body west side beam 5, a table body north side beam 6, a table body east side beam 11, and a table body south side beam 12, and the table body west side beam 5, the table body north side beam 6, the table body east side beam 11, and the table body south side beam 12 enclose a frame and form a closed space inside.
Example 6
Based on embodiment 4, both the swivel support 7 and the limit seat 8 are mounted on the north side beam 6 of the table body.
Example 7
Based on example 1, the leveling leg 1 is mounted to the beam body.
Example 8
Based on example 5, the moving step 10 was mounted by bolts on any one of the outer side walls of the side sill 5, the north sill 6, the east sill 11, and the south sill 12.
Example 9
Based on the above embodiment, as shown in fig. 1, the foundation connection 9 is connected to the launching site foundation by welding, and the body west side beam 5, the body north side beam 6, the body east side beam 11, and the body south side beam 12 are connected to each other and connected to the foundation connection by bolts and positioning steps. The platform adjusting body 3 is connected with the platform cover plate 4 through bolts and connected with the launching platform body through the leveling supporting legs 1, the diversion trench cover plate 2 is installed on the platform adjusting body 3, the slewing bearing 7 and the limiting seat 8 are installed on the north side beam 6 of the platform body, and the movable step ladder 10 is installed according to the use requirement. The adaptability is good, and the installation, debugging and production work is simplified. The table body west side beam 5, the table body north side beam 6, the table body east side beam 11 and the table body south side beam 12 are combined to form a relatively closed installation space, a relatively good protection environment is provided for installing accessories such as hydraulic pipelines, electric control combinations, cables and the like, and the protection work of vulnerable parts such as on-site pipelines, cables and the like before emission is reduced. The north side beam 6 and the south side beam 12 of the launching table body are reserved with a plurality of mounting interfaces of the leveling supporting legs 1, and the mounting positions and the mounting quantity of the leveling supporting legs can be adjusted according to the bearing requirements of the launching table. The modular design is adopted, so that the modules can be replaced according to the requirements, and the adaptability of the transmitting station is improved; the launching pad and the rocket interface are mainly arranged on the leveling pad main body 3, and the leveling pad main body 3 is arranged on the leveling supporting leg 1 through screw connection, so that the leveling pad main body 3 and the leveling pad cover plate 4 can be independently replaced according to the form of the rocket interface; the interface between the transmitting station and the transmitting site is converted into an internal interface by a basic connecting piece 9; the transmitting table body arranged on the basic connecting piece adopts a modularized design, and is mainly formed by assembling 7 modules, such as a table body west side beam 5, a table body north side beam 6, a rotary support 7, a limiting seat 8, a basic connecting piece 9, a table body east side beam 11, a table body south side beam 12 and the like. The north side beam 6 and the south side beam 12 of the bearing platform can be replaced according to the bearing requirement of the transmitting platform; the transmitting table is integrated with an interface of the erection device, the interfaces are arranged on the slewing bearing 7 and the limiting seat 8, and the slewing bearing 7 and the limiting seat 8 are both in threaded connection on the north side beam 6 of the table body and can be replaced according to the requirement of the erection device; and the integrated slewing bearing 7 and the limiting seat 8 can be installed according to the mechanical positioning interface on the north side beam 6 of the table body, so that the workload of independently installing the slewing bearing 7 in a transmitting field is reduced. The north side beam 6 of the table body and the south side beam 12 of the table body are reserved with a plurality of mounting interfaces of the leveling supporting legs 1, and the mounting positions and the mounting quantity of the leveling supporting legs can be adjusted according to the bearing requirements of the launching table.
Example 10
Based on the above embodiment, as shown in fig. 7, 8 leveling legs are installed, and the docking has 2 booster rocket states. The installation operation steps are as follows:
firstly, welding and installing a base connecting piece 9 on a ground of a transmitting field;
the quantity of the diversion trench cover plate 2, the leveling platform main body 3, the leveling platform cover plate 4, the north side beam 6 of the platform body, the south side beam 12 structure of the platform body and the leveling supporting legs 1 are determined according to the rocket structure and the weight;
a platform west side beam 5, a platform north side beam 6, a platform east side beam 11 and a platform south side beam 12 are arranged on a foundation connecting piece 9;
a leveling support leg 1 is arranged on a south side beam 12 of the platform body; a leveling supporting leg 1, a slewing bearing 7 and a limiting seat 8 are arranged on a north side beam 6 of the table body;
the device is connected with the diversion trench cover plate 2, the leveling table main body 3 and the leveling table cover plate 4;
the leveling support legs 1 and the leveling platform main body 3 are connected, and the launching platform has working conditions.
Thus, the present invention:
the rocket launching and erecting and slewing supporting functions are integrated, and the installation and debugging work of the rocket erecting support in the launching field is simplified;
the supporting force and the supporting position of the supporting leg can be lifted and leveled by replacing the local module of the lower table body of the launching table.
The positions of the leveling support legs can be increased or decreased and replaced, so that the rocket can meet different rocket requirements;
the adjustable platform main body can be replaced to adapt to the requirements of rocket launching with various diameters or boosting;
accessories such as leveling supporting legs, control combinations, hydraulic pipelines of related sensors, cable lines and the like are concentrated in the lower body of the launching table, so that the protection work of vulnerable parts is simplified.
Claims (8)
1. The utility model provides a large-scale modular rocket launching pad, is including transferring platform main part (3), its characterized in that: the bottom of the leveling table main body (3) is supported by leveling supporting legs (1), leveling table cover plates (4) are arranged around the leveling table main body (3) and connected into a plane, the leveling table cover plates (4) are arranged on a beam body at the bottom through bolts, the beam body is arranged on a foundation connecting piece (9) through bolts, and the foundation connecting piece (9) is welded and connected to a foundation of a launching site; the platform adjusting main body (3) has various specifications according to the rocket interface form.
2. A large modular rocket launching pad as recited in claim 1, wherein: the leveling table main body (3) is covered with a leveling table cover plate (4).
3. A large modular rocket launching pad as recited in claim 1, wherein: the middle part of the leveling platform main body (3) is provided with a diversion trench cover plate (2), and the diversion trench cover plate (2) has various specifications according to the rocket interface form.
4. A large modular rocket launching pad as recited in claim 1, wherein: the position swivel support (7) and the limit seat (8) which are positioned on the edge of the leveling table main body (3) on the leveling table cover plate (4) are connected to the beam body through bolts.
5. A large modular rocket launching pad as recited in claim 1, wherein: the beam body comprises a platform body west side beam (5), a platform body north side beam (6), a platform body east side beam (11) and a platform body south side beam (12), and the platform body west side beam (5), the platform body north side beam (6), the platform body east side beam (11) and the platform body south side beam (12) are enclosed into a frame and form a closed space inside.
6. A large modular rocket launching pad as recited in claim 4, wherein: the rotary support (7) and the limiting seat (8) are both arranged on the north side beam (6) of the table body.
7. A large modular rocket launching pad as recited in claim 1, wherein: the leveling support leg (1) is arranged on the beam body.
8. A large modular rocket launching pad as recited in claim 5, wherein: the movable step ladder (10) is mounted on the outer side wall of any one of the western side beam (5), the north side beam (6), the eastern side beam (11) and the south side beam (12) of the table body through bolts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310418615.5A CN116294806A (en) | 2023-04-18 | 2023-04-18 | Large-scale modularized rocket launching pad |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310418615.5A CN116294806A (en) | 2023-04-18 | 2023-04-18 | Large-scale modularized rocket launching pad |
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| Publication Number | Publication Date |
|---|---|
| CN116294806A true CN116294806A (en) | 2023-06-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310418615.5A Pending CN116294806A (en) | 2023-04-18 | 2023-04-18 | Large-scale modularized rocket launching pad |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116592707A (en) * | 2023-06-30 | 2023-08-15 | 东方空间技术(山东)有限公司 | Rocket launching pad |
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2023
- 2023-04-18 CN CN202310418615.5A patent/CN116294806A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116592707A (en) * | 2023-06-30 | 2023-08-15 | 东方空间技术(山东)有限公司 | Rocket launching pad |
| CN116592707B (en) * | 2023-06-30 | 2024-02-06 | 东方空间技术(山东)有限公司 | Rocket launching pad |
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