CN115060115A - Telescopic rocket launching container system - Google Patents
Telescopic rocket launching container system Download PDFInfo
- Publication number
- CN115060115A CN115060115A CN202210561813.2A CN202210561813A CN115060115A CN 115060115 A CN115060115 A CN 115060115A CN 202210561813 A CN202210561813 A CN 202210561813A CN 115060115 A CN115060115 A CN 115060115A
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- container
- sliding
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- telescopic
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- 230000007704 transition Effects 0.000 claims abstract description 63
- 230000007246 mechanism Effects 0.000 claims description 14
- 229910000831 Steel Inorganic materials 0.000 claims description 10
- 239000010959 steel Substances 0.000 claims description 10
- 230000000712 assembly Effects 0.000 claims description 4
- 238000000429 assembly Methods 0.000 claims description 4
- 230000033001 locomotion Effects 0.000 claims description 3
- 230000000452 restraining effect Effects 0.000 claims 1
- 235000015842 Hesperis Nutrition 0.000 abstract description 18
- 235000012633 Iberis amara Nutrition 0.000 abstract description 18
- 230000008901 benefit Effects 0.000 abstract description 5
- 238000006073 displacement reaction Methods 0.000 description 4
- 238000013459 approach Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
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
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
- Handcart (AREA)
Abstract
The invention relates to the technical field of rocket launching equipment, in particular to a telescopic rocket launching container system; the automobile chassis driving device comprises a driving assembly, a front fixing section, a middle transition section and a rear sliding section, wherein the front fixing section and the middle transition section are fixedly connected with an automobile chassis; the driving component is used for driving the rear sliding section to be close to or far away from the front fixing section; the driving assembly can drive the rear sliding section to be close to or far away from the front fixed section, so that the size of an accommodating space formed by the fixed container, the transition container and the sliding container is changed, rockets with different length sizes are suitable, the universality of the rockets and a launching platform is greatly improved, the utilization rate of the launching platform is improved, launching tasks of rockets with various types and different length sizes are completed, and the advantage of multiple rocket launching is formed; in addition, under the condition of wartime or emergency, the telescopic rocket launching container system can obviously reduce the harsh requirement of the rocket on the launching platform and ensure the successful launching of the rocket.
Description
Technical Field
The invention relates to the technical field of containers, in particular to a telescopic rocket launching container system.
Background
With the acceleration of the international space cause process, the launching frequency of the carrier rocket is obviously improved. The method has higher requirements for the technical development of civil rocket companies at home and abroad. In order to meet the launching requirements of rockets with different structure sizes, the task of improving the adaptability and the availability of the rocket launching device becomes a challenging task; in the prior art, when the container is used as a rocket launching platform, rocket launching containers with different sizes need to be made for rockets with different sizes, and the rocket launching container generally belong to one-for-one use, have large limitation and lack of universality and availability.
Disclosure of Invention
Aiming at the defects in the prior art, the invention provides a telescopic rocket launching container system, which solves the problems of large limitation, and lack of universality and availability of rocket launching containers in the prior art.
According to an embodiment of the invention, a telescopic rocket launching container system comprises a driving assembly, a front fixed section and a middle transition section which are fixedly connected with an automobile chassis, and a rear sliding section which is in sliding connection with the automobile chassis;
the front fixed section comprises a fixed auxiliary frame and a fixed container fixedly connected with the fixed auxiliary frame;
the middle transition section comprises a transition sub frame fixedly connected with the fixed sub frame and a transition container positioned above the transition sub frame, and the transition container is fixedly connected with the fixed container;
the rear sliding section comprises a sliding sub frame in sliding connection with the transition sub frame and a sliding container fixedly connected with the sliding sub frame, and the sliding container is in sliding connection with the transition container;
the driving component is used for driving the rear sliding section to be close to or far away from the front fixing section.
In the embodiment, the front fixing section and the middle transition section are fixedly connected to an automobile chassis of a carrier loader, the rear sliding section is in sliding connection with the automobile chassis, the front fixing section, the middle transition section and the rear sliding section respectively comprise an auxiliary frame and containers, the auxiliary frame is connected with the automobile chassis, and the containers on the auxiliary frame form a holding space for holding rockets; the fixed auxiliary frame is fixedly connected with the transition auxiliary frame, and the transition container is fixedly connected with the fixed container to form a whole; the sliding sub-frame is connected with the transition sub-frame in a sliding way, and the sliding container is connected with the transition container in a sliding way; the sliding sub-frame and the sliding container can be close to or far away from the fixed sub-frame and the fixed container, namely, the rear sliding section can be close to or far away from the front fixed section; the driving assembly can drive the rear sliding section to be close to or far away from the front fixed section, so that the size of an accommodating space formed by the fixed container, the transition container and the sliding container is changed, rockets with different length sizes are suitable, the universality of the rockets and a launching platform is greatly improved, the utilization rate of the launching platform is improved, launching tasks of rockets with various types and different length sizes are completed, and the advantage of multiple rocket launching is formed; in addition, under the condition of wartime or emergency, the telescopic rocket launching container system can obviously reduce the harsh requirement of the rocket on the launching platform and ensure the successful launching of the rocket.
Further, the driving assembly comprises a fixed rail and a moving mechanism movably mounted on the fixed rail.
Furthermore, one end of the fixed track is fixedly connected with the fixed container, the other end of the fixed track extends into the sliding container, and the moving mechanism is fixedly installed in the sliding container.
Further, the moving mechanism comprises a track wheel set arranged on the fixed track and a driving motor for driving the track wheel set, and the driving motor is fixedly connected with the sliding container.
Furthermore, the end part of the fixed track extending into the sliding container is fixedly connected with a limiting plate.
Further, the fixed rail is an I-shaped steel slide rail.
Furthermore, the sliding auxiliary frame is provided with a concave part for the transition auxiliary frame to extend into.
Furthermore, sliding grooves are formed in two sides of the transition auxiliary frame, and a plurality of movable wheels capable of sliding into the sliding grooves are movably connected to two sides of the concave portion.
Furthermore, leveling support legs are fixedly connected to the lower portions of the front fixing section and the rear sliding section.
Further, at least two sets of the driving assemblies are provided.
Compared with the prior art, the invention has the following beneficial effects:
the driving assembly can drive the rear sliding section to be close to or far away from the front fixed section, so that the size of an accommodating space formed by the fixed container, the transition container and the sliding container is changed, rockets with different length sizes are suitable, the universality of the rockets and a launching platform is greatly improved, the utilization rate of the launching platform is improved, launching tasks of rockets with various types and different length sizes are completed, and the advantage of multiple rocket launching is formed; in addition, under the condition of wartime or emergency, the telescopic rocket launching container system can obviously reduce the harsh requirement of the rocket on the launching platform and ensure the successful launching of the rocket.
Drawings
FIG. 1 is a schematic structural view of a telescopic rocket launch container according to an embodiment of the present invention;
FIG. 2 is a schematic perspective view of a fixed subframe, a transition subframe, a sliding subframe, leveling legs, and a drive assembly according to an embodiment of the present invention;
FIG. 3 is an enlarged schematic view at A in FIG. 2;
FIG. 4 is a schematic structural view of a fixed subframe, a transition subframe, a sliding subframe, leveling legs, and a drive assembly according to an embodiment of the present invention;
FIG. 5 is a schematic perspective view of a fixed subframe, a transition subframe, a sliding subframe, and leveling legs according to an embodiment of the present invention;
FIG. 6 is an enlarged schematic view at B of FIG. 5;
FIG. 7 is a schematic top sectional view of a telescopic rocket launch container according to an embodiment of the present invention;
FIG. 8 is a schematic side view of a secure container, a transition container, and a sliding container according to an embodiment of the present invention;
in the above drawings: 100. fixing the container; 110. fixing the auxiliary frame; 200. a transition container; 210. a transition sub-frame; 211. a chute; 300. sliding the container; 301. a hollow-out section; 310. sliding the subframe; 311. a movable wheel; 400. leveling the supporting legs; 500. a moving mechanism; 510. a drive motor; 520. a rail wheel set; 600. fixing a track; 610. and a limiting plate.
Detailed Description
The technical solution of the present invention is further described with reference to the drawings and the embodiments.
In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the invention.
Referring to fig. 1 to 8 together, the embodiment provides a telescopic rocket launching container system, which comprises a driving assembly, a front fixed section and a middle transitional section which are fixedly connected with an automobile chassis, and a rear sliding section which is slidably connected with the automobile chassis;
the front fixed section comprises a fixed sub-frame 110 and a fixed container 100 fixedly connected with the fixed sub-frame;
the middle transition section comprises a transition sub frame 210 fixedly connected with the fixed sub frame 110 and a transition container 200 positioned above the transition sub frame, and the transition container 200 is fixedly connected with the fixed container 100;
the rear sliding section comprises a sliding sub-frame 310 which is in sliding connection with the transition sub-frame 210 and a sliding container 300 which is fixedly connected with the sliding sub-frame, and the sliding container 300 is in sliding connection with the transition container 200;
the driving assembly is used for driving the rear sliding section to be close to or far away from the front fixing section.
In the embodiment, the front fixing section and the middle transition section are fixedly connected to an automobile chassis of a carrier loader, the rear sliding section is in sliding connection with the automobile chassis, the front fixing section, the middle transition section and the rear sliding section respectively comprise an auxiliary frame and containers, the auxiliary frame is connected with the automobile chassis, and the containers on the auxiliary frame form a holding space for holding rockets; the fixed sub-frame 110 is fixedly connected with the transition sub-frame 210, and the transition container 200 is fixedly connected with the fixed container 100 to form a whole; the sliding sub-frame 310 is connected with the transition sub-frame 210 in a sliding manner, and the sliding container 300 is connected with the transition container 200 in a sliding manner; allowing the sliding sub-frame 310 and sliding containers 300 to be closer to or farther from the fixed sub-frame 110 and the fixed containers 100, i.e., the rear sliding sections can be closer to or farther from the front fixed sections; the driving assembly can drive the rear sliding section to be close to or far away from the front fixed section, so that the size of an accommodating space formed by the fixed container 100, the transition container 200 and the sliding container 300 is changed, rockets with different length sizes are suitable, the universality of the rockets and a launching platform is greatly improved, the utilization rate of the launching platform is improved, the launching tasks of rockets with various types and different length sizes are completed, and the advantage of multiple rocket launchers is formed; in addition, under the condition of wartime or emergency, the telescopic rocket launching container system can obviously reduce the harsh requirement of the rocket on the launching platform and ensure the successful launching of the rocket.
Preferably, the driving assembly includes a fixed rail 600 and a moving mechanism 500 movably mounted on the fixed rail 600; one end of the fixed rail 600 is fixedly connected with the fixed container 100, the other end thereof extends into the sliding container 300, and the moving mechanism 500 is fixedly installed in the sliding container 300; the moving mechanism 500 includes a rail wheel set 520 installed on the fixed rail 600 and a driving motor 510 driving the rail wheel set 520, and the driving motor 510 is fixedly connected to the sliding container 300.
As shown in fig. 2, 3, 4 and 7, the driving assembly includes a fixed rail 600 and a moving mechanism 500, the fixed rail 600 is fixedly connected to the inner bottom surface of the fixed container 100; the moving mechanism 500 is installed in the sliding container 300, and includes a driving motor 510 fixedly installed on the inner bottom surface of the sliding container 300, and a rail wheel group 520 installed on a fixed rail 600; when the driving motor 510 drives the track wheel set 520 to operate, the track wheel set 520 can move on the fixed track 600, and drives the sliding container 300 fixedly connected with the driving motor 510 and the sliding sub-frame 310 at the bottom of the sliding container to approach the front fixed section; specifically, the driving motor 510 and the track wheel set 520 are mature moving devices in the prior art, and the rear sliding section can be driven to move through the mutual matching of the track wheel set 520, the driving motor 510 and the fixed track 600; more specifically, other mechanisms in the prior art can be adopted to drive the rear sliding section to move, for example, an electric slider in the prior art can be adopted, the electric slider is fixedly connected with the rear sliding section, and then the electric slider is movably installed on a track fixedly connected with the front fixed section, or a hydraulic telescopic rod is adopted, two ends of the hydraulic telescopic rod are respectively fixedly connected with the front fixed section and the rear sliding section, and the rear sliding section is driven to move through the expansion and contraction of the hydraulic telescopic rod.
Preferably, the end of the fixing rail 600 protruding into the sliding container 300 is fixedly connected with a limiting plate 610.
As shown in fig. 2 and 3, the limiting plate 610 can limit the track wheel set 520 and prevent the track wheel set 520 from being separated from the fixed track 600.
Preferably, the fixed rail 600 is an i-steel rail.
As shown in fig. 2 and 3, the fixed rail 600 is an i-shaped steel rail in the prior art, and is matched with the rail wheel set 520 having two rows of moving wheels, so that the matching between the moving mechanism 500 and the fixed rail 600 is more stable; specifically, the outer side wall of the wheel in the track wheel set 520 is provided with a gear, the bottom side of the grooves on both sides of the i-shaped steel slide rail is axially and uniformly provided with upper convex teeth, the gear on the track wheel set 520 is engaged with the convex teeth on the i-shaped steel slide rail, the track wheel set 520 can stably move on the i-shaped steel slide rail when rotating, and when the track wheel set 520 stops rotating, the gear is engaged with the convex teeth on the i-shaped steel slide rail to limit each other, so that the track wheel set 520 and the i-shaped steel slide rail are prevented from moving relative to each other, and the relative position between the track wheel set 520 and the i-shaped steel slide rail is kept, thereby keeping the stability of the sliding container 300.
Preferably, the sliding subframe 310 is recessed to allow the transition subframe 210 to extend into.
As shown in fig. 5 and 6, the recessed portion of the sliding subframe 310 allows the transition subframe 210 to extend into the recessed portion, and allows the sliding subframe 310 to approach the fixed subframe 110.
Preferably, sliding grooves 211 are formed in both sides of the transition subframe 210, and a plurality of movable wheels 311 capable of sliding into the sliding grooves 211 are movably connected to both sides of the recessed portion.
As shown in fig. 5 and 6, the movable wheels 311 on the side of the recessed portion are engaged with the sliding grooves 211 on the transition subframe 210, so that friction between the transition subframe 210 and the sliding subframe 310 can be reduced, and abrasion can be reduced.
Preferably, the leveling legs 400 are fixedly connected below the front fixing section and the rear sliding section.
As shown in fig. 1, 2, 4 and 5, when the container is placed on the ground, the container can be leveled by the leveling legs 400, which is beneficial to installation, loading and rocket launching; specifically, the leveling leg 400 is fixedly installed on the subframe or the container, and the leveling leg 400 may be an electro-hydraulic leg in the prior art.
Preferably, at least two sets of drive assemblies are provided.
As shown in fig. 2 and 7, the rear sliding section is driven by two sets of driving assemblies to move simultaneously, so that the movement of the rear sliding section is more stable.
Specifically, as shown in fig. 4, the edge on the sliding container 300 is provided with a hollow 301 for the middle transition section side wall to extend into, the bottom surface of the transition container 200 is located below the bottom surface of the sliding container 300, and the top surface of the transition container 200 is located below the top surface of the sliding container 300, so that the transition container 200 can be slidably connected with the sliding container 300, more specifically, as shown in fig. 4, the side wall of the sliding container 300 and the side wall of the transition container 200 are further provided with limiting protrusions which are matched with each other, thereby avoiding the separation of the side wall and the transition container.
Specifically, the carrier loader can be a carrier truck and a semitrailer in the prior art, the fixed auxiliary frame 110 and the transition auxiliary frame 210 can be fixedly connected with the automobile chassis by using tools such as U-shaped bolts, thrust connecting plates and connecting supports, the auxiliary frame of the rear sliding section is slidably connected with the automobile chassis, an upper pulley can be mounted at the bottom of the rear sliding section, and a sliding rail matched with the pulley is fixedly mounted on the automobile chassis.
Specifically, displacement sensors can be arranged on the front fixed section and the rear sliding section, the distance between the front fixed section and the rear sliding section is detected through the displacement sensors, the size of the whole container is convenient to adjust, and the rocket launcher can be replaced according to the size of the whole container; more specifically, the container further comprises a remote control device used by a worker, the remote control device is in communication connection with the displacement sensor and the driving motor 510, the remote control device can display the distance between the front fixed section and the rear sliding section in real time after receiving data of the displacement sensor, and the remote control device can control the driving motor 510 to be started and closed, so that the worker can conveniently and visually adjust the overall state of the container.
Compared with the prior art, the driving assembly can drive the rear sliding section to be close to or far away from the front fixed section, so that the size of an accommodating space formed by the fixed container 100, the transition container 200 and the sliding container 300 is changed, rockets with different length sizes are suitable, the universality of the rockets and a launching platform is greatly improved, the utilization rate of the launching platform is improved, rocket launching tasks of various types and different length sizes are finished, and the advantage of multiple rocket launching is formed; in addition, under the condition of wartime or emergency, the telescopic rocket launching container system can obviously reduce the harsh requirement of the rocket on the launching platform and ensure the successful launching of the rocket.
Finally, the above embodiments are only for illustrating the technical solutions of the present invention and not for limiting, although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made to the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, and all of them should be covered in the claims of the present invention.
Claims (10)
1. A telescopic rocket launching container system is characterized by comprising a driving assembly, a front fixed section and a middle transitional section which are fixedly connected with an automobile chassis, and a rear sliding section which is in sliding connection with the automobile chassis;
the front fixed section comprises a fixed auxiliary frame and a fixed container fixedly connected with the fixed auxiliary frame;
the middle transition section comprises a transition sub frame fixedly connected with the fixed sub frame and a transition container positioned above the transition sub frame, and the transition container is fixedly connected with the fixed container;
the rear sliding section comprises a sliding sub frame in sliding connection with the transition sub frame and a sliding container fixedly connected with the sliding sub frame, and the sliding container is in sliding connection with the transition container;
the driving component is used for driving the rear sliding section to be close to or far away from the front fixing section.
2. A telescopic rocket launch container system according to claim 1 wherein said drive assembly comprises a fixed track and a locomotion mechanism movably mounted on said fixed track.
3. A telescopic rocket launch container system according to claim 2 wherein said fixed track is fixedly attached at one end to said fixed container and at the other end extends into said sliding container, said locomotion mechanism being fixedly mounted within said sliding container.
4. A telescopic rocket launch container system according to claim 3 wherein said moving mechanism comprises a set of rail wheels mounted on said fixed rail and a drive motor for driving said set of rail wheels, said drive motor being fixedly connected to said sliding container.
5. A telescopic rocket launch container system according to claim 4 wherein the ends of said fixed rails extending into said sliding container are fixedly attached with restraining plates.
6. A telescopic rocket launch container system according to claim 5 wherein said fixed rail is an I-steel skid.
7. A telescopic rocket launch container system according to claim 1 wherein said sliding sub-frame defines a recess into which said transition sub-frame extends.
8. A telescopic rocket launch container system according to claim 7 wherein said transition sub-frame is provided with a plurality of sliding slots on both sides thereof, and a plurality of movable wheels are movably connected to both sides of said recessed portion for sliding into said sliding slots.
9. A telescopic rocket launch container system according to claim 1 wherein leveling legs are fixedly attached below both said front stationary section and said rear sliding section.
10. A telescopic rocket launch container system according to claim 2 wherein at least two sets of said drive assemblies are provided.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210561813.2A CN115060115B (en) | 2022-05-23 | 2022-05-23 | Telescopic rocket launching container system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210561813.2A CN115060115B (en) | 2022-05-23 | 2022-05-23 | Telescopic rocket launching container system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115060115A true CN115060115A (en) | 2022-09-16 |
| CN115060115B CN115060115B (en) | 2024-07-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202210561813.2A Active CN115060115B (en) | 2022-05-23 | 2022-05-23 | Telescopic rocket launching container system |
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2022
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| Publication number | Publication date |
|---|---|
| CN115060115B (en) | 2024-07-02 |
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