CN215622786U - Unloading vehicle for certain type air-ground missile - Google Patents
Unloading vehicle for certain type air-ground missile Download PDFInfo
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- CN215622786U CN215622786U CN202121576761.3U CN202121576761U CN215622786U CN 215622786 U CN215622786 U CN 215622786U CN 202121576761 U CN202121576761 U CN 202121576761U CN 215622786 U CN215622786 U CN 215622786U
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Abstract
The utility model discloses a certain type air-ground missile loading and unloading vehicle, which relates to the technical field of missile loading and unloading and comprises the following components: a movable base; the bracket is arranged on the upper side of the movable base; the supporting platform is movably connected with the bracket through a lifting mechanism; the bracket is movably arranged on the supporting platform and is provided with a limiting structure, and the limiting structure is matched with the appearance of the missile and used for limiting the missile; the unloading vehicle is simple in structure, low in cost and convenient to operate and move, guided missiles can be fixed and lifted through the limiting structure and the lifting structure, the guided missile loading and unloading difficulty is reduced, and guided missile loading and unloading efficiency is improved.
Description
Technical Field
The utility model belongs to the technical field of missile loading and unloading, and particularly relates to a certain type air-ground missile unloading vehicle.
Background
A certain type of air-to-ground missile is hung on a medium-large fixed wing unmanned aerial vehicle or a helicopter through a missile guide frame, the missile is lifted out of a missile box by a person in the current hanging process, then two persons respectively support the head and the tail of the missile and move to the lower part of the missile guide frame, the umbilical cable of the missile is firstly connected onto the missile guide frame by the other person, then a lock catch of the missile guide frame is unlocked, the sliding block of the missile is aligned to a mounting groove in the missile guide frame by the two persons supporting the missile, and then the missile is mounted on the missile guide frame.
Because before the guided missile installation, need alone wiring and open the hasp, two people are responsible for holding in the palm bullet and the work of mounting groove alignment, and this type guided missile weight is heavier, and the range of adjustment when personnel operate is great, and this process is consuming time longer, leads to the dress of hanging of guided missile inefficiency, and it is also inconvenient to dismantle simultaneously, consuming time and wasting force.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a certain type of air-ground missile unloading vehicle aiming at the defects in the prior art, the unloading vehicle is simple in structure, low in cost and convenient to operate and move, the missile can be fixed and lifted respectively through a limiting structure and a lifting structure, the missile unloading difficulty is reduced, and the missile unloading efficiency is improved.
In order to achieve the above object, the present invention provides an unloading vehicle for air-ground missiles of a certain type, comprising:
a movable base;
the bracket is arranged on the upper side of the movable base;
the supporting platform is movably connected with the bracket through a lifting mechanism;
the bracket is movably arranged on the supporting platform, a limiting structure is arranged on the bracket, and the limiting structure is matched with the appearance of the missile and used for limiting the missile.
Optionally, the movable base comprises a bottom plate, and casters with locks are arranged on the lower side of the bottom plate.
Optionally, handrails are arranged on two sides of the support.
Optionally, the lifting mechanism comprises:
the screw rod is rotatably arranged in the bracket, and one end of the supporting platform is in transmission fit with the screw rod;
the driving motor is connected with one end of the screw rod;
the guide rods are arranged on two sides of the screw rod, and one end of the supporting platform is sleeved on the guide rods in a sliding mode.
Optionally, the bracket includes layer board and spacing, spacing is provided with two pairs, two pairs spacing sets up respectively the both ends of the upside of layer board are every to spacing includes two limiting plates, two the one end of limiting plate with the layer board is connected and is formed V-arrangement groove structure, V-arrangement groove structure is inside can hold the guided missile and right the guided missile carries on spacingly.
Optionally, the support plate further comprises a guide rail plate, the guide rail plate is arranged on the lower side of the support plate, and a linear slide rail is arranged between the guide rail plate and the support plate.
Optionally, the linear sliding rail includes a protrusion disposed on the upper side of the rail plate and a recess disposed on the lower side of the supporting plate, and the protrusion is slidably embedded in the recess.
Optionally, the lower side of the guide rail plate is connected with the upper side of the support platform through a rotating table.
Optionally, a roller is rotatably arranged at the other end of the limit plate and can be in rolling fit with the outer surface of the missile.
Optionally, the top of the bracket is provided with a limiting block, the limiting block is matched with the missile guiding frame of the missile, and when the limiting block abuts against one side of the missile guiding frame, the sliding block of the missile on the limiting structure corresponds to the mounting groove on the missile guiding frame.
The utility model provides a certain type air-ground missile unloading vehicle, which has the beneficial effects that: the unloading vehicle is simple in structure, low in cost and convenient to operate and move, the guided missiles can be fixed and lifted through the limiting structure and the lifting structure respectively, the guided missile loading and unloading difficulty is reduced, and the guided missile loading and unloading efficiency is improved; the unloading vehicle enables the bracket to move, rotate and rotate on the supporting platform through the arrangement of the linear slide rail, the roller and the rotating platform, so that the loading and unloading of the guided missile are facilitated; the limiting block at the top of the support of the unloading vehicle is matched with the guide frame, so that the unloading vehicle can be conveniently positioned below the guide frame, the alignment difficulty of the sliding block and the mounting groove during installation of the guided missile is reduced, and the mounting efficiency is improved.
Additional features and advantages of the utility model will be set forth in the detailed description which follows.
Drawings
The above and other objects, features and advantages of the present invention will become more apparent by describing in more detail exemplary embodiments thereof with reference to the attached drawings, in which like reference numerals generally represent like parts throughout.
Figure 1 shows a schematic view of the structure of a missile.
Fig. 2 shows a schematic structural view of the hair-guiding frame.
Figure 3 shows a schematic of the overall structure of a type of air-to-ground missile unloading vehicle according to one embodiment of the utility model.
Figure 4 shows a schematic view of the underside of the mobile base of a type of air-to-ground missile unloading vehicle, according to one embodiment of the utility model.
Figure 5 shows a partial schematic view of a limit stop structure for a type of air-to-ground missile unloading vehicle according to one embodiment of the utility model.
Fig. 6 shows a schematic view of the connection of a limit structure of a type of air-ground missile unloading vehicle and a support platform according to one embodiment of the utility model.
Fig. 7 shows a schematic structural diagram of a linear guideway of a type of air-ground missile unloading vehicle according to an embodiment of the utility model.
Figure 8 shows a schematic diagram of the use of a type of air-to-ground missile unloading vehicle according to one embodiment of the utility model.
Description of reference numerals:
1. a support; 2. a support platform; 3. a missile; 4. a base plate; 5. a caster with a lock; 6. a handrail; 7. a screw rod; 8. a drive motor; 9. a guide bar; 10. a support plate; 11. a limiting plate; 12. a guide rail plate; 13. a boss portion; 14. a recessed portion; 15. a rotating table; 16. a roller; 17. a limiting block; 18. a hair guide frame; 19. a slider; 20. and (4) mounting the groove.
Detailed Description
Preferred embodiments of the present invention will be described in more detail below. While the following describes preferred embodiments of the present invention, it should be understood that the present invention may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the utility model to those skilled in the art.
The utility model provides a unloading vehicle for a certain type of air-ground missile, which comprises:
a movable base;
the bracket is arranged on the upper side of the movable base;
the supporting platform is movably connected with the bracket through a lifting mechanism;
the bracket is movably arranged on the supporting platform, and is provided with a limiting structure which is matched with the appearance of the missile and used for limiting the missile.
The missile loading and unloading device comprises a bracket, a movable base, a support, a lifting mechanism, a supporting platform, a missile lifting mechanism, a missile loading and unloading mechanism, a missile loading and unloading mechanism and a missile unloading mechanism.
Optionally, the movable base comprises a base plate, and casters with locks are arranged on the lower side of the base plate.
Specifically, the arrangement of the caster wheel with the lock not only facilitates the movement of the unloading vehicle, but also can lock the unloading vehicle after the unloading vehicle reaches a set position, so that the position of the unloading vehicle is kept still.
Optionally, handrails are provided on both sides of the support.
Specifically, the arrangement of the handrail is convenient for pushing the unloading vehicle.
Optionally, the lifting mechanism comprises:
the screw rod is rotatably arranged in the bracket, and one end of the supporting platform is in transmission fit with the screw rod;
the driving motor is connected with one end of the screw rod;
the guide rods are arranged on two sides of the screw rod, and one end of the supporting platform is sleeved on the guide rods in a sliding mode.
Specifically, driving motor can drive the lead screw and rotate, and supporting platform's one end is provided with the screw hole with lead screw thread fit, through the lift of the rotation drive supporting platform of lead screw, the guide bar plays the guide effect that supporting platform goes up and down.
Optionally, the bracket includes layer board and spacing, and spacing is provided with two pairs, and two pairs of spacing set up respectively at the both ends of the upside of layer board, and every pair of spacing includes two limiting plates, and the one end and the layer board of two limiting plates are connected and are formed V-arrangement groove structure, and V-arrangement groove structure is inside can hold the guided missile and carry on spacingly to the guided missile.
Specifically, the missile can be embedded into the V-shaped groove structure and is clamped and limited by the paired limiting plates.
Optionally, the support device further comprises a guide rail plate, the guide rail plate is arranged on the lower side of the support plate, and a linear slide rail is arranged between the guide rail plate and the support plate.
Specifically, the running direction of the linear slide rail is parallel to the axis direction of the missile.
Optionally, the linear sliding rail includes a protruding portion disposed on the upper side of the rail plate and a recessed portion disposed on the lower side of the supporting plate, and the protruding portion is slidably embedded in the recessed portion.
Specifically, the operation of the linear slide rail is realized through the sliding of the convex part in the concave part, and the operation of the linear slide rail is convenient for the slide block of the guided missile to be inserted into the mounting groove of the guided missile frame.
Optionally, the lower side of the guide rail plate is connected with the upper side of the support platform through a rotating table.
Specifically, the arrangement of the rotating table enables the bracket to horizontally rotate on the upper side of the supporting platform, and the position of the missile is conveniently adjusted.
Optionally, a roller is rotatably arranged at the other end of the limit plate and can be in rolling fit with the outer surface of the missile.
Specifically, the roller can be in rolling fit with the outer surface of the missile, so that the missile can roll in the V-shaped groove structure conveniently, and the orientation of the sliding block of the missile can be adjusted conveniently.
Optionally, the top of the support is provided with a limiting block, the limiting block is matched with the missile guiding frame of the missile, and when the limiting block is abutted against one side of the missile guiding frame, the sliding block of the missile on the limiting structure corresponds to the installation groove on the missile guiding frame.
The limiting block is abutted to one side of the hair guiding frame, the control of the relative position of the unloading vehicle and the hair guiding frame is achieved, the unloading vehicle is convenient to move to the position behind the lower portion of the hair guiding frame, and the position of the unloading vehicle can be kept still after the unloading vehicle is in place by locking the caster wheels with the lock.
Examples
As shown in fig. 1 to 8, the present invention provides a certain type of air-ground missile unloading vehicle, comprising:
a movable base;
the bracket 1 is arranged on the upper side of the movable base;
the supporting platform 2 is movably connected with the bracket 1 through a lifting mechanism;
the bracket is movably arranged on the supporting platform 2, and is provided with a limiting structure which is matched with the shape of the missile 3 and used for limiting the missile 3.
In this embodiment, the movable base comprises a bottom plate 4, and casters 5 with locks are arranged on the lower side of the bottom plate 4.
In this embodiment, handrails 6 are provided on both sides of the stand 1.
In this embodiment, the elevating mechanism includes:
the screw rod 7 is rotatably arranged in the bracket 1, and one end of the supporting platform 2 is in transmission fit with the screw rod 7;
the driving motor 8 is connected with one end of the screw rod 7;
and the guide rods 9 are arranged on two sides of the screw rod 7, and one end of the supporting platform 2 is sleeved on the guide rods 9 in a sliding manner.
In this embodiment, the bracket includes layer board 10 and spacing, and the spacing is provided with two pairs, and two pairs of spacing set up respectively at the both ends of the upside of layer board 10, and every pair of spacing includes two limiting plates 11, and the one end of two limiting plates 11 is connected with layer board 10 and is formed V-arrangement groove structure, and V-arrangement groove structure is inside can hold guided missile 3 and carry on spacingly to guided missile 3.
In the embodiment, the support plate further comprises a rail plate 12, the rail plate 12 is arranged on the lower side of the support plate 10, and a linear slide rail is arranged between the rail plate 12 and the support plate 10.
In the embodiment, the linear guideway comprises a convex part 13 arranged on the upper side of the guideway plate 12 and a concave part 14 arranged on the lower side of the supporting plate 10, and the convex part 13 is embedded in the concave part 14 in a sliding way.
In this embodiment, the underside of the rail plate 12 is connected to the upper side of the support platform 2 by a swivel 15.
In the embodiment, the other end of the limit plate 11 is rotatably provided with a roller 16, and the roller 16 can be in rolling fit with the outer surface of the missile 3.
In this embodiment, the top of the bracket 1 is provided with a limit block 17, the limit block 17 is matched with the missile guiding frame 18 of the missile 3, and when the limit block 17 is abutted against one side of the missile guiding frame 18, the slide block 19 of the missile 3 on the limit structure corresponds to the installation groove 20 on the missile guiding frame 18.
In summary, when the air-ground missile unloading vehicle provided by the utility model is used, taking one-time installation and disassembly of the missile 3 as an example, the operation steps are as follows, when loading is needed:
1. lifting the missile 3 out of the missile box, placing the missile on a bracket, pushing the unloading vehicle to the position right below the launching guide frame 18, enabling the limiting block 17 to abut against the launching guide frame 18, and locking the caster 5 with the lock;
2. starting the driving motor 8, lifting the missile 3 to a position about 5 centimeters away from the missile launcher 18, and connecting the umbilical cables;
3. the position and the direction of the missile 3 are adjusted by adjusting the rotating table 15, the roller 16 and the linear guide rail, and the slide block 19 of the missile 3 is aligned to the installation groove 20 of the missile guide frame 18;
4. the motor 8 is driven to slowly run, and the sliding block 19 of the missile 3 stops when entering the installation groove 20;
5. the lock catch of the missile guiding frame 18 is opened, the tail of the missile 3 is pushed, and the missile 3 is pushed into the missile guiding frame 18;
6. the driving motor 8 is started, the supporting platform 2 is lowered to the bottom of the unloading vehicle, and then the caster wheel 5 with the lock is unlocked and pushed away.
When the bullet needs to be unloaded:
1. pushing the unloading vehicle to the position right below the missile 3, wherein the limiting block 17 abuts against the hair-guiding frame 18 and locks the caster 5 with the lock;
2. starting a driving motor 8, and lifting the support platform 2 to a position 5 centimeters below the missile 3;
3. the sliding central line is ensured to be parallel to the axis of the missile 3 by adjusting the rotating table 15;
4. the driving motor 8 is slowly operated, and the bracket stops after being jacked to the missile body of the missile 3;
5. the lock catch of the missile guiding frame 18 is opened, the head of the missile 3 is pushed, and the missile 3 is pushed out from the inside of the missile guiding frame 18;
6. starting a driving motor 9, reducing the support platform 2 by 5 cm, and disconnecting the umbilical cable;
7. continuing to lower the support platform 2 to the bottom of the unloading vehicle, unlocking the caster 5 with the lock and pushing away the unloading vehicle;
8. the missile 3 is lifted out and placed in the missile box.
Having described embodiments of the present invention, the foregoing description is intended to be exemplary, not exhaustive, and not limited to the embodiments disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments.
Claims (10)
1. A certain type air-ground missile unloads car, its characterized in that, should unload the car and include:
a movable base;
the bracket is arranged on the upper side of the movable base;
the supporting platform is movably connected with the bracket through a lifting mechanism;
the bracket is movably arranged on the supporting platform, a limiting structure is arranged on the bracket, and the limiting structure is matched with the appearance of the missile and used for limiting the missile.
2. The type of air-to-ground missile unloading vehicle of claim 1, wherein the movable base comprises a bottom plate, and casters with locks are arranged on the lower side of the bottom plate.
3. An air-ground missile unloading vehicle according to claim 1, wherein handrails are arranged on two sides of the support.
4. An air-ground missile unloading vehicle of a certain type according to claim 1, wherein the lifting mechanism comprises:
the screw rod is rotatably arranged in the bracket, and one end of the supporting platform is in transmission fit with the screw rod;
the driving motor is connected with one end of the screw rod;
the guide rods are arranged on two sides of the screw rod, and one end of the supporting platform is sleeved on the guide rods in a sliding mode.
5. The type air-ground missile unloading vehicle of claim 1, wherein the bracket comprises a supporting plate and two pairs of limiting frames, the two pairs of limiting frames are respectively arranged at two ends of the upper side of the supporting plate, each pair of limiting frames comprises two limiting plates, one ends of the two limiting plates are connected with the supporting plate to form a V-shaped groove structure, and the V-shaped groove structure can contain the missile and limit the missile.
6. The type of air-ground missile unloading vehicle of claim 5, further comprising a guide rail plate, wherein the guide rail plate is arranged on the lower side of the supporting plate, and a linear slide rail is arranged between the guide rail plate and the supporting plate.
7. The type of air-ground missile unloading vehicle of claim 6, wherein the linear slide rail comprises a convex part arranged on the upper side of the guide rail plate and a concave part arranged on the lower side of the supporting plate, and the convex part is embedded in the concave part in a sliding manner.
8. An air-ground missile unloading vehicle according to claim 6, wherein the lower side of the guide rail plate is connected with the upper side of the support platform through a rotating table.
9. An air-ground missile unloading vehicle according to claim 5, wherein the other end of the limit plate is rotatably provided with a roller, and the roller can be in rolling fit with the outer surface of the missile.
10. The type of air-to-ground missile unloading vehicle of claim 1, wherein the top of the bracket is provided with a limiting block, the limiting block is matched with the missile guide frame of the missile, and when the limiting block abuts against one side of the missile guide frame, the sliding block of the missile on the limiting structure corresponds to the installation groove on the missile guide frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121576761.3U CN215622786U (en) | 2021-07-12 | 2021-07-12 | Unloading vehicle for certain type air-ground missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121576761.3U CN215622786U (en) | 2021-07-12 | 2021-07-12 | Unloading vehicle for certain type air-ground missile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215622786U true CN215622786U (en) | 2022-01-25 |
Family
ID=79889549
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121576761.3U Active CN215622786U (en) | 2021-07-12 | 2021-07-12 | Unloading vehicle for certain type air-ground missile |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215622786U (en) |
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2021
- 2021-07-12 CN CN202121576761.3U patent/CN215622786U/en active Active
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