CN207106298U - A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle - Google Patents
A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle Download PDFInfo
- Publication number
- CN207106298U CN207106298U CN201720892330.5U CN201720892330U CN207106298U CN 207106298 U CN207106298 U CN 207106298U CN 201720892330 U CN201720892330 U CN 201720892330U CN 207106298 U CN207106298 U CN 207106298U
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- Prior art keywords
- guided missile
- car body
- loading
- lifting
- motor
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Abstract
The utility model discloses a kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, including car body, vehicle control device, to level controller, walking mechanism, battery and automatic loading and unloading mechanism；Automatic loading and unloading mechanism includes lowering or hoisting gear and alignment device；Walking mechanism, battery and lowering or hoisting gear are connected with vehicle control device, and alignment device is connected with to level controller；Lowering or hoisting gear includes the lifting support being fixed on car body, and lifting support is provided with lifting base, and lifting base is provided with alignment device.The advantages of the utility model has small noise, compact-sized, energy automatic aligning, installation accuracy high and adapts to narrow space.
Description
Technical field
A kind of loading-unloading vehicle is the utility model is related to, it is particularly a kind of to carry additionally loading-unloading vehicle for military aircraft guided missile.
Background technology
Guided missile is related to aviation military field, is a kind of to involve the wide weapon of scope.Guided missile needs to lead when carrying additionally handling
Bullet transports the aircraft position specified, and accurately carrys additionally on airborne missile hanger.
And the guided missile that my each army of army and the world uses at present carrys additionally technology all using the larger device of volume, and it is artificial
Operation, the extension bullet mode of multi agent cooperation, the problem of need are manually operated, installation accuracy is poor, can not also adapt to narrow space be present.And
And handling facilities, using diesel source, noise is big, danger coefficient is high.
Therefore, current guided missile installation equipment has that volume is larger, need are manually operated, installation accuracy is low, noise is big and nothing
Method adapts to the defects of narrow space.
Utility model content
The purpose of this utility model is, there is provided a kind of multipurpose aircraft guided missile automatic aligning carrys additionally loading-unloading vehicle.This practicality
New the advantages of having small noise, compact-sized, energy automatic aligning, installation accuracy high and adapting to narrow space.
The technical solution of the utility model：A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, including car body, on car body
Walking mechanism is provided with provided with vehicle control device and to level controller, the bottom of car body, the inside of car body is provided with battery, car body
Front portion is provided with automatic loading and unloading mechanism；Described automatic loading and unloading mechanism includes lowering or hoisting gear and alignment device；Described walking mechanism,
Battery and lowering or hoisting gear are connected with vehicle control device, and described alignment device is connected with to level controller；The lowering or hoisting gear
Including the lifting support being fixed on car body, lifting support is provided with lifting base, and lifting base is provided with alignment device；It is described
Alignment device includes being arranged on lifting base moving forward and backward guide rail, and it is flat provided with regulation is moved forward and backward to move forward and backward guide rail
Platform, move forward and backward regulation platform and be provided with side-to-side movement guide rail, side-to-side movement guide rail is provided with left and right displacement regulation platform, left and right
Displacement regulation platform is provided with guided missile base；The guided missile base is provided with adjusting screw, and adjusting screw is provided with fixed hold tightly
Block and mobile holding block, the end of described adjusting screw is provided with handle.
In a kind of foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, described walking mechanism includes being arranged on car body
The front wheels and rear wheels of bottom, front-wheel are provided with front-wheel steer motor and front-wheel drive motor, and trailing wheel is provided with rear-axle steering motor
With rear wheel drive motor, the front-wheel steer motor, front-wheel drive motor, rear-axle steering motor and rear wheel drive motor are and car
Controller is connected.
In a kind of foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, the lifting base bottom is provided with lifting electricity
Machine, lifting motor are connected with vehicle control device；The regulation mesa base that moves forward and backward is provided with the first servomotor, the left and right
Displacement regulation mesa base is provided with the second servomotor, and the first servomotor and the second servomotor are connected to level controller
On.
In a kind of foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, described battery is connected with wagon control
Device, to level controller, front-wheel steer motor, front-wheel drive motor, rear-axle steering motor, rear wheel drive motor, the first servo electricity
Machine and the second servomotor.
In a kind of foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, the alignment device also includes the first contraposition and passed
Sensor and second pair of level sensor, first pair of level sensor are located on guided missile base, and second pair of level sensor is arranged on aircraft bullet
On storehouse, first pair of level sensor and second pair of level sensor are connected with to level controller.
In a kind of foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, the lifting base both sides are provided with installing plate.
Compared with prior art, the utility model adjusts the movement in guided missile vertical direction by lowering or hoisting gear, passes through
Motion of the regulation platform on guide rail is moved forward and backward is moved forward and backward to control the displacement on guided missile fore-and-aft direction, passes through left and right displacement
Motion of the platform on side-to-side movement guide rail is adjusted to control the displacement on guided missile left and right directions, the servo electricity that position adjustment uses
Function accurately controls positional precision, greatly improves the installation accuracy of guided missile；Also, using first pair of level sensor and the second contraposition
Sensor can automatic detection missile position and aircraft magazine position, can and by being adjusted to level controller to missile position
Guided missile is automatically mounted on aircraft hanger or removes guided missile from aircraft hanger and is transported to relevant position, using machinery
The function of hand substitutes artificial contraposition and installation, integrates automatic transportation and dismounts, and realizes multipurpose, high efficiency and high-precision
The effect of degree；In addition, used by the utility model four-wheel steering walking mechanism, in the tunnel of very little or inch of land
Also can flexibly it be moved on very little golden aircraft carrier, mobility is good；Further, original diesel source is changed to battery, both
Reduce noise pollution, also reduce danger；The utility model has small noise, compact-sized, energy automatic aligning, installation essence
The advantages of degree is high and adapts to narrow space.
Brief description of the drawings
Fig. 1 is front view of the present utility model；
Fig. 2 is top view of the present utility model；
Fig. 3 is left view of the present utility model；
Fig. 4 is the schematic diagram of walking mechanism of the present utility model；
Fig. 5 is the schematic diagram at battery of the present utility model.
Mark in accompanying drawing for：1- car bodies, 2- vehicle control devices, 3- is to level controller, 4- walking mechanisms, 5- batteries,
6- automatic loading and unloadings mechanism, 7- lowering or hoisting gears, 8- alignment devices, 9- lifting supports, 10- lifting bases, 11- move forward and backward guide rail,
12- moves forward and backward regulation platform, 13- side-to-side movement guide rails, 14- left and right displacements regulation platform, 15- guided missile bases, 16- regulations
Leading screw, 17-, which is fixed, holds block tightly, and block, 19- handles, 20- front-wheels, 21- trailing wheels, 22- front-wheel steer motors, 23- are held in 18- movements tightly
Front-wheel drive motor, 24- rear-axle steering motors, 25- rear wheel drive motors, 27- lifting motors, the servomotors of 28- first, 29-
Second servomotor, 30- first is to level sensor, and 31- second is to level sensor, 32- installing plates.
Embodiment
The utility model is further described with reference to the accompanying drawings and examples, but is not intended as to the utility model
The foundation of limitation.
Embodiment：A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, form as shown in Figures 1 to 5, including car body
1, car body 1 is provided with vehicle control device 2 and is provided with walking mechanism 4 to level controller 3, the bottom of car body 1, and the inside of car body 1 is set
There is battery 5, the front portion of car body 1 is provided with automatic loading and unloading mechanism 6；Described automatic loading and unloading mechanism 6 includes lowering or hoisting gear 7 and right
Position device 8；Described walking mechanism 4, battery 5 and lowering or hoisting gear 7 is connected with vehicle control device 2, described alignment device 8 with
Level controller 3 is connected；The lowering or hoisting gear 7 includes the lifting support 9 being fixed on car body 1, and lifting support 9, which is provided with, to be risen
Pedestal 10 drops, and lifting base 10 is provided with alignment device 8；The alignment device 8 is front and rear on lifting base 10 including being arranged on
Motion guide rail 11, guide rail 11 is moved forward and backward provided with regulation platform 12 is moved forward and backward, regulation platform 12 is moved forward and backward and is provided with a left side
Right motion guide rail 13, side-to-side movement guide rail 13 are provided with left and right displacement regulation platform 14, and left and right displacement regulation platform 14 is provided with
Guided missile base 15；The guided missile base 15 is provided with adjusting screw 16, and adjusting screw 16 is provided with fixed holding block 17 and movement
Hold block 18 tightly, the end of described adjusting screw 16 is provided with handle 19.
Described walking mechanism 4 includes being arranged on the front-wheel 20 and trailing wheel 21 of the bottom of car body 1, and front-wheel 20 is provided with preceding rotate
To motor 22 and front-wheel drive motor 23, trailing wheel 21 is provided with rear-axle steering motor 24 and rear wheel drive motor 25, the front-wheel
Steering motor 22, front-wheel drive motor 23, rear-axle steering motor 24 and rear wheel drive motor 25 are connected with vehicle control device 2.
The bottom of lifting base 10 is provided with lifting motor 27, and lifting motor 27 is connected with vehicle control device 2；It is described front and rear
Displacement regulation platform 12 bottom is provided with the first servomotor 28, and left and right displacement regulation platform 14 bottom is provided with the second servo electricity
Machine 29, the first servomotor 28 and the second servomotor 29 are connected to on level controller 3.
Described battery 5 is connected with vehicle control device 2, to level controller 3, front-wheel steer motor 22, front-wheel drive electricity
Machine 23, rear-axle steering motor 24, rear wheel drive motor 25, the first servomotor 28 and the second servomotor 29.
The alignment device 8 also includes first pair of level sensor 30 and second pair of level sensor 31, first pair of level sensor
30 are located on guided missile base 15, and second pair of level sensor 31 is arranged on aircraft magazine, first pair of level sensor 30 and second pair
Level sensor 31 is connected with to level controller 3.
The both sides of lifting base 10 are provided with installing plate 32.
The course of work：
Before transport, guided missile is arranged on guided missile base 15, adjusting screw 16 is adjusted by handle 19, further regulation
Mobile block 18 of holding tightly locks guided missile, avoids it from being moved.
During transport, starting the vehicle control device 2 of walking mechanism 4, front-wheel drive motor 23 controls front-wheel 20 to advance or retreat,
Front-wheel steer motor 22 controls the divertical motion of front-wheel 20；Rear-axle steering motor 24 controls trailing wheel 21 to advance or retreat, and trailing wheel drives
Dynamic motor 25 controls the divertical motion of trailing wheel 21.Walking mechanism 4 employs four-wheel steering design, makes missile dolly in very little
Also can flexibly it be moved in tunnel or on the aircraft carrier of an inch of land is an inch of gold, mobility is good.
During handling, missile transport is stopped to rough position, enables automatic loading and unloading mechanism 6, pass through first pair of level sensor
The physical location of 30 detection guided missile bases 15 is simultaneously transmitted information to level controller 3, is detected by second pair of level sensor 31
The physical location of aircraft magazine is simultaneously transmitted information to level controller 3, then by level controller 3 to both actual bits
Put after being analyzed, draw needed for adjustment relative displacement (x, y, z), wherein x to move left and right distance, y for it is movable away from
From z is vertical travel distance.Specific adjustment is as follows:1st, lowering or hoisting gear 7 is driven by lifting motor 27, moves lifting support 9
Dynamic distance z；2nd, front and rear adjusting screw is driven by the first servomotor 28 and moves forward and backward regulation platform 12 in front and rear fortune to adjust
Position on dynamic guide rail 11, make to move forward and backward regulation platform 12 displacement y；3rd, left and right is driven by the second servomotor 29
Adjusting screw adjusts position of the platform 14 on side-to-side movement guide rail 13 to adjust left and right displacement, left and right displacement is adjusted platform
14 displacement x.Finally, guided missile can be automatically mounted into by aircraft magazine by guided missile handgrip, or by guided missile from aircraft bullet
Storehouse, which is removed, to be arranged on guided missile base 15.The utility model substitutes artificial contraposition and installation in the form of manipulator, and collection is certainly
Dynamicization transport is dismounted in one, and controls positional precision by servomotor, realizes multipurpose, high efficiency and high-precision
Effect.Used lowering or hoisting gear 7 has good rigidity, the advantage do not rocked, even also can be from the shadow of electric wave on aircraft carrier
Ring.
Original diesel source is changed to battery by battery 5, is both reduced noise pollution, is also reduced danger.
Claims (6)
- A kind of 1. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, it is characterised in that：Including car body (1), car body (1) is provided with car Controller (2) and walking mechanism (4) is provided with to level controller (3), the bottom of car body (1), the inside of car body (1) is provided with electric power storage Pond (5), the front portion of car body (1) are provided with automatic loading and unloading mechanism (6)；Described automatic loading and unloading mechanism (6) include lowering or hoisting gear (7) and Alignment device (8)；Described walking mechanism (4), battery (5) and lowering or hoisting gear (7) is connected with vehicle control device (2), described Alignment device (8) be connected with to level controller (3)；The lowering or hoisting gear (7) includes the lifting support being fixed on car body (1) (9), lifting support (9) is provided with lifting base (10), and lifting base (10) is provided with alignment device (8)；The alignment device (8) include being arranged on lifting base (10) and moving forward and backward guide rail (11), move forward and backward guide rail (11) and be provided with and move forward and backward Platform (12) is adjusted, regulation platform (12) is moved forward and backward and is provided with side-to-side movement guide rail (13), side-to-side movement guide rail is set on (13) There is left and right displacement to adjust platform (14), left and right displacement regulation platform (14) is provided with guided missile base (15)；The guided missile base (15) adjusting screw (16) is provided with, adjusting screw (16) is provided with fixed holding block (17) and mobile holding block (18), described The end of adjusting screw (16) be provided with handle (19).
- A kind of 2. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 1, it is characterised in that：Described row Walking mechanism (4) includes being arranged on the front-wheel (20) and trailing wheel (21) of car body (1) bottom, and front-wheel (20) is provided with front-wheel steer motor (22) and front-wheel drive motor (23), trailing wheel (21) is provided with rear-axle steering motor (24) and rear wheel drive motor (25), described Front-wheel steer motor (22), front-wheel drive motor (23), rear-axle steering motor (24) and rear wheel drive motor (25) are and vehicle Controller (2) is connected.
- A kind of 3. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 2, it is characterised in that：The lifting Pedestal (10) bottom is provided with lifting motor (27), and lifting motor (27) is connected with vehicle control device (2)；It is described to move forward and backward regulation Platform (12) bottom is provided with the first servomotor (28), and described left and right displacement regulation platform (14) bottom is provided with the second servomotor (29), the first servomotor (28) and the second servomotor (29) are connected to on level controller (3).
- A kind of 4. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 3, it is characterised in that：The electric power storage Pond (5) is connected with vehicle control device (2), to level controller (3), front-wheel steer motor (22), front-wheel drive motor (23), trailing wheel Steering motor (24), rear wheel drive motor (25), the first servomotor (28) and the second servomotor (29).
- A kind of 5. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 4, it is characterised in that：The contraposition Device (8) also includes first pair of level sensor (30) and second pair of level sensor (31), and first pair of level sensor (30) is located at and led On projectile base (15), second pair of level sensor (31) is arranged on aircraft magazine, first pair of level sensor (30) and the second contraposition Sensor (31) is connected with to level controller (3).
- 6. a kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to any one of claim 1-5, its feature exist In：Lifting base (10) both sides are provided with installing plate (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720892330.5U CN207106298U (en) | 2017-07-21 | 2017-07-21 | A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720892330.5U CN207106298U (en) | 2017-07-21 | 2017-07-21 | A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207106298U true CN207106298U (en) | 2018-03-16 |
Family
ID=61585247
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720892330.5U Expired - Fee Related CN207106298U (en) | 2017-07-21 | 2017-07-21 | A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207106298U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107187372A (en) * | 2017-07-21 | 2017-09-22 | 杭州联荣电子科技有限公司 | Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
-
2017
- 2017-07-21 CN CN201720892330.5U patent/CN207106298U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107187372A (en) * | 2017-07-21 | 2017-09-22 | 杭州联荣电子科技有限公司 | Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180316 Termination date: 20200721 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |