CN107187372A - Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle - Google Patents
Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle Download PDFInfo
- Publication number
- CN107187372A CN107187372A CN201710601853.4A CN201710601853A CN107187372A CN 107187372 A CN107187372 A CN 107187372A CN 201710601853 A CN201710601853 A CN 201710601853A CN 107187372 A CN107187372 A CN 107187372A
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- Prior art keywords
- guided missile
- car body
- loading
- motor
- wheel
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 230000007246 mechanism Effects 0.000 claims abstract description 25
- 238000006073 displacement reaction Methods 0.000 claims description 20
- 230000033001 locomotion Effects 0.000 claims description 16
- 238000009434 installation Methods 0.000 abstract description 6
- 230000032258 transport Effects 0.000 description 4
- 238000001514 detection method Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- 229910052737 gold Inorganic materials 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P1/00—Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading
- B60P1/44—Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading having a loading platform thereon raising the load to the level of the load-transporting element
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- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Handcart (AREA)
Abstract
The invention 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 present invention has the advantages that small noise, compact conformation, energy automatic aligning, installation accuracy height and adapts to narrow space.
Description
Technical field
It is particularly a kind of to carry additionally loading-unloading vehicle for military aircraft guided missile the present invention relates to a kind of loading-unloading vehicle.
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, existing needs manually operated, installation accuracy poor, the problem of can not also adapting to narrow space.And
And, handling facilities use diesel source, and noise is big, danger coefficient is high.
Therefore, current guided missile installs equipment and has that volume is larger, needs that manually operated, installation accuracy is low, noise is big and nothing
Method adapts to the defect of narrow space.
The content of the invention
It is an object of the present invention to provide a kind of multipurpose aircraft guided missile automatic aligning carrys additionally loading-unloading vehicle.The present invention has
Noise is small, compact conformation, can automatic aligning, installation accuracy is high and adapts to the advantage of narrow space.
Technical scheme：A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, including car body, car body are provided with
Vehicle control device and to level controller, the bottom of car body is provided with walking mechanism, and the inside of car body is provided with battery, the front portion of car body
Provided with automatic loading and unloading mechanism；Described automatic loading and unloading mechanism includes lowering or hoisting gear and alignment device；Described walking mechanism, electric power storage
Pond 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 includes
The lifting support on car body is fixed on, lifting support is provided with lifting base, and lifting base is provided with alignment device；The contraposition
Device includes being arranged on lifting base moving forward and backward guide rail, moves forward and backward guide rail provided with regulation platform is moved forward and backward, preceding
Displacement regulation platform is provided with side-to-side movement guide rail afterwards, and side-to-side movement guide rail adjusts platform, left and right displacement provided with left and right displacement
Adjust platform and be provided with guided missile base；The guided missile base is provided with adjusting screw, adjusting screw provided with it is fixed hold tightly block and
Mobile to hold block tightly, the end of described regulation screw mandrel is provided with handle.
In foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, described walking mechanism includes being arranged on vehicle bottom
Front wheels and rear wheels, front-wheel be provided with front-wheel steer motor and front-wheel drive motor, trailing wheel provided with rear-axle steering motor and after
Wheel drive motor, the front-wheel steer motor, front-wheel drive motor, rear-axle steering motor and rear wheel drive motor with vehicle control
Device processed is connected.
In foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, the lifting base bottom is provided with lifting motor, rises
Drop motor is 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
Adjust mesa base and be provided with the second servomotor, the first servomotor and the second servomotor are connected to on level controller.
In foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, described battery is connected with vehicle control device, right
Level controller, front-wheel steer motor, front-wheel drive motor, rear-axle steering motor, rear wheel drive motor, the first servomotor and
Two servomotors.
In foregoing multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, the alignment device also includes first pair of level sensor
With second pair of level sensor, first pair of level sensor is located on guided missile base, and second pair of level sensor is arranged on aircraft magazine,
First pair of level sensor and second pair of level sensor are connected with to level controller.
In 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 present invention adjusts the movement in guided missile vertical direction by lowering or hoisting gear, by front and rear
Displacement adjusts motion of the platform on guide rail is moved forward and backward to control the displacement on guided missile fore-and-aft direction, is adjusted by left and right displacement
Motion of the platform on side-to-side movement guide rail is saved to control the displacement on guided missile left and right directions, the servomotor that position adjustment is used
Positional precision can be accurately controlled, the installation accuracy of guided missile is greatly improved；Also, passed using first pair of level sensor and the second contraposition
Sensor can automatic detection missile position and aircraft magazine position, can be by and by being adjusted to level controller to missile position
Guided missile, which is automatically mounted on aircraft hanger or removes guided missile from aircraft hanger, is transported to relevant position, using manipulator
Function substitute artificial contraposition and install, integrate automatic transportation and dismount, realize multipurpose, high efficiency and high accuracy
Effect；In addition, the walking mechanism of four-wheel steering of the present invention, in the tunnel of very little or an inch of land is an inch of gold
Also can flexibly it be moved on aircraft carrier, mobility is good；Further, original diesel source is changed to battery, both reduced
Noise pollution, also reduces danger；The present invention has small noise, compact conformation, energy automatic aligning, installation accuracy height and can fitted
Answer the advantage of narrow space.
Brief description of the drawings
Fig. 1 is the front view of the present invention；
Fig. 2 is the top view of the present invention；
Fig. 3 is the left view of the present invention；
Fig. 4 is the schematic diagram of the walking mechanism of the present invention；
Fig. 5 is the schematic diagram at the battery of the present invention.
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- moves 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- regulation silks
Thick stick, 17-, which is fixed, holds block tightly, and 18- movements are held tightly before block, 19- handles, 20- front-wheels, 21- trailing wheels, 22- front-wheel steer motors, 23-
Wheel drive motor, 24- rear-axle steering motors, 25- rear wheel drive motors, 27- lifting motors, the servomotors of 28- first, 29-
Two servomotors, 30- first is to level sensor, and 31- second is to level sensor, 32- installing plates.
Embodiment
The present invention is further illustrated with reference to the accompanying drawings and examples, but be not intended as to the present invention limit according to
According to.
Embodiment：Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle, is constituted as shown in Figures 1 to 5, including car body 1, car body
1 provided with vehicle control device 2 and to level controller 3, and the bottom of car body 1 is provided with walking mechanism 4, and the inside of car body 1 is provided with electric power storage
Pond 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 alignment device 8；
Described walking mechanism 4, battery 5 and lowering or hoisting gear 7 is connected with vehicle control device 2, and described alignment device 8 is controlled with contraposition
Device 3 is connected；The lowering or hoisting gear 7 includes the lifting support 9 being fixed on car body 1, and lifting support 9 is provided with lifting base 10,
Lifting base 10 is provided with alignment device 8；The alignment device 8 includes being arranged on lifting base 10 moving forward and backward guide rail
11, guide rail 11 is moved forward and backward provided with regulation platform 12 is moved forward and backward, and is moved forward and backward regulation platform 12 and is led provided with side-to-side movement
Rail 13, side-to-side movement guide rail 13 adjusts platform 14 provided with left and right displacement, 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 holds block 18 tightly provided with fixed holding block 17 with mobile,
The end of described regulation screw mandrel 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 rotation
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；Before and after described
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, it is to avoid it is moved.
During transport, start the vehicle control device 2 of walking mechanism 4, the control front-wheel 20 of front-wheel drive motor 23 advances or retreated,
Front-wheel steer motor 22 controls the divertical motion of front-wheel 20；The control trailing wheel 21 of rear-axle steering motor 24 advances or retreated, rear wheel driving
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, automatic loading and unloading mechanism 6 is enabled, passes 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 3 pairs of both actual bits of level controller
Put after being analyzed, the relative displacement (x, y, z) of adjustment needed for drawing, 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, lifting support 9 is moved
Move apart from 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, makes to move forward and backward regulation platform 12 displacement y；3rd, adjusted by the second servomotor 29 driving left and right
Section leading 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 and moves
Move apart from x.Finally, guided missile can be automatically mounted into by aircraft magazine by guided missile handgrip, or guided missile is taken from aircraft magazine
Under be arranged on guided missile base 15.The present invention is substituted artificial contraposition and installed in the form of manipulator, collects automatic transportation
Dismount in one, and positional precision is controlled by servomotor, realize multipurpose, high efficiency and high-precision effect.Institute
The lowering or hoisting gear 7 of use have good rigidity, the advantage do not rocked, even on aircraft carrier also can from electric wave influence.
Original diesel source is changed to battery by battery 5, is both reduced noise pollution, is also reduced danger.
Claims (6)
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 vehicle control
Device (2) processed and to level controller (3), the bottom of car body (1) is provided with walking mechanism (4), and the inside of car body (1) is provided with 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) is 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) provided with moving 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) holds block (18) tightly provided with fixed holding block (17) and movement, described
Regulation screw mandrel (16) end be provided with handle (19).
2. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 1, it is characterised in that：Described vehicle with walking machine
Structure (4) includes the front-wheel (20) and trailing wheel (21) for being arranged on car body (1) bottom, and front-wheel (20) is provided with front-wheel steer motor (22)
With 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 and wagon control
Device (2) is connected.
3. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 2, it is characterised in that：The lifting base
(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).
4. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 3, it is characterised in that：The battery
(5) it is connected with vehicle control device (2), to level controller (3), front-wheel steer motor (22), front-wheel drive motor (23), rear rotation
To motor (24), rear wheel drive motor (25), the first servomotor (28) and the second servomotor (29).
5. multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to claim 4, it is characterised in that：The alignment device
(8) first pair of level sensor (30) and second pair of level sensor (31) are also included, first pair of level sensor (30) is located at guided missile bottom
On seat (15), second pair of level sensor (31) is arranged on aircraft magazine, first pair of level sensor (30) and the second contraposition sensing
Device (31) is connected with to level controller (3).
6. the multipurpose aircraft guided missile automatic aligning loading-unloading vehicle according to any one of claim 1-5, it is characterised in that：Institute
Lifting base (10) both sides are stated provided with installing plate (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710601853.4A CN107187372A (en) | 2017-07-21 | 2017-07-21 | Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710601853.4A CN107187372A (en) | 2017-07-21 | 2017-07-21 | Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107187372A true CN107187372A (en) | 2017-09-22 |
Family
ID=59884966
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710601853.4A Pending CN107187372A (en) | 2017-07-21 | 2017-07-21 | Multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107187372A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110076809A (en) * | 2019-04-26 | 2019-08-02 | 杭州联荣电子科技有限公司 | Puma manipulator and multifunction missile bomb truck |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102519360A (en) * | 2011-12-23 | 2012-06-27 | 中国科学院长春光学精密机械与物理研究所 | Alignment measurer of full automatic missile hooking vehicle |
| CN106134331B (en) * | 2008-12-11 | 2014-01-22 | 上海卫星装备研究所 | The assembling car of large heavy unit dress star |
| CN204527665U (en) * | 2015-03-19 | 2015-08-05 | 柴丛众 | Guided missile is hung and is unloaded |
| CN105253317A (en) * | 2015-10-15 | 2016-01-20 | 青岛地恩地机电科技股份有限公司 | Missile loading vehicle |
| CN207106298U (en) * | 2017-07-21 | 2018-03-16 | 杭州联荣电子科技有限公司 | A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
-
2017
- 2017-07-21 CN CN201710601853.4A patent/CN107187372A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106134331B (en) * | 2008-12-11 | 2014-01-22 | 上海卫星装备研究所 | The assembling car of large heavy unit dress star |
| CN102519360A (en) * | 2011-12-23 | 2012-06-27 | 中国科学院长春光学精密机械与物理研究所 | Alignment measurer of full automatic missile hooking vehicle |
| CN204527665U (en) * | 2015-03-19 | 2015-08-05 | 柴丛众 | Guided missile is hung and is unloaded |
| CN105253317A (en) * | 2015-10-15 | 2016-01-20 | 青岛地恩地机电科技股份有限公司 | Missile loading vehicle |
| CN207106298U (en) * | 2017-07-21 | 2018-03-16 | 杭州联荣电子科技有限公司 | A kind of multipurpose aircraft guided missile automatic aligning loading-unloading vehicle |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110076809A (en) * | 2019-04-26 | 2019-08-02 | 杭州联荣电子科技有限公司 | Puma manipulator and multifunction missile bomb truck |
| CN110076809B (en) * | 2019-04-26 | 2021-03-30 | 杭州联荣电子科技有限公司 | Intelligent manipulator and multifunctional missile loading vehicle |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170922 |
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| WD01 | Invention patent application deemed withdrawn after publication |