CN105253317A - Missile loading vehicle - Google Patents
Missile loading vehicle Download PDFInfo
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- CN105253317A CN105253317A CN201510665959.1A CN201510665959A CN105253317A CN 105253317 A CN105253317 A CN 105253317A CN 201510665959 A CN201510665959 A CN 201510665959A CN 105253317 A CN105253317 A CN 105253317A
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Abstract
The invention relates to the technical field of the military equipment, especially to a missile loading vehicle comprising a vehicle body, a positioning mechanism, a walking mechanism, and a lifting mechanism. The positioning mechanism includes positioning guiding devices for transmitting signals and positioning receivers for receiving signals; and five signal transmitting sources corresponding to front, rear, left, right and center signal transmitting directions respectively are arranged on each positioning guiding device. Because of different signals transmitted by the five signal transmitting sources, a relative position relation between a missile and a missile installation position on a wing or a belly of the missile loading vehicle can be determined according to the signals received by the positioning receivers; and thus the vehicle body and the adjusting platform are controlled by a controller to move to complete the positioning process. According to the invention, the positioning becomes accurate and reliable; no manual readjustment is needed during the whole positioning process, so that the workload and the labor intensity of the operator can be reduced, the missile hanging time is reduced, and the missile hanging efficiency is improved.
Description
Technical field
The present invention relates to military equipment technical field, particularly relate to a kind of guided missile bomb truck.
Background technology
Bullet speed hung by the guided missile of fighter plane, and especially secondary hangs bullet speed block directly affects fighting capacity slowly; Current aircraft is hung bullet and is divided into by carry mode and manually hangs bullet and two kinds, bullet hung by machinery, and its medium-and-large-sized guided missile uses mechanical bomb truck, the artificial or scissors hydraulic efficiency equipment of medium and small use.Manual bomb truck, needs to rely on manpower to pull a cart, relies on hand-hydraulic lifting table lifting guided missile, and regulates the position of guided missile and angle, and the labour intensity of operating personal is high and cycle of operations is long, affects the extension bullet speed of guided missile.
At present, existing bomb truck comprises car body, described guided missile is hung to unload and is also comprised several lifting-positioning devices, lifting-positioning device comprises the base plate be connected with vehicle body-side end, adapter plate, the location mechanism be connected with adapter plate, wherein Ce Wei mechanism comprises Lateral register sensor and longitudinal register sensor, Lateral register sensor and longitudinal register sensor are proximity switch, proximity switch is that one directly contacts and manipulable position switch without the need to carrying out machinery with movable parts, when the guided missile on bomb truck is close to wing, during the guided missile installation sites such as ventral, proximity switch sends signal to control desk, control desk controls zigzag tread patterns oil cylinder and laterally drives oil cylinder stopping action realizing location, but the error of being carried out guided missile location by proximity switch is larger, microstructure cannot meet the adjustment of big error, need manually to readjust position, add the work capacity of operating personnel, reduce the efficiency of loading guided missile, this bomb truck needs when guided missile got by dress guided missile to be transported powder magazine again by crane lifting carry guided missile truck simultaneously, can not realize getting bullet, hanging bullet institutional operation, add the time of loading guided missile, reduce and hang bullet efficiency.
Summary of the invention
(1) technical matters that will solve
The technical problem to be solved in the present invention is: traditional bomb truck for loading guided missile, and it is positioned by artificial and proximity switch, and position error is large, affects the efficiency that bomb truck loads guided missile, too increases the work capacity of operating personal simultaneously; And existing bomb truck can not realize getting bullet, hanging bullet integration.
(2) technical scheme
In order to solve the problems of the technologies described above, the invention provides a kind of guided missile bomb truck, comprise car body, detent mechanism, traveling gear and lifting mechanism, described traveling gear moves for driving car body, and described lifting mechanism comprises to be located at bay-lift on car body and to be positioned on the upside of bay-lift for carrying the guided missile support bracket of guided missile; Described detent mechanism comprises the location receivers be located on guided missile support bracket and the positioning guide be located on the aircraft treating carry guided missile, described positioning guide is provided with five signal emitting-sources, the signal that each signal emitting-source is launched is all not identical, five described signal emitting-sources corresponding front, rear, left and right and five, middle part signal downrange respectively; The signal that described location receivers is launched for receiving positioning guide, and the signal received is supplied to controller.
Preferably, described positioning guide is cone-shaped in side, and five described signal emitting-sources are respectively on the end face of the cone-shaped positioning guide in the side of being arranged on and four sides.
Preferably, also comprise adjustment platform, described adjustment platform is positioned at the upside of described bay-lift, and is connected by sliding connector with described bay-lift; Described guided missile support bracket is located on described adjustment platform, and one end of described guided missile support bracket by rotating shaft and described adjustment platform hinged, described guided missile support bracket be provided with holder bullet depression.
Preferably, described sliding connector comprises the slide rail being located at bay-lift upper end and adjusts platform lower end and the chute coordinated with described slide rail with being located at, and described slide rail is perpendicular to the length direction of described guided missile support bracket.
Preferably, the driven unit for driving adjustment platform to slide also is comprised, the ball screw assembly, that described driven unit comprises the first drive motor and is connected with described first drive motor.
Preferably, described adjustment platform is provided with two groups of guided missile support brackets, often organizes described guided missile support bracket and is equipped with two location receivers.
Preferably, described traveling gear comprises the roller of being located at described car body bottom and the second drive motor for driving described roller to rotate.
Preferably, described roller is provided with three, and wherein two rollers are cardan wheel and are located at relative both sides, car body rear end; Another roller is the drive wheel be connected with described second drive motor, and described drive wheel is located at the front end of car body.
Preferably, also comprise brake-applying handle, described brake-applying handle is for separating of the gears meshing of drive wheel.
Preferably, described bay-lift is hydraulic fork type bay-lift, and described hydraulic pressure scissors lift table comprises scissor assembly, for the hydraulic actuating cylinder that drives scissor assembly to be elevated with for driving the HM Hydraulic Motor of described hydraulic actuating cylinder
(3) beneficial effect
Technique scheme tool of the present invention has the following advantages: the invention provides a kind of guided missile bomb truck, comprises lifting mechanism described in car body, detent mechanism, traveling gear and lifting mechanism and comprises the bay-lift be located on car body and be positioned on the upside of bay-lift for carrying the guided missile support bracket of guided missile, wherein detent mechanism comprises the location receivers be located on guided missile support bracket and the positioning guide be located on the aircraft treating carry guided missile, and each positioning guide is provided with respectively before correspondence, after, left, five signal emitting-sources of the right side and five the signal downranges in middle part, and the signal that each signal emitting-source is launched is all not identical, like this when positioning the installation site of carry guided missile, the signal of positioning guide transmitting is received by location receivers, the information received is supplied to controller by location receivers, the signal launched due to five signal sources is different, controller judges the relative position relation on guided missile on bomb truck and wing or ventral between guided missile installation site according to the signal received, and it is movable or control adjustment platform and horizontally slip relative to lifting table to control car body, until location receivers is merely able to the signal receiving middle part, guided missile (shell) now on bomb truck faces the guided missile installation site on wing or ventral, complete position fixing process, guided missile bomb truck location provided by the invention more accurately, reliably, long distance positioning can be realized guide, and do not need in whole position fixing process manually to readjust, reduce work capacity and the labour intensity of operating personal, realize the maximization application of mechanical equipment, final minimizing extension bullet time, raising are hung and are played efficiency.
Accompanying drawing explanation
The advantage of the above-mentioned and/or additional aspect of the present invention will become obvious and easy understand from accompanying drawing below combining to the description of embodiment, wherein:
Fig. 1 is the block diagram of the guided missile bomb truck described in the embodiment of the present invention;
Fig. 2 is the back view of the guided missile bomb truck described in the embodiment of the present invention;
Fig. 3 is the birds-eye view of the guided missile bomb truck described in the embodiment of the present invention;
Fig. 4 is the left view of the guided missile bomb truck described in the embodiment of the present invention;
Fig. 5 is the A portion enlarged drawing of Fig. 4;
Fig. 6 is the block diagram of positioning guide;
Fig. 7 is the birds-eye view of positioning guide;
Fig. 8 is the block diagram of location receivers.
Corresponding relation wherein in Fig. 1 to Fig. 8 between Reference numeral and component names is:
1, car body, 11, bay-lift, 111, slide rail, 112, scissor assembly, 113, hydraulic actuating cylinder, 114, clamp handle, 12, adjustment platform, 121, guided missile support bracket, 1211, location receivers, 1212, bullet depression is held in the palm, 1213, stay bearing plate, 122, rotating shaft, 123, chute, 124, leading screw, 125, belt, 126, belt wheel, the 13, first drive motor, 14, drive wheel, 15, cardan wheel, 16, electric cabinet, 17, control handle, 2, positioning guide, 21, signal emitting-source.
Detailed description of the invention
In describing the invention, it should be noted that, term " " center ", " longitudinal direction ", " transverse direction ", " on ", D score, " front ", " afterwards ", " left side ", " right side ", " vertically ", " level ", " top ", " end ", " " interior ", orientation or the position relationship of the instruction such as " outward " are based on orientation shown in the drawings or position relationship, only the present invention for convenience of description and simplified characterization, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore limitation of the present invention can not be interpreted as.In addition, term " first ", " second " only for describing object, and can not be interpreted as instruction or hint relative importance.
In describing the invention, it should be noted that, unless otherwise clearly defined and limited, term " installation ", " being connected ", " connection " should be interpreted broadly, and such as, can be fixedly connected with, also can be removably connect, or connect integratedly; Can be mechanical connection, also can be electrical connection; Can be directly be connected, also indirectly can be connected by intermediary, can be the connection of two element internals.For the ordinary skill in the art, particular case above-mentioned term concrete meaning in the present invention can be understood.In addition, in describing the invention, except as otherwise noted, the implication of " multiple " is two or more.
For making the object of the embodiment of the present invention, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the embodiment of the present invention, technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under the prerequisite not making creative work, all belongs to the scope of protection of the invention.
As shown in Figures 1 to 4, the invention provides a kind of guided missile bomb truck, comprise car body 1, detent mechanism, traveling gear and lifting mechanism, described traveling gear moves for driving car body 1, and described lifting mechanism comprises to be located at bay-lift on car body 1 11 and to be positioned on the upside of bay-lift 11 for carrying the guided missile support bracket 121 of guided missile; Described detent mechanism comprises the location receivers 1211 be located on guided missile support bracket 121 and the positioning guide 2 be located on the aircraft treating carry guided missile, described positioning guide 2 is provided with five signal emitting-sources 21, the signal that each signal emitting-source 21 is launched is all not identical, five described signal emitting-sources 21 corresponding front, rear, left and right and five, middle part signal downrange respectively; The signal that described location receivers 1211 is launched for receiving positioning guide 2, and the signal received is supplied to controller.
Guided missile bomb truck provided by the invention, detent mechanism on it comprises the location receivers 1211 be located on guided missile support bracket 121 and the positioning guide 2 be located on the aircraft treating carry guided missile, and each positioning guide 2 is provided with respectively before correspondence, after, left, five signal emitting-sources 21 of the right side and five the signal downranges in middle part, and the signal that each signal emitting-source 21 is launched is all not identical, like this when positioning the installation site of carry guided missile, the signal of positioning guide 2 transmitting is received by location receivers 1211, the signal launched due to five signal sources is different, therefore by the relative position relation judged on guided missile on bomb truck and wing or ventral between guided missile installation site of the signal that receives, the information received is supplied to controller by location receivers 1211, by the relative position relation that controller judges on guided missile on bomb truck and wing or ventral between guided missile installation site according to the information received, and it is movable or control adjustment platform 12 and horizontally slip relative to lifting table to control car body 1, until location receivers 1211 is merely able to receive the signal launched at middle part, guided missile now on bomb truck faces the guided missile installation site on wing or ventral, controls bay-lift 11 and to have hoisted installation.
Preferably, as shown in Figure 6 and Figure 7, described positioning guide 2 is cone-shaped in side, and (that is: its shape is similar pyramid shape, and its top is scabbled make end face parallel with bottom surface), five described signal emitting-sources 21 are respectively on the end face of the cone-shaped positioning guide 2 in the side of being arranged on and four sides, by by cone-shaped for its side of being arranged to, location, a signal emitting-source 21 is all established in the end face of the side's of making cone and four sides, before the signal that such five signal emitting-sources 21 are launched is sent to respectively, after, left, the right side and direction, five, middle part, controller just can receive signal according to location receivers 1211 (as shown in Figure 7), judge that bomb truck is relative to the relative position relation between guided missile installation site, it is more accurate to locate.
Also can: in the process of hoisting, position fixing system also at work, correction position at any time.
Alternatively, also can be the location first bay-lift 11 being raised up to certain altitude and then carrying out horizontal direction, like this because location receivers 1211 Distance positioning guide 2 is apart from nearer, it be more accurate to locate.
Wherein, the infrared pulse signal that signal emitting-source 21 is launched, can certainly launch other carrier wave light signals; The position of positioning guide 2 being installed signal emitting-source 21 forms a sunk area, and the infrared pulse signal reflected to allow each signal emitting-source 21 further is only launched to a direction, avoids occurring interference between signal.
It should be noted that; the structure of positioning guide 2 is not limited only to said structure; the different signal only needing on positioning guide 2 five signal emitting-sources 21 to launch be launch forwards, backwards, left and right and middle five different directions; as the locating plate that positioning guide 2 is one piece of rectangle or circle; and be provided with baffle plate; this locating plate is divided into five parts (or four parts) by baffle plate; the object of the application can be realized equally; its aim does not depart from design philosophy of the present invention, should belong to protection scope of the present invention.
Alternatively, as shown in Figure 3 and Figure 4, described traveling gear comprises is located at the roller of described car body 1 bottom and the second drive motor for driving described roller to rotate, wherein, described roller is provided with three, and wherein two rollers are cardan wheel 15 and are located at relative both sides, car body 1 rear end; Another roller is the drive wheel 14 be connected with described second drive motor, and described drive wheel 14 is located at the front end of car body 1, and the second drive motor drives drive wheel 14 by gears meshing, and then drives bomb truck to move; Positive and negative transferring by controlling the second drive motor controls the movable of bomb truck; Preferably, control handle 17 can also be comprised, described control handle 17 is for the rotating speed of the rotating and the second drive motor that control the second drive motor, and such operating personal realizes the stepless time adjustment of the second drive motor by control handle 17, operator thus obtain suitable running velocity; The energy of drive motor from battery, by transmission route, the transmission of motor driven gear realizable force; Movable motor realizes advance, fallback function by reversing arrangement;
Alternatively, described bomb truck being also provided with and switching handle (not shown), when being in an emergency as motor damage or unexpected dead electricity, switching handle can be pulled, be separated the engaging gear of drive wheel 14, realize manual control; Can realize manually promoting freely switching between motorized motions by brake-applying handle, safety factor is higher, and also can utilize when not having electric simultaneously and manually promote, practicality is better.
Shown in Fig. 1, Fig. 2 and Fig. 4, the upside of described bay-lift 11 is also provided with adjustment platform 12, and described bay-lift 11 is connected with adjustment platform 12 by sliding connector, preferably, described sliding connector comprises the slide rail 111 being located at bay-lift 11 upper end and adjusts platform 12 lower end and the chute 123 coordinated with described slide rail 111 with being located at, described slide rail 111 is perpendicular to the length direction of described guided missile support bracket 121, the slip of adjustment platform 12 on slide rail 111 realizes the left and right fine setting of guided missile the unknown, the guided missile on guided missile support bracket 121 is made to be the positive downside with guided missile installation site accurately, described guided missile support bracket 121 is located on described adjustment platform 12, and one end of described guided missile support bracket 121 is hinged by rotating shaft 122 and described adjustment platform 12, described guided missile support bracket 121 is provided with holder bullet depression 1212, because guided missile is vertically place in ammunition depot, if therefore guided missile support bracket 121 horizontal positioned always, when bomb truck gets guided missile from ammunition depot dress, need guided missile to transport powder magazine, then be lifted on by crane on bomb truck, add step and the time that guided missile got by dress, reduce and shoot efficiency, described adjustment platform 12 Shanghai is provided with clamp handle 114 alternatively, when off working state, clamp handle 114 is used adjustment platform 12 and bay-lift 11 to be locked, when needs slide adjustment platform 12, unclamp clamp handle 114, adjustment platform 12 is slided on bay-lift 11, and due to one end of the support bracket of guided missile described in the application 121 hinged with adjustment platform 12 by rotating shaft 122, therefore this guided missile support bracket 121 can erect, therefore bomb truck provided by the invention directly can enter in ammunition depot and load guided missile, do not need missile transport outbound, install with crane again, the speed shot is faster, the efficiency that bullet hung by bomb truck is higher, can realize getting bullet, hanging bullet institutional operation, in addition, stay bearing plate 1213 is also provided with in the rear end of described guided missile support bracket 121, by stay bearing plate 1213 at bomb truck and but ammunition depot is in-built carries out support to guided missile and prevent guided missile landing, and guided missile support bracket 121 is also formed holder bullet depression 1212, can fix guided missile when guided missile horizontal positioned.
Preferably, as shown in figures 1 and 3, described adjustment platform 12 is provided with two guided missile support brackets 121, each guided missile support is provided with two location receivers 1211, two location receivers 1211 are located at the relative two ends, diagonal angle of guided missile support bracket 121, the corresponding guided missile installed position on the aircraft treating carry guided missile arranges two positioning guide 2 equally, can guarantee the accuracy of locating like this; Can certainly be that multiple location receivers 1211 is set, as three, four, five etc., equally also can play pinpoint object.
It should be noted that, also can be that slide rail 111 is set on adjustment platform 12 in the above-described embodiments, and the chute 123 coordinated with described slide rail 111 is set on bay-lift 11, or adopt other sliding connector, the object adjusting platform 12 and lifting table sliding block joint in the application can be realized equally.
Alternatively, as shown in Figure 2 and Figure 5, described bomb truck also comprises the driven unit for driving adjustment platform 12 to slide, described driven unit comprises the first drive motor 13 and ball-screw 124 is secondary, described second drive motor is located on bay-lift 11, and driving pulley 126 rotates, belt wheel 126 to be connected with the nut of ball-screw 124 pair by belt 1245 or chain and to drive leading screw 124 to move linearly, and leading screw 124 is fixedly connected with adjustment platform 12, and then drive adjustment platform 12 to carry out sway along slide rail 111, the guided missile installation site on bomb truck is regulated.
Certainly, also can exchange by other devices the right position flattening platform 12 and regulate, as trapezoidal nut etc., equally also can realize the object of the application.
Preferably, described bay-lift 11 is hydraulic fork type bay-lift 11, and described hydraulic pressure scissors lift table 11 comprises scissor assembly 112, for the hydraulic actuating cylinder 113 that drives scissor assembly 112 to be elevated with for driving the HM Hydraulic Motor of described hydraulic actuating cylinder 113; Hydraulic efficiency gear is adopted to drive bay-lift 11, fast lifting can be realized, and can by hydraulic efficiency pressure system by regulate flow regulating valve, realize the change of rising or falling speed, realize accurately location, in the emergency moment, by fast dismantling except electricity drives hydraulic actuating cylinder 113, being replaced by pedal hydraulic actuating cylinder 113 can continue manual operation; Bay-lift 11 also can adopt other actuating devices such as actuating devices such as cylinder to drive.
It should be noted that, the base of described car body 1 is also provided with electric cabinet 16, and described controller, HM Hydraulic Motor and the second drive motor are all located in described electric cabinet 16.
Illustrate the working process of guided missile bomb truck provided by the invention below;
First bomb truck is driven to ammunition depot, by guided missile support bracket 121 around the shaft 122 rotating vertical uprightly rise, after guided missile enters guided missile support bracket 121, guided missile is set level, now the inserting in holder bullet depression 1212 of front end of guided missile fixes, and then use as guided missile is fixed on guided missile support bracket 121 by rope firmly, or other fixed sturctures are fixed like this, as semicircular in shape, the upper cover of V-arrangement, be buckled in the top of guided missile, and use screw or bolt to be fixed by upper cover, drive wheel 14 is driven to rotate by the second drive motor, and then band motor vehicles bodies 1 moves, then travel direction and moving velocity is controlled by control handle 17, arrive below wing, the master cock of lifting mechanism is started after range estimation coarse positioning, location receivers 1211 accepts the signal that positioning guide 2 is launched, and be supplied to controller, the signal that controller analysis is remembered, judge the relative position between the guided missile on the installation site of guided missile on wing or ventral and bomb truck, (be specially by controller laggard Row sum-equal matrix of dealing with, if location receivers 1211 receives the infrared pulse signal that positioning guide 2 is launched to the left, then bomb truck is positioned at the left side of guided missile installation site, driven by the first drive motor 13 and moved right by ball-screw 124 subband dynamic adjustment platform 12, owing to passing through range estimation Primary Location, therefore position error can not differ large especially, do not need to drive whole bomb truck to move, only need to move accurately can complete location by adjustment platform 12, when location receivers 1211 is merely able to receive the infrared pulse signal launched in the middle part of positioning guide 2, guided missile on bomb truck faces guided missile installation site, now only need to control bay-lift 11 rising and can complete extension bullet), order about the adjustment that hydraulic actuating cylinder 113 makes rising or falling speed, provide control signal simultaneously, control the first drive motor 13 and the second drive motor makes rotating campaign, drive adjustment platform 12 to make movable, wherein bomb truck carries out the location of short transverse by proximity switch formula sensor.
In sum, the invention provides a kind of guided missile bomb truck, comprise lifting mechanism described in car body, detent mechanism, traveling gear and lifting mechanism and comprise the bay-lift be located on car body and be positioned on the upside of bay-lift for carrying the guided missile support bracket of guided missile, wherein detent mechanism comprises the location receivers be located on guided missile support bracket and the positioning guide be located on the aircraft treating carry guided missile, and each positioning guide is provided with respectively before correspondence, after, left, five signal emitting-sources of the right side and five the signal downranges in middle part, and the signal that each signal emitting-source is launched is all not identical, like this when positioning the installation site of carry guided missile, the signal of positioning guide transmitting is received by location receivers, the signal launched due to five signal sources is different, the information received is supplied to controller by location receivers, controller judges the relative position relation on guided missile on bomb truck and wing or ventral between guided missile installation site according to the signal received, and it is movable or control adjustment platform and horizontally slip relative to lifting table to control car body, until location receivers is merely able to the signal receiving middle part, now bomb truck faces the guided missile installation site on wing or ventral, complete position fixing process, guided missile bomb truck location provided by the invention more accurately, reliably, long distance positioning can be realized guide, and do not need in whole position fixing process manually to readjust, reduce work capacity and the labour intensity of operating personal, realize the maximization application of mechanical equipment, final minimizing extension bullet time, raising are hung and are played efficiency.
Last it is noted that above embodiment is only in order to illustrate technical scheme of the present invention, be not intended to limit; Although with reference to previous embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of various embodiments of the present invention technical scheme.
Claims (10)
1. a guided missile bomb truck, it is characterized in that: comprise car body, detent mechanism, traveling gear and lifting mechanism, described traveling gear moves for driving car body, and described lifting mechanism comprises to be located at bay-lift on car body and to be positioned on the upside of bay-lift for carrying the guided missile support bracket of guided missile; Described detent mechanism comprises the location receivers be located on guided missile support bracket and the positioning guide be located on the aircraft treating carry guided missile, described positioning guide is provided with five signal emitting-sources, the signal that each signal emitting-source is launched is all not identical, five described signal emitting-sources corresponding front, rear, left and right and five, middle part signal downrange respectively; The signal that described location receivers is launched for receiving positioning guide, and the signal received is supplied to controller.
2. guided missile bomb truck according to claim 1, is characterized in that: described positioning guide is cone-shaped in side, and five described signal emitting-sources are respectively on the end face of the cone-shaped positioning guide in the side of being arranged on and four sides.
3. guided missile bomb truck according to claim 1, it is characterized in that: also comprise adjustment platform, described adjustment platform is positioned at the upside of described bay-lift, and is connected by sliding connector with described bay-lift; Described guided missile support bracket is located on described adjustment platform, and one end of described guided missile support bracket by rotating shaft and described adjustment platform hinged, described guided missile support bracket be provided with holder bullet depression.
4. guided missile bomb truck according to claim 3, it is characterized in that: described sliding connector comprises the slide rail being located at bay-lift upper end and adjusts platform lower end and the chute coordinated with described slide rail with being located at, and described slide rail is perpendicular to the length direction of described guided missile support bracket.
5. guided missile bomb truck according to claim 3, is characterized in that: also comprise the driven unit for driving adjustment platform to slide, the ball screw assembly, that described driven unit comprises the first drive motor and is connected with described first drive motor.
6. guided missile bomb truck according to claim 3, is characterized in that: described adjustment platform is provided with two groups of guided missile support brackets, often organizes described guided missile support bracket and is equipped with two location receivers.
7. guided missile bomb truck according to claim 1, is characterized in that: described traveling gear comprises the roller of being located at described car body bottom and the second drive motor for driving described roller to rotate.
8. guided missile bomb truck according to claim 7, is characterized in that: described roller is provided with three, and wherein two rollers are cardan wheel and are located at relative both sides, car body rear end; Another roller is the drive wheel be connected with described second drive motor, and described drive wheel is located at the front end of car body.
9. guided missile bomb truck according to claim 1, is characterized in that: also comprise brake-applying handle, and described brake-applying handle is for separating of the gears meshing of drive wheel.
10. the guided missile bomb truck according to any one of claim 1-9, it is characterized in that: described bay-lift is hydraulic fork type bay-lift, described hydraulic pressure scissors lift table comprises scissor assembly, for the hydraulic actuating cylinder that drives scissor assembly to be elevated with for driving the HM Hydraulic Motor of described hydraulic actuating cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510665959.1A CN105253317A (en) | 2015-10-15 | 2015-10-15 | Missile loading vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510665959.1A CN105253317A (en) | 2015-10-15 | 2015-10-15 | Missile loading vehicle |
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|---|---|
| CN105253317A true CN105253317A (en) | 2016-01-20 |
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|---|---|---|---|
| CN201510665959.1A Pending CN105253317A (en) | 2015-10-15 | 2015-10-15 | Missile loading vehicle |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628238A (en) * | 2016-12-26 | 2017-05-10 | 中国航空工业集团公司西安飞机设计研究所 | Loading and unloading vehicle for airplane suspender |
| CN106742034A (en) * | 2017-02-13 | 2017-05-31 | 荆门创佳机械科技有限公司 | A kind of aircraft carrier fast loading device |
| 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 |
| CN108773379A (en) * | 2017-11-08 | 2018-11-09 | 陆卫华 | Super width iron cluster |
| CN110160416A (en) * | 2018-04-16 | 2019-08-23 | 北京机电工程研究所 | Hold in the palm firing mount provision for disengagement and technique preparation vehicle |
| CN111977549A (en) * | 2020-07-14 | 2020-11-24 | 浙江大工新能源有限公司 | Automatic lifting device for integrated box body |
| CN113682976A (en) * | 2021-07-06 | 2021-11-23 | 河北汉光重工有限责任公司 | Ship-borne vertical-launched missile loading device utilizing multi-stage hydraulic cylinders |
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2015
- 2015-10-15 CN CN201510665959.1A patent/CN105253317A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628238A (en) * | 2016-12-26 | 2017-05-10 | 中国航空工业集团公司西安飞机设计研究所 | Loading and unloading vehicle for airplane suspender |
| CN106742034A (en) * | 2017-02-13 | 2017-05-31 | 荆门创佳机械科技有限公司 | A kind of aircraft carrier fast loading device |
| CN106742034B (en) * | 2017-02-13 | 2019-04-26 | 荆门创佳机械科技有限公司 | A kind of aircraft carrier fast loading device |
| 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 |
| CN108773379A (en) * | 2017-11-08 | 2018-11-09 | 陆卫华 | Super width iron cluster |
| CN110160416A (en) * | 2018-04-16 | 2019-08-23 | 北京机电工程研究所 | Hold in the palm firing mount provision for disengagement and technique preparation vehicle |
| CN111977549A (en) * | 2020-07-14 | 2020-11-24 | 浙江大工新能源有限公司 | Automatic lifting device for integrated box body |
| CN113682976A (en) * | 2021-07-06 | 2021-11-23 | 河北汉光重工有限责任公司 | Ship-borne vertical-launched missile loading device utilizing multi-stage hydraulic cylinders |
| CN113682976B (en) * | 2021-07-06 | 2024-04-12 | 河北汉光重工有限责任公司 | Ship-borne vertical missile loading device utilizing multistage hydraulic cylinders |
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Application publication date: 20160120 |
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