CN105333776A - Antitank rocket fuse hood bottom screw disassembling machine - Google Patents
Antitank rocket fuse hood bottom screw disassembling machine Download PDFInfo
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- CN105333776A CN105333776A CN201510625307.5A CN201510625307A CN105333776A CN 105333776 A CN105333776 A CN 105333776A CN 201510625307 A CN201510625307 A CN 201510625307A CN 105333776 A CN105333776 A CN 105333776A
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Abstract
The invention discloses an antitank rocket fuse hood bottom screw disassembling machine, and relates to the technical field of cartridge disassembling devices. A hood box is located on the left side of a crossed main frame. A bottom screw box and a fuse box are arranged on the right side of the crossed main frame in the front-back direction of the crossed main frame. The fuse box is opposite to the hood box. A clamping device is located at the portion, between the hood box and the fuse box, of the crossed main frame. Moving parts on the hood box, the fuse box and the bottom screw box can rotate and move left and right under the drive of a hydraulic system. A screw device is arranged on the most front side of the middle of the crossed main frame. The clamping device can move back and forth along the crossed main frame under the drive of the screw device. The hydraulic system is controlled by an electrical control system. The disassembling machine can automatically disassemble antitank rocket bottom fuses, hoods and initiating explosive column positioning bottom screws and has the beneficial effects of being safe to use and high in efficiency.
Description
Technical field
The present invention relates to the provision for disengagement technical field of ammunition, particularly relate to spiral at the bottom of a kind of antitank rocket fuse blast cap and unload the goods from the airplane.
Background technology
Antitank rocket do scrap ammunition process time, base fuze, blast cap and primary explosive column location end spiral shell and body is needed to decompose, but there is no a kind of device being specially adapted for antitank rocket dismounting in prior art, make can only process by hand the decomposition of antitank rocket, inefficiency and dangerous.
Summary of the invention
Technical problem to be solved by this invention is to provide spiral at the bottom of a kind of antitank rocket fuse blast cap and unloads the goods from the airplane, described in revolve to unload the goods from the airplane there is use safety, feature that efficiency is high.
For solving the problems of the technologies described above, the technical solution used in the present invention is: at the bottom of a kind of antitank rocket fuse blast cap, spiral unloads the goods from the airplane, it is characterized in that: comprise cross mainframe, electric-control system, hydraulic system, blast cap case, fuse case, end spiral shell case, clamping device and feed screw apparatus, described blast cap case is positioned at the left side of described cross mainframe front and rear part, spiral shell case of the described end and fuse case are before cross mainframe, rear is to the right side being arranged at described cross mainframe front and rear part, described fuse case and described blast cap case are oppositely arranged, on the front and rear part of the cross mainframe of described clamping device between blast cap case and fuse case, described blast cap case, moving component on fuse case and end spiral shell case is rotatable and move left and right under the driving of hydraulic system, described lead screw device is arranged on the front side of described cross mainframe front and rear part, described clamping device can movable along cross mainframe under the driving of lead screw device, described hydraulic system is controlled by described electric-control system.
Further technical scheme is: described spiral unloads the goods from the airplane and also comprises explosion-protection equipment, and explosion-protection equipment comprises explosion proof door, explosion-proof oil cylinder and blast wall, and explosion-proof oil cylinder is contained on blast wall, and explosion proof door realizes opening and closing under the drive of explosion-proof oil cylinder.
Further technical scheme is: described spiral unloads the goods from the airplane and also comprises positioner, and described positioner is positioned at the downside of described cross mainframe front portion.
Further technical scheme is: described blast cap case comprises blast cap case hydraulic motor, the clutch end of described blast cap case hydraulic motor is connected with blast cap case motor drive shaft, blast cap case motor drive shaft is connected with blast cap casing axle by bearing, the periphery of blast cap case motor drive shaft is fixed with the first driving wheel, blast cap case hollow spindle is connected with blast cap casing axle by bearing, first revolves and unloads axle and be plugged in described blast cap case hollow spindle, and revolve by first and unload screw and be connected with blast cap case hollow spindle, first revolves being provided with between left end and blast cap case hollow spindle of unloading axle first revolves to unload and pushes away spring, the left end of described blast cap case hollow spindle is fixed with first and pushes away spring lid, described first pushes away spring covers and is provided with the first proximity switch, blast cap case hollow spindle between described blast cap casing and the first proximity switch is provided with the first counting floral disc, described first revolves to unload in axle and is provided with blast cap case push rod, the left end of blast cap case push rod is connected with blast cap case tip-lever support, the right-hand member of blast cap case push rod is free end, blast cap case tip-lever support is fixedly connected with described cross mainframe, the periphery of described blast cap case hollow spindle is fixed with the first driven pulley, described first driving wheel is meshed with the first driven pulley, revolve and unload chuck and be connected to first by left hand thread and revolve the right-hand end of unloading axle, blast cap case propelling cylinder is fixed on cross mainframe, the clutch end of blast cap case propelling cylinder is connected with blast cap casing.
Further technical scheme is: described in revolve and unload chuck and comprise chuck seat, chuck body, eccentric claw, chuck planetary gear, claw sun gear, locating piece and reset tension spring, chuck seat is connected with blast cap case hollow spindle by left hand thread, eccentric claw is contained on chuck planet wheel spindle, the outside of chuck planet wheel spindle is provided with chuck planetary gear, chuck planetary gear is evenly distributed between chuck body and claw sun gear, eccentric claw is milled with pawl tooth and with the tapering identical with body; Locating piece is fixed on the side of described eccentric claw, for ensureing that claw opens suitable angle under the traction of reset tension spring.
Further technical scheme is: described fuse case comprises fuse case hydraulic motor, the clutch end of described fuse case hydraulic motor is connected with fuse case motor drive shaft, fuse case motor drive shaft is connected with fuse casing axle by bearing, the periphery of fuse case motor drive shaft is fixed with the second driving wheel, fuse case hollow spindle is connected with fuse casing axle by bearing, second revolves and unloads axle and be plugged in described fuse case hollow spindle, and revolve by second and unload screw and be connected with fuse case hollow spindle, second revolves being provided with between right-hand end and fuse case hollow spindle of unloading axle second revolves to unload and pushes away spring, the right-hand end of described fuse case hollow spindle is fixed with second and pushes away spring lid, described second pushes away spring covers and is provided with the second proximity switch, fuse case hollow spindle between described fuse casing and the second proximity switch is provided with the second counting floral disc, described second revolves to unload in axle and is provided with fuse case push rod, the right-hand member of fuse case push rod is connected with cross mainframe by support bar, the left end of fuse case push rod is free end, fuse case tip-lever support is fixedly connected with described cross mainframe, the periphery of described fuse case hollow spindle is fixed with the second driven pulley, described second driving wheel is meshed with the second driven pulley, fuse revolves and unloads parts and be connected to second by left hand thread and revolve the left end of unloading axle, fuse case propelling cylinder is fixed on cross mainframe, the clutch end of fuse case propelling cylinder is connected with fuse casing.
Further technical scheme is: spiral shell case of the described end comprises end spiral shell case hydraulic motor, the clutch end of spiral shell case hydraulic motor of the described end is connected with end spiral shell case motor drive shaft, end spiral shell case motor drive shaft is connected with end spiral shell casing axle by bearing, the periphery of end spiral shell case motor drive shaft is fixed with the 3rd driving wheel, end spiral shell case hollow spindle is connected with end spiral shell casing axle by bearing, 3rd revolves and unloads axle and be plugged in spiral shell case hollow spindle of the described end, and revolve by the 3rd and unload screw and be connected with end spiral shell case hollow spindle, 3rd revolves being provided with between right-hand end and end spiral shell case hollow spindle of unloading axle the 3rd revolves to unload and pushes away spring, the right-hand end of spiral shell case hollow spindle of the described end is fixed with the 3rd and pushes away spring lid, described 3rd pushes away spring covers and is provided with the 3rd proximity switch, end spiral shell case hollow spindle between spiral shell casing of the described end and the 3rd proximity switch is provided with the 3rd and counts floral disc, the periphery of spiral shell case hollow spindle, the described end is fixed with the 3rd driven pulley, described 3rd driving wheel is meshed with the 3rd driven pulley, end spiral unloads parts and is connected to the 3rd by left hand thread and revolves the left end of unloading axle, the outside that spiral of the described end unloads parts is provided with end spiral shell discharging seat, end spiral shell case propelling cylinder is fixed on cross mainframe, the end clutch end of spiral shell case propelling cylinder is connected with end spiral shell casing.
Further technical scheme is: described clamping device comprises dragging case, clamping cylinder is fixed on described dragging case by oil cylinder seat, right jaw is threaded connection the clutch end at described clamping cylinder, left jaw and right jaw are oppositely arranged, left jaw by pinned connection on left jaw seat, left jaw seat is fixed on described dragging case, the left side of left jaw seat is provided with block, the outside of block is provided with left jaw puller bolt, 4th proximity switch is positioned on described oil cylinder seat, the right jaw relative with the 4th proximity switch is provided with detecting head, described left jaw seat is fixed on described dragging case, V-block is provided with between described left jaw seat and oil cylinder seat, screw is provided with in described dragging case, described screw is fixedly connected with dragging case by nut seat, leading screw on described screw and feed screw apparatus cooperatively interacts.
Further technical scheme is: described feed screw apparatus comprises leading screw, the outside of described leading screw is provided with screw, screw is fixedly connected with the dragging case on clamping device by nut seat, the right-hand member of screw mandrel is connected with cross mainframe with bearing block by bearing, the left end of leading screw is connected with transmission case axle by bearing, the left end of leading screw is provided with the 4th follower, driving shaft is arranged in transmission case by bearing is rotating, the outside of driving shaft is provided with the 4th driving wheel, 4th driving wheel engages with the 4th follower, and the left end of driving shaft is connected with screw mandrel hydraulic motor.
Further technical scheme is: described positioner comprises positional cylinder, the base of described positional cylinder is connected with positional cylinder lower connecting plate, positional cylinder lower connecting plate is by lifting bar and lifting seat and be connected, positional cylinder pull bar is fixed on the left and right sides of positional cylinder lower connecting plate, the upper end of each positional cylinder pull bar arranges an alignment pin, connected by pitman shaft between two alignment pins, the upper side end of described alignment pin is provided with roller.
The beneficial effect adopting technique scheme to produce is: after putting antitank rocket, shell clamps by clamping device, and after reaching setting pressure, the pressure sensor on clamping device sends signal; The lifting of positional cylinder pull bar, alignment pin stretches out and is in positioning states, screw mandrel hydraulic motor starts quick rotation simultaneously, driven by leading screw and drag case rapid movement, antitank rocket body soon arrive fuse blast cap revolve unload station time, corresponding proximity switch sends reduce-speed sign, and leading screw becomes slow rotation, drags case and slowly moves; When encountering alignment pin arrival station, corresponding proximity switch sends the signal that puts in place, and leading screw stops operating, and position is now exactly revolve the position of unloading blast cap and fuse.
After signal received by explosion-proof oil cylinder, drive explosion proof door to close, close proximity switch after putting in place and send signal.Blast cap case propelling cylinder drives blast cap case to move forward after receiving the signal that explosion proof door transmits, when arrival appointment is revolved and is unloaded distance, the proximity switch of setting sends signal, after signal lag 0.1s received by blast cap case hydraulic motor, start low speed rotation to carry out revolving unloading, now count floral disc counting, revolve after turning around, change fast rotary into and unload.Revolve and unload after the number of turns unloads blast cap reaching appointment, counting floral disc sends signal, blast cap case hydraulic motor stops operating, blast cap case propelling cylinder drives blast cap case travelling backwards recession, the blast cap unloaded will by blast cap case push rod from roof fall chuck, and after travelling backwards puts in place, the signal of proximity switch will pass to fuse case propelling cylinder.
Fuse case is driven to move forward after fuse case propelling cylinder receives the signal of transmission, when arrival appointment is revolved and is unloaded distance, proximity switch sends signal, fuse case hydraulic motor to be received after signal after time delay 0.1s, start low speed rotation to carry out revolving unloading, now counter switch starts counting, revolves after turning around, changes fast rotary into and unload.Revolve and unload after the number of turns unloads fuse reaching appointment, counter switch sends signal, and fuse case hydraulic motor stops operating, and fuse case propelling cylinder drives the recession of fuse case, fuse revolves and unloads parts (fuse pulling claw) by fuse pull-out, and is fallen in pulp-collecting box below by fuse case push rod roof fall.Send signal after the infrared photoelectric sensor arranged in pulp-collecting box both sides detects object, after position got back to by fuse case simultaneously, proximity switch also sends signal.
After receiving two signals that blast cap case and fuse case send, leading screw reversion moves certain distance after driving and dragging case, disengages, stop after time delay 1s with alignment pin.Positional cylinder drives alignment pin to decline after receiving signal, gets out of the way and drags case forwarding route.Leading screw hydraulic motor is received positional cylinder and is declined after the signal that puts in place, fast rotational again, drives to drag case and advance.When soon arriving that spiral unloads station at the end, corresponding proximity switch sends reduce-speed sign, and leading screw becomes slow rotation, drags case and slowly moves; When encountering the alignment pin of positioner, arrive end spiral and unload station, corresponding proximity switch sends the signal that puts in place, and leading screw stops operating, and position is now exactly revolve the position of unloading end spiral shell.
End spiral shell case reach is driven after spiral shell case propelling cylinder receives the signal transmitted at the end, arrival appointment is revolved and is unloaded apart from rear time delay 0.1s, proximity switch sends signal, after signal received by spiral shell case hydraulic motor at the end, start low speed rotation to carry out revolving unloading, now counter switch starts counting, revolves after turning around, changes fast rotary into and unload.Revolve and unload after the number of turns unloads spiral shell of going to the bottom reaching appointment, counter switch sends signal, motor stops operating, end spiral shell case propelling cylinder drives end spiral shell case recession, the end spiral shell unloaded is unloaded parts (spring clip) pull-out by end spiral, after encountering end spiral shell discharging seat, roof fall falls in pulp-collecting box below, and after position got back to by end spiral shell case, proximity switch sends signal.
Receive after end spiral shell case retreats the signal that puts in place that sends of putting in place, anti-detonation promotes and is opened by explosion proof door.After explosion proof door is opened and put in place, proximity switch sends signal, and reversion fast received by leading screw motor, drives and drags case Quick-return.When soon reaching initial upper material level by blast wall, run into deceleration and take over switch, leading screw becomes slow rotation.Drag case slowly movement, after meeting next proximity switch, leading screw stops operating, and drag case and get back to original material loading position, clamping cylinder unclamps shell, and a workflow terminates.
Fall in pulp-collecting box if fuse is not drawn out after not screwing off or screwing off, the photosignal on pulp-collecting box would not send (namely photosignal is sent signal by object shield), and revolving below is unloaded end spiral shell operation and just can not be carried out.In this case explosion proof door will be opened, and leading screw reversion is sent shell outside blast wall, and the fuse do not unloaded and end spiral shell are by manually completing.
The control of each work position hydraulic motor rotating cycle has been come by the proximity switch being contained in main shaft rear portion and the counting floral disc that is milled with colored groove above.Floral disc rotate time, when flower groove send by not having signal during proximity switch, when card by time then have signal to send.Therefore the adjustable range of the number of turns can be as accurate as 1/6 circle.Clamping cylinder unclamps the signal put in place and is controlled by proximity switch.
Describedly revolve base fuze, blast cap and the primary explosive column location end spiral shell unloading the goods from the airplane and can dismantle antitank rocket automatically, there is use safety, feature that efficiency is high.
Accompanying drawing explanation
Fig. 1 is main TV structure schematic diagram of the present invention;
Fig. 2 is plan structure schematic diagram of the present invention;
Fig. 3 is the structural representation revolving the Apoplexy cap case that unloads the goods from the airplane of the present invention;
Fig. 4-5 revolves the structural representation unloading chuck in Fig. 3;
Fig. 6 is the structural representation revolving the middle fuse case that unloads the goods from the airplane of the present invention;
Fig. 7 is the structural representation revolving the spiral shell case of the middle end that unloads the goods from the airplane of the present invention;
Fig. 8 is the structural representation revolving the middle clamping device that unloads the goods from the airplane of the present invention;
Fig. 9 is the structural representation revolving the middle feed screw apparatus that unloads the goods from the airplane of the present invention;
Figure 10 is the structural representation revolving the middle positioner that unloads the goods from the airplane of the present invention;
Figure 11 is the schematic diagram revolving the middle electrical system that unloads the goods from the airplane of the present invention;
Figure 12 is the outside drawing of switch board in the present invention;
Figure 13 is the outside drawing of hand-held control box in the present invention;
Wherein: 1, cross mainframe
2, blast cap case 21, blast cap case hydraulic motor 22, blast cap case motor drive shaft 23, blast cap casing 24, first driving wheel 25, blast cap case hollow spindle 26, first revolve and unload axle 27, first and revolve and unload screw 28, first and revolve to unload and push away spring 29, first and push away spring lid 210, first proximity switch 211, first counting floral disc 212, blast cap case push rod 213, blast cap case tip-lever support 214, first driven pulley 215, revolve and unload chuck; 2151, chuck seat 2152, chuck body 2153, eccentric claw 2154, chuck planetary gear 2155, claw sun gear 2156, locating piece 2157, reset tension spring;
3, fuse case 31, fuse case hydraulic motor 32, fuse case motor drive shaft 33, fuse casing 34, second driving wheel 35, fuse case hollow spindle 36, second revolve and unload axle 37, second and revolve and unload screw 38, second and revolve to unload and push away that spring 39, second pushes away spring lid 310, second proximity switch 311, second counting floral disc 312, second driven pulley 313, fuse revolves and unloads parts;
4, end spiral shell case 41, end spiral shell case hydraulic motor 42, end spiral shell case motor drive shaft 43, end spiral shell casing the 44, the 3rd driving wheel 45, end spiral shell case hollow spindle the 46, the 3rd revolve and unload axle 47, the 3rd and revolve and unload screw 48, the 3rd and revolve to unload and push away that spring 49, the 3rd pushes away spring lid 410, the 3rd proximity switch 411, the 3rd counting floral disc 412, the 3rd driven pulley 413, end spiral unload parts 414, end spiral shell discharging seat;
5, clamping device 51, dragging case 52, clamping cylinder 53, oil cylinder seat 54, right jaw 55, left jaw 56, left jaw seat 57, block 58, left jaw puller bolt 59, bearing pin 510, the 4th proximity switch 511, detecting head 512, V-block;
6, feed screw apparatus 61, leading screw 62, screw 63, nut seat 64, the 4th follower 65, driving shaft 66, the 4th driving wheel 67, screw mandrel hydraulic motor 68, transmission case;
7, explosion-protection equipment 71, explosion proof door 72, explosion-proof oil cylinder 73, blast wall;
8, positioner 81, positional cylinder 82, positional cylinder lower connecting plate 83, lift bar 84, lift seat 85, positional cylinder pull bar 86, alignment pin 87, pitman shaft 88, roller.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
Set forth a lot of detail in the following description so that fully understand the present invention, but the present invention can also adopt other to be different from alternate manner described here to implement, those skilled in the art can when without prejudice to doing similar popularization when intension of the present invention, therefore the present invention is by the restriction of following public specific embodiment.
Described in the application all around, refer to that Fig. 2 up and down.
As shown in Figure 1-2, the invention discloses spiral at the bottom of a kind of antitank rocket fuse blast cap and unload the goods from the airplane, comprise cross mainframe 1, electric-control system, hydraulic system, blast cap case 2, fuse case 3, end spiral shell case 4, clamping device 5 and feed screw apparatus 6.Described blast cap case 2 is positioned at the left side of described cross mainframe 1 front and rear part, spiral shell case of the described end 4 and fuse case 3 are arranged at the right side of described cross mainframe 1 front and rear part along the front and rear direction of cross mainframe 1, described fuse case 3 is oppositely arranged, on the front and rear part of the cross mainframe of described clamping device 5 between blast cap case 2 and fuse case 3 with described blast cap case 2; Moving component on described blast cap case 2, fuse case 3 and end spiral shell case 4 is rotatable and move left and right under the driving of hydraulic system, described lead screw device 6 is arranged on the front side of described cross mainframe 1 front and rear part, described clamping device 5 can movable along cross mainframe 1 under the driving of lead screw device, and described hydraulic system is controlled by described electric-control system.
Hydraulic system and cross mainframe design for integral type, and hydraulic oil container is placed in cross mainframe lathe bed upper left side.Electric-control system is divided into hand held controller and electrical control cubicles two separate units.Hand held controller is placed near electrical control cubicles, is convenient to closely manually debug in explosion-proof, and electrical control cubicles is placed on by the outside upper bullet station of blast wall, for formal operation.
As shown in Figure 3, described blast cap case 2 comprises blast cap case hydraulic motor 21, the clutch end of described blast cap case hydraulic motor 21 is connected with blast cap case motor drive shaft 22, blast cap case motor drive shaft 22 is connected with blast cap casing 23 axle by bearing, the periphery of blast cap case motor drive shaft 22 is fixed with the first driving wheel 24, blast cap case hollow spindle 25 is connected with blast cap casing 23 axle by bearing, first revolves and unloads axle 26 and be plugged in described blast cap case hollow spindle 25, and revolve by first and unload screw 27 and be connected with blast cap case hollow spindle 25, first revolves being provided with between left end and blast cap case hollow spindle 25 of unloading axle 26 first revolves to unload and pushes away spring 28, the left end of described blast cap case hollow spindle 25 is fixed with first and pushes away spring lid 29, described first pushes away spring lid 29 is provided with the first proximity switch 210, blast cap case hollow spindle 25 between described blast cap casing 23 and the first proximity switch 210 is provided with the first counting floral disc 211, described first revolves to unload in axle 26 and is provided with blast cap case push rod 212, the left end of blast cap case push rod 212 is connected with blast cap case tip-lever support 213, the right-hand member of blast cap case push rod 212 is free end, blast cap case tip-lever support 213 is fixedly connected with described cross mainframe 1, the periphery of described blast cap case hollow spindle 25 is fixed with the first driven pulley 214, described first driving wheel 24 is meshed with the first driven pulley 214, revolve and unload chuck 215 and be connected to first by left hand thread and revolve the right-hand end of unloading axle 26, blast cap case propelling cylinder is fixed on cross mainframe 1, the clutch end of blast cap case propelling cylinder is connected with blast cap casing 23.
Blast cap case hydraulic motor drives the first driving wheel to rotate by blast cap case motor drive shaft, and the first driving wheel drives blast cap case hollow spindle to rotate by the first driven pulley.First revolves and unloads axle and be inserted in blast cap case hollow spindle, unloads screw transmission campaign, and can move axially along self guide key groove by being contained in revolving on blast cap case hollow spindle.Revolve and unload chuck and unload axle by left hand thread and be connected with revolving.First revolves that to unload the effect pushing away spring be give first to revolve unload the certain axial thrust of axle when chuck pressurized.These parts are contained on blast cap casing, under the drive of blast cap propelling cylinder, can realize moving forward and backward.
As illustrated in figures 4-5, revolve described in and unload chuck 215 and comprise chuck seat 2151, chuck body 2152, eccentric claw 2153, chuck planetary gear 2154, claw sun gear 2155, locating piece 2156 and reset tension spring 2157.Chuck seat 2151 is connected with blast cap case hollow spindle 25 by left hand thread, eccentric claw 2153 is contained on chuck planet wheel spindle, the outside of chuck planet wheel spindle is provided with chuck planetary gear 2154, chuck planetary gear 2154 is evenly distributed between chuck body 2152 and claw sun gear 2155, eccentric claw 2153 is milled with pawl tooth and with the tapering identical with body; Locating piece 2156 is fixed on the side of described eccentric claw 2153, for ensureing that claw opens suitable angle under the traction of reset tension spring 2157.
Eccentric claw is contained on chuck planet wheel spindle, is evenly distributed on chuck body, forms turn round train with claw sun gear.Eccentric claw is milled with pawl tooth and with the tapering identical with body, can ensures to fit with the body conical surface.The effect of locating piece ensures that eccentric claw opens suitable angle under the traction of reset tension spring.After claw withstands the corresponding conical surface of body, once chuck rotates, due to the effect of bias, pawl tooth tightly will bite composition surface, turns tighter and tighter, until unscrew.
As shown in Figure 6, described fuse case 3 comprises fuse case hydraulic motor 31, the clutch end of described fuse case hydraulic motor 31 is connected with fuse case motor drive shaft 32, fuse case motor drive shaft 32 is connected with fuse casing 33 axle by bearing, the periphery of fuse case motor drive shaft 32 is fixed with the second driving wheel 34, fuse case hollow spindle 35 is connected with fuse casing 33 axle by bearing, second revolves and unloads axle 36 and be plugged in described fuse case hollow spindle 35, and revolve by second and unload screw 37 and be connected with fuse case hollow spindle 35, second revolves being provided with between right-hand end and fuse case hollow spindle 35 of unloading axle 36 second revolves to unload and pushes away spring 38, the right-hand end of described fuse case hollow spindle 35 is fixed with second and pushes away spring lid 39, described second pushes away spring lid 39 is provided with the second proximity switch 310, fuse case hollow spindle 35 between described fuse casing 33 and the second proximity switch 310 is provided with the second counting floral disc 311, described second revolves to unload in axle 36 and is provided with fuse case push rod, the right-hand member of fuse case push rod is connected with cross mainframe 1 by support bar, the left end of fuse case push rod is free end, fuse case tip-lever support is fixedly connected with described cross mainframe 1, the periphery of described fuse case hollow spindle 35 is fixed with the second driven pulley 312, described second driving wheel 34 is meshed with the second driven pulley 312, fuse revolves and unloads parts 313 and be connected to second by left hand thread and revolve the left end of unloading axle 36, fuse case propelling cylinder is fixed on cross mainframe 1, the clutch end of fuse case propelling cylinder is connected with fuse casing 33.
Fuse case hydraulic motor drives the second driving wheel to rotate by fuse case motor drive shaft, and the second driving wheel drives fuse case hollow spindle to rotate by the second driven pulley.Second revolves and unloads axle and be inserted in fuse case hollow spindle, unloads screw transmission campaign, and can move axially along self guide key groove by being contained in revolving on fuse case hollow spindle.Fuse revolves and unloads parts and unloaded axle by left hand thread and be connected with revolving.Second revolves that to unload the effect pushing away spring be give second when fuse revolves and unloads parts pressurized to revolve and unload the certain axial thrust of axle.These parts are contained on fuse casing, under the drive of fuse propelling cylinder, can realize moving forward and backward.
As shown in Figure 7, spiral shell case of the described end 4 comprises end spiral shell case hydraulic motor 41, the clutch end of spiral shell case hydraulic motor of the described end 41 is connected with end spiral shell case motor drive shaft 42, end spiral shell case motor drive shaft 42 is connected with end spiral shell casing 43 axle by bearing, the periphery of end spiral shell case motor drive shaft 42 is fixed with the 3rd driving wheel 44, end spiral shell case hollow spindle 45 is connected with end spiral shell casing 43 axle by bearing, 3rd revolves and unloads axle 46 and be plugged in spiral shell case hollow spindle of the described end 45, and revolve by the 3rd and unload screw 47 and be connected with end spiral shell case hollow spindle 45, 3rd revolves being provided with between right-hand end and end spiral shell case hollow spindle 45 of unloading axle 46 the 3rd revolves to unload and pushes away spring 48, the right-hand end of spiral shell case hollow spindle of the described end 45 is fixed with the 3rd and pushes away spring lid 49, described 3rd pushes away spring lid 49 is provided with the 3rd proximity switch 410, end spiral shell case hollow spindle 45 between spiral shell casing of the described end 43 and the 3rd proximity switch 410 is provided with the 3rd and counts floral disc 411, the periphery of spiral shell case hollow spindle of the described end 45 is fixed with the 3rd driven pulley 412, described 3rd driving wheel 44 is meshed with the 3rd driven pulley 412, end spiral unloads parts 413 and is connected to the 3rd by left hand thread and revolves the left end of unloading axle 46, the outside that spiral of the described end unloads parts 413 is provided with end spiral shell discharging seat 414, end spiral shell case propelling cylinder is fixed on cross mainframe 1, the clutch end of end spiral shell case propelling cylinder is connected with end spiral shell casing 43.
End spiral shell case hydraulic motor drives the 3rd driving wheel to rotate by end spiral shell case motor drive shaft, and the 3rd driving wheel drives end spiral shell case hollow spindle to rotate by the 3rd driven pulley.3rd revolves and unloads axle and be inserted in end spiral shell case hollow spindle, unloads screw transmission campaign, and can move axially along self guide key groove by being contained in revolving on end spiral shell case hollow spindle.End spiral is unloaded parts and is revolved by left hand thread and the 3rd and unload axle and be connected.3rd revolves that to unload the effect pushing away spring be give the 3rd to revolve unload the certain axial thrust of axle when end spiral unloads parts pressurized.These parts are contained on end spiral shell casing, under the drive of end spiral shell propelling cylinder, can realize moving forward and backward.
As shown in Figure 8, described clamping device 5 comprises dragging case 51, clamping cylinder 52 is fixed on described dragging case 51 by oil cylinder seat 53, right jaw 54 is threaded connection the clutch end at described clamping cylinder 52, left jaw 55 is oppositely arranged with right jaw 54, left jaw 55 is connected on left jaw seat 56 by bearing pin 59, left jaw seat 56 is fixed on described dragging case 51, the left side of left jaw seat 56 is provided with block 57, the outside of block 57 is provided with left jaw puller bolt 58, 4th proximity switch 510 is positioned on described oil cylinder seat 53, the right jaw 54 relative with the 4th proximity switch 510 is provided with detecting head 511, described left jaw seat 56 is fixed on described dragging case 51, V-block 512 is provided with between described left jaw seat 56 and oil cylinder seat 53, screw is provided with in described dragging case 51, described screw is fixedly connected with dragging case 51 by nut seat, leading screw on described screw and feed screw apparatus cooperatively interacts.
Left jaw is contained on left jaw seat, upwards can turn an angle around bearing pin, is convenient to place take out shell.Left jaw seat can move left and right 5mm by adjusting bolt, and V-block also can move left and right 5mm, is convenient to elastomer axis and adjusts to and revolve the position of unloading axis collinear.The effect of block is the position limiting body placement, ensures that each body is placed identical.Drag case under the drive of leading screw, can rectilinear motion be realized, reach the object sending bullet.
As shown in Figure 9, described feed screw apparatus 6 comprises leading screw 61, the outside of described leading screw 61 is provided with screw 62, screw 62 is fixedly connected with the dragging case 51 on clamping device 5 by nut seat 63, the right-hand member of screw mandrel 61 is connected with cross mainframe 1 with bearing block by bearing, the left end of leading screw is connected with transmission case 68 axle by bearing, the left end of leading screw 61 is provided with the 4th follower 64, driving shaft 65 is arranged in transmission case 68 by bearing is rotating, the outside of driving shaft 65 is provided with the 4th driving wheel 66, 4th driving wheel 65 engages with the 4th follower 64, the left end of driving shaft 65 is connected with screw mandrel hydraulic motor 67.
Screw mandrel hydraulic motor drives the 4th driving wheel to rotate by driving shaft, and the 4th driving wheel drives lead screw transmission by the 4th follower.It is movable that leading screw drives dragging case to realize on guiderail base by screw and nut seat.
As shown in Figure 1, described spiral unloads the goods from the airplane and also comprises explosion-protection equipment 7, and explosion-protection equipment comprises explosion proof door 71, explosion-proof oil cylinder 72 and blast wall 73, and explosion-proof oil cylinder 72 is contained on blast wall 73, and explosion proof door 71 realizes opening and closing under the drive of explosion-proof oil cylinder 72.
As shown in Fig. 1 and Figure 10, described spiral unloads the goods from the airplane and also comprises positioner 8, and described positioner 8 is positioned at the downside of described cross mainframe 1 front portion.Described positioner 8 comprises positional cylinder 81, the base of described positional cylinder 81 is connected with positional cylinder lower connecting plate 82, positional cylinder lower connecting plate 82 is by lifting bar 83 and lifting seat 84 and be connected, positional cylinder pull bar 85 is fixed on the left and right sides of positional cylinder lower connecting plate 82, the upper end of each positional cylinder pull bar 85 arranges an alignment pin 86, connected by pitman shaft 87 between two alignment pins 86, the upper side end of described alignment pin 86 is provided with roller 88.
Positional cylinder pull bar drives alignment pin to move up and down by pitman shaft, when alignment pin stretches out, the dragging casing of clamping device not by, when alignment pin is regained, dragging casing can pass through.Lift seat and lift bar and play supplemental support effect, the height lifting bar can regulate.The effect of positioner limits to drag case revolving position when unloading blast cap and fuse, and the phenomenon can not accurately located due to inertia when preventing leading screw from stopping operating occurs.
As shown in figure 11, wiring: electric moter voltage is AC380V, penetrates rear introducing regulator cubicle by three-phase power line explosion stack to electrical schematic diagram.Motor three phase connection and each control line have made 4 aviation plugs, only need corresponding plug to dock with the connector assembly on regulator cubicle.Should notice during motor wiring that observing oil pump turns to, oil pump housing is cast with direction indicator note signal arrow.Be not inconsistent with the direction of arrow if turned to, electric power incoming line joint can be exchanged.Notice that machine must reliable ground.
As shown in figure 12, electrical control cabinet has following function to electrical control cabinet:
Start: switch on power switch, and after pressing, hydraulic oil pump is started working.
Stop: after pressing, stop various action.
Automatic: perform automatic running program, each action completes automatically item by item.
Manual: to perform manual working procedure.Each action can run by Non-follow control separately.
Reset: respective initial set position got back to by each oil cylinder and motor.
Blast cap position: after manual mode presses this button, can each single step run state of Non-follow control blast cap case, comprises advance, retrogressing, to turn soon, slow-speed.
Spiral shell position, the end: after manual mode presses this button, can each single step run state of spiral shell case at the bottom of Non-follow control, comprises advance, retrogressing, to turn soon, slow-speed.
Fuse position: after manual mode presses this button, can each single step run state of Non-follow control fuse case, comprises advance, retrogressing, to turn soon, slow-speed.
Reset: respective initial set position got back to by each oil cylinder and motor.
After pressing each button above-mentioned, above corresponding indicator lamp light.
Clamping: clamping cylinder performs pinching action.
Loosen: clamping cylinder performs and unclamps action.
Advance: propulsion cylinder lever reclaims, drive casing reach.
Retreat: propulsion cylinder lever stretches out, move after driving casing.
Fast turn: revolve and unload axle quick rotation.
Slow-speed: revolve and unload axle slow rotation.
Men Sheng: explosion proof door is opened.
Door falls: explosion proof door cuts out.
Fast charging: leading screw drives dragging case fast approaching to revolve and unloads station.
The fast material returned: leading screw drive dragging case is withdrawn fast to revolve and unloaded station.
Slow-motion material: leading screw drives dragging case to unload station close to revolving at a slow speed.
The slow material returned: leading screw drive dragging case is withdrawn at a slow speed to revolve and unloaded station.
Location rises: positional cylinder drives alignment pin lifting, blocks and drags case moving line.
Location falls: positional cylinder drives alignment pin to decline, and gets out of the way and drags case moving line.
Suddenly stop: after pressing this button, power supply cuts off rapidly.
Run: after pressing the Auto button, often press " RUN " button next time, machine is by automatic running program complete for execution one.Under " manually " state, by this button inactive.
Touch-screen setting parameter:
Table 1 is depicted as touch-screen setting parameter table.
Table 1 touch-screen setting parameter table
First as required select bullet kind, unload 120 antitank rockets if revolved, then touch by " 120 antitank rocket " frame; Unload 93 antitank rockets if revolved, then touch by " 93 antitank rocket " frame.Because 93 antitank rockets do not have blast cap, therefore revolve when unloading 93 antitank rocket, the each action (comprise manually with automatic) relevant to blast cap case no longer performs, only perform to revolve and unload the fuse each action relevant with end spiral shell, now under " manually " adjustment state, press this button, corresponding indicator lamp will not work.
In the first lattice, input 10, represent that Oil pump electrical machinery start-up study setting parameter is 0.1 second (10*0.1=0.1).
In the second lattice, input 300, represent that limiting each rotational time setting parameter of main shaft is 30 seconds (300*0.1=30).After 30 seconds, main shaft stops the rotation no longer to revolve and unloads, and prevents fault and revolves and unload overlong time and cause frictional heating.This time is main according to revolving the time setting of unloading, slightly longer than the time of actual needs.
In the 3rd lattice input 30, represent blast cap revolve at every turn unload the number of turns be set as enclose (30*1/6=5).This number of turns is more bigger than the connection number of turns of body and blast cap, ensures can unsnatch completely at every turn.
In the 4th lattice, input 42, represent that fuse revolves at every turn and unload the number of turns and be set as 7 circles (40*1/6=7).This number of turns is more bigger than the connection number of turns of fuse, ensures can unsnatch completely at every turn.
In the 5th lattice, input 30, represent that end spiral shell revolves at every turn and unload the number of turns and be set as 5 circles (30*1/6=5).This number of turns is more bigger than the connection number of turns of end spiral shell, ensures can unsnatch completely at every turn.
During setup parameter, with finger at corresponding square frame place click and convertible numerical value, if numerical value is improper, can touches and reset with regard to energy clear 0 by " clear 0 " frame below." determination " key is pressed after parameter all sets.
Machine for a long time need not after, the parameter of setting will be lost, and will reset each parameter on the touchscreen when again enabling.
Hand-held control box: except regulator cubicle, specialized designs, with the hand-held control box of removable cable, is placed on by machine, can debugs before machine easily.Hand-held control box can only carry out the debugging under manual mode, and on it, button is identical with the corresponding control button action on regulator cubicle guidance panel.Hand-held control box as shown in figure 13.
After putting antitank rocket, shell clamps by clamping device, and after reaching setting pressure, the pressure sensor on clamping device sends signal; The lifting of positional cylinder pull bar, alignment pin stretches out and is in positioning states, screw mandrel hydraulic motor starts quick rotation simultaneously, driven by leading screw and drag case rapid movement, antitank rocket body soon arrive fuse blast cap revolve unload station time, corresponding proximity switch sends reduce-speed sign, and leading screw becomes slow rotation, drags case and slowly moves; When encountering alignment pin arrival station, corresponding proximity switch sends the signal that puts in place, and leading screw stops operating, and position is now exactly revolve the position of unloading blast cap and fuse.
After signal received by explosion-proof oil cylinder, drive explosion proof door to close, close proximity switch after putting in place and send signal.Blast cap case propelling cylinder drives blast cap case to move forward after receiving the signal that explosion proof door transmits, when arrival appointment is revolved and is unloaded distance, the proximity switch of setting sends signal, after signal lag 0.1s received by blast cap case hydraulic motor, start low speed rotation to carry out revolving unloading, now count floral disc counting, revolve after turning around, change fast rotary into and unload.Revolve and unload after the number of turns unloads blast cap reaching appointment, counting floral disc sends signal, blast cap case hydraulic motor stops operating, blast cap case propelling cylinder drives blast cap case travelling backwards recession, the blast cap unloaded will by blast cap case push rod from roof fall chuck, and after travelling backwards puts in place, the signal of proximity switch will pass to fuse case propelling cylinder.
Fuse case is driven to move forward after fuse case propelling cylinder receives the signal of transmission, when arrival appointment is revolved and is unloaded distance, proximity switch sends signal, fuse case hydraulic motor to be received after signal after time delay 0.1s, start low speed rotation to carry out revolving unloading, now counter switch starts counting, revolves after turning around, changes fast rotary into and unload.Revolve and unload after the number of turns unloads fuse reaching appointment, counter switch sends signal, and fuse case hydraulic motor stops operating, and fuse case propelling cylinder drives the recession of fuse case, fuse revolves and unloads parts (fuse pulling claw) by fuse pull-out, and is fallen in pulp-collecting box below by fuse case push rod roof fall.Send signal after the infrared photoelectric sensor arranged in pulp-collecting box both sides detects object, after position got back to by fuse case simultaneously, proximity switch also sends signal.
After receiving two signals that blast cap case and fuse case send, leading screw reversion moves certain distance after driving and dragging case, disengages, stop after time delay 1s with alignment pin.Positional cylinder drives alignment pin to decline after receiving signal, gets out of the way and drags case forwarding route.Leading screw hydraulic motor is received positional cylinder and is declined after the signal that puts in place, fast rotational again, drives to drag case and advance.When soon arriving that spiral unloads station at the end, corresponding proximity switch sends reduce-speed sign, and leading screw becomes slow rotation, drags case and slowly moves; When encountering the alignment pin of positioner, arrive end spiral and unload station, corresponding proximity switch sends the signal that puts in place, and leading screw stops operating, and position is now exactly revolve the position of unloading end spiral shell.
End spiral shell case reach is driven after spiral shell case propelling cylinder receives the signal transmitted at the end, arrival appointment is revolved and is unloaded apart from rear time delay 0.1s, proximity switch sends signal, after signal received by spiral shell case hydraulic motor at the end, start low speed rotation to carry out revolving unloading, now counter switch starts counting, revolves after turning around, changes fast rotary into and unload.Revolve and unload after the number of turns unloads spiral shell of going to the bottom reaching appointment, counter switch sends signal, motor stops operating, end spiral shell case propelling cylinder drives end spiral shell case recession, the end spiral shell unloaded is unloaded parts (spring clip) pull-out by end spiral, after encountering end spiral shell discharging seat, roof fall falls in pulp-collecting box below, and after position got back to by end spiral shell case, proximity switch sends signal.
Receive after end spiral shell case retreats the signal that puts in place that sends of putting in place, anti-detonation promotes and is opened by explosion proof door.After explosion proof door is opened and put in place, proximity switch sends signal, and reversion fast received by leading screw motor, drives and drags case Quick-return.When soon reaching initial upper material level by blast wall, run into deceleration and take over switch, leading screw becomes slow rotation.Drag case slowly movement, after meeting next proximity switch, leading screw stops operating, and drag case and get back to original material loading position, clamping cylinder unclamps shell, and a workflow terminates.
Fall in pulp-collecting box if fuse is not drawn out after not screwing off or screwing off, the photosignal on pulp-collecting box would not send (namely photosignal is sent signal by object shield), and revolving below is unloaded end spiral shell operation and just can not be carried out.In this case explosion proof door will be opened, and leading screw reversion is sent shell outside blast wall, and the fuse do not unloaded and end spiral shell are by manually completing.
The control of each work position hydraulic motor rotating cycle has been come by the proximity switch being contained in main shaft rear portion and the counting floral disc that is milled with colored groove above.Floral disc rotate time, when flower groove send by not having signal during proximity switch, when card by time then have signal to send.Therefore the adjustable range of the number of turns can be as accurate as 1/6 circle.Clamping cylinder unclamps the signal put in place and is controlled by proximity switch.
Claims (10)
1. at the bottom of an antitank rocket fuse blast cap, spiral unloads the goods from the airplane, it is characterized in that: comprise cross mainframe (1), electric-control system, hydraulic system, blast cap case (2), fuse case (3), end spiral shell case (4), clamping device (5) and feed screw apparatus (6), described blast cap case (2) is positioned at the left side of described cross mainframe (1) front and rear part, described end spiral shell case (4) and fuse case (3) are before cross mainframe (1), rear is to the right side being arranged at described cross mainframe (1) front and rear part, described fuse case (3) and described blast cap case (2) are oppositely arranged, described clamping device (5) is positioned on the front and rear part of the cross mainframe between blast cap case (2) and fuse case (3), described blast cap case (2), fuse case (3) and the moving component at end spiral shell case (4) are rotatable and move left and right under the driving of hydraulic system, described lead screw device (6) is arranged on the front side of described cross mainframe (1) front and rear part, described clamping device (5) can movable along cross mainframe (1) under the driving of lead screw device, described hydraulic system is controlled by described electric-control system.
2. at the bottom of antitank rocket fuse blast cap as claimed in claim 1, spiral unloads the goods from the airplane, it is characterized in that: described spiral unloads the goods from the airplane and also comprises explosion-protection equipment (7), explosion-protection equipment comprises explosion proof door (71), explosion-proof oil cylinder (72) and blast wall (73), explosion-proof oil cylinder (72) is contained on blast wall (73), and explosion proof door (71) realizes opening and closing under the drive of explosion-proof oil cylinder (72).
3. at the bottom of antitank rocket fuse blast cap as claimed in claim 1, spiral unloads the goods from the airplane, and it is characterized in that: described spiral unloads the goods from the airplane and also comprises positioner (8), and described positioner (8) is positioned at the anterior downside of described cross mainframe (1).
4. at the bottom of antitank rocket fuse blast cap as claimed in claim 1, spiral unloads the goods from the airplane, it is characterized in that: described blast cap case (2) comprises blast cap case hydraulic motor (21), the clutch end of described blast cap case hydraulic motor (21) is connected with blast cap case motor drive shaft (22), blast cap case motor drive shaft (22) is connected with blast cap casing (23) axle by bearing, the periphery of blast cap case motor drive shaft (22) is fixed with the first driving wheel (24), blast cap case hollow spindle (25) is connected with blast cap casing (23) axle by bearing, first revolves and unloads axle (26) and be plugged in described blast cap case hollow spindle (25), and revolve by first and unload screw (27) and be connected with blast cap case hollow spindle (25), first revolves being provided with between left end and blast cap case hollow spindle (25) of unloading axle (26) first revolves to unload and pushes away spring (28), the left end of described blast cap case hollow spindle (25) is fixed with first and pushes away spring lid (29), described first pushes away spring lid (29) is provided with the first proximity switch (210), blast cap case hollow spindle (25) between described blast cap casing (23) and the first proximity switch (210) is provided with the first counting floral disc (211), described first revolves to unload in axle (26) and is provided with blast cap case push rod (212), the left end of blast cap case push rod (212) is connected with blast cap case tip-lever support (213), the right-hand member of blast cap case push rod (212) is free end, blast cap case tip-lever support (213) is fixedly connected with described cross mainframe (1), the periphery of described blast cap case hollow spindle (25) is fixed with the first driven pulley (214), described first driving wheel (24) is meshed with the first driven pulley (214), revolve and unload chuck (215) and be connected to first by left hand thread and revolve the right-hand end of unloading axle (26), blast cap case propelling cylinder is fixed on cross mainframe (1), the clutch end of blast cap case propelling cylinder is connected with blast cap casing (23).
5. at the bottom of antitank rocket fuse blast cap as claimed in claim 4, spiral unloads the goods from the airplane, it is characterized in that: described in revolve and unload chuck (215) and comprise chuck seat (2151), chuck body (2152), eccentric claw (2153), chuck planetary gear (2154), claw sun gear (2155), locating piece (2156) and reset tension spring (2157), chuck seat (2151) is connected with blast cap case hollow spindle (25) by left hand thread, eccentric claw (2153) is contained on chuck planet wheel spindle, the outside of chuck planet wheel spindle is provided with chuck planetary gear (2154), chuck planetary gear (2154) is evenly distributed between chuck body (2152) and claw sun gear (2155), eccentric claw (2153) is milled with pawl tooth and with the tapering identical with body, locating piece (2156) is fixed on the side of described eccentric claw (2153), for ensureing that claw opens suitable angle under the traction of reset tension spring (2157).
6. at the bottom of antitank rocket fuse blast cap as claimed in claim 1, spiral unloads the goods from the airplane, it is characterized in that: described fuse case (3) comprises fuse case hydraulic motor (31), the clutch end of described fuse case hydraulic motor (31) is connected with fuse case motor drive shaft (32), fuse case motor drive shaft (32) is connected with fuse casing (33) axle by bearing, the periphery of fuse case motor drive shaft (32) is fixed with the second driving wheel (34), fuse case hollow spindle (35) is connected with fuse casing (33) axle by bearing, second revolves and unloads axle (36) and be plugged in described fuse case hollow spindle (35), and revolve by second and unload screw (37) and be connected with fuse case hollow spindle (35), second revolves being provided with between right-hand end and fuse case hollow spindle (35) of unloading axle (36) second revolves to unload and pushes away spring (38), the right-hand end of described fuse case hollow spindle (35) is fixed with second and pushes away spring lid (39), described second pushes away spring lid (39) is provided with the second proximity switch (310), fuse case hollow spindle (35) between described fuse casing (33) and the second proximity switch (310) is provided with the second counting floral disc (311), described second revolves to unload in axle (36) and is provided with fuse case push rod, the right-hand member of fuse case push rod is connected with cross mainframe (1) by support bar, the left end of fuse case push rod is free end, fuse case tip-lever support is fixedly connected with described cross mainframe (1), the periphery of described fuse case hollow spindle (35) is fixed with the second driven pulley (312), described second driving wheel (34) is meshed with the second driven pulley (312), fuse revolves and unloads parts (313) and be connected to second by left hand thread and revolve the left end of unloading axle (36), fuse case propelling cylinder is fixed on cross mainframe (1), the clutch end of fuse case propelling cylinder is connected with fuse casing (33).
7. at the bottom of antitank rocket fuse blast cap as claimed in claim 1, spiral unloads the goods from the airplane, it is characterized in that: described end spiral shell case (4) comprises end spiral shell case hydraulic motor (41), the clutch end of described end spiral shell case hydraulic motor (41) is connected with end spiral shell case motor drive shaft (42), end spiral shell case motor drive shaft (42), is connected with end spiral shell casing (43) axle by bearing, the periphery at end spiral shell case motor drive shaft (42) is fixed with the 3rd driving wheel (44), end spiral shell case hollow spindle (45), is connected with end spiral shell casing (43) axle by bearing, 3rd revolves and unloads axle (46) and be plugged in described end spiral shell case hollow spindle (45), and revolve by the 3rd and unload screw (47) and be connected with end spiral shell case hollow spindle (45), 3rd revolves the right-hand end of unloading axle (46) and is provided with the 3rd at the end spiral shell case hollow spindle (45) and revolve to unload and push away spring (48), the right-hand end of described end spiral shell case hollow spindle (45) is fixed with the 3rd and pushes away spring lid (49), described 3rd pushes away spring lid (49) is provided with the 3rd proximity switch (410), end spiral shell case hollow spindle (45) between described end spiral shell casing (43) and the 3rd proximity switch (410), is provided with the 3rd and counts floral disc (411), the periphery of described end spiral shell case hollow spindle (45) is fixed with the 3rd driven pulley (412), described 3rd driving wheel (44) is meshed with the 3rd driven pulley (412), end spiral unloads parts (413) and is connected to the 3rd by left hand thread and revolves the left end of unloading axle (46), the outside that spiral of the described end unloads parts (413) is provided with end spiral shell discharging seat (414), end spiral shell case propelling cylinder is fixed on cross mainframe (1), the clutch end of end spiral shell case propelling cylinder was connected with end spiral shell casing (43).
8. at the bottom of antitank rocket fuse blast cap as claimed in claim 1, spiral unloads the goods from the airplane, it is characterized in that: described clamping device (5) comprises dragging case (51), clamping cylinder (52) is fixed on described dragging case (51) by oil cylinder seat (53), right jaw (54) is threaded connection the clutch end in described clamping cylinder (52), left jaw (55) and right jaw (54) are oppositely arranged, left jaw (55) is connected on left jaw seat (56) by bearing pin (59), left jaw seat (56) is fixed on described dragging case (51), the left side of left jaw seat (56) is provided with block (57), the outside of block (57) is provided with left jaw puller bolt (58), 4th proximity switch (510) is positioned on described oil cylinder seat (53), the right jaw (54) relative with the 4th proximity switch (510) is provided with detecting head (511), described left jaw seat (56) is fixed on described dragging case (51), V-block (512) is provided with between described left jaw seat (56) and oil cylinder seat (53), screw is provided with in described dragging case (51), described screw is fixedly connected with dragging case (51) by nut seat, leading screw on described screw and feed screw apparatus cooperatively interacts.
9. at the bottom of antitank rocket fuse blast cap as claimed in claim 1, spiral unloads the goods from the airplane, it is characterized in that: described feed screw apparatus (6) comprises leading screw (61), the outside of described leading screw (61) is provided with screw (62), screw (62) is fixedly connected with the dragging case (51) on clamping device (5) by nut seat (63), the right-hand member of screw mandrel (61) is connected with cross mainframe (1) with bearing block by bearing, the left end of leading screw is connected with transmission case (68) axle by bearing, the left end of leading screw (61) is provided with the 4th follower (64), driving shaft (65) is arranged in transmission case (68) by bearing is rotating, the outside of driving shaft (65) is provided with the 4th driving wheel (66), 4th driving wheel (65) engages with the 4th follower (64), the left end of driving shaft (65) is connected with screw mandrel hydraulic motor (67).
10. at the bottom of antitank rocket fuse blast cap as claimed in claim 3, spiral unloads the goods from the airplane, it is characterized in that: described positioner (8) comprises positional cylinder (81), the base of described positional cylinder (81) is connected with positional cylinder lower connecting plate (82), positional cylinder lower connecting plate (82) is by lifting bar (83) and lifting seat (84) and be connected, positional cylinder pull bar (85) is fixed on the left and right sides of positional cylinder lower connecting plate (82), the upper end of each positional cylinder pull bar (85) arranges an alignment pin (86), connected by pitman shaft (87) between two alignment pins (86), the upper side end of described alignment pin (86) is provided with roller (88).
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| CN201510625307.5A CN105333776B (en) | 2015-09-28 | 2015-09-28 | Spiral at the bottom of antitank rocket fuse blast cap unloads the goods from the airplane |
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| CN201510625307.5A CN105333776B (en) | 2015-09-28 | 2015-09-28 | Spiral at the bottom of antitank rocket fuse blast cap unloads the goods from the airplane |
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| CN106624724A (en) * | 2016-12-02 | 2017-05-10 | 中国人民解放军63981部队司令部 | Portable primer disassembling tool |
| CN110608640A (en) * | 2019-10-17 | 2019-12-24 | 中国人民解放军32181部队 | Riveting formula detonator automation separator |
| CN113375512A (en) * | 2021-06-07 | 2021-09-10 | 河北迥然科技有限公司 | Air-fried ammunition compound spacing method and device and terminal equipment |
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| CN201041480Y (en) * | 2006-12-14 | 2008-03-26 | 中国人民解放军总装备部军械技术研究所 | Bullet fuse rotary-detaching device |
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| CN205014906U (en) * | 2015-09-28 | 2016-02-03 | 中国人民解放军63908部队 | Spiral unloads machine at bottom of antitank rocket detonator hood |
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| CN201041480Y (en) * | 2006-12-14 | 2008-03-26 | 中国人民解放军总装备部军械技术研究所 | Bullet fuse rotary-detaching device |
| RU2466348C1 (en) * | 2011-06-16 | 2012-11-10 | Федеральное Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" | Munitions disassembly device |
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| Publication number | Publication date |
|---|---|
| CN105333776B (en) | 2017-01-04 |
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