CN207684330U - A kind of ribbon conveyer for not shutting down dismounting fuselage - Google Patents

Abstract

A kind of ribbon conveyer for not shutting down dismounting fuselage,The conveyer includes the first delivery section,Second delivery section,First delivery section includes changer tail unit,Dismount case unit,Changer tail unit,Case unit head and the tail are dismounted to be rigidly connected,Dismounting case unit is located at the right side of changer tail unit,Second delivery section is set to the right side of the dismounting case unit of the first delivery section,Second delivery section includes multiple arranged side by side and end to end unit fuselages,First delivery section and the second delivery section of multiple unit fuselages composition work in coordination to form complete conveying cycle,Make the first delivery section by using external force,Relative movement is generated between second delivery section,Prepackage modular unit fuselage in the first delivery section is set to become normal supply unit fuselage,It effectively realizes and is solved under ribbon conveyer not shutdown situation by increasing or decreasing unit fuselage,Quickly increase and decrease conveyer unit fuselage,It is automatic to realize the flexible of conveyer,Improve the working efficiency of entire fully-mechanized mining working.

Description

A kind of ribbon conveyer for not shutting down dismounting fuselage

Technical field

The utility model is related to ribbon conveyer equipment technical field, more particularly to a kind of belt for not shutting down dismounting fuselage Conveyer.

Background technology

Leather Belt Conveyance system not only has the characteristics that freight volume is big, haul distance is long, is easy to centralized control, but also can fit Various complicated landforms are answered, are current most important bulk transportation systems.During underground coal mine mechanization comprehensive is mined, or it is existing For in tunnel piercing system, with the propulsion of coalcutter or shield machine, mating belt conveyor tail will also move accordingly Distance, this just needs ribbon conveyer frequently to shut down, dismounting（Increase）Fuselage shortens（Extend）The length of conveyer.Therewith Mating equipment also wants break-off, drastically influences working efficiency.

Invention content

In view of this, against the above deficiency, it is necessary to propose a kind of belt for not shutting down dismounting fuselage that work efficiency is high Conveyer.

A kind of ribbon conveyer for not shutting down dismounting fuselage, which includes the first delivery section, the second delivery section, described First delivery section includes changer tail unit, dismounting case unit, the changer tail unit, dismounting case unit head and the tail rigidity Connection, the dismounting case unit are located at the right side of changer tail unit, and second delivery section is set to the first delivery section The right side of case unit is dismounted, second delivery section includes multiple arranged side by side and end to end unit fuselages, and first is defeated It send portion to be driven by external drive mechanism to move forward relative to second delivery section, so that the dismounting fuselage list of the first delivery section The space for accommodating a unit fuselage is formed between member and the front end of the second delivery section, and a unit fuselage is put into above-mentioned space It is interior, so that the unit fuselage being put into above-mentioned space is connect with the left end of the second delivery section, and then by being put into a list The mode of first fuselage elongates the fuselage length of the second delivery section, to realize that ribbon conveyer does not shut down dismounting fuselage.

Preferably, first delivery section further include conveyer belt, dismounting head unit, storage tape cell, the conveyer belt according to It is secondary to pass through changer tail unit, dismounting case unit, the second delivery section, dismounting head unit, storage tape cell, formation annular conveying Band.

Preferably, the changer tail unit includes horizontal translocation oil cylinder, tail platform, aircraft tail cylinder, tail upper supporting roller Group, tail subiculum roller group, tail supporting leg, tail piston shoes；One end of the horizontal translocation oil cylinder connects with the left part of tail platform It connects, the other end and anchor of the horizontal translocation oil cylinder are transported broken all-in-one machine and connect；The aircraft tail cylinder, tail pop-up roller group are installed on On tail platform, the aircraft tail cylinder is installed on tail platform upper left end, and multiple tail upper supporting rollers are mounted on tail rolling The right side of cylinder, multiple tail subiculum roller groups are equipped with below tail platform, tail is equipped in tail platform both sides Supporting leg is equipped with tail piston shoes in the bottom of tail supporting leg；The dismounting case unit includes that fuselage pop-up roller group, dismounting fuselage are flat Platform, fuselage supporting leg, fuselage piston shoes；The fuselage pop-up roller group is installed on the top of dismounting fuselage platform, the fuselage supporting leg peace Both sides loaded on dismounting fuselage platform are equipped with fuselage piston shoes in the bottom of fuselage supporting leg；The dismounting head unit includes head Roller, conveyer belt pass sequentially through aircraft tail cylinder, tail pop-up roller group, fuselage pop-up roller group, multiple unit fuselages upper supporting roller, machine Head roller, storage tape cell, the snub pulley of multiple unit fuselages, tail subiculum roller group form cycloconveyor belt.

Preferably, which is additionally provided with tuningout unit, and the tuningout unit includes deviation adjusting rack, leveling cyclinder, tune Inclined oil cylinder, one end and the upper end of tail supporting leg or fuselage supporting leg of the leveling cyclinder are hinged, the other end of the leveling cyclinder It is hinged with corresponding tail piston shoes or fuselage piston shoes, the side of the deviation adjusting rack and corresponding tail piston shoes or fuselage piston shoes it is corresponding Side is fixedly connected, and one end of the tuningout oil cylinder and deviation adjusting rack are hinged, the other end and tail supporting leg or the machine of tuningout oil cylinder The lower end of body supporting leg is hinged.

Preferably, the tail pop-up roller group, fuselage pop-up roller group, multiple unit fuselages upper supporting roller from each other perpendicular Histogram to height it is different, to form anti-" V " font arrangement in main view direction.

Preferably, the tail pop-up roller group or fuselage pop-up roller group include three mutual indepedent fixed impact idlers, Three impact idlers in each tail pop-up roller group or fuselage pop-up roller group form flute profile.

Preferably, lift rolling is also equipped with below the dismounting case unit left-hand end, by the conveying of corresponding position Band raises its level height.

Preferably, the unit fuselage includes two sub-cell fuselages, tracks；The sub-cell fuselage include body, on String hanging prop roller group, lower V Hinge linked supporting rollers, shift fork adjusting deviation device, locking plate structure, briquette structure；The upper string hanging prop roller group is set to machine The top of body, the lower V Hinge linked supporting rollers are mounted on the lower section of string hanging prop roller group, and the upper string hanging prop roller group is cut with scissors by three section head and the tail The suspension type carrying roller connect forms, and string hanging prop roller group, which is mutually parallel, on six groups is alternatively arranged, the both ends of string hanging prop roller group on each group It is fixed on the longeron of body by shift fork adjusting deviation device, the lower V Hinge linked supporting rollers group is by the hinged suspension type support of two section head and the tail Roller group is at V Hinge linked supporting rollers group, which is mutually parallel, under two groups is alternatively arranged, and the both ends of V Hinge linked supporting rollers group pass through jam plate knot under each group Structure is fixed on the middle frame that body both sides are vertically arranged, and is set in the organism bottom and is alternatively arranged cunning there are two being mutually parallel Sled, the setting of skid vertical sub-cell fuselage length direction, and have elongated end, the track logical to sub-cell fuselage both sides It crosses on the elongated end for the skid that briquette structure is fixed on two sub-cell fuselage both sides that head and the tail dock, by two sub-cell machines Body links into an integrated entity.

Preferably, the shift fork adjusting deviation device includes ring part, shift fork tuningout bar, connecting plate, the shift fork tuningout bar one End is equipped with crook, and the middle part of the shift fork tuningout bar is rotatablely connected by one end of axis pin and connecting plate, connecting plate it is another End is fixedly connected with the longeron of body, and described ring part one end and the end of the upper string hanging prop roller group are hinged, and the other end is inserted in The crook of shift fork tuningout bar, hanging prop roller group of being gone here and there by shift fork tuningout bar around axis pin rotation, and then in drive leans forward or hypsokinesis.

Preferably, the locking plate structure includes round-link chain, snap-gauge, and the round-link chain is formed by connecting by multiple torus, phase The axial direction of adjacent two torus is mutually perpendicular to, and is provided with through-hole on the middle frame of the body, described round-link chain one end with it is described One end of lower V Hinge linked supporting roller groups is hinged, and the other end of the round-link chain passes through the through-hole on middle frame, a side of the snap-gauge It is provided with the notch extended to middle part, snap-gauge is inserted into a torus of round-link chain, the briquette structure includes pin stick, fixation Block, briquetting；The fixed block is fixed on the elongated end of body, and pin hole, one end of the briquetting and machine are provided on fixed block The elongated end of body is hinged, and the other end and the track side of the briquetting are welded, and one end of the pin stick and the other side of track are welded It connects, one end of the pin stick is inserted into the pin hole of fixed block.

In the utility model, the second delivery section of the first delivery section and multiple unit fuselages composition works in coordination to be formed completely Conveying cycle, by using external force make between the first delivery section, the second delivery section generate relative movement, make in the first delivery section Prepackage modular unit fuselage becomes normal supply unit fuselage, effectively realizes by increasing or decreasing unit fuselage to solve Under ribbon conveyer not shutdown situation, quickly increase and decrease conveyer unit fuselage, it is automatic to realize the flexible of conveyer, it improves entire The working efficiency of fully-mechanized mining working.

Description of the drawings

Fig. 1 is a kind of structure chart of ribbon conveyer for not shutting down dismounting fuselage.

Fig. 2 is a kind of head section structural schematic diagram of ribbon conveyer for not shutting down dismounting fuselage.

Fig. 3 is a kind of structure chart of the changer tail unit of ribbon conveyer for not shutting down dismounting fuselage.

Fig. 4 is a kind of structure chart of the dismounting case unit of ribbon conveyer for not shutting down dismounting fuselage.

Fig. 5 is a kind of ribbon conveyer for not shutting down dismounting fuselage described in Fig. 1 along A-A sectional views.

Fig. 6 is a kind of ribbon conveyer for not shutting down dismounting fuselage described in Fig. 1 along B-B sectional views.

Fig. 7 is a kind of ribbon conveyer for not shutting down dismounting fuselage described in Fig. 1 along C-C sectional views.

Fig. 8 is a kind of ribbon conveyer for not shutting down dismounting fuselage described in Fig. 1 along D-D sectional views.

Fig. 9 is the axonometric drawing of the unit fuselage.

Figure 10 is the partial enlarged view of the shift fork adjusting deviation device.

Figure 11 is the partial enlarged view of the locking plate structure.

Figure 12 is the partial enlarged view of the briquette structure.

In figure：First delivery section 10, changer tail unit 11, horizontal translocation oil cylinder 111, tail platform 112, aircraft tail cylinder 113, tail pop-up roller group 114, tail subiculum roller group 115, tail supporting leg 116, tail piston shoes 117, dismounting case unit 12, machine Roller station 121, dismounting fuselage platform 122, fuselage supporting leg 123, fuselage piston shoes 124, conveyer belt 13, dismounting head unit with it 14, head drum 141, storage tape cell 15, the second delivery section 20, unit fuselage 21, sub-cell fuselage 211, body 2111, longeron 21111, middle frame 21112, skid 21113, upper string hanging prop roller group 2112, lower V Hinge linked supporting rollers 2113, shift fork adjusting deviation device 2114, ring part 21141, shift fork tuningout bar 21142, crook 211421, axis pin 211422, connecting plate 21143, locking plate structure 2115, round-link chain 21151, torus 211511, snap-gauge 21152, notch 211521, briquette structure 2116, pin stick 21161, solid Determine block 21162, briquetting 21163, track 212, tuningout unit 30, deviation adjusting rack 31, leveling cyclinder 32, tuningout oil cylinder 33, lift rolling 40, guardrail 50, protecting wire net 60.

Specific implementation mode

It, below will be to required use in embodiment in order to illustrate more clearly of the technical solution of the utility model embodiment Attached drawing be briefly described, it should be apparent that, the accompanying drawings in the following description is some embodiments of the utility model, for this For the those of ordinary skill of field, without creative efforts, others are can also be obtained according to these attached drawings Attached drawing.

Referring to Fig. 1, the utility model embodiment provides a kind of ribbon conveyer for not shutting down dismounting fuselage, the conveyer Including the first delivery section 10, the second delivery section 20, the first delivery section 10 includes changer tail unit 11, dismounts case unit 12, Changer tail unit 11, dismounting case unit 12 are rigidly connected from beginning to end, and dismounting case unit 12 is located at changer tail unit 11 Right side, the second delivery section 20 are set to the right side of the dismounting case unit 12 of the first delivery section 10, and the second delivery section 20 includes more A arranged side by side and end to end unit fuselage 21, the first delivery section 10 are driven by external drive mechanism relative to the second conveying Portion 20 moves forward, and is accommodated so as to be formed between dismounting case unit 12 and the front end of the second delivery section 20 of the first delivery section 10 One unit fuselage 21 is put into above-mentioned space by the space of one unit fuselage 21, so as to be put into the unit in above-mentioned space Fuselage 21 is connect with the left end of the second delivery section 20, and then it is defeated by way of being put into a unit fuselage 21 to elongate second The fuselage length for sending portion 20, to realize that ribbon conveyer does not shut down dismounting fuselage.

In the utility model, the second delivery section 20 of the first delivery section 10 and multiple unit fuselages 21 composition is worked in coordination shape It is recycled at complete conveying, makes to generate relative movement between the first delivery section 10, the second delivery section 20 by using external force, make the Prepackage modular unit fuselage 21 becomes normal supply unit fuselage 21 in one delivery section 10, effectively realizes and is added deduct by increasing Few unit fuselage 21 quickly increases and decreases conveyer unit fuselage 21, realizes automatically defeated to solve under ribbon conveyer not shutdown situation The flexible of machine is sent, the working efficiency of entire fully-mechanized mining working is improved.

Referring to Fig. 1 and Fig. 2, further, the first delivery section 10 further includes conveyer belt 13, dismounting head unit 14, storage band list Member 15, conveyer belt 13 pass sequentially through changer tail unit 11, dismounting case unit 12, the second delivery section 20, dismounting head unit 14, tape cell 15 is stored up, cycloconveyor belt 13 is formed.

Present embodiment give adding unit fuselage 21 realize conveyer it is flexible when, the reality of conveyer belt 13 in conveyer A kind of specific embodiment now extended；

Referring to Fig. 2 to Fig. 8, further, changer tail unit 11 includes horizontal translocation oil cylinder 111, tail platform 112, machine Stern barrel 113, tail pop-up roller group 114, tail subiculum roller group 115, tail supporting leg 116, tail piston shoes 117；Horizontal translocation oil One end of cylinder 111 is connect with the left part of tail platform 112, and the other end of horizontal translocation oil cylinder 111 breaks all-in-one machine with anchor fortune and connects It connects；Aircraft tail cylinder 113, tail pop-up roller group 114 are installed on tail platform 112, and aircraft tail cylinder 113 is installed on tail platform 112 upper left-hand ends, multiple tail pop-up roller groups 114 are set to the right side of aircraft tail cylinder 113, in the lower section of tail platform 112 Multiple tail subiculum roller groups 115 are installed, tail supporting leg 116 are installed in 112 both sides of tail platform, in tail supporting leg 116 Bottom is equipped with tail piston shoes 117；It includes fuselage pop-up roller group 121, dismounting fuselage platform 122, fuselage branch to dismount case unit 12 Leg 123, fuselage piston shoes 124；Fuselage pop-up roller group 121 is installed on the top of dismounting fuselage platform 122, and fuselage supporting leg 123 is installed In the both sides of dismounting fuselage platform 122, fuselage piston shoes 124 are equipped in the bottom of fuselage supporting leg 123；Head unit 14 is dismounted to wrap Include head drum 141, conveyer belt 13 passes sequentially through aircraft tail cylinder 113, tail pop-up roller group 114, fuselage pop-up roller group 121, more Upper supporting roller, head drum 141, storage tape cell 15, the snub pulley of multiple unit fuselages 21, the tail snub pulley of a unit fuselage 21 Group 115 forms cycloconveyor belt 13.

Specifically, not shutting down the ribbon conveyer course of work of dismounting fuselage：It is carried below dismounting fuselage platform 122 first The unit fuselage 21 of preceding overlapping prepackage certain length, after anchor fortune breaks all-in-one machine one step pitch of Forward, horizontal translocation oil cylinder 111 is with anchor It is that fulcrum pulls one step pitch of entire first delivery section, 10 integral forward lead that fortune, which breaks all-in-one machine, the list of the certain length of overlapping prepackage at this time First fuselage 21 will be staggered with the first delivery section 10, become the conveyer fuselage of normal work, again in fast assembling-disassembling fuselage branch The unit fuselage 21 of overlapping prepackage certain length, recycles the above process below frame, realizes ribbon conveyer in non-stop-machine situation Lower automatic telescopic.

When above-mentioned implementation process is that working face tunnels, the automatic adding unit under the non-stop-machine operating mode of ribbon conveyer is needed Fuselage 21 can equally be well applied to reduce unit fuselage automatically under the non-stop-machine operating mode of ribbon conveyer to extend ribbon conveyer 21 to shorten ribbon conveyer, only opposite with the above process.

In present embodiment, piston shoes are divided into changer tail unit 11, dismounting case unit 12, ensure that whole system is flat Surely, lower resistance is run, and is transported using anchor and is broken all-in-one machine effect in advance in horizontal translocation oil cylinder 111, then takes the changer of integrally connected to Tail unit 11, the 12 whole advance of dismounting case unit, the interior prepackage modular unit fuselage 21 of dismounting case unit 12, changer Tail unit 11, dismounting case unit 12 work in coordination to form complete conveying cycle with multiple unit fuselages 21, effectively realize It is solved under ribbon conveyer not shutdown situation by increasing or decreasing unit fuselage 21, quickly increases and decreases conveyer unit fuselage 21, it is automatic to realize the flexible of conveyer, improve the working efficiency of entire fully-mechanized mining working.

Referring to Fig. 5 to Fig. 8, further, which is additionally provided with tuningout unit 30, and tuningout unit 30 includes deviation adjusting rack 31, leveling cyclinder 32, tuningout oil cylinder 33, one end and the upper end of tail supporting leg 116 or fuselage supporting leg 123 of leveling cyclinder 32 are cut with scissors It connects, the other end of leveling cyclinder 32 and corresponding tail piston shoes 117 or fuselage piston shoes 124 are hinged, side and the phase of deviation adjusting rack 31 The corresponding side of tail piston shoes 117 or fuselage piston shoes 124 is answered to be fixedly connected, one end and the deviation adjusting rack 31 of tuningout oil cylinder 33 are cut with scissors It connects, the other end of tuningout oil cylinder 33 and the lower end of tail supporting leg 116 or fuselage supporting leg 123 are hinged.

It, can be by controlling leveling cyclinder if encounter tunnel injustice run-off the straight during above-mentioned horizontal translocation 32 complete leveling, make 10 holding of the first delivery section horizontal always.

During above-mentioned horizontal translocation, if the first delivery section 10 occur sideslip, can by control leveling cyclinder 32, Tuningout is completed in the combination of tuningout oil cylinder 33, and 10 center line of the first delivery section is made to be overlapped with the center line of ribbon conveyer always.

Tuningout process is specially：First, operation 32 control valve of leveling cyclinder lifts piston shoes；Secondly, tuningout oil cylinder is operated Piston shoes are elapsed to the side of the first delivery section 10, make 10 disalignment of piston shoes center line and the first delivery section by 33 control valves The stroke of one tuningout oil cylinder 33；Again, 32 control valve of leveling cyclinder is operated, piston shoes are fallen；Finally, operation tuningout oil cylinder 33 First delivery section 10 is elapsed to by piston shoes offset side, completes tuningout process by control valve；If 10 sideslip of the first delivery section is tighter Weight, can repeat above-mentioned tuningout process, until 10 center line of the first delivery section is overlapped with ribbon conveyer center line.

Specifically, a tuningout is respectively set on the supporting leg at changer tail unit 11, the both ends for dismounting case unit 12 Unit 30, to complete tuningout process.

Referring to Fig. 5 to Fig. 8, further, tail pop-up roller group 114, fuselage pop-up roller group 121, multiple unit fuselages 21 Upper supporting roller is from each other in the height of vertical direction difference, to form anti-" V " font arrangement in main view direction.

Referring to Fig. 1, further, tail pop-up roller group 114 or fuselage pop-up roller group 121 include three fixed independently of each other Impact idler, three impact idlers in each tail pop-up roller group 114 or fuselage pop-up roller group 121 form flute profile.

Referring to Fig. 1, further, lift rolling 40 is also equipped with below dismounting 12 left-hand end of case unit, by corresponding positions The conveyer belt 13 set raises its level height.

Referring to Fig. 9, further, unit fuselage 21 includes two sub-cell fuselages 211, track 212；Sub-cell fuselage 211 Including body 2111, upper string hanging prop roller group 2112, lower V Hinge linked supporting rollers 2113, shift fork adjusting deviation device 2114, locking plate structure 2115； Upper string hanging prop roller group 2112 is set to the top of body 2111, and lower V Hinge linked supporting rollers 2113 are mounted under string hanging prop roller group 2112 Side, upper string hanging prop roller group 2112 are made of the hinged suspension type carrying roller of three section head and the tail, and hanging prop roller group 2112 of being gone here and there on six groups is mutually flat Between-line spacing arranges, and the vertical of body 2111 is fixed in the both ends of string hanging prop roller group 2112 by shift fork adjusting deviation device 2114 on each group On beam 21111,2113 groups of lower V Hinge linked supporting rollers are made of the hinged suspension type carrying roller of two section head and the tail, V Hinge linked supporting rollers 2113 under two groups Group, which is mutually parallel, to be alternatively arranged, and body is fixed in the both ends of 2113 groups of V Hinge linked supporting rollers by locking plate structure 2115 under each group On the middle frame 21112 that 2111 both sides are vertically arranged, is set in 2111 bottom of body and be alternatively arranged skid there are two being mutually parallel 21113, the setting of 21113 vertical 211 length direction of sub-cell fuselage of skid, and have elongated end to 211 both sides of sub-cell fuselage, Track 212 is fixed on the extension of the skid 21113 of two 211 both sides of sub-cell fuselage of head and the tail docking by briquette structure 2116 On end, two sub-cell fuselages 211 are linked into an integrated entity.

It is connected by fish platee between the track 212 of two unit fuselages 21, by two neighboring unit fuselage 21 It is connected as an entirety.

Parallel shifting is set, fan-shaped shifting is set or parallel fan joint is moved when setting, shifting sets machine idler wheel clamp and blocks track 212 and carry Playing 100-20Omm pulls out a step pitch from original position, moves the machine that sets and is parallel to the y direction of conveyer and travels back and forth, gradually will Unit fuselage 21 moves on to new position, thereby realizes the transverse shifting of conveyer, real by increasing and decreasing 21 quantity of unit fuselage Existing conveyer longitudinal movement.

The unit fuselage 21 is using the modularized design connected by track 212 between sub-cell fuselage 211, installation letter Single, after eliminating working face change, the high problem of repeated removal, mounting cost shortens the installation duration.

Referring to Figure 10, further, shift fork adjusting deviation device 2114 includes ring part 21141, shift fork tuningout bar 21142, connection Plate 21143,21142 one end of shift fork tuningout bar are equipped with crook 211421, and the middle part of shift fork tuningout bar 21142 passes through axis pin 211422 are rotatablely connected with one end of connecting plate 21143, and the other end of connecting plate 21143 is solid with the longeron 21111 of body 2111 Fixed connection, 21141 one end of ring part and the end of upper string hanging prop roller group 2112 are hinged, and the other end is inserted in shift fork tuningout bar 21142 Crook 211421, shift fork tuningout bar 21142 is rotated around axis pin 211422, and then before driving string hanging prop roller group 2112 Incline or hypsokinesis.

Upper string hanging prop roller group 2112 is connected by shift fork tuningout bar 21142 with longeron 21111, by external force to shift fork tune The rotation of side spin 21142 can play the role of good tuningout.

Referring to Figure 11 and 12, further, locking plate structure 2115 includes round-link chain 21151, snap-gauge 21152, round-link chain 21151 It is formed by connecting by multiple torus 211511, the axial direction of two neighboring torus 211511 is mutually perpendicular to, in body 2111 Through-hole is provided on a structure of an essay 21112,21151 one end of round-link chain and one end of lower 2113 groups of V Hinge linked supporting rollers are hinged, round-link chain 21151 The other end pass through the through-hole on middle frame 21112, a side of snap-gauge 21152 is provided with the notch 211521 extended to middle part, Snap-gauge 21152 to be inserted into a torus 211511 of round-link chain 21151；There is annulus at lower 2113 both ends of V Hinge linked supporting rollers respectively Chain 21151, round-link chain 21151 is stuck on unit fuselage 21 with snap-gauge 21152 can be at V-groove angle, simple in structure, installation side Just；Briquette structure 2116 includes pin stick 21161, fixed block 21162, briquetting 21163；Fixed block 21162 is fixed on body 2111 Elongated end on, be provided with pin hole on fixed block 21162, one end of briquetting 21163 is hinged with the elongated end of body 2111, briquetting 21163 other end is welded with 212 side of track, and the one end for selling stick 21161 and the other side of track 212 are welded, and stick 21161 is sold One end be inserted into fixed block 21162 pin hole in.

Further, guardrail 50 is installed in the both sides on 122 top of dismounting fuselage platform, in 122 lower part of dismounting fuselage platform Both sides protecting wire net 60 is installed.

Module or unit in the utility model embodiment device can be merged, divide and be deleted according to actual needs Subtract.

Above disclosures are merely preferred embodiments of the utility model, with this utility model cannot be limited certainly Interest field, those skilled in the art can understand all or part of the processes for realizing the above embodiment, and according to this reality The equivalent variations made by novel claim, still fall within the scope of the utility model.

Claims (10)

1. a kind of ribbon conveyer for not shutting down dismounting fuselage, it is characterised in that：The conveyer includes the first delivery section, second defeated It includes changer tail unit, dismounting case unit, the changer tail unit, dismounting fuselage list to send portion, first delivery section First head and the tail are rigidly connected, and the dismounting case unit is located at the right side of changer tail unit, and second delivery section is set to the The right side of the dismounting case unit of one delivery section, second delivery section include multiple arranged side by side and end to end unit machines Body, the first delivery section are driven by external drive mechanism and are moved forward relative to second delivery section, so that the first delivery section The space for being formed between case unit and the front end of the second delivery section and accommodating a unit fuselage is dismounted, a unit fuselage is put Enter in above-mentioned space, so that the unit fuselage being put into above-mentioned space is connect with the left end of the second delivery section, and then passes through The mode for being put into a unit fuselage elongates the fuselage length of the second delivery section, to realize that ribbon conveyer does not shut down changer Body.

2. a kind of ribbon conveyer for not shutting down dismounting fuselage as described in claim 1, it is characterised in that：First conveying Portion further includes conveyer belt, dismounting head unit, storage tape cell, and the conveyer belt passes sequentially through changer tail unit, dismounting fuselage Unit, the second delivery section, dismounting head unit, storage tape cell, form cycloconveyor belt.

3. a kind of ribbon conveyer for not shutting down dismounting fuselage as claimed in claim 2, it is characterised in that：The dismounting tail Unit includes horizontal translocation oil cylinder, tail platform, aircraft tail cylinder, tail pop-up roller group, tail subiculum roller group, tail supporting leg, machine Tail piston shoes；One end of the horizontal translocation oil cylinder is connect with the left part of tail platform, the other end of the horizontal translocation oil cylinder Broken all-in-one machine is transported with anchor to connect；The aircraft tail cylinder, tail pop-up roller group are installed on tail platform, the aircraft tail cylinder installation In tail platform upper left end, multiple tail upper supporting rollers are mounted on the right side of aircraft tail cylinder, pacify in the lower section of tail platform Equipped with multiple tail subiculum roller groups, tail supporting leg is installed in tail platform both sides, machine is equipped in the bottom of tail supporting leg Tail piston shoes；The dismounting case unit includes fuselage pop-up roller group, dismounting fuselage platform, fuselage supporting leg, fuselage piston shoes；The machine Roller station is installed on the top of dismounting fuselage platform with it, and the fuselage supporting leg is installed on the both sides of dismounting fuselage platform, in machine The bottom of body supporting leg is equipped with fuselage piston shoes；The dismounting head unit includes head drum, conveyer belt pass sequentially through aircraft tail cylinder, Tail pop-up roller group, fuselage pop-up roller group, the upper supporting roller of multiple unit fuselages, head drum, storage tape cell, multiple unit fuselages Snub pulley, tail subiculum roller group formed cycloconveyor belt.

4. a kind of ribbon conveyer for not shutting down dismounting fuselage as claimed in claim 3, it is characterised in that：The fuselage device is also Equipped with tuningout unit, the tuningout unit includes deviation adjusting rack, leveling cyclinder, tuningout oil cylinder, one end of the leveling cyclinder with The upper end of tail supporting leg or fuselage supporting leg is hinged, and the other end of the leveling cyclinder is cut with scissors with corresponding tail piston shoes or fuselage piston shoes It connects, the side of the deviation adjusting rack is fixedly connected with the corresponding side of corresponding tail piston shoes or fuselage piston shoes, the tuningout oil cylinder One end and deviation adjusting rack it is hinged, the other end of tuningout oil cylinder and the lower end of tail supporting leg or fuselage supporting leg are hinged.

5. a kind of ribbon conveyer for not shutting down dismounting fuselage as claimed in claim 3, it is characterised in that：The tail pop-up Roller group, fuselage pop-up roller group, the upper supporting roller of multiple unit fuselages are different in the height of vertical direction from each other, in main view side It is arranged to anti-" V " font is formed.

6. a kind of ribbon conveyer for not shutting down dismounting fuselage as claimed in claim 3, it is characterised in that：The tail pop-up Roller group or fuselage pop-up roller group include three mutual indepedent fixed impact idlers, each tail pop-up roller group or fuselage pop-up Three impact idlers in roller group form flute profile.

7. a kind of ribbon conveyer for not shutting down dismounting fuselage as claimed in claim 3, it is characterised in that：In the changer It is also equipped with lift rolling below body unit left-hand end, the conveyer belt of corresponding position is raised into its level height.

8. a kind of ribbon conveyer for not shutting down dismounting fuselage as described in claim 1, it is characterised in that：The unit fuselage Including two sub-cell fuselages, tracks；The sub-cell fuselage includes body, upper string hanging prop roller group, lower V Hinge linked supporting rollers, shift fork Adjusting deviation device, locking plate structure, briquette structure；The upper string hanging prop roller group is set to the top of body, and the lower V Hinge linked supporting rollers group is set In the lower section of upper string hanging prop roller group, the upper string hanging prop roller group is made of the hinged suspension type carrying roller of three section head and the tail, is gone here and there on six groups Hanging prop roller group, which is mutually parallel, to be alternatively arranged, and body is fixed in the both ends of string hanging prop roller group by shift fork adjusting deviation device on each group On longeron, the lower V Hinge linked supporting rollers group is made of the hinged suspension type carrying roller of two section head and the tail, and V Hinge linked supporting rollers group is mutual under two groups Parallel interval arranges, and the both ends of V Hinge linked supporting roller groups are fixed on by locking plate structure during body both sides are vertically arranged under each group On a structure of an essay, is set in the organism bottom and be alternatively arranged skid there are two being mutually parallel, the vertical sub-cell fuselage length of the skid Direction is arranged, and has elongated end, the track to be fixed on the two of head and the tail docking by briquette structure to sub-cell fuselage both sides On the elongated end of the skid of a sub-cell fuselage both sides, two sub-cell fuselages are linked into an integrated entity.

9. a kind of ribbon conveyer for not shutting down dismounting fuselage as claimed in claim 8, it is characterised in that：The shift fork tuningout Mechanism includes ring part, shift fork tuningout bar, connecting plate, and described shift fork tuningout bar one end is equipped with crook, the shift fork tuningout bar Middle part by one end of axis pin and connecting plate be rotatablely connected, the other end of connecting plate is fixedly connected with the longeron of body, described Ring part one end and the end of the upper string hanging prop roller group are hinged, and the other end is inserted in the crook of shift fork tuningout bar, by shift fork Hanging prop roller group of tuningout bar going here and there around axis pin rotation, and then in drive leans forward or hypsokinesis.

10. a kind of ribbon conveyer for not shutting down dismounting fuselage as claimed in claim 8, it is characterised in that：The jam plate knot Structure includes round-link chain, snap-gauge, and the round-link chain is formed by connecting by multiple torus, and the axial of two neighboring torus is mutually hung down Directly, through-hole is provided on the middle frame of the body, described round-link chain one end and one end of the lower V Hinge linked supporting rollers group are hinged, The other end of the round-link chain passes through the through-hole on middle frame, a side of the snap-gauge to be provided with the notch extended to middle part, with Snap-gauge is inserted into a torus of round-link chain, the briquette structure includes pin stick, fixed block, briquetting；The fixed block is fixed In on the elongated end of body, being provided with pin hole on fixed block, one end of the briquetting and the elongated end of body are hinged, the briquetting The other end and track side weld, one end of the pin stick and the other side of track are welded, and one end of the pin stick is inserted into solid Determine in the pin hole of block.