CN207189874U - Trigger squeeze - Google Patents

Abstract

The utility model discloses a kind of trigger squeeze, the problem of causing sheet material to press Quality Down for apparatus for feeding, provide following technical scheme, including fuselage, lower platen, top board and hydraulic cylinder, slided on lower platen and be provided with the first conveying arrangement, the first driving means of driving the first conveying arrangement sliding disengaging lower platen are additionally provided with fuselage, be also hinged with support can horizontal sliding suction cup carrier, suction cup carrier be provided with can vertical lifting sucker.Using above-mentioned technical proposal, sheet material reduces the resistance for promoting lower platen by the first conveying arrangement, sucker suction sheet material drives sheet material to enter on lower platen, first conveying arrangement leaves lower plate, sheet material is stayed on lower platen, operation finishes posterior sucker riser material, first conveying arrangement is entered on lower platen below sheet material, carry out discharge operation, because lower platen does not carry out the destruction such as slot, uniform force when sheet material presses, having reached reduction charging discharging labor intensity reduces while ensures the effect of pressing plate quality.

Description

Trigger squeeze

Technical field

A kind of presser device is the utility model is related to, more specifically, it relates to a kind of trigger squeeze.

Background technology

Need to use cold press in sheet material recombination process, if the mutually glued sheet material of dried layer is cold-pressed one using cold press Rise, wherein cold press is a kind of machinery for being used to press sheet material commonly used in carpenter field.But traditional cold press is specific Some defects during use be present, such as：It is artificial to carry feeding difficulty, using the equipment quilt such as external sucker because sheet material is overweight Fuselage stops can not normal feeding etc..

At present, in the market discloses a kind of trigger squeeze, and reference picture 1, it includes fuselage 1, and the lower end of fuselage 1, which is provided with, to be pushed Plate 143, the upper end of fuselage 1, which is provided with the piston rod 141 of hydraulic cylinder 14, hydraulic cylinder 14, is connected with top board 142, lower platen 143 push the belt conveyer 8 of plate thickness direction oscilaltion provided with that can run through, and are additionally provided with fuselage 1 for driving belt The drive device of the oscilaltion of conveyer 8, rise the transmission for making belt conveyer 8 by drive device driving belt conveyer 8 Sheet material is transmitted into trigger squeeze with the width along fuselage 1 higher than the plate face of lower platen 143 in face.

Although this trigger squeeze can drive sheet material to enter in fuselage 1 by rising belt conveyer 8, transporting Bi Hou, in order to prevent belt conveyer 8 from being destroyed by the pressure of top board 142, belt conveyer 8 need to be dropped to lower platen 143 Plate face lower section, cause lower platen 143 plate face and belt conveyer 8 transportation surface formed each groove of groove rib making Stress concentration can be all produced during industry so that sheet material impression occurs or even destroyed, also room for improvement.

Utility model content

In view of the deficienciess of the prior art, the purpose of this utility model is to provide a kind of trigger squeeze, have reduce into Material discharging labor intensity reduces ensures pressing plate quality advantage simultaneously.

To achieve the above object, the utility model provides following technical scheme：

A kind of trigger squeeze, including fuselage, lower platen is fixedly connected with the fuselage, is slidably connected on the fuselage Pressing plate, the hydraulic cylinder that driving top board vertically slides is provided with the fuselage, slides to be provided with the lower platen and uses The first of lower platen is passed in and out in being additionally provided with driving the first conveying arrangement sliding on the first conveying arrangement of transport sheet material, the fuselage Drive device, be also hinged with the fuselage can horizontal sliding suction cup carrier, the suction cup carrier be provided with can vertical lifting use In the sucker of adsorbent.

Using above-mentioned technical proposal, moved downward by Driven by Hydraulic Cylinder top board, and then pressed with lower platen, made Industry, because provided with the first conveying arrangement, sheet material can reduce the resistance for promoting lower platen by the first conveying arrangement, while pass through suction Disk adsorbent, and then drive sheet material to enter on lower platen, reduces hand labor intensity, due to sucker suction sheet material, when the Sheet material will not follow the first conveying arrangement to leave when one conveying arrangement is driven away from lower platen by first driving means, realize Lower platen directly contacts sheet material and pressed, and sheet material is lifted and then the first conveying arrangement from plate by sucker after operation Entered to below material on lower platen, carry out discharge operation, because lower platen does not carry out the destruction such as slot, stress when sheet material presses Uniformly, having reached reduction charging discharging labor intensity reduces while ensures the effect of pressing plate quality.

Preferably, the second chute is provided with the fuselage in the width direction, first conveying arrangement includes length direction Both ends be slidably connected at the first plate conveyor in the second chute.

Using above-mentioned technical proposal, because the first conveying arrangement is connected by the first plate conveyor with the second slide, make Obtain the first conveying arrangement and enter line slip along the second chute, limit the glide direction of the first conveying arrangement, while pass through second The conveying arrangement of chute supported first, reach the effect of stable operation.

Preferably, first conveying arrangement also includes being rotatably connected in the first plate conveyor around the first plate conveyor length side To the first roller of rotation.

Using above-mentioned technical proposal, sliding friction is converted to by the first roller being rotatably connected in the first plate conveyor Rolling friction so that sheet material is easier to promote, and reaches the effect for reducing labor intensity.

Preferably, one end away from first driving means is provided with and extends to ground for transporting on the width of the fuselage The second conveying arrangement on input board material to the first conveying arrangement.

Using above-mentioned technical proposal, by the second conveying arrangement by conveying sheet to first driving means, reduce plate Material is carried to the resistance of first driving means, reaches the effect for reducing labor intensity.

Preferably, second conveying arrangement includes the second plate conveyor being fixedly connected on fuselage, second transport The second roller rotated around the second plate conveyor length direction is rotatably connected on plate.

Using above-mentioned technical proposal, sliding friction is converted into by the second roller being rotatably connected in the second plate conveyor Rolling friction, reduce the resistance of sheet material propulsion, reach the effect for reducing labor intensity.

Preferably, the slipping column slid along fuselage width direction is provided with the fuselage below lower platen, it is described Slipping column is provided with the second pressure compensation device slided along the length direction of slipping column straight up.

Using above-mentioned technical proposal, by fuselage width side's upward sliding slipping column and in slipping column length side Upward sliding second pressure compensation device so that second pressure compensation device reaches lower concave part, starts second pressure compensation device Pressure compensation is carried out to lower concave part, reaches the effect of targeted accurate pressure compensation.

Preferably, first below lower platen is provided with the length direction both ends of the fuselage in the width direction to slide Groove, both ends are slidably connected in the first chute on the length direction of the slipping column.

Using above-mentioned technical proposal, by the first chute supported and support column glide direction is limited so that support column is run Stabilization, glide direction are accurate, reach stable operation, pinpoint effect.

Preferably, the second guide rail, the length direction two of the slipping column are provided with first chute along its length End is provided with the second pulley component being slidably connected on the second guide rail.

Using above-mentioned technical proposal, coordinated by the second guide rail and second pulley component, further limit the cunning of support column Dynamic direction, because sliding friction is converted to rolling friction by pulley so that slipping column sliding speed is accelerated, and reaches quick, smart It is determined that the effect of position.

Preferably, the upper wall of the slipping column is provided with the 3rd guide rail, the second pressure compensation device along its length The second power part provided with the 3rd pulley assembly of the 3rd pulley assembly and driving being slidably connected on the 3rd guide rail.

Using above-mentioned technical proposal, coordinated by the 3rd guide rail and the 3rd pulley assembly, limit second pressure compensation dress The glide direction on slipping column is put, because sliding friction is converted to rolling friction by pulley so that second pressure compensation dress Quick movement is put, driving force is given by the second power part, removes manual operation from, reaches quick, be accurately positioned and reduce work The effect of intensity.

Preferably, vertical on the fuselage to be provided with rack, level is provided with trunnion axis on the top board, on the trunnion axis Provided with the gear pressed with rack.

Using above-mentioned technical proposal, because trunnion axis and top board are horizontal, while gear is fixed with trunnion axis and and rack Pressing, when top board moves up and down, gear is limited by gear is in horizontality all the time, and then limits top board and be always positioned at Horizontality, so that pressing effect reaches optimal, reach the effect for improving pressing plate operation quality.

In summary, the utility model has the advantages that：Reduce charging discharging labor intensity and reduce and ensure simultaneously Pressing plate quality, stable equipment operation, pressure compensation is carried out to sheet material lower concave part, be quickly accurately positioned pressure compensation and improve pressure Plate operation quality.

Brief description of the drawings

Fig. 1 is trigger squeeze structural representation in the prior art；

Fig. 2 is the overall structure diagram of the utility model center platen machine face；

Fig. 3 is the overall structure diagram at the utility model center platen machine back side；

Fig. 4 is the structural representation of first pressure compensation section in the utility model；

Fig. 5 is the structural representation of second pressure compensation section in the utility model；

Fig. 6 is the enlarged diagram in A portions in Fig. 5；

Fig. 7 is the structural representation of the first conveying arrangement in the utility model；

Fig. 8 is the structural representation of suction disc device in the utility model；

Fig. 9 is the structural representation of horizontal device in the utility model.

In figure：1st, fuselage；11st, bearing；12nd, support column；13rd, top plate；14th, hydraulic cylinder；141st, piston rod；142nd, upper pressure Plate；143rd, lower platen；15th, the first guide rail；2nd, first pressure compensation section；21st, telescopic prop；211st, flange slide rail；22nd, it is spacing Ring；23rd, first pulley；24th, the first power part；25th, first pressure compensation device；26th, first pulley component；261st, first pulley Support；262nd, second pulley；263rd, the second power part；3rd, second pressure compensation section；31st, the first chute；32nd, the second guide rail；33、 Slipping column；34th, second pulley component；341st, the 3rd pulley；342nd, the 4th pulley；343rd, the 3rd power part；35th, the 3rd lead Rail；36th, second pressure compensation device；37th, the 3rd pulley assembly；371st, second pulley support；372nd, the 5th pulley；373rd, the 4th Power part；4th, the first conveying arrangement；41st, the first plate conveyor；42nd, the first roller；43rd, the 6th pulley；44th, the second chute；45th, One drive device；451st, screw rod bracket；452nd, the first screw mandrel；453rd, electric machine support；454th, the first motor；5th, the second transport dress Put；51st, the second plate conveyor；52nd, the second roller；6th, suction disc device；61st, the 4th guide rail；62nd, sliding sleeve；63rd, suction cup carrier；64th, gas Cylinder；65th, sucker；66th, the second motor；67th, the second screw mandrel；68th, the 3rd motor；7th, horizontal device；71st, rack；72nd, gear；73、 Trunnion axis.

Embodiment

Below in conjunction with the accompanying drawings and embodiment, the utility model is described in detail.

A kind of trigger squeeze, reference picture 1, including fuselage 1, the lower platen 143 for being arranged on the lower end of fuselage 1, setting are on the fuselage 1 The hydraulic cylinder 14 at end, the top board 142 being connected on the piston rod 141 of hydraulic cylinder 14, the first pressure on top board 142 Compensation section 2, the second pressure compensation section 3 positioned at the lower section of lower platen 143, the first transport dress positioned at the top of lower platen 143 Put, the suction disc device 6 of the second conveying arrangement 5 positioned at the front of fuselage 1 and setting on the fuselage 1.

Fuselage 1 includes the bearing 11 positioned at the length direction both ends of fuselage 1, and the length direction both ends of bearing 11 are fixedly connected There is support column 12, the upper end of support column 12 is fixedly connected with top plate 13, is provided with hydraulic cylinder 14 on top plate 13 vertically, hydraulic cylinder 14 is common Two length directions along top plate 13 are distributed on the center line of short side, and the piston rod 141 of hydraulic cylinder 14 injects through top plate 13 In fuselage 1, top board 142 is fixedly connected with piston rod 141, lower platen 143 is fixedly connected with bearing 11, passes through hydraulic cylinder 14 driving top boards 142 are moved downwardly on lower platen 143, and top board 142 carries out pressing plate operation with the pressing of lower platen 143.

Reference picture 1 and Fig. 3, first pressure compensation section 2 is hinged with piston rod 141, and first pressure compensation section 2 includes hinge The telescopic prop 21 being connected on piston rod 141, piston rod 141 are provided with the spacing ring 22 that limitation telescopic prop 21 slides up and down, Center line of the upper surface of top board 142 along plate week and long side is provided with the first square guide rail 15, and four angles of the first guide rail 15 are Fillet, totally two and in the same size uniform along the length direction of top board 142, the first guide rail 15, two phases of the first guide rail 15 are connected on length On the center line on side, one end rotatable connection of the telescopic prop 21 away from piston rod 141 has first pulley 23, and first pulley 23 rolls It is connected on the first guide rail 15, the first power part 24 for driving first pulley 23 is additionally provided with telescopic prop 21, branch of stretching Post 21 is rolled and can rotated around piston rod 141 along the first guide rail 15 by first pulley 23.

Telescopic prop 21 extends along its length is provided with flange slide rail 211, is connected with straight down on telescopic prop 21 First pressure compensation device 25, first pressure compensation device 25 is hydraulic cylinder in the present embodiment, can be in other embodiment cylinder, Lead screw transmission mechanism etc., the upper end of first pressure compensation device 25 are fixedly connected with the component of first pulley 23,23 groups of first pulley Part includes the support of first pulley 23 being fixedly connected with first pressure compensation device 25, is rotatably connected on the support of first pulley 23 Second pulley 262, second pulley 262 are rolled and are connected on flange slide rail 211, length of the second pulley 262 along flange slide rail 211 Direction is rolled, and the second power part 263 for driving second pulley 262 is additionally provided with the support of first pulley 23, and first pressure is mended Repay the length direction that device 25 follows the component of first pulley 23 along telescopic prop 21 to slide, coordinate telescopic prop 21 around piston rod 141 rotate, and reach in the range of the first guide rail 15 surrounds anywhere.

Reference picture 2, Fig. 4 and Fig. 5, bearing 11 are provided with the first chute 31 on the end face at the center of fuselage 1 along length, First chute is provided with the second guide rail 32 along its length on inwall about 31, the lower section of lower platen 143 compensates provided with second pressure Portion 3, second pressure compensation section 3 include the slipping column 33 being slidably connected on the first chute 31, the length side of slipping column 33 Second pulley component 34 is provided with to both ends, second pulley component 34 includes the 3rd pulley 341 for being arranged on the top of slipping column 33 And the 4th pulley 342 of the lower section of slipping column 33 is arranged on, the 3rd pulley 341 rolls the upper rail for being connected to the second guide rail 32 On, the 4th pulley 342, which rolls, to be connected on the lower guideway of the second guide rail 32 and the second pulley component 34 of the 4th pulley 342 is by the Three pulleys 341 and the 4th pulley 342, which roll, to be connected on the second guide rail 32 so that slipping column 33 is movably connected on bearing 11 And slided along the width of fuselage 1, the 3rd power part for driving the 4th pulley 342 is additionally provided with second pulley component 34 343。

The 3rd guide rail 35 is provided with slipping column 33 along its length, slidably connects on the 3rd guide rail 35 straight up Two pressure compensators 36, are hydraulic cylinder in the present embodiment, can be cylinder, lead screw transmission mechanism etc. in other embodiment, second The lower end of pressure compensator 36 is fixedly connected with the 3rd pulley assembly 37, and the 3rd pulley assembly 37 includes second pulley support 371 and the 5th pulley 372 that is rotatably connected on second pulley support 371, the 5th pulley 372 roll and be connected to the 3rd guide rail On 35, second pressure compensation device 36 follows length direction of the 3rd pulley assembly 37 along slipping column 33 to slide, and coordinates and slides Width of the pillar 33 along fuselage 1 slides, and on the optional position for reaching lower platen 143, is also set on second pulley support 371 There is the 4th power part 373 for driving the 5th pulley 372.

Reference picture 1 and Fig. 6, the top of lower platen 143 are provided with the first conveying arrangement 4, and the first conveying arrangement 4 includes sliding The first plate conveyor 41 and rotatable connection being connected on lower platen 143 turn in the first plate conveyor 41 around the length direction of fuselage 1 The first dynamic roller 42, the both ends of the length direction of the first plate conveyor 41 are rotatably connected to the 6th pulley 43, and support column 12 is along fuselage 1 Width is provided with the second horizontal chute 44, and the 6th pulley 43 is rolled and is connected in the second chute 44, and the first plate conveyor 41 is logical The 6th pulley 43 is crossed to slide on the width of fuselage 1, the length of the second chute 44 for twice of the length of the first plate conveyor 41 with The first plate conveyor 41 is set to exit lower platen 143 completely, the second chute 44 stretches out the rear of fuselage 1, is additionally provided with fuselage 1 for driving The first driving means 45 that dynamic first plate conveyor 41 is slided, first driving means 45 include being fixedly connected on lower platen 143 to The screw rod bracket 451 of the rear extension of fuselage 1, the first screw mandrel 452 is threaded with screw rod bracket 451, and the first screw mandrel 452 is solid Surely it is connected in the first plate conveyor 41, is plugged with electric machine support 453 in screw rod bracket 451, electric machine support 453 is provided with driving the The first motor 454 that one screw mandrel 452 rotates, the first plate conveyor 41 is driven to pass in and out lower platen 143 by rotating the first screw mandrel 452 Upper surface.

Reference picture 1 and Fig. 7, suction disc device 6, suction disc dress are provided between the support column 12 at the length direction both ends of bearing 11 6 the 4th guide rails 61 for including being connected between support column 12 are put, slip cap is provided with sliding sleeve 62 on the 4th guide rail 61, is gone back on fuselage 1 Be hinged with can horizontal sliding suction cup carrier 63, suction cup carrier 63 is hinged on sliding sleeve 62, on the one end of suction cup carrier 63 away from sliding sleeve 62 Cylinder 64 is provided with straight down, and sucker 65, suction cup carrier 63 and the hinged place of sliding sleeve 62 are fixedly connected with the piston rod 141 of cylinder 64 Provided with the second motor 66 for driving suction cup carrier 63 to rotate, second screw mandrel parallel with the 4th guide rail 61 is threaded with sliding sleeve 62 67, the 3rd motor 68 of the second screw mandrel 67 of driving is additionally provided with support column 12, sliding sleeve 62 is driven in fuselage 1 by the second screw mandrel 67 Width on slide.

Reference picture 1, the front of fuselage 1 are provided with the second conveying arrangement 5 that ground is extended to from lower platen 143, the second transport Device 5 includes the second plate conveyor 51 and is rotatably connected on the second roller rotated in the second plate conveyor 51 around the length direction of fuselage 1 Cylinder 52.

Horizontal device 7 is additionally provided with reference picture 1 and Fig. 8 top boards 142, horizontal device 7 includes being vertically arranged in support Rack 71, top board 142 on post 12 are consolidated through the both ends of the axial direction of trunnion axis 73 and trunnion axis 73 set along its length Surely the gear 72 being engaged with rack 71 connected, during ensureing that top board 142 pushes by gear 72 and the pressing of rack 71 Levelness.

In the present embodiment, the first power part, the second power part, the 3rd power part and the 4th power part are motor, other Can be sprocket wheel chain structure, turbine and worm structure etc. in embodiment.

After pressing plate operation starts, start the first power part 24 and the second power part 263, by the angle for adjusting telescopic prop 21 The position of degree and first pressure compensation device 25 on telescopic prop 21 so that first pressure compensation device 25 reaches sheet material Lug boss, start first pressure compensation device 25 and local pressure compensation is carried out to lug boss, while start the He of the 3rd power part 343 4th power part 373 drives slipping column 33 to adjust position of the slipping column 33 on the width of fuselage 1 and driving the Two pressure compensators 36 are to adjust position of the second pressure compensation device 36 on slipping column 33 so that second pressure compensates Device 36 reaches the lower concave part of sheet material, starts second pressure compensation device 36 and carries out local pressure compensation to lower concave part, to reach The effect of local pressure compensation.Described above is only preferred embodiment of the present utility model, the scope of protection of the utility model Above-described embodiment is not limited merely to, all technical schemes belonged under the utility model thinking belong to protection of the present utility model Scope.It should be pointed out that for those skilled in the art, under the premise of the utility model principle is not departed from Some improvements and modifications, these improvements and modifications also should be regarded as the scope of protection of the utility model.

Claims (10)

1. a kind of trigger squeeze, including fuselage (1), lower platen (143) is fixedly connected with the fuselage (1), on the fuselage (1) Top board (142) is slidably connected, the hydraulic pressure that driving top board (142) vertically slides is provided with the fuselage (1) Cylinder (14), it is characterized in that：The first conveying arrangement (4) being provided with for transport sheet material, the machine are slided on the lower platen (143) The first driving means (45) of the first conveying arrangement of driving (4) sliding disengaging lower platen (143), the machine are additionally provided with body (1) Also be hinged with body (1) can horizontal sliding suction cup carrier (63), the suction cup carrier (63) be provided with can vertical lifting be used for inhale The sucker (65) of attached plate material.

2. trigger squeeze according to claim 1, it is characterized in that：The second chute is provided with the fuselage (1) in the width direction (44), both ends of first conveying arrangement (4) including length direction are slidably connected at the first transport in the second chute (44) Plate (41).

3. trigger squeeze according to claim 2, it is characterized in that：First conveying arrangement (4) also includes being rotatably connected on The first roller (42) rotated in first plate conveyor (41) around the first plate conveyor (41) length direction.

4. trigger squeeze according to claim 1, it is characterized in that：Away from the first driving on the width of the fuselage (1) One end of device (45), which is provided with, extends to the second conveying arrangement (5) that ground is used on transport sheet material to the first conveying arrangement (4).

5. trigger squeeze according to claim 4, it is characterized in that：Second conveying arrangement (5) includes being fixedly connected on machine The second plate conveyor (51) on body (1), it is rotatably connected to around the second plate conveyor (51) length side on second plate conveyor (51) To the second roller (52) of rotation.

6. trigger squeeze according to claim 1, it is characterized in that：It is provided with the fuselage (1) below lower platen (143) The slipping column (33) slid along fuselage (1) width, the slipping column (33) are provided with along slipping column straight up (33) the second pressure compensation device (36) that length direction slides.

7. trigger squeeze according to claim 6, it is characterized in that：Along width side on the length direction both ends of the fuselage (1) To provided with the first chute (31) below lower platen (143), both ends are slided on the length direction of the slipping column (33) It is connected in the first chute (31).

8. trigger squeeze according to claim 7, it is characterized in that：Second is provided with first chute (31) along its length Guide rail (32), the length direction both ends of the slipping column (33) are provided with the second pulley being slidably connected on the second guide rail (32) Component (34).

9. trigger squeeze according to claim 6, it is characterized in that：The upper wall of the slipping column (33) is provided with along its length 3rd guide rail (35), the second pressure compensation device (36) are provided with the 3rd assembly pulley being slidably connected on the 3rd guide rail (35) Part (37) and the second power part (263) for driving the 3rd pulley assembly (37).

10. trigger squeeze according to claim 1, it is characterized in that：Rack (71) is provided with vertically on the fuselage (1), it is described Horizontal on top board (142) to be provided with trunnion axis (73), the trunnion axis (73) is provided with the gear (72) with rack (71) pressing.