CN209794693U - Aircraft box folding device - Google Patents
Aircraft box folding device Download PDFInfo
- Publication number
- CN209794693U CN209794693U CN201920234900.0U CN201920234900U CN209794693U CN 209794693 U CN209794693 U CN 209794693U CN 201920234900 U CN201920234900 U CN 201920234900U CN 209794693 U CN209794693 U CN 209794693U
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- synchronous belt
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- 230000000712 assembly Effects 0.000 claims abstract description 17
- 238000000429 assembly Methods 0.000 claims abstract description 17
- 238000005096 rolling process Methods 0.000 claims abstract description 7
- 230000001360 synchronised effect Effects 0.000 claims description 90
- 230000003287 optical effect Effects 0.000 claims description 37
- 230000005540 biological transmission Effects 0.000 claims description 33
- 238000007493 shaping process Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 1
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Abstract
The utility model discloses an aircraft box folding device. The size of the folding box of the existing airplane box folding mechanism is fixed. The utility model realizes the X-direction opposite movement of two Y-axis adjusting components through the X-axis adjusting component, and adjusts the distance between the two Y-axis adjusting components to adapt to the size of the airplane box; then, synchronously driving a first sliding block of the two Y-axis adjusting assemblies to adjust in the Y direction, driving the movable elastic baffle to be far away from the fixed elastic baffle by the first sliding block, and adjusting until the distance between the movable elastic baffle and the fixed elastic baffle adapts to the size of the airplane box; then, the Z-axis pressing mechanism presses downwards, and the side face of the airplane box realizes folding action along the guide plates of the dynamic elastic baffle and the fixed elastic baffle; and finally, the elastic grabs of the two Y-axis adjusting assemblies synchronously complete the folding action of the top surface of the airplane box. The utility model discloses can realize the box action of rolling over of unidimensional aircraft box.
Description
Technical Field
The utility model belongs to the technical field of mechanical equipment, especially, relate to a novel aircraft box is folding device.
background
The size that current aircraft box folding mechanism folded the box is fixed, if will carry out the box of the not unidimensional aircraft box and roll over the box machine just must be changed the aircraft box of renewal, and cost is huge, and the function is realized singly, can not realize the not unidimensional aircraft box shaping problem through motor control. Therefore, it is extremely important to design a folding mechanism that can accommodate a variety of aircraft box sizes.
Disclosure of Invention
The utility model aims at providing an easy operation, the quick novel aircraft box folding device of adjustment to prior art not enough.
The purpose of the utility model can be realized through the following technical scheme:
the utility model discloses a mechanism is pushed down to X axle adjustment subassembly, Y axle adjustment subassembly and Z axle.
The X-axis adjusting assembly comprises a stepping motor I, a synchronous belt transmission mechanism II, an optical axis I and an X-axis driving block; a base of the first stepping motor is fixed on the frame; the synchronous belt transmission mechanism I consists of a synchronous belt I and two synchronous wheels I; one synchronizing wheel I is fixed on an output shaft of the stepping motor, and the other synchronizing wheel I is fixed on the transmission shaft; the two first synchronous wheels are connected through a first synchronous belt of the first synchronous belt transmission mechanism; the synchronous belt transmission mechanism II consists of a synchronous belt I and two synchronous wheels II; one second synchronizing wheel is fixed on the transmission shaft, and the other second synchronizing wheel is hinged on the rack; the two synchronous wheels II are connected through a synchronous belt I of a synchronous belt transmission mechanism II; the transmission shaft is supported on the frame through a rolling bearing; the two optical axes I are arranged in parallel and are fixed on the frame; each optical axis I is connected with the two X-axis driving blocks through sliding bearings; two X-axis driving blocks on one of the first optical shafts are respectively fixed with a top belt section and a bottom belt section of a first synchronous belt in the first synchronous belt transmission mechanism, and two X-axis driving blocks on the other of the first optical shafts are respectively fixed with a top belt section and a bottom belt section of a first synchronous belt in the second synchronous belt transmission mechanism.
The Y-axis adjusting assembly comprises a second stepping motor, a second synchronous wheel, a third synchronous wheel, a fourth synchronous wheel, a second synchronous belt, a linear guide rail, a first sliding block, a third stepping motor, a second optical axis, an elastic gripper, a fixed elastic baffle, a movable elastic baffle and a bearing seat; the base of the stepping motor II is fixed on a stepping motor base, and the stepping motor base is fixed on the linear guide rail; the third synchronizing wheel and the fourth synchronizing wheel are hinged with the frame; the synchronous wheel II, the synchronous wheel III and the synchronous wheel four-way are connected through a synchronous belt II; the first sliding block is arranged between the third synchronous wheel and the fourth synchronous wheel, is fixed with the second synchronous belt and forms a sliding pair with the linear guide rail; the fixed elastic baffle and the movable elastic baffle are both composed of an L-shaped plate and two guide plates which are integrally formed, and the tops of two arms of the L-shaped plate are respectively provided with one guide plate; one arm of the L-shaped plate of the fixed elastic baffle is fixed with the linear guide rail, and the other arm of the L-shaped plate of the fixed elastic baffle is towards the Z-axis pressing mechanism; one arm of the L-shaped plate of the dynamic elastic baffle is fixed with the first sliding block; the fixed elastic baffle and the movable elastic baffle are arranged in an aligned mode along the axial direction of the optical axis. A base of the third stepping motor is fixed on the linear guide rail, and an output shaft of the third stepping motor is connected with the second optical axis through a coupler; the second optical axis is supported on the bearing seat through a rolling bearing; the bottom of the elastic gripper is fixed with the second optical axis, and the top of the elastic gripper is freely arranged. Two Y-axis adjusting assemblies are arranged, and two ends of a linear guide rail of each Y-axis adjusting assembly are respectively fixed with two X-axis driving blocks which are aligned with different optical axes.
The Z-axis pressing mechanism comprises a speed reducing motor, a crank, a connecting rod and a second sliding block; the base of the speed reducing motor is fixed on the frame, and the output shaft of the speed reducing motor is fixed with one end of the crank; two ends of the connecting rod are respectively hinged with the other end of the crank and the second sliding block; the second sliding block and the machine frame form a sliding pair; the second sliding block is arranged between the two Y-axis adjusting assemblies and between the two optical axes I of the X-axis adjusting assemblies.
And a tension wheel hinged with the frame is arranged on the outer side of the synchronous belt II.
And the signal control ends of the first stepping motor, the second stepping motor, the third stepping motor and the speed reducing motor are connected with the controller.
Compared with the prior art, the utility model has the advantages of it is following:
The utility model discloses according to aircraft box parameter size, utilize controller control step motor drive hold-in range to drive the slider, the slider drives elastic baffle and then changes the size of a box, and through Z axle pushing down mechanism and the automatic folding cardboard shaping of deflector of fixed elastic baffle and dynamic elastic baffle 5, realize the novel folding operation of aircraft box, easy operation, it is convenient to adjust, stable durable, a tractor serves several purposes, extensive applicability; the structure is simple, and the daily maintenance and the use are convenient; compact size, light weight, and is suitable for families and Taobao merchants.
Drawings
FIG. 1 is a perspective view of the overall structure of the present invention;
FIG. 2 is a perspective view of the X-axis adjustment assembly of the present invention;
Fig. 3 is an assembly perspective view of the Y-axis adjusting assembly of the present invention.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings.
as shown in fig. 1, an airplane box folding device comprises an X-axis adjusting assembly, a Y-axis adjusting assembly and a Z-axis pressing mechanism.
As shown in fig. 1 and 2, the X-axis adjusting assembly includes a first stepping motor 11, a first synchronous belt transmission mechanism, a second synchronous belt transmission mechanism, a first optical axis 1 and an X-axis driving block 2; the base of the first stepping motor 11 is fixed on the frame 13; the synchronous belt transmission mechanism I consists of a synchronous belt I3 and two synchronous wheels I15; one synchronizing wheel I15 is fixed on an output shaft of the stepping motor 11, and the other synchronizing wheel I15 is fixed on a transmission shaft; the two synchronous wheels I15 are connected through a synchronous belt I3 of the synchronous belt transmission mechanism I; the synchronous belt transmission mechanism II consists of a synchronous belt I3 and two synchronous wheels II 16; one second synchronizing wheel 16 is fixed on the transmission shaft, and the other second synchronizing wheel 16 is hinged on the rack 13; the two second synchronous wheels 16 are connected through a first synchronous belt 3 of the second synchronous belt transmission mechanism; the transmission shaft is supported on the frame through a rolling bearing; the two optical axes I1 are arranged in parallel and are fixed on the frame; each optical axis I1 is connected with two X-axis driving blocks 2 through sliding bearings 12; two X-axis drive blocks on one of the optical axis I1 are fixed with a top belt section and a bottom belt section of a synchronous belt I in the synchronous belt transmission mechanism I respectively, and two X-axis drive blocks on the other optical axis I1 are fixed with the top belt section and the bottom belt section of the synchronous belt I in the synchronous belt transmission mechanism II respectively, namely when the synchronous belt I rotates, the two X-axis drive blocks on the same synchronous belt I move in opposite directions or back to back.
As shown in fig. 1 and 3, the Y-axis adjusting assembly includes a second stepping motor 20, a second synchronizing wheel 22, a third synchronizing wheel 23, a fourth synchronizing wheel 24, a second synchronizing belt 21, a linear guide rail 4, a first slider 17, a third stepping motor 25, a second optical axis 9, an elastic gripper 8, a fixed elastic baffle, a movable elastic baffle 5 and a bearing seat 7; the base of the second stepping motor 20 is fixed on the stepping motor base 19, and the stepping motor base 19 is fixed on the linear guide rail 4; a second synchronizing wheel 22 is fixed on an output shaft of the stepping motor 11, and a third synchronizing wheel 23 and a fourth synchronizing wheel 24 are hinged with the frame; the synchronous wheel II 22, the synchronous wheel III 23 and the synchronous wheel IV 24 are connected through a synchronous belt II 21; a tension wheel hinged with the frame is arranged on the outer side of the second synchronous belt 21; the first sliding block 17 is arranged between the third synchronous wheel 23 and the fourth synchronous wheel 24, is fixed with the second synchronous belt 21 and forms a sliding pair with the linear guide rail 4; the fixed elastic baffle and the dynamic elastic baffle 5 are respectively composed of an L-shaped plate and two guide plates which are integrally formed, and the tops of two arms of the L-shaped plate are respectively provided with one guide plate; one arm of the L-shaped plate of the fixed elastic baffle is fixed with the linear guide rail 4, and the other arm of the L-shaped plate of the fixed elastic baffle is towards the Z-axis pressing mechanism; one arm of the L-shaped plate of the dynamic elastic baffle 5 is fixed with the first sliding block 17; the fixed elastic baffle and the movable elastic baffle 5 are arranged in an aligned mode along the first optical axis 1 in the axial direction. A base of the third stepping motor 25 is fixed on the linear guide rail 4, and an output shaft of the third stepping motor 25 is connected with the second optical shaft 9 through a coupler; the second optical axis 9 is supported on the bearing seat 7 through a rolling bearing; the bottom of the elastic gripper 8 is fixed with the second optical axis 9, and the top of the elastic gripper is freely arranged. Two Y-axis adjusting assemblies are provided, and two ends of a linear guide rail 4 of each Y-axis adjusting assembly are respectively fixed with two X-axis driving blocks 2 which are aligned with the positions of the first optical axis 1.
the Z-axis pressing mechanism comprises a speed reducing motor 18, a crank 14, a connecting rod and a second sliding block 6; the base of the gear motor 18 is fixed on the frame, and the output shaft of the gear motor 18 is fixed with one end of the crank 14; two ends of the connecting rod are respectively hinged with the other end of the crank 14 and the second sliding block 6; the second sliding block 6 and the machine frame form a sliding pair; the second sliding block 6 is arranged between the two Y-axis adjusting assemblies and between the two optical axes I1 of the X-axis adjusting assemblies.
The signal control ends of the first stepping motor 11, the second stepping motor 20, the third stepping motor 25 and the speed reducing motor 18 are all connected with the controller 10.
The utility model discloses a theory of operation:
According to the size of the airplane box, a controller firstly drives a first stepping motor, the first stepping motor drives a first synchronous belt transmission mechanism and a first synchronous belt 3 of a second synchronous belt transmission mechanism to move synchronously, X-direction opposite movement of two Y-axis adjusting assemblies is achieved, and the distance between the two Y-axis adjusting assemblies is adjusted to be suitable for the size of the airplane box; then, synchronously driving the stepping motors II of the two Y-axis adjusting assemblies through the controller to realize synchronous adjustment of the slide blocks I17Y directions of the two Y-axis adjusting assemblies, and at the moment, driving the movable elastic baffle 5 to be far away from the fixed elastic baffle by the slide blocks I17 to adjust the distance between the movable elastic baffle 5 and the fixed elastic baffle to be suitable for the size of the airplane box; then, the airplane box is flatly placed on the movable elastic baffle 5 and the fixed elastic baffle, the speed reducing motor 18 is driven by the controller, the speed reducing motor 18 drives the second sliding block 6 to press down through the crank 14 and the connecting rod, and the side face of the airplane box realizes folding action along the guide plates of the movable elastic baffle 5 and the fixed elastic baffle. And finally, synchronously driving a third stepping motor 25 of the two Y-axis adjusting assemblies through the controller, driving an elastic gripper 8 by the third stepping motor 25 through a second optical axis 9, and synchronously completing the folding action of the top surface of the airplane box by the elastic grippers 8 of the two Y-axis adjusting assemblies to achieve the folding purpose of the airplane box. After the folding is finished, the controller drives the first stepping motor 11, the second stepping motor 20, the third stepping motor 25 and the speed reducing motor 18 to reset.
Claims (3)
1. The utility model provides an aircraft box folding device, includes that X axle adjusting part, Y axle adjusting part and Z axle push down the mechanism, its characterized in that:
The X-axis adjusting assembly comprises a stepping motor I, a synchronous belt transmission mechanism II, an optical axis I and an X-axis driving block; a base of the first stepping motor is fixed on the frame; the synchronous belt transmission mechanism I consists of a synchronous belt I and two synchronous wheels I; one synchronizing wheel I is fixed on an output shaft of the stepping motor, and the other synchronizing wheel I is fixed on the transmission shaft; the two first synchronous wheels are connected through a first synchronous belt of the first synchronous belt transmission mechanism; the synchronous belt transmission mechanism II consists of a synchronous belt I and two synchronous wheels II; one second synchronizing wheel is fixed on the transmission shaft, and the other second synchronizing wheel is hinged on the rack; the two synchronous wheels II are connected through a synchronous belt I of a synchronous belt transmission mechanism II; the transmission shaft is supported on the frame through a rolling bearing; the two optical axes I are arranged in parallel and are fixed on the frame; each optical axis I is connected with the two X-axis driving blocks through sliding bearings; two X-axis driving blocks on one of the first optical axes are respectively fixed with a top belt section and a bottom belt section of a first synchronous belt in a first synchronous belt transmission mechanism, and two X-axis driving blocks on the other of the first optical axes are respectively fixed with a top belt section and a bottom belt section of a first synchronous belt in a second synchronous belt transmission mechanism;
The Y-axis adjusting assembly comprises a second stepping motor, a second synchronous wheel, a third synchronous wheel, a fourth synchronous wheel, a second synchronous belt, a linear guide rail, a first sliding block, a third stepping motor, a second optical axis, an elastic gripper, a fixed elastic baffle, a movable elastic baffle and a bearing seat; the base of the stepping motor II is fixed on a stepping motor base, and the stepping motor base is fixed on the linear guide rail; the third synchronizing wheel and the fourth synchronizing wheel are hinged with the frame; the synchronous wheel II, the synchronous wheel III and the synchronous wheel four-way are connected through a synchronous belt II; the first sliding block is arranged between the third synchronous wheel and the fourth synchronous wheel, is fixed with the second synchronous belt and forms a sliding pair with the linear guide rail; the fixed elastic baffle and the movable elastic baffle are both composed of an L-shaped plate and two guide plates which are integrally formed, and the tops of two arms of the L-shaped plate are respectively provided with one guide plate; one arm of the L-shaped plate of the fixed elastic baffle is fixed with the linear guide rail, and the other arm of the L-shaped plate of the fixed elastic baffle is towards the Z-axis pressing mechanism; one arm of the L-shaped plate of the dynamic elastic baffle is fixed with the first sliding block; the fixed elastic baffle and the movable elastic baffle are arranged in an alignment manner along the axial direction of the optical axis; a base of the third stepping motor is fixed on the linear guide rail, and an output shaft of the third stepping motor is connected with the second optical axis through a coupler; the second optical axis is supported on the bearing seat through a rolling bearing; the bottom of the elastic gripper is fixed with the second optical axis, and the top of the elastic gripper is freely arranged; two Y-axis adjusting assemblies are arranged, and two ends of a linear guide rail of each Y-axis adjusting assembly are respectively fixed with two X-axis driving blocks which are aligned with the upper positions of different optical axes I;
the Z-axis pressing mechanism comprises a speed reducing motor, a crank, a connecting rod and a second sliding block; the base of the speed reducing motor is fixed on the frame, and the output shaft of the speed reducing motor is fixed with one end of the crank; two ends of the connecting rod are respectively hinged with the other end of the crank and the second sliding block; the second sliding block and the machine frame form a sliding pair; the second sliding block is arranged between the two Y-axis adjusting assemblies and between the two optical axes I of the X-axis adjusting assemblies.
2. an aircraft box folding apparatus according to claim 1, wherein: and a tension wheel hinged with the frame is arranged on the outer side of the synchronous belt II.
3. An aircraft box folding apparatus according to claim 1 or 2, wherein: and the signal control ends of the first stepping motor, the second stepping motor, the third stepping motor and the speed reducing motor are connected with the controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920234900.0U CN209794693U (en) | 2019-02-25 | 2019-02-25 | Aircraft box folding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920234900.0U CN209794693U (en) | 2019-02-25 | 2019-02-25 | Aircraft box folding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209794693U true CN209794693U (en) | 2019-12-17 |
Family
ID=68822773
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920234900.0U Active CN209794693U (en) | 2019-02-25 | 2019-02-25 | Aircraft box folding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209794693U (en) |
-
2019
- 2019-02-25 CN CN201920234900.0U patent/CN209794693U/en active Active
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