CN217415038U - Forming mechanism of paper case folding machine of airplane - Google Patents

Forming mechanism of paper case folding machine of airplane Download PDF

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Publication number
CN217415038U
CN217415038U CN202220752751.9U CN202220752751U CN217415038U CN 217415038 U CN217415038 U CN 217415038U CN 202220752751 U CN202220752751 U CN 202220752751U CN 217415038 U CN217415038 U CN 217415038U
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China
Prior art keywords
baffle
forming
airplane
shell
forming mechanism
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CN202220752751.9U
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Chinese (zh)
Inventor
王莹
曾学龙
杨东杰
王宏亮
董杰
李敏
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Gree Electric Appliances Inc of Zhuhai
Gree Hefei Electric Appliances Co Ltd
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Gree Electric Appliances Inc of Zhuhai
Gree Hefei Electric Appliances Co Ltd
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Priority to CN202220752751.9U priority Critical patent/CN217415038U/en
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Abstract

The utility model provides a roll over aircraft paper case machine forming mechanism, includes the kerve, forming device, removes adjusting device, translation mechanism, the kerve constitute by first baffle and second baffle, first baffle with second baffle inboard be provided with the guide rail, remove adjusting device with first baffle or the second baffle connect, forming device be located the kerve top, with be located the kerve below translation mechanism connects. The utility model has the advantages of prevent that aircraft shell side arch from buckling not in place and prevent that the aircraft shell from rising along with the function that the anchor clamps raised, improved product quality and production efficiency.

Description

Forming mechanism of paper case folding machine of airplane
Technical Field
The utility model relates to a packing carton technical field, especially a roll over aircraft paper case machine forming mechanism.
Background
The aircraft paper shell is formed by folding, bending and enclosing a plurality of surfaces. The packaging of articles is now performed in factories by using aircraft paper shells, and there are common: aircraft casings, quadrilateral boxes, profile boxes, and the like. Currently aircraft enclosures are made by manual folding. The labor intensity of workers is high, and the working efficiency is low. In the forming stage of the airplane shell, the forming is often incomplete, the side edge of the airplane shell is provided with a bulge, and the bulge needs to be buckled into a paper shell bottom plate of the airplane. The incomplete molding of the side panel of the aircraft shell has become a problem to be solved urgently.
SUMMERY OF THE UTILITY MODEL
The utility model provides a roll over aircraft paper case machine forming mechanism has solved one or more of prior art problem.
The utility model provides a technical scheme that its technical problem adopted is: the utility model provides a roll over aircraft paper case machine forming mechanism, includes the kerve, forming device, removes adjusting device, translation mechanism, the kerve constitute by first baffle and second baffle, first baffle with second baffle inboard be provided with the guide rail, remove adjusting device with first baffle or the second baffle connect, forming device be located the kerve top, with be located the kerve below translation mechanism connects.
As a further improvement of the utility model: the movable adjusting device is a movable adjusting plate which is provided with a vertical guide groove and a plurality of clamping through holes.
As a further improvement of the utility model: the forming device comprises a side forming rod, a prepressing device and a first driving device, wherein the side forming rod is fixed in the middle of the prepressing device, and the prepressing device is connected with the first driving device.
As a further improvement of the utility model: the prepressing device is at least two prepressing plates.
As a further improvement of the utility model: one end of the side forming rod is provided with a lateral pressure groove.
As a further improvement of the utility model: the first baffle or the second baffle is provided with a buckle matched with the clamping through hole.
As a further improvement of the utility model: the translation mechanism comprises a horizontal screw rod, a second driving device, a clamp and a sucker, one end of the second driving device is connected with the horizontal screw rod, the other end of the second driving device is connected with the bottom of the clamp, and the top of the clamp is connected with the sucker.
As a further improvement of the utility model: the first driving device is a first driving cylinder
As a further improvement of the utility model: the second driving device is a second driving cylinder.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model provides a roll over aircraft paper case machine forming mechanism, through increasing the removal regulating block, can reach and adjust its high advantage that satisfies the side push pedal and accomplish aircraft shell side preflex, increase the design of side direction indent through flying shell side shaping pole simultaneously, guarantee fly the protruding card of shell side and go into in the kerve, and aircraft shell shaping district translation mechanism anchor clamps increase two sucker structure, can increase the power of vertical direction, reach and prevent that the aircraft shell from following the effect that the cylinder moved upwards.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic side view of the present invention.
Fig. 3 is a schematic sectional view of the present invention.
Fig. 4 is a schematic structural view of the mobile adjusting device of the present invention.
Description of the reference numerals: 1. a bottom groove; 11. a first baffle plate; 12. a second baffle; 13. a guide rail; 2. a molding device; 21. a side molding rod; 211. lateral pressure grooves; 22. a pre-pressing device; 221. pre-pressing a plate; 23. a first driving device; 3. moving the adjusting device; 31. a vertical guide groove; 32. a through hole; 4. a translation mechanism; 41. a horizontal screw rod; 42. a second driving device; 43. a clamp; 44. and (4) sucking discs.
Detailed Description
To make the purpose, technical solution and advantages of the present invention clearer, the following will combine the embodiments of the present invention and the corresponding drawings to clearly and completely describe the technical solution of the present invention. It is to be understood that the embodiments described are only some embodiments of the invention, and not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
It should be noted that the terms "first," "second," and the like in the description and claims of the present invention and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used is interchangeable under appropriate circumstances such that the embodiments of the invention described herein are capable of operation in sequences other than those illustrated or otherwise described herein. Furthermore, the terms "comprising" and "having," as well as any variations thereof, are intended to cover non-exclusive inclusions:
the utility model provides a roll over aircraft paper case machine forming mechanism, includes kerve, forming device, removal adjusting device, translation mechanism, the kerve constitute by first baffle and second baffle, first baffle with second baffle inboard be provided with the guide rail, removal adjusting device with first baffle or the second baffle connect, forming device be located the kerve top, with be located the kerve below translation mechanism connects.
The movable adjusting device is a movable adjusting plate which is provided with a vertical guide groove and a plurality of clamping through holes.
The forming mechanism comprises a side forming rod, a prepressing device and a first driving device, wherein the side forming rod is fixed in the middle of the prepressing device, and the prepressing device is connected with the first driving device.
The prepressing device is at least two prepressing plates.
One end of the side forming rod is provided with a lateral pressure groove.
The first baffle or the second baffle is provided with a buckle matched with the clamping through hole.
The translation mechanism comprises a horizontal screw rod, a second driving device, a clamp and a sucker, one end of the second driving device is connected with the horizontal screw rod, the other end of the second driving device is connected with the bottom of the clamp, and the top of the clamp is connected with the sucker.
The first driving device is a first driving cylinder
The second driving device is a second driving cylinder.
The utility model provides a roll over aircraft paper case machine forming mechanism, through increasing the removal regulating block, can reach and adjust its high advantage that satisfies the side push pedal and accomplish aircraft shell side preflex, increase the design of side direction indent through flying shell side shaping pole simultaneously, guarantee fly the protruding card of shell side and go into in the kerve, and aircraft shell shaping district translation mechanism anchor clamps increase two sucker structure, can increase the power of vertical direction, reach and prevent that the aircraft shell from following the effect that the cylinder moved upwards.
The utility model discloses a detailed description:
the utility model provides a roll over aircraft paper case machine forming mechanism, includes kerve 1, forming device 2, removes adjusting device 3, translation mechanism 4, kerve 1 constitute by first baffle 11 and second baffle 12, first baffle 11 with second baffle 12 inboard be provided with the guide rail, remove adjusting device 3 with first baffle 11 or second baffle 12 connect, forming device 2 be located kerve 1 top, with be located kerve 1 below translation mechanism 4 connects.
The movable adjusting device 3 is a movable adjusting plate, and the movable adjusting plate is provided with a vertical guide groove 31 and a plurality of clamping through holes 32.
The forming device 2 comprises a side forming rod 21, a prepressing device 22 and a first driving device 23, wherein the side forming rod 21 is fixed in the middle of the prepressing device 22, and the prepressing device 22 is connected with the first driving device 23.
The prepressing device 22 is at least two prepressing plates 221.
One end of the side forming rod 21 is provided with a lateral pressing groove 211.
The first baffle 11 or the second baffle 12 is provided with a buckle matched with the clamping through hole.
The translation mechanism 4 comprises a horizontal screw rod 41, a second driving device 42, a clamp 43 and a sucker 44, wherein one end of the second driving device 42 is connected with the horizontal screw rod 41, the other end of the second driving device 42 is connected with the bottom of the clamp 43, and the top of the clamp 43 is connected with the sucker 44.
The first driving device 23 is a first driving cylinder.
The second driving device 42 is a second driving cylinder.
The utility model discloses a theory of operation: a paper case folding machine forming mechanism is additionally provided with a movable adjusting plate, and the movable adjusting plate can be manually adjusted in the vertical direction. The pre-pressing device 22 is close to the airplane shell under the action of the air cylinder and pre-presses the side edge of the airplane shell. After the side plates reach the designated positions, the air cylinders operate, the forming rods 21 on the side edges of the airplane shell move circumferentially, and the side plates of the airplane shell are pre-pressed again. The cylinder operates, and the whole mechanism operates back to the airplane paper shell, so that the side edge of the airplane shell is protruded to be pressed into the bottom shell, and the forming is successful.
In the horizontal direction, the folded aircraft shell moves from the press-fitting station to the molding station, and the cylinder on the bottom plate ensures that the aircraft shell cannot be lifted along with the lifting of the clamp 43.
The implementation case is as follows:
in connection with the figures 1-4,
the plane shell folding machine is a machine for fully automatically bending a flat plane shell into a formed plane shell. The device consists of a lifting mechanism, a translation mechanism, a forming mechanism and a main body frame.
What this scheme mainly said is that roll over regional mechanism design of aircraft shell machine shaping, a roll over aircraft paper shell machine forming mechanism, includes kerve 1, forming device 2, remove adjusting device 3, translation mechanism 4, kerve 1 constitute by first baffle 11 and second baffle 12, first baffle 11 with second baffle 12 inboard be provided with guide rail 13, removal adjusting device 3 with first baffle 11 or second baffle 12 connect, forming device 2 be located kerve 1 top, with be located kerve 1 below translation mechanism 4 connects.
The movable adjusting device 3 is a movable adjusting plate which is provided with a vertical guide groove 31 and a plurality of clamping through holes 32, the movable adjusting plate is added, the movable adjusting plate can be manually adjusted in the vertical direction, and the requirement of the height of the movable adjusting plate on side push plates is met to complete the side pre-bending of the airplane shell.
The first baffle 11 and the second baffle 12 form a bottom groove 1, and the bottom groove 1 for placing the aircraft shell can be formed because guide rails are arranged on the inner sides of the first baffle 11 and the second baffle 12.
Forming device 2 includes side shaping pole 21, pre-compaction device 22, first drive arrangement 23, side shaping pole 21 fix pre-compaction device 22 in the middle of, pre-compaction device 22 with first drive arrangement 23 connect, 21 one end of side shaping pole be equipped with the side direction indent, aircraft shell side shaping pole 21 increases the design of side direction indent, ensures that aircraft shell side arch card goes into the kerve 1.
Translation mechanism 4 include horizontal lead screw 41, second drive arrangement 42, anchor clamps 43, sucking disc 44, second drive arrangement 42 one end with horizontal lead screw 41 connect, the other end with anchor clamps 43 bottom connect, anchor clamps 43 top be connected with sucking disc 44, aircraft shell shaping district translation mechanism anchor clamps 43 increase two sucking disc 44 structures, increase the power of vertical direction, prevent that the aircraft shell from following the cylinder and upwards moving.
In the horizontal direction, the folded aircraft shell moves from the press-fitting station to the molding station, and the two cylinders on the bottom plate ensure that the aircraft shell cannot be lifted along with the lifting of the clamp 43.
The specific implementation mode is as follows:
the prepressing device 22 is close to the airplane shell under the action of the cylinder to prepress the side edge of the airplane shell. And after the airplane arrives at the designated position, the second air cylinder operates, the forming rod 21 on the side edge of the airplane shell moves circumferentially, and the side plate of the airplane shell is pre-pressed again. And the cylinder III operates, the integral mechanism operates back to the airplane paper shell, and the side edge of the airplane shell is protruded to be pressed into the bottom shell, so that the forming is successful.
The method comprises the following steps: the aircraft housing clamp 43 is depressed.
Step two: and forming the side edge of the airplane shell.
Step three: the horizontal screw 41 is operated, and the suction cup 44 sucks the aircraft shell and moves the whole to the forming station.
Step four: the first cylinder is operated, the whole body is operated towards the inner side, and the side edge of the airplane shell is preformed.
Step five: the second cylinder operates, the forming rod 21 on the side edge of the airplane shell does circular motion, and the side edge of the airplane shell is pre-pressed.
Step six: and the third cylinder operates, and the side edge of the airplane shell is protruded and pressed into the shell, so that the airplane is completely molded.
The utility model discloses a main function: a forming mechanism of an airplane paper shell folding machine has the functions of preventing the lateral edge of an airplane shell from being bent incompletely in a protruding mode and preventing the airplane shell from rising along with a rising clamp 43.
In conclusion, after the ordinary skilled in the art reads the document of the present invention, according to the present invention, the technical solution and technical concept of the present invention do not need creative mental labor to make other various corresponding transformation schemes, which all belong to the protection scope of the present invention.

Claims (9)

1. A forming mechanism of a paper shell folding machine of an airplane is characterized by comprising a bottom groove, a forming device, a moving adjusting device and a translation mechanism, wherein the bottom groove is composed of a first baffle and a second baffle, guide rails are arranged on the inner sides of the first baffle and the second baffle, the moving adjusting device is connected with the first baffle or the second baffle, and the forming device is located above the bottom groove and connected with the translation mechanism located below the bottom groove.
2. The forming mechanism of a paper folding machine for an airplane as claimed in claim 1, wherein: the movable adjusting device is a movable adjusting plate which is provided with a vertical guide groove and a plurality of clamping through holes.
3. The forming mechanism of a paper folding machine for an airplane as claimed in claim 1, wherein: the forming device comprises a side forming rod, a prepressing device and a first driving device, wherein the side forming rod is fixed in the middle of the prepressing device, and the prepressing device is connected with the first driving device.
4. A folding aircraft paper shell machine forming mechanism as claimed in claim 3, characterized in that: the prepressing device is at least two prepressing plates.
5. A folding aircraft paper shell machine forming mechanism as claimed in claim 3, characterized in that: one end of the side forming rod is provided with a lateral pressure groove.
6. A forming mechanism for a folding airplane paper case machine according to claim 2, characterized in that: the first baffle or the second baffle is provided with a buckle matched with the clamping through hole.
7. The forming mechanism of a paper folding machine for an airplane as claimed in claim 1, wherein: the translation mechanism comprises a horizontal screw rod, a second driving device, a clamp and a sucker, one end of the second driving device is connected with the horizontal screw rod, the other end of the second driving device is connected with the bottom of the clamp, and the top of the clamp is connected with the sucker.
8. The forming mechanism of a paper folding airplane shell machine as claimed in any one of claims 3 to 5, wherein: the first driving device is a first driving cylinder.
9. The forming mechanism of a paper folding machine for an airplane as claimed in claim 7, wherein: the second driving device is a second driving cylinder.
CN202220752751.9U 2022-04-02 2022-04-02 Forming mechanism of paper case folding machine of airplane Active CN217415038U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220752751.9U CN217415038U (en) 2022-04-02 2022-04-02 Forming mechanism of paper case folding machine of airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220752751.9U CN217415038U (en) 2022-04-02 2022-04-02 Forming mechanism of paper case folding machine of airplane

Publications (1)

Publication Number Publication Date
CN217415038U true CN217415038U (en) 2022-09-13

Family

ID=83180682

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220752751.9U Active CN217415038U (en) 2022-04-02 2022-04-02 Forming mechanism of paper case folding machine of airplane

Country Status (1)

Country Link
CN (1) CN217415038U (en)

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