CN113320742B - Aircraft box sealing equipment - Google Patents
Aircraft box sealing equipment Download PDFInfo
- Publication number
- CN113320742B CN113320742B CN202110648120.2A CN202110648120A CN113320742B CN 113320742 B CN113320742 B CN 113320742B CN 202110648120 A CN202110648120 A CN 202110648120A CN 113320742 B CN113320742 B CN 113320742B
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- China
- Prior art keywords
- top cover
- plate
- tongue
- assembly
- folding
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65B—MACHINES, APPARATUS OR DEVICES FOR, OR METHODS OF, PACKAGING ARTICLES OR MATERIALS; UNPACKING
- B65B35/00—Supplying, feeding, arranging or orientating articles to be packaged
- B65B35/10—Feeding, e.g. conveying, single articles
- B65B35/24—Feeding, e.g. conveying, single articles by endless belts or chains
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65B—MACHINES, APPARATUS OR DEVICES FOR, OR METHODS OF, PACKAGING ARTICLES OR MATERIALS; UNPACKING
- B65B57/00—Automatic control, checking, warning, or safety devices
- B65B57/02—Automatic control, checking, warning, or safety devices responsive to absence, presence, abnormal feed, or misplacement of binding or wrapping material, containers, or packages
- B65B57/04—Automatic control, checking, warning, or safety devices responsive to absence, presence, abnormal feed, or misplacement of binding or wrapping material, containers, or packages and operating to control, or to stop, the feed of such material, containers, or packages
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65B—MACHINES, APPARATUS OR DEVICES FOR, OR METHODS OF, PACKAGING ARTICLES OR MATERIALS; UNPACKING
- B65B7/00—Closing containers or receptacles after filling
- B65B7/16—Closing semi-rigid or rigid containers or receptacles not deformed by, or not taking-up shape of, contents, e.g. boxes or cartons
- B65B7/20—Closing semi-rigid or rigid containers or receptacles not deformed by, or not taking-up shape of, contents, e.g. boxes or cartons by folding-down preformed flaps
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65B—MACHINES, APPARATUS OR DEVICES FOR, OR METHODS OF, PACKAGING ARTICLES OR MATERIALS; UNPACKING
- B65B7/00—Closing containers or receptacles after filling
- B65B7/16—Closing semi-rigid or rigid containers or receptacles not deformed by, or not taking-up shape of, contents, e.g. boxes or cartons
- B65B7/26—Closing semi-rigid or rigid containers or receptacles not deformed by, or not taking-up shape of, contents, e.g. boxes or cartons by closing hinged lids
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65G—TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
- B65G15/00—Conveyors having endless load-conveying surfaces, i.e. belts and like continuous members, to which tractive effort is transmitted by means other than endless driving elements of similar configuration
- B65G15/30—Belts or like endless load-carriers
- B65G15/58—Belts or like endless load-carriers with means for holding or retaining the loads in fixed position, e.g. magnetic
Abstract
The invention relates to the technical field of airplane box packaging, and discloses airplane box sealing equipment. The airplane box sealing equipment is used for assembling a top cover component of an airplane box into a bottom box, the top cover component comprises a top cover, a top cover side wing, a tongue plate and a tongue side wing, the airplane box sealing equipment comprises a conveying device and a box sealing device, and the conveying device is used for bearing and conveying the airplane box; the box sealing device comprises a bracket component, a top cover flank folding component, a top cover supporting component, a tongue flank folding component and a tongue folding component, wherein the top cover flank folding component, the top cover supporting component, the tongue flank folding component and the tongue folding component are arranged on the bracket component; the conveying device is configured to convey the airplane box into the box sealing device; a cap side flap assembly configured to flap the cap side flap; the top cover supporting component is used for supporting the top cover when the top cover flank folding component folds the top cover flank; the top cover folding assembly is used for folding the top cover to the bottom box; the tongue side wing folding component is used for folding the tongue side wing; the tongue folding assembly is used for folding the tongue plate and the tongue side wings into the bottom box.
Description
Technical Field
The invention relates to the technical field of airplane box packaging, in particular to airplane box packaging equipment.
Background
The airplane box packaging has the advantages of low cost and good protection effect on products, and is widely applied to product packaging. In the industry at present, the automation operation is realized in the box opening process of the airplane box, but the box sealing action of the airplane box adopts manual box sealing, the tongue side wing is firstly turned over by 90 degrees relative to the top cover manually, then the top cover is turned over to the bottom box, then the tongue plate and the tongue side wing are turned over, and the tongue side wing is inserted into the bottom box after being turned over, so that the box sealing operation of the airplane box is realized. The manual mode production efficiency is low, and is with high costs, and the quality uncertainty is high.
Based on this, there is a need for an aircraft box sealing device to solve the above existing problems.
Disclosure of Invention
Based on the above, the invention aims to provide the airplane box sealing equipment, which realizes automatic box sealing of the airplane box, saves labor cost, improves production efficiency and improves product quality.
In order to achieve the purpose, the invention adopts the following technical scheme:
an aircraft box closure apparatus for fitting a canopy assembly of an aircraft box into a base box, the canopy assembly including a canopy, a canopy side wing, a tongue plate and a tongue side wing, the aircraft box closure apparatus comprising:
a conveyor for carrying and conveying the aircraft box;
the box sealing device comprises a bracket component, a top cover flank turnover component, a top cover supporting component, a tongue flank turnover component and a tongue turnover component, wherein the top cover flank turnover component, the top cover supporting component, the tongue flank turnover component and the tongue turnover component are arranged on the bracket component;
the conveying device is configured to convey the airplane box into the box sealing device;
the top cover side flap assembly is configured to flap the top cover side flaps;
the top cover support assembly is configured to support the top cover when the top cover side flap assembly flaps the top cover side flaps;
the top cover folding assembly is configured to fold the top cover onto the bottom case;
the tongue side flap assembly is configured to flap the tongue side flap;
the tongue folding assembly is configured to fold the tongue plate and the tongue side wings into the base box.
As a preferred technical scheme of the airplane box sealing equipment, the conveying device comprises a conveying belt and a first driving piece, a plurality of groups of positioning ridges are arranged on the conveying belt at intervals, and the airplane box is arranged on the positioning ridges;
the first drive is configured to drive the conveyor belt to transport the aircraft box.
As an optimal technical scheme of aircraft box sealing equipment, top cap flank turns over a subassembly and includes first cylinder and the first folded plate that turns over, first cylinder set up in on the bracket component, the first folded plate install in the output of first cylinder, the drive of first cylinder the first folded plate is flexible, in order to drive the top cap flank is relative the top cap turns over the book.
As an optimal technical scheme of the aircraft box sealing device, the support assembly comprises a first connecting plate and a first supporting rod, the top cover side wing turnover assembly is installed on the first connecting plate, and the first connecting plate is slidably installed on the first supporting rod to adjust the height of the top cover side wing turnover assembly.
As a preferred technical scheme of an aircraft box sealing device, the top cover supporting assembly comprises a first driving part and a supporting plate, the first driving part comprises a fixed frame, a second cylinder, a transmission plate and a connecting plate, the fixed frame is mounted on the bracket assembly, the second cylinder is fixed on the fixed frame, the transmission plate is mounted at the output end of the second cylinder, the transmission plate is connected to the fixed frame in a sliding manner, the connecting plate is hinged to the fixed frame, a first end of the connecting plate is fixed to the transmission plate, and a second end of the connecting plate is fixed to the supporting plate;
when the top cover side wing folding component folds the top cover side wing, the second cylinder drives the first end of the connecting plate to move through the transmission plate, so that the supporting plate supports the inner wall of the top cover.
As an optimal technical scheme of the airplane box sealing equipment, the top cover turnover assembly comprises a second turnover plate and a rotary cylinder, the rotary cylinder is installed on the support assembly, the second turnover plate is fixed at the output end of the rotary cylinder, the second turnover plate is located on the outer side of the top cover, and the rotary cylinder drives the second turnover plate to rotate, so that the second turnover plate turns over the top cover to the bottom box.
As a preferred technical scheme of an aircraft box sealing device, the tongue folding assembly includes:
a tongue depression member configured to fold the tongue plate by a preset angle;
a tongue advancement member configured to advance the tongue plate at the predetermined angle into the chassis.
As a preferred technical scheme of the airplane box sealing equipment, the bracket assembly comprises a top plate, a third cylinder, a second connecting plate and a second supporting rod, wherein the top plate is arranged at the top end of the second supporting rod;
the third cylinder is arranged on the top plate, the second connecting plate is slidably mounted on the second supporting rod, the second connecting plate is connected to the output end of the third cylinder, and the third cylinder is configured to drive the second connecting plate to lift;
the tongue flank turnover assembly comprises a second driving part and a third turnover plate, the second driving part is installed on the second connecting plate, the second driving part is in transmission connection with the third turnover plate, and the second driving part is configured to drive the third turnover plate to turn over the tongue flank.
As an optimal technical scheme of the airplane box sealing equipment, the tongue pressing part comprises a fourth cylinder and a fourth turnover plate, the fourth cylinder is arranged at the bottom of the second connecting plate, and the fourth turnover plate is arranged at the output end of the fourth cylinder.
As a preferred technical solution of the aircraft box sealing device, the box sealing device further includes a tongue support assembly, the tongue support assembly includes a fifth cylinder and a tongue support plate, the fifth cylinder is mounted on the bracket assembly, the tongue support plate is mounted at an output end of the fifth cylinder, and the fifth cylinder can drive the tongue support plate to move up and down, so that the tongue support plate supports a joint portion between the tongue plate and the top cover.
The beneficial effects of the invention are as follows:
when the airplane box sealing device works, an unpackaged airplane box is placed on the conveying device, and the top cover, the top cover side wings, the tongue plate and the tongue side wings of the airplane box are all in the same plane and are all perpendicular to the bottom box of the airplane box. When the conveying device conveys the airplane box to be sealed to the box sealing device, the top cover supporting assembly supports the top cover, and then the top cover side wing folding assembly folds the top cover side wing; and after the top cover side wings are turned over, the support of the top cover support assembly is removed, the top cover is turned over to the bottom box by the top cover turning-over assembly, in the process, the top cover side wings are guided by the top cover side wing turning-over assembly, then the tongue side wings are turned over by the tongue side wing turning-over assembly, finally the tongue plate is turned over by the tongue turning-over assembly, and the tongue side wings are turned over into the bottom box. This aircraft box seals box equipment has realized that the automation of aircraft box seals the box, the cost of using manpower sparingly improves production efficiency, has improved the product quality.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings used in the description of the embodiments of the present invention will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the contents of the embodiments of the present invention and the drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an aircraft box sealing device according to an embodiment of the present invention;
FIG. 2 is a schematic structural diagram of an aircraft case provided by an embodiment of the invention;
FIG. 3 is a schematic diagram of a first perspective of a delivery device according to an embodiment of the present invention;
FIG. 4 is a schematic diagram of a second perspective of a delivery device according to an embodiment of the present invention;
FIG. 5 is an enlarged view of FIG. 1 at A;
FIG. 6 is a schematic structural view of a canopy support assembly provided in accordance with an embodiment of the present invention;
fig. 7 is an enlarged view of fig. 4 at B.
The figures are labeled as follows:
10. an aircraft box; 101. a cap assembly; 1011. a top cover; 1012. a top cover flank; 1013. a tongue plate; 1014. a tongue flank; 102. a bottom case;
1. a conveying device; 11. a conveyor belt; 111. positioning ridges; 12. a first driving member;
2. a box sealing device;
21. a bracket assembly; 211. a first connecting plate; 212. a first support bar; 213. a top plate; 214. a third cylinder; 215. a second connecting plate; 216. a second support bar; 217. a third connecting plate;
22. a top cover side wing folding component; 221. a first cylinder; 222. a first flap plate;
23. a top cover turnover assembly; 231. a second flap plate; 232. a rotating cylinder;
24. a top cover support assembly; 241. a first drive member; 2411. a fixed mount; 2412. a second cylinder; 2413. a drive plate; 2414. a connecting plate; 242. a support plate;
25. a tongue side wing folding component; 251. a second drive member; 252. a third flap plate;
26. a tongue turnover assembly; 261. a tongue depressing member; 2611. a fourth cylinder; 2612. a fourth flap plate; 262. a tongue forward-pushing member; 2621. a sixth cylinder; 2622. a front push plate;
27. a tongue support assembly; 271. a fifth cylinder; 272. a tongue support plate.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not limiting of the invention. It should be further noted that, for the convenience of description, only some structures related to the present invention are shown in the drawings, not all of them.
In the description of the present invention, unless expressly stated or limited otherwise, the terms "connected," "connected," and "fixed" are to be construed broadly, e.g., as meaning permanently connected, removably connected, or integral to one another; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature "on," "above" and "over" the second feature may include the first feature being directly above and obliquely above the second feature, or simply indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
In the description of the present embodiment, the terms "upper", "lower", "left", "right", and the like are used based on the orientations and positional relationships shown in the drawings, and are only for convenience of description and simplicity of operation, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used only for descriptive purposes and are not intended to be limiting.
The airplane box packaging is low in cost, good in product protection and widely applied to product packaging. In the current industry, the automatic operation is realized in the box opening process of the airplane box, but the box sealing action of the airplane box adopts manual box sealing, the tongue flank is firstly turned over by 90 degrees relative to the top cover manually, then the top cover is turned over to the bottom box, then the tongue plate and the tongue flank are turned over, and the tongue flank is turned over and then inserted into the bottom box, so that the box sealing operation of the airplane box is realized. The manual mode production efficiency is low, and is with high costs, and the quality uncertainty is high.
In order to solve the above problem, as shown in fig. 1 to 7, the present embodiment provides an aircraft box sealing device for assembling a top cover assembly 101 of an aircraft box 10 into a bottom box 102, the aircraft box sealing device includes a conveying device 1 and a box sealing device 2, the box sealing device 2 includes a bracket assembly 21 and a top cover side flap assembly 22, a top cover flap assembly 23, a top cover support assembly 24, a tongue side flap assembly 25 and a tongue flap assembly 26 mounted on the bracket assembly 21.
Specifically, as shown in fig. 1-4, the top cover assembly 101 includes a top cover 1011, a top cover flap 1012, a tongue plate 1013, and a tongue flap 1014, and in the unsealed state, the top cover assembly 101 is disposed at a 90 ° angle to the bottom box 102. The conveying device 1 is configured to convey the aircraft box 10 into the box sealing device 2; the top cap side flap assembly 22 is configured to flap the top cap side flaps 1012; the top cover support assembly 24 is configured to support the top cover 1011 when the top cover flap folding assembly 22 folds the top cover flaps 1012; the top cover folding assembly 23 is configured to fold the top cover 1011 onto the back box 102; tongue side flap assembly 25 is configured to flap tongue side flap 1014; the tongue turnover assembly 26 is configured to fold the tongue plate 1013 and tongue flank 1014 into the back box 102.
In operation, the unpackaged aircraft box 10 is first placed on the conveyor 1, and at this time, the top cover 1011, the top cover wing 1012, the tongue plate 1013, and the tongue wing 1014 of the aircraft box 10 are all in the same plane and are all perpendicular to the bottom box 102 of the aircraft box 10. When the conveying device 1 conveys the airplane box 10 to be sealed to the box sealing device 2, the top cover supporting component 24 supports the top cover 1011, then the top cover side wing folding component 22 folds the top cover side wing 1012, and due to the support of the top cover supporting component 24, when the top cover side wing 1012 is prevented from being folded, the top cover 1011 shakes against the folding force of the top cover side wing folding component 22, so that poor packaging is generated; after the top cover side wings 1012 are turned over, the support of the top cover support assembly 24 is removed, the top cover turning assembly 23 turns over the top cover 1011 to the bottom case 102, and in the process, the top cover side wing turning assemblies 22 play a guiding role on the top cover side wings 1012; tongue flap flip assembly 25 then flips tongue flap 1014, and finally tongue flip assembly 26 flips tongue plate 1013 and inserts tongue flap 1014 into bottom box 102. This aircraft box seals box equipment has realized the automation of aircraft box 10 and has sealed the box, the cost of using manpower sparingly improves production efficiency, has improved the product quality.
Preferably, as shown in fig. 1 and 5, the conveying device 1 includes a conveyor belt 11 and a first driving member 12, a plurality of sets of positioning ridges 111 are arranged on the conveyor belt 11 at intervals, and the aircraft box 10 is mounted on the positioning ridges 111; the first drive 12 is configured to drive the conveyor belt 11 to transport the aircraft box 10. In this embodiment, the first driving element 12 is a motor, and the positioning ridge 111 is arranged, so that on one hand, the fixation of the aircraft box 10 is realized, and the conveying stability of the aircraft box 10 is improved; on the other hand, the spaces among the plurality of aircraft boxes 10 on the conveying device 1 are kept consistent, the conveying device 1 is favorable for being matched with an electric control device to convey the aircraft boxes 10 to the designated positions, and the position adjustment of the aircraft boxes 10 is facilitated. The conveyor belt 11 is controlled by a PLC or an upper computer, so that each aircraft box 10 can be accurately conveyed into the box sealing device 2 without position deviation.
Further, as shown in fig. 2 and 3, the top cover side flap folding assembly 22 includes a first cylinder 221 and a first folding plate 222, the first cylinder 221 is disposed on the bracket assembly 21, the first folding plate 222 is mounted at an output end of the first cylinder 221, and the first cylinder 221 drives the first folding plate 222 to extend and retract so as to drive the top cover side flap 1012 to fold 90 ° relative to the top cover 1011. In this embodiment, the two top cover side flap assemblies 22 are provided in two sets, and are respectively matched with the two top cover side flaps 1012. Preferably, the bracket assembly 21 includes a first connecting plate 211 and a first supporting rod 212, the top cover side flap assembly 22 is installed on the first connecting plate 211, and the first connecting plate 211 is slidably installed on the first supporting rod 212 to adjust the height of the top cover side flap assembly 22 to match with different types of top cover side flaps 1012, and the folding position of the top cover side flap assembly 22 can be controlled to achieve the best folding effect. The number of the first support rods 212 is two, and the first support rods are located on one side of the aircraft box 10 close to the joint part between the top cover 1011 and the bottom box 102; both ends of the first connection plate 211 are slidably connected to the second support rods 216.
Further preferably, as shown in fig. 2, fig. 4 and fig. 6, the top cover supporting assembly 24 includes a first driving part 241 and a supporting plate 242, the first driving part 241 includes a fixing frame 2411, a second air cylinder 2412, a driving plate 2413 and a connecting plate 2414, the fixing frame 2411 is installed on the supporting assembly 21, the second air cylinder 2412 is fixed on the fixing frame 2411, the driving plate 2413 is installed at an output end of the second air cylinder 2412, the driving plate 2413 is slidably connected to the fixing frame 2411, the connecting plate 2414 is hinged to the fixing frame 2411, a first end of the connecting plate 2414 is fixed to the driving plate 2413, and a second end of the connecting plate 2414 is fixed to the supporting plate 242; when the top cover side wing folding assembly 22 folds the top cover side wing 1012, the second cylinder 2412 drives the first end of the connecting plate 2414 to move through the driving plate 2413, so that the supporting plate 242 on the second end of the connecting plate 2414 supports the inner wall of the top cover 1011, and the top cover 1011 is prevented from moving along with the pushing force when the first folding plate 222 pushes the top cover side wing 1012 in a state that the top cover 1011 is not supported, thereby causing poor folding of the top cover side wing 1012. The bracket assembly 21 further includes a top plate 213, the top plate 213 is mounted on the top end of the first support rod 212, and the fixing bracket 2411 is mounted on the top plate 213.
Preferably, as shown in fig. 2, 3, 4 and 7, the top cover folding assembly 23 includes a second folding plate 231 and a rotating cylinder 232, the rotating cylinder 232 is mounted on the bracket assembly 21, the second folding plate 231 is fixed on the output end of the rotating cylinder 232, the second folding plate 231 is located outside the top cover 1011, and when the rotating cylinder 232 drives the second folding plate 231 to rotate, the second folding plate 231 folds the top cover 1011 to the bottom case 102. In this embodiment, the second folding plate 231 corresponds to the middle portion of the outer side of the top cover 1011, and improves the folding quality of the top cover 1011.
Preferably, the tongue turnover assembly 26 includes a tongue hold-down 261 and a tongue pushforward 262, the tongue hold-down 261 being configured to turn the tongue plate 1013 a predetermined angle; the tongue pusher member 262 is configured to push the tongue plate 1013 at a preset angle into the back box 102. The preset angle in this embodiment is 60 °.
In order to prevent the tongue pressing member 261 and the tongue side flap assembly 25 from interfering with the downward folding process of the top cover 1011, in the present embodiment, both the tongue pressing member 261 and the tongue side flap assembly 25 are of a lifting structure. Specifically, the bracket assembly 21 includes a top plate 213, a third cylinder 214, a second connecting plate 215 and a second supporting rod 216, the top plate 213 is disposed on the second supporting rod 216, the third cylinder 214 is disposed on the top plate 213, the second connecting plate 215 is slidably mounted on the second supporting rod 216, the second connecting plate 215 is connected to an output end of the third cylinder 214, and the third cylinder 214 is configured to drive the second connecting plate 215 to move up and down; two second support rods 216 are provided, and are located on one side of the aircraft box 10 away from the joint portion between the top cover 1011 and the bottom box 102, and two ends of the second connecting plate 215 are slidably connected to the second support rods 216; the tongue-side flap assembly 25 includes a second driving member 251 and a third flap plate 252, the second driving member 251 is mounted on the second connecting plate 215, and performs a lifting function of the tongue-side flap assembly 25, the second driving member 251 is connected to the third flap plate 252 in a driving manner, and the second driving member 251 is configured to drive the third flap plate 252 to fold the tongue-side flap 1014.
Further preferably, in this embodiment, the second driving part 251 has the same structure as the first driving part 241, and the second driving part 251 also includes a fixed frame 2411, a second air cylinder 2412, a transmission plate 2413 and a connection plate 2414, etc., wherein the fixed frame 2411 of the second driving part 251 is mounted on the second connection plate 215, the third flipping plate 252 is fixed on the connection plate 2414 of the second driving part 251, and when the tongue flipping wing assembly 25 flips the tongue wing 1014, the second air cylinder 2412 of the second driving part 251 drives the first end of the connection plate 2414 to move through the transmission plate 2413 of the second driving part 251, so that the third flipping plate 252 on the second end of the connection plate 2414 flips the tongue wing 1014. In this embodiment, there are two sets of tongue flap assemblies 25, and the positions of the two third flap panels 252 match the positions of the two tongue flaps 1014, respectively.
When the third cylinder 214 is expanded or contracted to the maximum extent, the tongue flap assembly 25 can fold the tongue flap 1014 at this time, but in this state, the tongue depressing member 261 cannot depress the tongue plate 1013, and therefore the tongue depressing member 261 includes a fourth cylinder 2611 and a fourth flap plate 2612, the fourth cylinder 2611 is provided at the bottom of the second connection plate 215, and the fourth flap plate 2612 is attached to the output end of the fourth cylinder 2611. Preferably, a guide sleeve is disposed on the second connecting plate 215, and a guide post is disposed on the fourth flipping plate 2612, and the guide post is slidably mounted in the guide sleeve to improve the motion stability of the fourth flipping plate 2612. When the top cover assembly 101 is pressed against the bottom case 102, the third cylinder 214 drives the second link plate 215 to extend, the tongue flap assembly 25 folds the tongue flap 1014 such that the tongue flap 1014 is folded 90 ° relative to the tongue plate 1013, and then the fourth cylinder 2611 extends to drive the fourth flap 2612 to press the tongue plate 1013 downward such that the tongue plate 1013 is folded 60 ° relative to the top cover 1011, and then the tongue pushing member 262 pushes the tongue plate 1013 at a predetermined angle into the bottom case 102, thereby completing the closing operation of the aircraft case 10.
The tongue pushing assembly 262 includes a sixth cylinder 2621 and a front pushing plate 2622, the sixth cylinder 2621 is mounted on the bracket assembly 21, the front pushing plate 2622 is fixed to the output end of the sixth cylinder 2621, and the sixth cylinder 2621 can drive the front pushing plate 2622 to push the tongue plate 1013 at a predetermined angle into the bottom case 102. The tongue forward-pushing member 262 is height-adjustable relative to the bracket assembly 21, which improves flexibility of debugging the apparatus.
Preferably, the box sealing device 2 further comprises a tongue supporting assembly 27, the tongue supporting assembly 27 comprises a fifth cylinder 271 and a tongue supporting plate 272, the fifth cylinder 271 is mounted on the bracket assembly 21, the tongue supporting plate 272 is mounted at the output end of the fifth cylinder 271, when the tongue plate 1013 needs to be pressed down, the fifth cylinder 271 can drive the tongue supporting plate 272 to move up and down, so that the tongue supporting plate 272 supports the joint of the tongue plate 1013 and the top cover 1011, the stress on the bottom box 102 is reduced, the bottom box 102 is prevented from being deformed in the pressing down process of the tongue plate 1013, and the product quality is improved. Further preferably, the bracket assembly 21 further includes a third connecting plate 217, two ends of the third connecting plate 217 are slidably connected to the two second support rods 216, the third connecting plate 217 is connected to an output end of the fifth cylinder 271, the tongue plate 272 is disposed on the third connecting plate 217, and the tongue plate 272 is connected to the output end of the fifth cylinder 271 through the third connecting plate 217, so as to improve the stability of the movement of the tongue plate 272.
It should be particularly noted that, the present embodiment further improves the working steps of the aircraft box sealing device, and the specific steps are as follows:
the method comprises the following steps: the conveying device 1 conveys the airplane box 10 to be sealed to the box sealing device 2;
step two: the top cover support assembly 24 supports the inside of the top cover 1011;
step three; the top cover flap folding assembly 22 folds the top cover flaps 1012 90 degrees relative to the top cover 1011;
step four; removing the support from the cap support assembly 24;
step five: the top cover folding assemblies 23 fold the top cover assembly 101 onto the bottom box 102, and the top cover side wing folding assemblies 22 continue to guide the top cover side wings 1012 during this process, ensuring that the top cover side wings 1012 are inserted into the bottom box 102;
step six: the third cylinder 214 drives the tongue side wing folding assembly 25 to descend, and simultaneously the tongue side wing folding assembly 25 folds the tongue side wing 1014 downwards by 90 degrees;
step seven: the tongue support assembly 27 supports the joint of the tongue plate 1013 and the top cover 1011 while the tongue hold-down member 261 holds down the tongue plate 1013 such that the tongue plate 1013 is folded 60 ° relative to the top cover 1011;
step eight: the tongue pusher 262 pushes the tongue plate 1013 at a predetermined angle into the back box 102 so that the tongue wings 1014 are inserted into the back box 102, thereby completing the box closing operation of the entire aircraft box 10.
The aircraft box sealing equipment solves the problems of low manual box sealing work efficiency, high cost and uncertain quality. The positioning edge 111 of the conveying device 1 improves the conveying stability and the accurate positioning accuracy of the aircraft box 10. This box sealing device 2 of aircraft box equipment has realized that top cap 1011, top cap flank 1012, tongue board 1013 and tongue flank 1014 of aircraft box 10 are automatic to be sealed the box, saves the human cost, improves production efficiency, has improved the product quality. Moreover, all the top cover flank turnover assemblies 22, the tongue flank turnover assemblies 25, the tongue turnover assemblies 26 and the tongue supporting assemblies 27 can be movably arranged on the support assembly 21, so that the flexibility is high, the box sealing device 2 can be conveniently debugged, the box sealing requirement of multiple types of airplane boxes 10 can be met, and the universality is high.
It is to be noted that the foregoing description is only exemplary of the invention and that the principles of the technology may be employed. It will be understood by those skilled in the art that the present invention is not limited to the particular embodiments described herein, but is capable of various obvious changes, rearrangements and substitutions as will now become apparent to those skilled in the art without departing from the scope of the invention. Therefore, although the present invention has been described in greater detail by the above embodiments, the present invention is not limited to the above embodiments, and may include other equivalent embodiments without departing from the spirit of the present invention, and the scope of the present invention is determined by the scope of the appended claims.
Claims (7)
1. An aircraft box closure apparatus for fitting a top cover assembly (101) of an aircraft box (10) into a bottom box (102), the top cover assembly (101) comprising a top cover (1011), top cover side wings (1012), tongue plates (1013), and tongue side wings (1014), the aircraft box closure apparatus comprising:
a conveying device (1) for carrying and conveying the aircraft box (10);
the box sealing device (2) comprises a bracket component (21), and a top cover flank folding component (22), a top cover folding component (23), a top cover supporting component (24), a tongue flank folding component (25) and a tongue folding component (26) which are arranged on the bracket component (21);
the conveying device (1) is configured to convey the aircraft box (10) into the box sealing device (2);
the top cap side flap assembly (22) is configured to flap the top cap side flaps (1012);
the top cover support assembly (24) is configured to support the top cover (1011) when the top cover side flap assembly (22) flaps the top cover side flaps (1012);
the top cover folding assembly (23) is configured to fold the top cover (1011) onto the bottom box (102);
the tongue side flap folding assembly (25) is configured to fold the tongue side flap (1014);
said tongue tucker assembly (26) configured to tuck said tongue plate (1013) and said tongue side flap (1014) into said back box (102);
the bracket assembly (21) comprises a first connecting plate (211) and a first supporting rod (212), the top cover side wing folding assembly (22) is installed on the first connecting plate (211), and the first connecting plate (211) is installed on the first supporting rod (212) in a sliding mode so that the height of the top cover side wing folding assembly (22) can be adjusted;
the top cover folding assembly (23) comprises a second folding plate (231) and a rotating cylinder (232), the rotating cylinder (232) is mounted on the bracket assembly (21), the second folding plate (231) is fixed at the output end of the rotating cylinder (232), the second folding plate (231) is located on the outer side of the top cover (1011), and when the rotating cylinder (232) drives the second folding plate (231) to rotate, the second folding plate (231) folds the top cover (1011) onto the bottom box (102);
the tongue turnover assembly (26) comprises:
a tongue depressing member (261) configured to fold the tongue plate (1013) over a preset angle;
a tongue advancement member (262) configured to advance said tongue plate (1013) at said preset angle into said back box (102).
2. The aircraft box sealing device according to claim 1, characterized in that the conveying device (1) comprises a conveyor belt (11) and a first driving member (12), a plurality of groups of positioning ridges (111) are arranged on the conveyor belt (11) at intervals, and the aircraft box (10) is mounted on the positioning ridges (111);
the first drive (12) is configured to drive the conveyor belt (11) to transport the aircraft box (10).
3. The aircraft box sealing device of claim 1, wherein the top cover side wing folding assembly (22) comprises a first air cylinder (221) and a first folding plate (222), the first air cylinder (221) is arranged on the bracket assembly (21), the first folding plate (222) is installed at the output end of the first air cylinder (221), and the first air cylinder (221) drives the first folding plate (222) to extend and retract so as to drive the top cover side wing (1012) to fold relative to the top cover (1011).
4. The aircraft cassette sealing device of claim 1, wherein the top cover supporting assembly (24) comprises a first driving part (241) and a supporting plate (242), the first driving part (241) comprises a fixing frame (2411), a second cylinder (2412), a transmission plate (2413) and a connecting plate (2414), the fixing frame (2411) is installed on the support assembly (21), the second cylinder (2412) is fixed on the fixing frame (2411), the transmission plate (2413) is installed at the output end of the second cylinder (2412), the transmission plate (2413) is slidably connected to the fixing frame (2411), the connecting plate (2414) is hinged to the fixing frame (2411), and the first end of the connecting plate (2414) is fixed on the transmission plate (2413) and the second end is fixed on the supporting plate (242);
when the top cover side wing folding assembly (22) folds the top cover side wing (1012), the second cylinder (2412) drives the first end of the connecting plate (2414) to move through the transmission plate (2413), so that the supporting plate (242) supports the inner wall of the top cover (1011).
5. The aircraft box sealing device of claim 1, wherein the bracket assembly (21) comprises a top plate (213), a third cylinder (214), a second connecting plate (215) and a second supporting rod (216), the top plate (213) is arranged at the top end of the second supporting rod (216);
the third air cylinder (214) is arranged on the top plate (213), the second connecting plate (215) is slidably mounted on the second supporting rod (216), the second connecting plate (215) is connected to the output end of the third air cylinder (214), and the third air cylinder (214) is configured to drive the second connecting plate (215) to ascend and descend;
the tongue side flap assembly (25) comprises a second drive member (251) and a third flap plate (252), the second drive member (251) being mounted on the second connecting plate (215), the second drive member (251) being in driving connection with the third flap plate (252), the second drive member (251) being configured to drive the third flap plate (252) to flap the tongue side flap (1014).
6. The aircraft box sealing device of claim 5, wherein the tongue depressing member (261) comprises a fourth cylinder (2611) and a fourth flap plate (2612), the fourth cylinder (2611) being disposed at the bottom of the second connecting plate (215), the fourth flap plate (2612) being mounted to an output end of the fourth cylinder (2611).
7. An aircraft box sealing device according to claim 1, characterized in that the box sealing device (2) further comprises a tongue support member (27), the tongue support member (27) comprises a fifth cylinder (271) and a tongue plate (272), the fifth cylinder (271) is mounted on the bracket assembly (21), the tongue plate (272) is mounted at the output end of the fifth cylinder (271), and the fifth cylinder (271) can drive the tongue plate (272) to move up and down, so that the tongue plate (272) supports the engagement part of the tongue plate (1013) and the top cover (1011).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110648120.2A CN113320742B (en) | 2021-06-10 | 2021-06-10 | Aircraft box sealing equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110648120.2A CN113320742B (en) | 2021-06-10 | 2021-06-10 | Aircraft box sealing equipment |
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| Publication Number | Publication Date |
|---|---|
| CN113320742A CN113320742A (en) | 2021-08-31 |
| CN113320742B true CN113320742B (en) | 2023-02-28 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110648120.2A Active CN113320742B (en) | 2021-06-10 | 2021-06-10 | Aircraft box sealing equipment |
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| Country | Link |
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| CN (1) | CN113320742B (en) |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN113320742A (en) | 2021-08-31 |
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