CN217269658U - Automatic assembly device of aluminum frame structure - Google Patents

Automatic assembly device of aluminum frame structure Download PDF

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Publication number
CN217269658U
CN217269658U CN202220297584.3U CN202220297584U CN217269658U CN 217269658 U CN217269658 U CN 217269658U CN 202220297584 U CN202220297584 U CN 202220297584U CN 217269658 U CN217269658 U CN 217269658U
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Prior art keywords
frame structure
sliding
recited
locking
supporting plate
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CN202220297584.3U
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Chinese (zh)
Inventor
叶霆
王晶晶
邓传广
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Jiangsu Wuxi Oupai Integrated Home Co ltd
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Jiangsu Wuxi Oupai Integrated Home Co ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
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    • Y02E10/50Photovoltaic [PV] energy

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Abstract

The utility model relates to an automatic assembly device of aluminium frame structure, including sliding portion and two group frame portions, group frame portion slides and is equipped with two aircraft noses that are used for locking the angle sign indicating number, and group frame portion still is equipped with two glide machanism, and two glide machanism are used for ordering about two aircraft noses respectively and slide, wherein: the sliding part is used for driving the two frame assembling parts to approach or depart from; the machine head comprises a supporting plate for supporting the door frame and a locking block for locking the corner code, the locking block is in sliding fit with the supporting plate along the vertical direction, and the supporting plate is further provided with a first air cylinder for driving the locking block to slide along the vertical direction; and the sliding mechanism is used for driving the two machine heads to approach or move away from each other. The angle connector is locked by the aid of the machine head, production efficiency can be improved, locking precision of the angle connector is improved, the consistency of the overall dimension of a finished aluminum frame structure is guaranteed, and the quality of a finished product is improved.

Description

Automatic assembly device of aluminum frame structure
Technical Field
The utility model relates to a field of aluminium frame structure equipment especially relates to an automatic assembly device of aluminium frame structure.
Background
The assembly of the existing aluminum frame structure (such as an aluminum frame structure window) is generally completely carried out manually, the aluminum frame structure comprises four aluminum frames which are sequentially connected, and adjacent frames are locked by using corner connectors. When assembling the aluminum frame structure, an operator firstly needs to install the corner connectors at the end of one frame and then sequentially installs other frames and the corner connectors. Then, the side face of the corner connector is required to be knocked, so that the corner connector and the frame are clamped tightly to form a complete aluminum frame structure.
The following problems mainly exist in the process of manually assembling the aluminum frame structure:
1. the manual control precision is poor, so that the appearance size of the finished product aluminum frame structure is uneven, and the quality of the finished product is poor;
2. the production efficiency of manual assembly is low, and the human cost is high.
SUMMERY OF THE UTILITY MODEL
To overcome the above-mentioned drawbacks of the prior art, an object of the present invention is to provide an automatic assembling device for aluminum frame structure, which solves one or more problems in the prior art.
In order to achieve the above purpose, the technical scheme of the utility model is as follows:
the utility model provides an automatic assembly device of aluminium frame structure, includes sliding part and two group frame portions, group frame portion slides and is equipped with two aircraft noses that are used for locking the angle sign indicating number, group frame portion still is equipped with two glide machanism, two glide machanism is used for driving two respectively the aircraft nose slides, wherein:
the sliding part is used for driving the two group frame parts to approach or depart from each other;
the machine head comprises a supporting plate for supporting a door frame and a locking block for locking the corner brace, the locking block is in sliding fit with the supporting plate along the vertical direction, and the supporting plate is also provided with a first air cylinder for driving the locking block to slide along the vertical direction;
and the sliding mechanism is used for driving the two machine heads to approach or move away from each other.
Furthermore, the top surface of layer board is connected with the support, first cylinder sets up on the support, the piston rod of first cylinder extends downwards along vertical direction, the latch segment with the piston rod of first cylinder is connected.
Furthermore, the locking block is connected with a guide rod, the guide rod is arranged along the vertical direction, and the guide rod is in sliding fit with the support.
Furthermore, the sliding mechanism comprises a guide rod, a first ball screw assembly and a first motor, the machine head is arranged on the guide rod in a sliding mode, a screw rod of the first ball screw assembly is in transmission connection with the first motor, and a nut of the first ball screw assembly is connected with the machine head.
Furthermore, the top surface of layer board is equipped with the locating part, the locating part has the breach, the angle sign indicating number that is located aluminium frame structure four corners respectively with four the breach gomphosis of locating part.
Further, in the two guide bars of the same set frame portion, both ends of the two guide bars that are close to each other are inclined in a direction toward the other set frame portion.
Furthermore, the limiting piece is detachably connected with the supporting plate.
Furthermore, the layer board slides and is equipped with the slider, the layer board is equipped with and is used for ordering about the second cylinder that the slider slided, the slider is equipped with the tray, the tray passes along vertical direction the layer board to offset with the bottom surface of angle sign indicating number, the layer board is seted up and is used for supplying the hole of dodging that the tray slided.
Furthermore, still include the workstation, the portion of sliding and group frame portion all set up on the workstation, the portion of sliding includes second ball screw subassembly and second motor, the screw rod of second ball screw subassembly with second motor transmission is connected, one group frame portion with workstation fixed connection, another group frame portion with workstation sliding fit, and with the nut of second ball screw subassembly is connected.
Furthermore, the workstation is equipped with limit switch, limit switch is used for monitoring the slide position of group frame portion, limit switch is used for controlling the operation of second motor.
Compared with the prior art, the utility model discloses a beneficial technological effect as follows:
the frame that will assemble and angle sign indicating number are placed between four aircraft noses, and first cylinder drives the latch segment and slides to lock four angle signs respectively, form complete aluminium frame structure, utilize aircraft nose locking angle sign indicating number in this scheme, can improve production efficiency, improve the locking precision of angle sign indicating number simultaneously, guarantee that the overall dimension of finished product aluminium frame structure is unanimous, improve off-the-shelf quality.
And (II) the sliding part drives the two assembling frame parts to be close to or far away from each other, and the sliding mechanism drives the two machine heads to be close to or far away from each other, so that the distance between the four machine heads is adjusted, and the sliding mechanism is adapted to assembling aluminum frame structures with different length and width sizes.
And thirdly, the top surface of the supporting plate is provided with a limiting part, the corner connectors at the four corners of the aluminum frame structure are respectively embedded into the notches of the limiting parts, the position of the corner connector can be locked by using the limiting parts, the corner connector is tightly matched with the frame, and the consistency of the overall dimension of the finished aluminum frame structure is ensured.
(IV) the one end that the guide bar is close to each other inclines to the direction that is close to another group frame portion, and then when glide machanism drove two aircraft noses and is close to each other, the locating part slided towards aluminium frame structure aslope to four angle sign indicating numbers of extrusion are to the skew of the centre of aluminium frame structure, make angle sign indicating number and frame cooperation inseparable.
(V) when producing different aluminium frame structures, the angle sign indicating number of using is different, if there is outstanding decoration or lines angle sign indicating number bottom surface, leads to the unable direct top surface with the layer board of bottom surface of angle sign indicating number to offset, then can install suitable tray, utilizes the bottom surface of tray and angle sign indicating number to support the angle sign indicating number, can avoid the in-process of locking the angle sign indicating number to damage the decoration of angle sign indicating number.
Drawings
Fig. 1 shows a schematic structural diagram of an automatic assembling device for an aluminum frame structure in an embodiment of the present invention;
fig. 2 shows the matching schematic diagram of the handpiece and the sliding mechanism in the embodiment of the present invention.
In the drawings, the reference numbers:
1. a work table; 11. a slide rail; 111. a limit switch; 12. a second ball screw assembly; 13. a second motor; 2. a frame assembling part; 21. a guide bar; 22. a first ball screw assembly; 23. a first motor; 3. a support plate; 31. a support; 311. a first cylinder; 312. a locking block; 313. a guide bar; 32. a second cylinder; 321. a slider; 322. a support block; 33. a limiting member; 331. and (4) a notch.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the following description will be made in detail with reference to the accompanying drawings and the following detailed description of the present invention. The advantages and features of the present invention will become more apparent from the following description. It is to be noted that the drawings are in a very simplified form and are not to precise scale, which is merely for the purpose of facilitating and distinctly claiming the embodiments of the present invention. To make the objects, features and advantages of the present invention more comprehensible, please refer to the attached drawings. It should be understood that the structure, ratio, size and the like shown in the drawings attached to the present specification are only used for matching with the content disclosed in the specification, so as to be known and read by those skilled in the art, and are not used for limiting the limitation of the implementation of the present invention, so that the present invention does not have the essential significance in the technology, and any modification of the structure, change of the ratio relationship or adjustment of the size should still fall within the scope of the technical content disclosed in the present invention without affecting the function and the achievable purpose of the present invention.
Examples
Referring to fig. 1 and 2, the present application provides an automatic assembling device for an aluminum frame structure, which includes a sliding portion and two assembling frame portions 2, wherein the assembling frame portions 2 are slidably provided with two machine heads for locking corner connectors, the assembling frame portions 2 are further provided with two sliding mechanisms, the two sliding mechanisms are respectively used for driving the two machine heads to slide, wherein:
the sliding part is used for driving the two assembling frame parts 2 to approach or depart from each other;
the machine head comprises a supporting plate 3 for supporting the door frame and a locking block 312 for locking an angle code, wherein the locking block 312 is in sliding fit with the supporting plate 3 along the vertical direction, and the supporting plate 3 is also provided with a first cylinder 311 for driving the locking block 312 to slide along the vertical direction;
and the sliding mechanism is used for driving the two machine heads to approach or move away from each other.
Referring to fig. 1 and 2, in particular, the automatic assembling device for an aluminum frame structure further includes a workbench 1, and the sliding portion and the assembling frame portion 2 are both mounted on a top surface of the workbench 1. The sliding part comprises a second ball screw component 12 and a second motor 13 which are arranged on the top surface of the workbench 1, the screw rod of the second ball screw component 12 is in running fit with the workbench 1, and a bevel gear set is arranged between the output shaft of the second motor 13 and the screw rod of the second ball screw component 12 for transmission.
Referring to fig. 1 and 2, specifically, two slide rails 11 are bolted to the top surface of the worktable 1, and both the slide rails 11 are parallel to the screw of the second ball screw assembly 12. The two frame assembly portions 2 are respectively a first frame assembly portion 2 and a second frame assembly portion 2, the first frame assembly portion 2 is bolted to the top surface of the workbench 1, the second frame assembly portion 2 is arranged on the two slide rails 11 in a sliding manner, and the second frame assembly portion 2 is connected with a nut of the second ball screw assembly 12. The screw axes of the slide rail 11 and the second ball screw assembly 12 are both directed to the first group frame portion 2. In order to limit the sliding distance of the second group of frame portions 2 and avoid the second group of frame portions 2 from sliding off the slide rails 11, four limit switches 111 are installed on the top surface of the workbench 1, the four limit switches 111 are respectively located at two ends of the two slide rails 11, a contact of the limit switch 111 faces the second group of frame portions 2, each limit switch 111 is electrically connected with the second motor 13, and the limit switch 111 is used for monitoring the sliding position of the second group of frame portions 2 and controlling the second motor 13 to stop running when the second group of frame portions 2 slides to the edges of the slide rails 11.
Referring to fig. 1 and fig. 2, further, each sliding mechanism includes a first ball screw assembly 22 mounted on the top surface of the frame assembly 2, a first motor 23, and a pair of guide rods 21, and the length direction of the first ball screw assembly 22 is parallel to the axes of the pair of guide rods 21. Two pairs of guide rods 21 on the top surface of the same group frame portion 2 are placed along the horizontal direction, and the ends of the two pairs of guide rods 21 point to the other adjacent group frame portion 2. The two pairs of guide bars 21 come closer gradually in a direction toward the other group frame portion 2. The equal carriage of every aircraft nose is established on a pair of guide bar 21, and the aircraft nose is connected with adjacent first ball screw assembly 22's nut, and first ball screw assembly 22's screw rod rotating rack is established at the top surface of group frame portion 2, is equipped with shaft coupling transmission connection between first ball screw assembly 22's the screw rod and the output shaft of first motor 23.
Referring to fig. 1 and 2, specifically, an L-shaped bracket 31 is bolted to the top surface of the pallet 3, the bracket 31 includes a vertical portion and a horizontal portion, the vertical portion of the bracket 31 is bolted to the top surface of the pallet 3, a first cylinder 311 is bolted to the horizontal portion of the bracket 31, a piston rod of the first cylinder 311 is downward along the vertical direction and passes through the horizontal portion of the bracket 31, a locking block 312 is located right above the pallet 3, and the locking block 312 is connected to the piston rod of the first cylinder 311. When the first cylinder 311 operates, the locking block 312 can be driven to slide in the vertical direction.
Referring to fig. 1 and 2, in order to prevent the locking block 312 from deflecting when sliding in the vertical direction, a guide rod 313 is welded to the top surface of the locking block 312, and a top end of the guide rod 313 penetrates through a horizontal portion of the bracket 31 in the vertical direction and is in sliding fit with the bracket 31.
Referring to fig. 1 and fig. 2, further, a limiting member 33 is bolted to the top surface of the supporting plate 3, a notch 331 is formed in a side surface of the limiting member 33 close to the aluminum frame structure, and a shape of the notch 331 is adapted to a shape of the corner brace. Before compressing tightly the angle sign indicating number, place the frame that assembles and angle sign indicating number on four layer boards 3 at first, need compress tightly the aluminium frame structure of angle sign indicating number and put after on four layer boards 3, be located the angle sign indicating number in door frame four corners and imbed the breach 331 of four locating parts 33 respectively, control frame portion 2 and aircraft nose slide afterwards for four locating parts 33 support tightly with the angle sign indicating number in door frame four corners respectively. When the glide machanism drives two aircraft noses and is close to each other towards another group frame portion 2, two aircraft noses are close to each other to four angle sign indicating numbers of extrusion are squinted to aluminium frame structure centre, finally make angle sign indicating number and frame cooperation inseparable. The limiting piece 33 is bolted on the supporting plate 3, and when different corner connectors are used for locking the aluminum frame structure, different limiting pieces 33 can be replaced, so that the shape matching of the notch 331 of the limiting piece 33 and the corner connector is ensured.
Referring to fig. 1 and 2, further, a sliding block 321 is slidably disposed on the bottom surface of the supporting plate 3, a sliding direction of the sliding block 321 is parallel to an axis of the adjacent guide rod 21, a sliding direction of the sliding block 321 is parallel to a length direction of the adjacent guide rod 21, a second cylinder 32 for driving the sliding block 321 to slide is further disposed under the supporting plate 3, a supporting block 322 is bolted to the top surface of the sliding block 321, the supporting block 322 extends upward through the supporting plate 3 along a vertical direction and abuts against the bottom surface of the corner brace, and an avoiding hole for allowing the supporting block 322 to slide is further formed in the supporting plate 3. In this embodiment, the head further comprises a mounting base sliding on the guide bar 21, two parallel side plates are bolted to the top surface of the mounting base, a connecting plate is further bolted between the two side plates, the support plate 3 is bolted to the top surfaces of the two side plates, and the second cylinder 32 is bolted to the top surface of the connecting plate. When producing different aluminium frame structures, the angle sign indicating number of using is different, if there is outstanding decoration or lines angle sign indicating number bottom surface, leads to the unable direct top surface with layer board 3 of bottom surface of angle sign indicating number to offset, then can install suitable tray 322, utilizes the bottom surface of tray 322 and angle sign indicating number to support the angle sign indicating number, can avoid the in-process of locking the angle sign indicating number to damage the decoration of angle sign indicating number. Different pallets 322 can be selected according to the type of corner brace.
The working principle is as follows:
before compressing tightly the angle sign indicating number, at first accomplish frame and angle sign indicating number assembly, place the frame that will assemble again and angle sign indicating number between four aircraft noses, every angle sign indicating number all is located a layer board 3, and each aircraft nose of glide machanism drive slides towards aluminium frame structure to press from both sides the tight four locating parts 33 of aluminium frame structure clamp. First cylinder 311 drives latch segment 312 lapse afterwards, locks four angle sign indicating numbers respectively, forms complete aluminium frame structure, utilizes aircraft nose locking angle sign indicating number in this scheme, can improve production efficiency, improves the locking precision of angle sign indicating number simultaneously, guarantees that the overall dimension of finished product aluminium frame structure is unanimous, improves off-the-shelf quality.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only represent several embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.

Claims (10)

1. The utility model provides an automatic assembly device of aluminium frame structure which characterized in that: including sliding portion and two group frame portions, group frame portion slides and is equipped with two aircraft noses that are used for locking the angle sign indicating number, group frame portion still is equipped with two glide machanism, two glide machanism is used for driving two respectively the aircraft nose slides, wherein:
the sliding part is used for driving the two group frame parts to approach or depart from each other;
the machine head comprises a supporting plate for supporting the door frame and a locking block for locking the corner brace, the locking block is in sliding fit with the supporting plate along the vertical direction, and the supporting plate is further provided with a first air cylinder for driving the locking block to slide along the vertical direction;
and the sliding mechanism is used for driving the two machine heads to approach or move away from each other.
2. An aluminum frame structure automatic assembling device as recited in claim 1, wherein: the top surface of layer board is connected with the support, first cylinder sets up on the support, the piston rod of first cylinder extends downwards along vertical direction, the latch segment with the piston rod of first cylinder is connected.
3. The automatic assembling device for aluminum frame structure as recited in claim 2, wherein: the locking block is connected with a guide rod, the guide rod is arranged in the vertical direction, and the guide rod is in sliding fit with the support.
4. The automatic assembling device for aluminum frame structure as recited in claim 1, wherein: the slippage mechanism comprises a guide rod, a first ball screw assembly and a first motor, the machine head is arranged on the guide rod in a sliding mode, a screw rod of the first ball screw assembly is in transmission connection with the first motor, and a nut of the first ball screw assembly is connected with the machine head.
5. An aluminum frame structure automatic assembling device as recited in claim 4, wherein: the top surface of layer board is equipped with the locating part, the locating part has the breach, the corner sign indicating number that is located aluminium frame structure four corners respectively with four the locating part breach gomphosis.
6. An aluminum frame structure automatic assembling device as recited in claim 5, wherein: for the two guide rods on the same group frame part, the ends of the two guide rods close to each other are inclined towards the direction close to the other group frame part.
7. An aluminum frame structure automatic assembling device as recited in claim 5, wherein: the limiting piece is detachably connected with the supporting plate.
8. An aluminum frame structure automatic assembling device as recited in claim 1, wherein: the layer board slides and is equipped with the slider, the layer board is equipped with and is used for ordering about the second cylinder that the slider slided, the slider is equipped with the tray, the tray passes along vertical direction the layer board to offset with the bottom surface of angle sign indicating number, the layer board is seted up and is used for supplying the hole of dodging that the tray slided.
9. The automatic assembling device for aluminum frame structure as recited in claim 1, wherein: the sliding part and the group frame part are arranged on the workbench, the sliding part comprises a second ball screw assembly and a second motor, a screw of the second ball screw assembly is in transmission connection with the second motor, one group frame part is fixedly connected with the workbench, and the other group frame part is in sliding fit with the workbench and is connected with a nut of the second ball screw assembly.
10. An aluminum frame structure automatic assembling device as recited in claim 9, wherein: the workbench is provided with a limit switch, the limit switch is used for monitoring the sliding position of the frame assembling portion, and the limit switch is used for controlling the operation of the second motor.
CN202220297584.3U 2022-02-15 2022-02-15 Automatic assembly device of aluminum frame structure Active CN217269658U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220297584.3U CN217269658U (en) 2022-02-15 2022-02-15 Automatic assembly device of aluminum frame structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220297584.3U CN217269658U (en) 2022-02-15 2022-02-15 Automatic assembly device of aluminum frame structure

Publications (1)

Publication Number Publication Date
CN217269658U true CN217269658U (en) 2022-08-23

Family

ID=82854771

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220297584.3U Active CN217269658U (en) 2022-02-15 2022-02-15 Automatic assembly device of aluminum frame structure

Country Status (1)

Country Link
CN (1) CN217269658U (en)

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