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Automatic gap filling device

[Application publication number: CN110578397A; applicant: Hangzhou Shuodian Technology Co., Ltd .; inventor: Yang Siqing;]
Summary:
An automatic gap filling device includes a fuselage, an automatic movement device is installed at a lower portion of the fuselage, and an automatic filling device is installed at an upper portion of the fuselage, wherein the automatic movement device includes a first support installed at a bottom of the fuselage Wheel, second support wheel, third support wheel, the first support wheel and the second support wheel are fixedly connected with a synchronization wheel 1 and a synchronization wheel 2, the first support wheel and the second support wheel A guide wheel is installed at both ends of the third support wheel, and a forward wheel is fixedly connected between the first support wheel and the second support wheel. The synchronous wheel 1 and the synchronous wheel 2 are connected to each other through a timing belt. The synchronous wheel three moves together. The synchronous wheel three is fixed on the output shaft of the driving motor. The driving motor is mounted on a driving motor bracket. The driving motor bracket is mounted on the upper end of the inside of the fuselage.
Sovereign items:
An automatic gap filling device comprising a fuselage (1), an automatic movement device (2) is installed at a lower portion of the fuselage (1), and an automatic filling device (3) is installed at an upper portion of the fuselage, characterized in that: The automatic movement device (1) includes a first support wheel (2.1), a second support wheel (2.2), a third support wheel (2.3), and the first support wheel (2.1) installed at the bottom of the fuselage (1). A synchronous wheel one (2.1.1) and a synchronous wheel two (2.2.1) are fixedly connected to the second support wheel (2.2), the first support wheel (2.1) and the second support wheel (2.2 ) And the third support wheel (2.3) are provided with guide wheels (2.4) at both ends, and a forward wheel (2.5) is fixedly connected between the first support wheel (2.1) and the second support wheel (2.2). , The synchronous wheel one (2.1.1) and the synchronous wheel two (2.2.1) move together through a synchronous belt (2.6) and a synchronous wheel three (2.7), and the synchronous wheel three (2.7) is fixedly connected at On the output shaft of the drive motor (2.8), the drive motor (2.8) is mounted on a drive motor bracket (2.9), and the drive motor bracket (2.9) is mounted on the upper end inside the fuselage (1).
Claim:
An automatic gap filling device comprising a fuselage (1), an automatic movement device (2) is installed at a lower portion of the fuselage (1), and an automatic filling device (3) is installed at an upper portion of the fuselage, characterized in that: The automatic movement device (1) includes a first support wheel (2.1), a second support wheel (2.2), a third support wheel (2.3), and the first support wheel (2.1) installed at the bottom of the fuselage (1). A synchronous wheel one (2.1.1) and a synchronous wheel two (2.2.1) are fixedly connected to the second support wheel (2.2), the first support wheel (2.1) and the second support wheel (2.2 ) And the third support wheel (2.3) are provided with guide wheels (2.4) at both ends, and a forward wheel (2.5) is fixedly connected between the first support wheel (2.1) and the second support wheel (2.2). , The synchronous wheel one (2.1.1) and the synchronous wheel two (2.2.1) move together through a synchronous belt (2.6) and a synchronous wheel three (2.7), and the synchronous wheel three (2.7) is fixedly connected at On the output shaft of the drive motor (2.8), the drive motor (2.8) is mounted on a drive motor bracket (2.9), and the drive motor bracket (2.9) is mounted on the upper end inside the fuselage (1).
The automatic gap filling device according to claim 1, characterized in that: the forward gear (2.5) is provided with forward teeth (2.5.1) along the circumference, and the forward teeth (2.5.1) are With a convex cross-sectional structure, a small cylinder at the front end of the forward wheel (2.5) is nested in a small circular hole (2.5.2) at the outer circumference of the forward wheel (2.5), and a large cylinder at the lower end of the forward tooth (2.5.1) It is nested in a large circular hole (2.5.3) inside the forward wheel (2.5). The forward teeth (2.5.1) can move up and down in the small circular hole (2.5.2) and the large circular hole (2.5.3). A compression spring (2.5.4) is provided between the bottom of the large circular hole (2.5.3) and the bottom surface of the advancing tooth (2.5.1), and the upper end of the advancing tooth (2.5.1) is arranged in a linear structure Also provided with sawtooth.
3. An automatic seam filling device according to claim 1, characterized in that the principle adopted by the automatic filling device (3) is to directly push the double-tube beautiful seam tube (3.2) at a uniform speed by using a push rod (3.1) so that To achieve uniform filling, the double-tube beautiful seam tube (3.2) is fixed on the beautiful seam tube bracket (3.3) at the upper part of the fuselage (1), and the beautiful seam tube bracket (3.3) and the double-tube beautiful seam tube (3.2) The shape is the same. The upper part of the fuselage (1) is also provided with a limited position bracket (3.4) to limit the double-tube beautiful seam tube (3.2). The tail end of the push rod (3.1) is fixed to the slider (3.5). ), The slider (3.5) can be rotated forward and backward by a screw (3.6), and one end of the screw (3.6) is connected to a stepper motor (3.8) through a coupling (3.7). The other end is mounted on the bearing seat (3.9), the stepper motor (3.8) is mounted on the body (1) through a stepper motor bracket (3.10), and the slider (3.5) is provided with a dovetail groove (3.5) .1), a dovetail bar (3.11) is nested in the dovetail groove (3.5.1), and the dovetail bar (3.11) is installed on the fuselage.
Automatic gap filling device
Technical field
The invention relates to a decoration tool, in particular to an automatic gap filling device.
Background technique
At present, in the decoration and decoration projects, wall and floor tiles are generally used to prevent thermal expansion and cracking of the tiles. When the tiles are laid, gaps of 1-1.5 mm are left between the tiles. These gaps are filled with a filler. In order to ensure the waterproofness of the floor, but it is not easy to grasp when filling in the grout, because the grout is filled well or poorly, the intelligence is measured according to the personal level of the paving worker or the good or bad mood, if the operation is improper The floor or wall surface that is laid out often does not achieve the expected effect; the excess jointing agent and grout on the surface of the tile is difficult to clean.
Summary of the invention
The invention aims at the problems existing in the prior art, and proposes an automatic gap filling device.
In order to achieve the above object, the present invention adopts the following technical solution: an automatic gap filling device including a fuselage, an automatic movement device is installed at a lower portion of the fuselage, and an automatic filling device is installed at an upper portion of the fuselage, wherein The automatic movement device includes a first support wheel, a second support wheel, and a third support wheel installed at the bottom of the fuselage. The first support wheel and the second support wheel are fixedly connected with a synchronization wheel 1 and a synchronization wheel 2, A guide wheel is installed at both ends of the first support wheel, the second support wheel, and the third support wheel, and a forward wheel is fixedly connected between the first support wheel and the second support wheel. The synchronous wheel 1 and the synchronous wheel 2 move together with the synchronous wheel 3 through a synchronous belt. The synchronous wheel 3 is fixed on the output shaft of the driving motor, the driving motor is installed on the driving motor bracket, and the driving motor The bracket is installed at the upper end inside the fuselage.
Further, the forward gear is provided with forward teeth along the circumference, the forward teeth have a convex cross-section structure, a small cylinder at the front end of the forward teeth is nested in a small circular hole at the outer circumference of the forward wheel, and the forward path The large cylindrical at the lower end is nested in a large circular hole inside the forward wheel, the forward teeth can move up and down in the small circular hole and the large circular hole, and a compression spring is provided between the bottom of the large circular hole and the bottom surface of the forward teeth, The upper end of the advancing teeth is arranged in a linear structure and is provided with saw teeth.
Further, the principle of the automatic filling device is to use a push rod to directly push the double-tube beautiful seam tube at a uniform speed to achieve uniform filling. The double-tube beautiful seam tube is fixed on a beautiful seam tube bracket at the upper part of the fuselage. The shape of the beautiful sewing tube bracket is the same as that of the double sewing tube. The upper part of the fuselage is also provided with a limiter to limit the double sewing tube. The tail end of the push rod is fixed on the slider. It can be rotated forward and backward by a screw rod. One end of the screw rod is connected to a stepper motor through a coupling, and the other end is mounted on a bearing seat. The stepper motor is mounted on the body through a stepper motor bracket. On the slider, a dovetail groove is provided, a dovetail bar is nested in the dovetail groove, and the dovetail bar is installed on the fuselage.
Further, a mixing head is installed at the front end of the double-tube beautiful seam tube. When in use, the outlet of the mixing head is located under the tile.
The advantage of the invention is that the invention can advance at a uniform speed under the action of a driving motor, and can discharge the material at a uniform speed under the action of a stepper motor to achieve the consistency of the material. The elasticity of the forward teeth of the forward wheel can be guaranteed at The different levels of the floor in the tile joint can ensure the grip, and in addition to ensuring the quality of the tile joint, the joint filling efficiency is improved.
BRIEF DESCRIPTION OF THE DRAWINGS
Automatic gap filling device
FIG. 1 is a schematic diagram 1 of the overall structure of the present invention.
Automatic gap filling device
FIG. 2 is a second schematic diagram of the overall structure of the present invention.
Automatic gap filling device
FIG. 3 is a schematic diagram of the internal structure of the forward wheel of the present invention.
detailed description
The following is a specific embodiment of the present invention in combination with the drawings to further describe the technical solution of the present invention. As shown in FIG. 1 and FIG. 2 and FIG. 3, an automatic gap filling device includes a fuselage 1, 1 An automatic movement device 2 is installed at the lower part, and an automatic filling device 3 is installed at the upper part of the fuselage, characterized in that the automatic movement device 1 includes a first support wheel 2.1 and a second support wheel 2.2 installed at the bottom of the fuselage 1, The third support wheel 2.3, the first support wheel 2.1 and the second support wheel 2.2 are fixedly connected with a synchronous wheel 1.2.1 and a synchronous wheel two 2.2.1, the first support wheel 2.1 and the first A guide wheel 2.4 is installed at both ends of the second support wheel 2.2 and the third support wheel 2.3, and a forward wheel 2.5 is fixedly connected between the first support wheel 2.1 and the second support wheel 2.2, and the synchronous wheel 2.1 .1 and the synchronous wheel two 2.2.1 move together with the synchronous wheel three 2.7 through the synchronous belt 2.6, the synchronous wheel three 2.7 is fixedly connected to the output shaft of the drive motor 2.8, and the drive motor 2.8 is installed on the drive motor On the bracket 2.9, the driving motor bracket 2.9 is mounted on the upper end inside the fuselage 1.
A forward tooth 2.5.1 is provided along the circumference of the forward wheel 2.5. The forward tooth 2.5.1 has a convex cross-sectional structure. A small cylinder at the front end of the forward tooth 2.5.1 is nested at the outer periphery of the forward wheel 2.5. In the small circular hole 2.5.2, the large cylinder at the lower end of the forward tooth 2.5.1 is nested in the large circular hole 2.5.3 inside the forward wheel 2.5, and the forward tooth 2.5.1 may be in the small circular hole 2.5.2 and A large circular hole 2.5.3 moves up and down. A compression spring 2.5.4 is provided between the bottom of the large circular hole 2.5.3 and the bottom surface of the forward tooth 2.5.1, and the upper end of the forward tooth 2.5.1 is arranged in a linear structure. Also provided with sawtooth.
The principle of the automatic filling device 3 is to use a push rod 3.1 to directly push the double-tube beautiful seam tube 3.2 at a uniform speed to achieve uniform filling. The double-tube beautiful seam tube 3.2 is fixed to the beautiful seam tube bracket 3.3 on the upper part of the fuselage 1. In the above, the shape of the beautiful sewing tube bracket 3.3 is the same as that of the double-tube beautiful sewing tube 3.2. The upper part of the fuselage 1 is also provided with a limiter 3.4 to limit the double-tube beautiful sewing tube 3.2, and the tail end of the push rod 3.1 It is fixed on the slider 3.5, which can be rotated forward and backward by the screw rod 3.6. One end of the screw rod 3.6 is connected to the stepper motor 3.8 through the coupling 3.7, and the other end is installed in the bearing seat. On 3.9, the stepper motor 3.8 is mounted on the body 1 through a stepper motor bracket 3.10, the slider 3.5 is provided with a dovetail slot 3.5.1, and the dovetail slot 3.5.1 is nested with a dovetail bar 3.11 The dovetail 3.11 is installed on the fuselage.
A mixing head 3.12 is installed at the front end of the double-tube beautiful seam 3.2. In use, the outlet of the mixing head 3.12 is located below the tile 4.
The present invention works as follows: First, a worker places a double-tube beautiful sewing tube 3.2 on the beautiful sewing tube bracket 3.3 and a limit stop 3.4 on the fuselage 1, and then starts the machine, and the machine can drive the motor 2.8 drive forward wheel 2.5, drive wheel 2.5 forward teeth 2.5.1 can grip the body 1 to move forward, and retractable forward teeth 2.5.1 ensure that the depth of the gap between tiles 4 does not affect the forward teeth 2.5. The grip effect of 1 can still ensure that the fuselage 1 advances at a uniform speed, and the stepper motor 3.8 can push the push rod 3.1 at a uniform speed to ensure uniform discharge.
The protection scope of the present invention includes, but is not limited to, the above embodiments. The protection scope of the present invention is subject to the claims. Any replacement, deformation, and improvement easily made by those skilled in the art made to this technology fall into the scope of the present invention. protected range.
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