CN213730847U - A edging device for aircraft bolt production - Google Patents

A edging device for aircraft bolt production Download PDF

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Publication number
CN213730847U
CN213730847U CN202022686806.4U CN202022686806U CN213730847U CN 213730847 U CN213730847 U CN 213730847U CN 202022686806 U CN202022686806 U CN 202022686806U CN 213730847 U CN213730847 U CN 213730847U
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Prior art keywords
fixed
bolt
box
supporting
edging
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CN202022686806.4U
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Chinese (zh)
Inventor
宋宗强
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Jiangxi Jindu Aviation Parts Co ltd
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Jiangxi Jindu Aviation Parts Co ltd
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Abstract

The utility model discloses an edging device for aircraft bolt production, including supporting box, collecting box, the cover of breathing in, fixed plate and supporting shoe, the bottom four corners of supporting box is fixed with four supporting legs through the bolt symmetry, the bottom plate surface of supporting box has the collecting box through the bolt fastening, the bottom plate surface of the left supporting box of collecting box has the suction fan through the bolt fastening, the intake pipe of suction fan extends to in the collecting box, the welded surface of supporting box is fixed with the cover of breathing in, the cover of breathing in is linked together with the collecting box through the connecting pipe, the welded surface of the left supporting box of the cover of breathing in is fixed with the fixed plate, the welded surface of the supporting box on the cover right side of breathing in is fixed with the supporting shoe. This an edging device for aircraft bolt production not only can carry out the edging operation to the bolt of different specifications, can adsorb the dust that the edging produced moreover.

Description

A edging device for aircraft bolt production
Technical Field
The utility model belongs to the technical field of the bolt production facility, concretely relates to an edging device for aircraft bolt production.
Background
The bolt is an essential accessory in mechanical equipment and parts. The bolt is a fastener consisting of a head part and a screw rod, needs to be matched with a nut and is used for fastening and connecting two parts with through holes. This form of connection is known as a bolted connection. If the nut is unscrewed from the bolt, the two parts can be separated, so that the bolt connection belongs to detachable connection.
When producing the bolt in the mill, need use the edging device to polish its border position more smoothly. During the edging process, a lot of scraps are generated and float in the air, and certain harm is caused to the body of workers.
Therefore, in order to meet the current situation, the design and production of an edging device for aircraft bolt production are urgently needed to meet the requirements of practical use.
Disclosure of Invention
An object of the utility model is to provide an edging device for aircraft bolt production to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an edging device for aircraft bolt production, includes supporting box, collecting box, the cover of breathing in, fixed plate and supporting shoe, the bottom four corners of supporting box is fixed with four supporting legs through the bolt symmetry, the bottom plate surface of supporting box has the collecting box through the bolt fastening, the bottom plate surface of the left supporting box of collecting box has the suction fan through the bolt fastening, the intake pipe of suction fan extends to in the collecting box, the welded surface of supporting box is fixed with the cover of breathing in, the cover of breathing in is linked together with the collecting box through the connecting pipe, the welded surface of the left supporting box of cover of breathing in is fixed with the fixed plate, the welded surface of the supporting box on the cover right side of breathing in is fixed with the supporting shoe.
Preferably, the outer wall of the left side of the fixed plate is fixed with a rotating motor through a bolt, an output shaft of the rotating motor is fixed with a rotating shaft through a coupler, and the right end face of the rotating shaft is fixedly welded with a edging disc.
Preferably, a stepping motor is fixed on the outer wall of one side of the supporting block through a bolt, a moving groove is formed in the surface of the supporting block, an adjusting screw rod is rotatably connected into the moving groove of the supporting block through a welded bearing, the outer wall of the adjusting screw rod is in threaded connection with two connecting blocks, fixed blocks are fixed on the surfaces of the two connecting blocks through bolts, and arc-shaped grooves are formed in opposite surfaces of the two fixed blocks.
Preferably, a filter plate is fixed in the collection box through a bolt, a driving motor is fixed on the surface of a top plate of the collection box through a bolt, a guide screw rod is also rotatably connected in the collection box through a welded bearing, and the top of the guide screw rod is also fixedly connected with an output shaft of the driving motor through a coupler;
the outer wall of the guide screw is in threaded connection with a moving block, the outer wall of one side, close to the filter plate, of the moving block is fixedly provided with a cleaning brush through bolts, a limiting column is welded in the collecting box, and the moving block slides outside the limiting column.
Preferably, the outer wall of the adjusting screw is fixedly welded with a separating ring, and the threads of the adjusting screws on the two sides of the separating ring are opposite in direction.
The utility model discloses a technological effect and advantage: according to the edging device for producing the aircraft bolt, through the arrangement of the suction fan, in the process of edging the bolt, the suction fan sucks air into the collection box, so that negative pressure is formed in the collection box and the suction hood, and then scraps generated by edging can be adsorbed into the collection box, so that the harm of the scraps to the health of workers is avoided; the stepping motor drives the adjusting screw rod to rotate, so that the position between the two groups of fixing blocks can be adjusted, bolts of different specifications can be fixed, and the bolts of different specifications can be edge-ground by matching with the edge grinding disc; through the setting of filter, can avoid the piece to discharge from the collecting box, drive lead screw through driving motor and rotate, can drive the cleaning brush and reciprocate on the surface of filter to carry out effectual clearance to the filter, avoid influencing the dust absorption effect because of the filter blocks up, this an edging device for aircraft bolt production not only can carry out the edging operation to the bolt of different specifications, can adsorb the dust that the edging produced in addition.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a front view of the present invention in an edge grinding state;
fig. 3 is a cross-sectional view of the present invention;
fig. 4 is a cross-sectional view of the support block of the present invention;
fig. 5 is an enlarged view of a portion a in fig. 3 according to the present invention.
In the figure: the device comprises a supporting box 1, a collecting box 2, an air suction cover 3, a fixing plate 4, a rotating motor 5, a rotating shaft 6, a edging disc 7, a supporting block 8, a stepping motor 9, an adjusting screw rod 10, a connecting block 11, a fixing block 12, a suction fan 13, a filter plate 14, a driving motor 15, a guide screw rod 16, a cleaning brush 17 and a limiting column 18.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, 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.
Unless the direction is defined separately, the directions of up, down, left, right, front, back, etc. referred to herein are the directions of up, down, left, right, front, back, etc. in the drawings of the present invention, and are herein incorporated by reference.
The utility model provides a edging device for aircraft bolt production as shown in fig. 1-5, including supporting box 1, collecting box 2, suction hood 3, fixed plate 4 and supporting shoe 8, the bottom four corners of supporting box 1 is fixed with four supporting legs through the bolt symmetry, the bottom plate surface of supporting box 1 has collecting box 2 through the bolt fastening, the bottom plate surface of 2 left supporting boxes 1 of collecting box has suction fan 13 through the bolt fastening, suction fan 13's model can select to be: RB-73D-1, the intake pipe of suction fan 13 extends to in the collecting box 2, the welded surface of supporting box 1 is fixed with the cover 3 of breathing in, the cover 3 of breathing in is linked together through connecting pipe and collecting box 2, the welded surface of the left supporting box 1 of the cover 3 of breathing in is fixed with fixed plate 4, the welded surface of the supporting box 1 on the right side of the cover 3 of breathing in is fixed with supporting shoe 8, it has two sets of chamber doors to articulate through the hinge on the supporting box 1, it has sealing door to articulate through the hinge on the collecting box 2, is convenient for clear up collecting box 2.
Specifically, the left side outer wall of fixed plate 4 is fixed with rotating electrical machines 5 through the bolt, rotating electrical machines 5's model is optional: the two-phase step motor of 86BYG, the output shaft of rotating electrical machines 5 is fixed with rotation axis 6 through the shaft coupling, the right-hand member face welded fastening of rotation axis 6 has edging dish 7.
Specifically, the outer wall of one side of supporting shoe 8 is fixed with step motor 9 through the bolt, step motor 9's model can be selected as: the surface of the supporting block 8 is provided with a moving groove, the moving groove of the supporting block 8 is rotatably connected with an adjusting screw 10 through a welded bearing, the outer wall of the adjusting screw 10 is in threaded connection with two connecting blocks 11, the surfaces of the two connecting blocks 11 are both fixed with fixing blocks 12 through bolts, the opposite surfaces of the two fixing blocks 12 are both provided with arc-shaped grooves, and anti-slip pads are bonded in the arc-shaped grooves of the fixing blocks 12.
Specifically, there is filter 14 through the bolt fastening in the collecting box 2, there is driving motor 15 on the roof surface of collecting box 2 through the bolt fastening, driving motor 15's model can be selected as: the inside of the collection box 2 is also rotatably connected with a guide screw 16 through a welded bearing, and the top of the guide screw 16 is also fixedly connected with an output shaft of a driving motor 15 through a coupler;
the outer wall of the guide screw 16 is in threaded connection with a moving block, the outer wall of one side, close to the filter plate 14, of the moving block is fixedly provided with a cleaning brush 17 through bolts, a limiting column 18 is welded in the collection box 2, and the moving block slides outside the limiting column 18.
Specifically, a separating ring is welded and fixed on the outer wall of the adjusting screw 10, and the screw threads of the adjusting screw 10 on the two sides of the separating ring are opposite in direction.
The working principle of the edge grinding device for aircraft bolt production is that when the edge grinding device is used, a bolt to be ground is placed between two groups of fixing blocks 12, a stepping motor 9 is started, the stepping motor 9 drives an adjusting screw rod 10 to rotate, the adjusting screw rod 10 adjusts the position between the two groups of fixing blocks 12 through two groups of connecting blocks 11, the two groups of fixing blocks 12 are abutted to the outer wall of the bolt, the bolt is fixed, one end of the bolt is in contact with an edge grinding disc 7, a rotating motor 5 is started, the rotating motor 5 drives the edge grinding disc 7 to rotate through a rotating shaft 6, so that the edge grinding operation is performed on the bolt, in the process of performing the edge grinding operation on the bolt, a suction fan 13 and a driving motor 15 are simultaneously started, the suction fan 13 sucks air into a collecting box 2, negative pressure is formed in the collecting box 2 and a suction hood 3, further, fragments generated by edge grinding are adsorbed into the collecting box 2, the driving motor 15 drives a guide screw rod 16 to perform forward rotation and reverse rotation, the guide screw 16 drives the cleaning brush 17 to move up and down on the surface of the filter plate 14 through the moving block, so that the filter plate 14 is effectively cleaned, and the influence on the dust collection effect due to the blockage of the filter plate 14 is avoided.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.

Claims (5)

1. The utility model provides an edging device for aircraft bolt production, includes supporting box (1), collecting box (2), cover (3), fixed plate (4) and supporting shoe (8) of breathing in, its characterized in that: the bottom four corners of supporting box (1) is fixed with four supporting legs through the bolt symmetry, the bottom plate surface of supporting box (1) has collecting box (2) through the bolt fastening, the bottom plate surface of collecting box (2) left supporting box (1) has suction fan (13) through the bolt fastening, the intake pipe of suction fan (13) extends to in collecting box (2), the welded surface of supporting box (1) is fixed with cover (3) of breathing in, cover (3) of breathing in is linked together through connecting pipe and collecting box (2), the welded surface of cover (3) left supporting box (1) of breathing in is fixed with fixed plate (4), the welded surface of supporting box (1) on cover (3) right side of breathing in is fixed with supporting shoe (8).
2. Edging device for the production of aircraft bolts according to claim 1, characterized in that: the left side outer wall of fixed plate (4) is fixed with rotating electrical machines (5) through the bolt, the output shaft of rotating electrical machines (5) is fixed with rotation axis (6) through the shaft coupling, the right-hand member face welded fastening of rotation axis (6) has edging dish (7).
3. Edging device for the production of aircraft bolts according to claim 1, characterized in that: the outer wall of one side of supporting shoe (8) is fixed with step motor (9) through the bolt, the shifting chute has been seted up on the surface of supporting shoe (8), rotate through welded bearing in the shifting chute of supporting shoe (8) and be connected with adjusting screw (10), the outer wall threaded connection of adjusting screw (10) has two connecting blocks (11), two the surface of connecting block (11) all is fixed with fixed block (12) through the bolt, two the arc wall has all been seted up to the opposite face of fixed block (12).
4. Edging device for the production of aircraft bolts according to claim 1, characterized in that: a filter plate (14) is fixed in the collection box (2) through a bolt, a driving motor (15) is fixed on the surface of a top plate of the collection box (2) through a bolt, a guide screw (16) is also rotatably connected in the collection box (2) through a welded bearing, and the top of the guide screw (16) is also fixedly connected with an output shaft of the driving motor (15) through a coupler;
the outer wall of the guide screw (16) is in threaded connection with a moving block, the outer wall of one side, close to the filter plate (14), of the moving block is fixedly provided with a cleaning brush (17) through bolts, a limiting column (18) is welded in the collection box (2), and the moving block slides outside the limiting column (18).
5. Edging device for the production of aircraft bolts according to claim 3, characterized in that: the outer wall of the adjusting screw rod (10) is fixedly welded with a separating ring, and the threads of the adjusting screw rods (10) on the two sides of the separating ring are opposite in direction.
CN202022686806.4U 2020-11-19 2020-11-19 A edging device for aircraft bolt production Active CN213730847U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022686806.4U CN213730847U (en) 2020-11-19 2020-11-19 A edging device for aircraft bolt production

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022686806.4U CN213730847U (en) 2020-11-19 2020-11-19 A edging device for aircraft bolt production

Publications (1)

Publication Number Publication Date
CN213730847U true CN213730847U (en) 2021-07-20

Family

ID=76826263

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202022686806.4U Active CN213730847U (en) 2020-11-19 2020-11-19 A edging device for aircraft bolt production

Country Status (1)

Country Link
CN (1) CN213730847U (en)

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