CN210112985U - Aerospace aluminum alloy gap runner cutting tool - Google Patents

Aerospace aluminum alloy gap runner cutting tool Download PDF

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Publication number
CN210112985U
CN210112985U CN201920985534.2U CN201920985534U CN210112985U CN 210112985 U CN210112985 U CN 210112985U CN 201920985534 U CN201920985534 U CN 201920985534U CN 210112985 U CN210112985 U CN 210112985U
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CN
China
Prior art keywords
mounting
aluminum alloy
movable
installation piece
mounting panel
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201920985534.2U
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Chinese (zh)
Inventor
蔡瑞蓉
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Shuaiyichi Aluminum Alloy New Material Chongqing Co Ltd
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Shuaiyichi Aluminum Alloy New Material Chongqing Co Ltd
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Application filed by Shuaiyichi Aluminum Alloy New Material Chongqing Co Ltd filed Critical Shuaiyichi Aluminum Alloy New Material Chongqing Co Ltd
Priority to CN201920985534.2U priority Critical patent/CN210112985U/en
Application granted granted Critical
Publication of CN210112985U publication Critical patent/CN210112985U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an aerospace aluminum alloy gap waters cutting means, including the mounting panel, symmetrical threaded connection has two screw thread bracing pieces, two on the diapire of mounting panel the bottom of screw thread bracing piece all is equipped with fixing device, but horizontal movable mounting has the installation piece on the lateral wall of mounting panel one side, movable mounting has driving motor about can on the installation piece, the pivot is installed to driving motor's output, fixed mounting has cutting blade in the pivot. The utility model discloses in with the help of vacuum chuck with mounting panel, installation piece and cutting device fixed connection in the cutting position department of aluminum alloy, the thickness and the degree of depth of cutting as required adjust cutting device to the suitable position on the installation piece, and manual promotion installation piece is just can be convenient waters the aluminum alloy gap and is cut, convenient operation not only, and cutting accuracy is high moreover, effectual to aerospace aluminum alloy's result of use has been improved.

Description

Aerospace aluminum alloy gap runner cutting tool
Technical Field
The utility model relates to a cutting means technical field especially relates to an aerospace aluminum alloy gap waters cutting means.
Background
Experiments show that the thickness of the vertical seam of the aluminum alloy gap pouring gate is very important for the mold filling process of molten metal, the thin or thick vertical seam is difficult to obtain a desired mold filling mode, a thick vertical cylinder is beneficial to stable filling of a cavity, a rough coating layer can enable a coating and molten metal to form a microscopic heat insulation gas film, and the gas film can promote smoothness of a feeding channel from the vertical cylinder to the vertical seam, prolong feeding time and be beneficial to feeding of castings.
In traditional aerospace aluminum alloy gap runner cutting process, an operator often holds a power supply saw and directly cuts the aluminum alloy, and the cutting effect is poor due to the fact that the cutting thickness and the cutting depth cannot be accurately controlled during manual cutting, so that the using effect of the aerospace aluminum alloy is poor, and therefore improvement needs to be made.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the problem that the aerospace aluminum alloy gap is watered and the cutting effect is relatively poor among the prior art, and the aerospace aluminum alloy gap is watered cutting means.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an aerospace aluminum alloy gap runner cutting means, includes the mounting panel, symmetrical threaded connection has two screw thread bracing pieces, two on the diapire of mounting panel the bottom of screw thread bracing piece all is equipped with fixing device, but horizontal movable mounting has the installation piece on the lateral wall of mounting panel one side, movable mounting has driving motor about can on the installation piece, the pivot is installed to driving motor's output, fixed mounting has cutting blade in the pivot.
Preferably, fixing device includes the vacuum chuck of fixed mounting in threaded support pole bottom, fixed mounting has the connecting pipe on the lateral wall on vacuum chuck top, install the control valve on the connecting pipe, the one end that vacuum chuck was kept away from to the connecting pipe can be dismantled and be connected with evacuating device.
Preferably, fixed mounting has first fixed block on the lateral wall that the installation piece is close to installation panel one side, and first fixed block inserts and establishes on the mounting panel, set up the first movable groove of mutually supporting with first fixed block on the lateral wall that the mounting panel is close to installation piece one side, fixed mounting has the guide bar of mutually supporting with first fixed block in the first movable groove, and the guide bar runs through first fixed block setting.
Preferably, a plurality of balls are uniformly installed on the inner side wall of the first movable groove, and the balls are in mutual contact with the first fixed block.
Preferably, the driving motor is close to symmetrical fixed mounting on the lateral wall of installation piece one side has two second movable blocks, and two second movable blocks all insert and establish on the installation piece, set up the second movable groove of mutually supporting with the second movable block on the installation piece, two equal fixed mounting has the threaded rod on the lateral wall of second movable block one side, and the threaded rod all runs through the inside wall of second movable groove one side and extends to the outside of installation piece, set up the third movable groove of mutually supporting with the threaded rod on the lateral wall of installation piece one end, two equal threaded connection has fastening nut on the threaded rod, and fastening nut's diameter all is greater than the width in third movable groove.
Compared with the prior art, the utility model discloses there is following beneficial effect:
1. the mounting plate, the mounting block and the cutting device are fixedly connected to the cutting position of the aluminum alloy by means of the vacuum chuck, the cutting device is adjusted to a proper position on the mounting block according to the cutting thickness and depth required, the mounting block is manually pushed, the aluminum alloy gap runner can be conveniently cut, the operation is convenient, the cutting precision is high, the effect is good, and the using effect of the aerospace aluminum alloy is improved;
2. simple structure, convenient operation, low manufacturing and using cost, good economic applicability and suitability for popularization and use.
Drawings
Fig. 1 is a schematic front structural view of an aerospace aluminum alloy gap runner cutting tool provided by the present invention;
FIG. 2 is a cross-sectional side view of an aerospace aluminum alloy gap runner cutting tool according to the present invention;
fig. 3 is a schematic side structure view of an aerospace aluminum alloy gap runner cutting tool provided by the present invention;
fig. 4 is the utility model provides an A partial structure's of aerospace aluminum alloy gap runner cutting tool enlargedly.
In the figure: the device comprises a mounting plate 1, a threaded supporting rod 2, a vacuum chuck 3, a connecting pipe 4, a control valve 5, a mounting block 6, a first fixed block 7, a first movable groove 8, a ball 9, a guide rod 10, a driving motor 11, a rotating shaft 12, a cutting blade 13, a second movable block 14, a second movable groove 15, a threaded rod 16, a third movable groove 17 and a fastening nut 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.
Referring to fig. 1-4, an aerospace aluminum alloy gap runner cutting tool comprises a mounting plate 1, wherein two threaded support rods 2 are symmetrically and threadedly connected to the bottom wall of the mounting plate 1, the height of each threaded support rod 2 can be conveniently adjusted, fixing devices are arranged at the bottom ends of the two threaded support rods 2 and comprise vacuum chucks 3 fixedly mounted at the bottom ends of the threaded support rods 2, connecting pipes 4 are fixedly mounted on the outer side walls of the top ends of the vacuum chucks 3, control valves 5 are mounted on the connecting pipes 4, one ends, far away from the vacuum chucks 3, of the connecting pipes 4 are detachably connected with vacuumizing devices, the bottom ends of the vacuum chucks 3 are placed on the surface of aluminum alloy and tightly pressed, air in the vacuum chucks 3 is pumped out through the connecting pipes 4 by means of the vacuumizing devices, the vacuumizing devices are detached after the connecting pipes 4 are tightly sealed by the tightening control valves 5, and then the vacuum chucks 3, The threaded support rod 2 and the mounting plate 1 are fixedly connected to the aluminum alloy.
But horizontal movable mounting has installation piece 6 on the lateral wall of mounting panel 1 one side, fixed mounting has first fixed block 7 on the lateral wall that installation piece 6 is close to mounting panel 1 one side, and first fixed block 7 is inserted and is established on mounting panel 1, set up the first movable groove 8 of mutually supporting with first fixed block 7 on the lateral wall that mounting panel 1 is close to installation piece 6 one side, evenly install a plurality of balls 9 on the inside wall of first movable groove 8, and ball 9 all contacts each other with first fixed block 7, can reduce the frictional force between first fixed block 7 and the first movable groove 8 inside wall, fixed mounting has the guide bar 10 of mutually supporting with first fixed block 7 in the first movable groove 8, and guide bar 10 runs through first fixed block 7 and sets up, horizontal promotion installation piece 6 that can be convenient.
Movable mounting has driving motor 11 about can on the installation piece 6, pivot 12 is installed to driving motor 11's output, fixed mounting has cutting blade 13 in the pivot 12, driving motor 11 is close to on the lateral wall of installation piece 6 one side symmetrical fixed mounting have two second movable blocks 14, and two second movable blocks 14 all insert and establish on installation piece 6, set up the second movable groove 15 with second movable block 14 mutually supporting on the installation piece 6, equal fixed mounting has threaded rod 16 on the lateral wall of two second movable blocks 14 one sides, and threaded rod 16 all runs through the inside wall of second movable groove 15 one side and extends to the outside of installation piece 6, reciprocating driving motor 11 that can be convenient, pivot 12 and cutting blade 13.
Set up the third movable groove 17 of mutually supporting with threaded rod 16 on the lateral wall of installation piece 6 one end, equal threaded connection has fastening nut 18 on two threaded rods 16, and fastening nut 18's diameter all is greater than the width of third movable groove 17, changes tightly fastening nut 18 and makes fastening nut 18 and installation piece 6's lateral wall contact each other, just can be convenient fix fastening nut 18, threaded rod 16, second movable block 14, driving motor 11, pivot 12 and cutting blade 13.
The utility model discloses in, install suitable cutting blade 13 in pivot 12 as required, with the help of vacuum chuck 3 with mounting panel 1, installation piece 6 and 11 fixed connection of driving motor in the aluminium alloy wait to cut the department, thickness and the degree of depth of cutting as required adjust cutting blade 13 to the suitable position on installation piece 6, and horizontal promotion installation piece 6 is just can be convenient waters the aluminium alloy gap and is cut.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (5)

1. The utility model provides an aerospace aluminum alloy gap runner cutting means, includes mounting panel (1), its characterized in that: symmetrical threaded connection has two threaded support pole (2), two on the diapire of mounting panel (1) the bottom of threaded support pole (2) all is equipped with fixing device, but horizontal movable mounting has installation piece (6) on the lateral wall of mounting panel (1) one side, movable mounting has driving motor (11) about can on installation piece (6), pivot (12) are installed to the output of driving motor (11), fixed mounting has cutting blade (13) on pivot (12).
2. An aerospace aluminum alloy slot runner cutting tool according to claim 1, wherein: fixing device includes vacuum chuck (3) of fixed mounting in threaded support pole (2) bottom, fixed mounting has connecting pipe (4) on the lateral wall on vacuum chuck (3) top, install control valve (5) on connecting pipe (4), the one end that vacuum chuck (3) were kept away from in connecting pipe (4) can be dismantled and be connected with evacuating device.
3. An aerospace aluminum alloy slot runner cutting tool according to claim 1, wherein: the mounting block (6) are close to on the lateral wall of mounting panel (1) one side fixed mounting have first fixed block (7), and first fixed block (7) insert and establish on mounting panel (1), set up on the lateral wall of mounting panel (1) one side close to mounting block (6) first movable groove (8) of mutually supporting with first fixed block (7), fixed mounting has guide bar (10) of mutually supporting with first fixed block (7) in first movable groove (8), and guide bar (10) run through first fixed block (7) and set up.
4. An aerospace aluminum alloy slot runner cutting tool according to claim 3, wherein: a plurality of balls (9) are uniformly arranged on the inner side wall of the first movable groove (8), and the balls (9) are in mutual contact with the first fixed block (7).
5. An aerospace aluminum alloy slot runner cutting tool according to claim 1, wherein: two second movable blocks (14) are symmetrically and fixedly arranged on the outer side wall of one side of the driving motor (11) close to the mounting block (6), and the two second movable blocks (14) are inserted on the mounting block (6), the mounting block (6) is provided with second movable grooves (15) which are matched with the second movable blocks (14), the outer side wall of one side of each of the two second movable blocks (14) is fixedly provided with a threaded rod (16), and the threaded rods (16) penetrate through the inner side wall of one side of the second movable groove (15) and extend to the outer side of the mounting block (6), a third movable groove (17) matched with the threaded rods (16) is formed in the outer side wall of one end of the mounting block (6), fastening nuts (18) are connected to the two threaded rods (16) in a threaded manner, and the diameters of the fastening nuts (18) are all larger than the width of the third movable groove (17).
CN201920985534.2U 2019-06-27 2019-06-27 Aerospace aluminum alloy gap runner cutting tool Expired - Fee Related CN210112985U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920985534.2U CN210112985U (en) 2019-06-27 2019-06-27 Aerospace aluminum alloy gap runner cutting tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920985534.2U CN210112985U (en) 2019-06-27 2019-06-27 Aerospace aluminum alloy gap runner cutting tool

Publications (1)

Publication Number Publication Date
CN210112985U true CN210112985U (en) 2020-02-25

Family

ID=69572392

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920985534.2U Expired - Fee Related CN210112985U (en) 2019-06-27 2019-06-27 Aerospace aluminum alloy gap runner cutting tool

Country Status (1)

Country Link
CN (1) CN210112985U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20200225

Termination date: 20200627

CF01 Termination of patent right due to non-payment of annual fee