CN212025198U - Cutter backing device for front end cover of wire drawing machine head - Google Patents
Cutter backing device for front end cover of wire drawing machine head Download PDFInfo
- Publication number
- CN212025198U CN212025198U CN202020477053.3U CN202020477053U CN212025198U CN 212025198 U CN212025198 U CN 212025198U CN 202020477053 U CN202020477053 U CN 202020477053U CN 212025198 U CN212025198 U CN 212025198U
- Authority
- CN
- China
- Prior art keywords
- end cover
- wire drawing
- drawing machine
- sword piece
- tool bit
- Prior art date
- 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.)
- Active
Links
Images
Landscapes
- Processing Of Stones Or Stones Resemblance Materials (AREA)
Abstract
The utility model relates to a wire drawing machine aircraft nose front end cover pad sword device, including the pad sword piece, be equipped with a plurality of tool bit mounting grooves on the end cover lateral wall, be equipped with the spout of placing the pad sword piece on the inner both sides wall of tool bit mounting groove, the spout upper end extends to the top of end cover always, is equipped with the installation through-hole in the pad sword piece, and the spout lower extreme is equipped with the screw hole, and the bolt passes the installation through-hole and fixes in the screw hole. The thickness of the shim block is 7-12 mm. The utility model discloses a pad sword piece supports the inboard of tool bit, can prevent that the tool bit from damaging the aircraft nose end cover to prevent that the aircraft nose end cover from changing because of damaging, practice thrift the cost, and the convenient change of pad sword piece practices thrift the change time, and pad sword piece live time is longer in addition.
Description
Technical Field
The utility model belongs to the technical field of glass fiber production facility, concretely relates to wire drawing machine aircraft nose front end housing pad sword device.
Background
The glass fiber yarn is made by using glass balls or waste glass as raw materials and through the processes of high-temperature melting, wire drawing, winding, weaving and the like. The glass fiber yarn is mainly used as an electrical insulating material, an industrial filtering material, an anticorrosion material, a moisture-proof material, a heat-insulating material, a sound-insulating material and a shock-absorbing material. The glass fiber yarn is formed by melting and drawing, the melted glass liquid flows out from the leakage hole of the leakage plate and is cooled, and after being oiled and lubricated by an oiler, the glass fiber yarn is wound on the machine head of the drawing machine to form a bundle of glass fiber yarn. The aircraft nose end cover department of present wire drawing machine can set up wire drawing machine tool bit mounting groove, but tool bit direct mount leads to the aircraft nose front end housing to damage owing to frequent use in the mounting groove, and it is higher to change the aircraft nose cost.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a wire drawing machine aircraft nose front end housing pad sword device solves present wire drawing machine cutter piece direct mount in the mounting groove, because frequent use leads to the aircraft nose front end housing to damage, changes the higher problem of aircraft nose cost.
The utility model relates to a wire drawing machine aircraft nose front end cover pad sword device, including the pad sword piece, be equipped with a plurality of tool bit mounting grooves on the end cover lateral wall, be equipped with the spout of placing the pad sword piece on the inner both sides wall of tool bit mounting groove, the spout upper end extends to the top of end cover always, is equipped with the installation through-hole in the pad sword piece, and the spout lower extreme is equipped with the screw hole, and the bolt passes the installation through-hole to be fixed in the screw hole, and the pad sword piece passes through bolt fixed mounting. The end cover is high-strength aluminum alloy, and a cover plate is fixed to the top of the end cover through bolts.
The thickness of the shim cutter block is 7-12 mm. Moderate thickness and long service time.
The side wall of the sliding groove is arc-shaped, and the side walls of the two sides of the shim block are arc surfaces matched with the sliding groove. The knife cushion block is convenient to put in and take out.
The threaded hole is located on the outer side of the cutter head mounting groove. The strength of the shim block is increased.
The shim knife block is made of stainless steel materials.
Compared with the prior art, the utility model has the advantages of:
the inner side of the cutter head is supported by the cutter cushion block, so that the cutter head can be prevented from damaging the end cover of the machine head, the cost is saved, the cutter cushion block is convenient to replace, the replacement time is saved, and the service life of the cutter cushion block is longer.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of a shim block;
in the figure: 1. the end cover comprises an end cover body 2, a cutter supporting block 3, a bolt 4, a cutter head mounting groove 5, a sliding groove 6, a mounting through hole 7 and an arc surface.
Detailed Description
The following describes the embodiments of the present invention in further detail with reference to the accompanying drawings.
The cutter backing device for the front end cover of the machine head of the wire drawing machine comprises a cutter backing block 2, a plurality of cutter head mounting grooves 4 are formed in the side wall of the end cover 1, sliding grooves 5 for placing the cutter backing block 2 are formed in the two side walls of the inner end of each cutter head mounting groove 4, the upper ends of the sliding grooves 5 extend to the top of the end cover 1, mounting through holes 6 are formed in the cutter backing block 2, threaded holes are formed in the lower ends of the sliding grooves 5, and bolts 3 penetrate through the mounting through holes 6 and are fixed in the threaded holes.
The thickness of the shim cutter block 2 is 7-12 mm. Most preferably 9 mm.
The side wall of the sliding groove 5 is arc-shaped, and the side walls on the two sides of the cutter supporting block 2 are arc surfaces 7 matched with the sliding groove 5.
The threaded hole is located outside the bit mounting groove 4. The shim block was replaced for approximately 10 minutes.
The shim knife block 2 is made of stainless steel materials. The cutter supporting block can be used for both reverse and forward, the service life of the cutter supporting block is prolonged, and the cutter supporting block is replaced for 1 time in 9 months.
During the installation, can lift the apron of end cover front end off, then slide in backing up the sword piece from the spout, then pass the threaded hole that the installation through-hole was twisted in the spout with the bolt, install the tool bit, fixed upper cover plate accomplishes the installation, when changing, only need lift off the apron and then take off the tool bit, unscrew the bolt and can take out backing up the sword piece and change convenient and fast. When the end cover cutting device works, the cutter backing block can bear the acting force of the cutter head on the end cover, and the end cover is prevented from being damaged.
To sum up, the utility model discloses a pad sword piece supports the inboard of tool bit, can prevent that the tool bit from damaging the aircraft nose end cover to prevent that the aircraft nose end cover from changing because of damaging, practice thrift the cost, and the convenient change of pad sword piece practices thrift the change time, and pad sword piece live time is longer in addition.
In the description of the present invention, the terms "inside", "outside", "longitudinal", "lateral", "up", "down", "top", "bottom", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for convenience of description of the present invention rather than requiring the present invention to be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.
Claims (5)
1. The utility model provides a wire drawing machine aircraft nose front end lid backing sword device which characterized in that: including laying up sword piece (2), be equipped with a plurality of tool bit mounting grooves (4) on end cover (1) lateral wall, be equipped with spout (5) of placing laying up sword piece (2) on the inner both sides wall of tool bit mounting groove (4), spout (5) upper end extends to the top of end cover (1) always, is equipped with installation through-hole (6) in laying up sword piece (2), and spout (5) lower extreme is equipped with the screw hole, and bolt (3) pass installation through-hole (6) and fix in the screw hole.
2. The bushing knife device for the front end cover of the wire drawing machine head according to claim 1, characterized in that: the thickness of the shim knife block (2) is 7-12 mm.
3. The bushing knife device for the front end cover of the wire drawing machine head according to claim 2, characterized in that: the side wall of the sliding groove (5) is arc-shaped, and the side walls of the two sides of the shim block (2) are arc surfaces (7) matched with the sliding groove (5).
4. The bushing knife device for the front end cover of the wire drawing machine head according to claim 1, characterized in that: the threaded hole is positioned on the outer side of the cutter head mounting groove (4).
5. The bushing knife device for the front end cover of the wire drawing machine head according to claim 1, characterized in that: the shim knife block (2) is made of stainless steel materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020477053.3U CN212025198U (en) | 2020-04-03 | 2020-04-03 | Cutter backing device for front end cover of wire drawing machine head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020477053.3U CN212025198U (en) | 2020-04-03 | 2020-04-03 | Cutter backing device for front end cover of wire drawing machine head |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212025198U true CN212025198U (en) | 2020-11-27 |
Family
ID=73490937
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020477053.3U Active CN212025198U (en) | 2020-04-03 | 2020-04-03 | Cutter backing device for front end cover of wire drawing machine head |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212025198U (en) |
-
2020
- 2020-04-03 CN CN202020477053.3U patent/CN212025198U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN213352154U (en) | High-strength clamp based on new material | |
| CN212025198U (en) | Cutter backing device for front end cover of wire drawing machine head | |
| CN215035720U (en) | Quick accurate cutting device for machine-building | |
| CN211615053U (en) | Lathe guide rail locking device convenient to oil supply is lubricated | |
| CN215251435U (en) | Aluminum rod spindle with replaceable yarn cutter | |
| CN211446364U (en) | Super-thick carbon fiber preform cutting device | |
| CN208183104U (en) | A kind of electro-plating roller device | |
| CN214290999U (en) | Alloy step drill with straight groove | |
| CN210702627U (en) | Sleeve boring cutter for outer diameter machining | |
| CN219684188U (en) | Fixing mechanism for machining internal thread milling cutter | |
| CN213970845U (en) | Fixing mechanism for machining tapered roller bearing | |
| CN218983927U (en) | High-precision power head of numerical control core walking machine | |
| CN104674302A (en) | High-strength guide plate for electrolytic aluminum crust breaker | |
| CN220407221U (en) | Corrosion-resistant hard alloy milling cutter | |
| CN213827649U (en) | Transmission device of welding machine | |
| CN218396133U (en) | Aviation key part forming milling cutter convenient to install | |
| CN212823791U (en) | One-way sleeve pin press-fitting device | |
| CN212822877U (en) | Be used for V type engine organism camshaft dead eye bore hole device | |
| CN213410688U (en) | Single-tooth internal thread milling cutter | |
| CN210476176U (en) | Anti-deformation numerical control gantry beam | |
| CN214867467U (en) | Multi-mode switching cutter seat of fine boring device | |
| CN216447238U (en) | Novel corner tailboard hydro-cylinder | |
| CN207873621U (en) | A kind of double-position drilling Milling Machining equipment | |
| CN219974489U (en) | Fixed pick-shaped coal cutting pick | |
| CN220216745U (en) | Spindle box of vertical processing machine tool |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |