CN209955216U - Complicated oblique position structure of moving of mould around aircraft nose lid - Google Patents

Complicated oblique position structure of moving of mould around aircraft nose lid Download PDF

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Publication number
CN209955216U
CN209955216U CN201920346949.5U CN201920346949U CN209955216U CN 209955216 U CN209955216 U CN 209955216U CN 201920346949 U CN201920346949 U CN 201920346949U CN 209955216 U CN209955216 U CN 209955216U
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CN
China
Prior art keywords
die
column
embedded
oblique
block
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Expired - Fee Related
Application number
CN201920346949.5U
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Chinese (zh)
Inventor
吴又强
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Foshan Xinjiayou Mould Products Co Ltd
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Foshan Xinjiayou Mould Products Co Ltd
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Priority to CN201920346949.5U priority Critical patent/CN209955216U/en
Application granted granted Critical
Publication of CN209955216U publication Critical patent/CN209955216U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a complicated oblique line bit architecture of mould around aircraft nose lid, includes: the front die and the rear die are provided with guide chutes on the die core of the rear die, pull rods are arranged in the guide chutes, one ends of the pull rods are provided with air cylinders connected with the air cylinders, the other ends of the air cylinders are provided with triangular oblique sliders, the oblique sliders face upwards, the inclined planes are provided with chutes, the oblique sliders are provided with push posts, the push posts extend towards the oblique upper parts and extend from the lower die to the die core of the upper die, the lower ends of the push posts are clamped into the chutes of the oblique sliders, embedded posts are arranged at the upper ends of the push posts, the top ends of the embedded posts are provided with the pull rods, ejector blocks are arranged in the middle of the pull rods, springs are mounted on the ejector blocks and are embedded on the pull rods, so that the convenient and rapid demoulding can be carried out, when the position of an engine oil adding port of an engine cover is produced, the demoulding process can be carried out wirelessly and manually, avoid unnecessary accident, effectual automatic drawing of patterns that carries on simultaneously.

Description

Complicated oblique position structure of moving of mould around aircraft nose lid
Technical Field
The utility model belongs to the technical field of the mould and specifically relates to a complicated oblique line bit architecture of mould around aircraft nose lid is related to.
Background
The mould is various moulds and tools for obtaining required products by injection molding, blow molding, extrusion, die casting or forging forming, smelting, stamping and other methods in industrial production. In short, a mold is a tool used to make a shaped article, the tool being made up of various parts, different molds being made up of different parts. The processing of the appearance of an article is realized mainly through the change of the physical state of a formed material. The element has the name of "industrial mother".
When the automobile engine hood is produced, most plastic engine hoods need to be subjected to injection molding, and when the existing automobile engine hood is subjected to injection molding and demolding, the engine oil adding hole protruding on the engine hood is easily clamped on a mold during demolding, so that demolding is difficult to carry out.
SUMMERY OF THE UTILITY MODEL
The utility model discloses an it is not enough to overcome above-mentioned condition, aims at providing the technical scheme that can solve above-mentioned problem.
The utility model provides a complicated oblique line bit architecture of mould around aircraft nose lid, includes: the front die and the rear die are respectively provided with a front die core and a rear die core, the front die core corresponds to the die core surface of the rear die, the upper end surface of the front die is provided with a front die plate, the die core of the rear die is provided with a guide chute, a pull column is arranged in the guide chute, one end of the pull column is provided with a cylinder and is connected with the cylinder, the other end of the pull column is provided with a triangular oblique slide block, the oblique surface of the oblique slide block faces upwards, the oblique surface is provided with a chute, the oblique slide block is provided with a push column, the push column extends towards the oblique upper part and extends from the lower die to the die core of the upper die, the lower end of the push column is clamped into the chute of the oblique slide block, the upper end of the push column is provided with an embedded column, the side end of the upper part of the embedded column is provided with a groove, the side end of the embedded column is provided with a hook block, the hook block, when the front mould is sunk into the front mould, the hook block is provided with a threaded hole, the threaded hole is provided with a mounting screw, the mounting screw penetrates through the front mould plate and is connected with the hook block, the hook block is mounted on the front mould plate through a mounting screw key, the top end of the embedded column is provided with a pull rod, the middle part of the pull rod is provided with an ejector block, a spring is mounted on the ejector block, the spring is embedded on the pull rod, and the pull rod extends into the front mould plate.
As a further aspect of the present invention: the lower end of the embedded column is provided with a thread groove.
As a further aspect of the present invention: and a pressing ring is arranged on the pull rod at the top of the spring.
As a further aspect of the present invention: the front mold core and the rear mold core are automobile engine cover mold cores.
Compared with the prior art, the beneficial effects of the utility model are that: carry out convenient quick drawing of patterns, when the machine oil of production bonnet adds the position of mouth, the processing of drawing of patterns of carrying on of quick convenience, wireless artificial drawing of patterns that carries on causes the scald to the workman when avoiding the shaping back to cross because of the product and make the manual demoulding, avoids the unnecessary accident, the effectual automatic drawing of patterns that carries on simultaneously.
Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a structural sectional view of the present invention.
In the figure: 1. the device comprises a front template, 2, a front mould, 3, a rear mould, 4, an inclined slide block, 5, a pull rod, 6, a pressing ring, 7, a spring, 8, a hook block, 9, a top block, 10, an embedded column, 11, a push column, 12, a pull rod, 13, an air cylinder, 14 and a guide chute.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely below, and it should be understood that the described embodiments are only some embodiments of the present invention, but 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.
Referring to fig. 1-2, in an embodiment of the present invention, a complex diagonal structure of front and rear molds of a nose cover includes: the front die and the rear die are respectively provided with a front die core 2 and a rear die core inside the front die 2 and the rear die, the front die core 2 corresponds to the die core surface of the rear die, the upper end surface of the front die 2 is provided with a front die plate 1, the die core of the rear die is provided with a guide chute 14, a pull column 12 is arranged in the guide chute 14, one end of the pull column 12 is provided with a cylinder 13 which is connected with the cylinder 13, the other end of the pull column 12 is provided with a triangular inclined slide block 4, the inclined surface of the inclined slide block 4 faces upwards, the inclined surface is provided with a chute, the inclined slide block 4 is provided with a push column 11, the push column 11 extends towards the inclined upper part and extends from the lower die to the die core of the upper die, the lower end of the push column 11 is clamped into the chute of the inclined slide block 4, the upper end of the push column 11 is provided with an embedded column 10, the embedded column 10 is arranged in the, inlay the side of post 10 and be provided with and collude piece 8, collude and be provided with bellied arch on the piece 8, protruding card is gone into the recess of inlaying post 10, collude piece 8 and set up between front mould 2 and front form 1, is absorbed in front mould 2, colludes and is provided with the screw hole on the piece 8, is provided with the installation screw on the screw hole, the installation screw runs through front form 1 and colludes piece 8 and is connected, colludes piece 8 through the installation screw key and installs in front form 1, the top of inlaying post 10 is provided with pull rod 5, and pull rod 5 middle part is provided with kicking block 9, installs spring 7 on the kicking block 9, and spring 7 nests on pull rod 5, pull rod 5 extends to in the front form 1.
The lower end of the embedded column 10 is provided with a thread groove, so that threads can appear on a hole formed in the outer wall of the embedded column 10 during molding.
And a pressing ring 6 is arranged on the pull rod 5 at the top of the spring 7, and the pressing ring 6 is used for pressing the upper end surface of the spring 7 to prevent the spring 7 from leaving the pull rod 5.
And the front mold 2 and the rear mold are automobile engine cover mold cores and are used for producing the automobile engine cover.
The utility model discloses a theory of operation is: when the die is closed, the front diaphragm plate is pressed downwards, the hook block 8 is pushed downwards, the pull rod 5 is pushed to move downwards, the compression spring 7 pushes the embedded column 10 to move downwards through the downward movement of the pull rod 5, the hook block 8 is clamped into a groove of the embedded column 10, the position of the embedded column 10 is ensured, meanwhile, the air rod operates, the pull column 12 is pushed forwards, the inclined slide block 4 is enabled to move forwards, the push column 11 slides on the inclined slide block 4, the push column 11 moves upwards, the lower end of the embedded column 10 is abutted, the position of the embedded column 10 is fixed, and injection molding is carried out;
after injection moulding accomplished, when dividing the mould, the gas pole function, will draw post 12 to draw back, make slider 4 backward to one side, make and push away post 11 and slide at slider 4 to one side, make and push away post 11 downstream, thereby make and push away post 11 downstream, simultaneously preceding lamina membranacea and preceding membrane separation, make the pressure on the spring 7 disappear, spring 7 lower extreme is because of the effect of kicking block 9, make spring 7 can only go up the return stroke earlier, make spring 7 will inlay post 10 and draw back, make and inlay post 10 and withdraw from the mold core surface, collude piece 8 simultaneously and inlay post 10 and separate, then separate through the thimble board.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims (4)

1. The utility model provides a complicated oblique line bit architecture of mould around aircraft nose lid, includes: the front die and the rear die are respectively provided with a front die core and a rear die core, the front die core corresponds to the die core surface of the rear die, the upper end surface of the front die is provided with a front die plate, the front die and the rear die are respectively internally provided with a guide chute, a pull column is arranged in the guide chute, one end of the pull column is provided with a cylinder and is connected with the cylinder, the other end of the pull column is provided with a triangular oblique slide block, the oblique slide block is obliquely upward and provided with a chute, a push column is arranged on the oblique slide block and extends obliquely upward to the upper die core from the lower die, the lower end of the push column is clamped into the chute of the oblique slide block, the upper end of the push column is provided with an embedded column, the side end of the upper part of the embedded column is provided with a groove, the side end of the embedded column is provided with a hook block, the hook block is provided with a raised bulge, the bulge block is clamped into the groove of the embedded column, when the front mould is sunk into the front mould, the hook block is provided with a threaded hole, the threaded hole is provided with a mounting screw, the mounting screw penetrates through the front mould plate and is connected with the hook block, the hook block is mounted on the front mould plate through a mounting screw key, the top end of the embedded column is provided with a pull rod, the middle part of the pull rod is provided with an ejector block, a spring is mounted on the ejector block, the spring is embedded on the pull rod, and the pull rod extends into the front mould plate.
2. The complicated inclined position structure of the front and rear dies of the nose cover as claimed in claim 1, wherein the lower end of the stud is provided with a threaded groove.
3. The complicated inclined position structure of the front and rear dies of the nose cover as claimed in claim 1, wherein the spring top and the pull rod are provided with a pressing ring.
4. The complex diagonal position structure of the front die and the rear die of the engine cover as claimed in claim 1, wherein the front die core and the rear die core are automobile engine cover cores.
CN201920346949.5U 2019-03-21 2019-03-21 Complicated oblique position structure of moving of mould around aircraft nose lid Expired - Fee Related CN209955216U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920346949.5U CN209955216U (en) 2019-03-21 2019-03-21 Complicated oblique position structure of moving of mould around aircraft nose lid

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920346949.5U CN209955216U (en) 2019-03-21 2019-03-21 Complicated oblique position structure of moving of mould around aircraft nose lid

Publications (1)

Publication Number Publication Date
CN209955216U true CN209955216U (en) 2020-01-17

Family

ID=69239252

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920346949.5U Expired - Fee Related CN209955216U (en) 2019-03-21 2019-03-21 Complicated oblique position structure of moving of mould around aircraft nose lid

Country Status (1)

Country Link
CN (1) CN209955216U (en)

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

Granted publication date: 20200117

Termination date: 20210321