CN213195532U - Forming die for aviation check bolt - Google Patents

Forming die for aviation check bolt Download PDF

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Publication number
CN213195532U
CN213195532U CN202021718797.6U CN202021718797U CN213195532U CN 213195532 U CN213195532 U CN 213195532U CN 202021718797 U CN202021718797 U CN 202021718797U CN 213195532 U CN213195532 U CN 213195532U
Authority
CN
China
Prior art keywords
forming die
forming
mould
die
section mould
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.)
Expired - Fee Related
Application number
CN202021718797.6U
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Chinese (zh)
Inventor
黎福喜
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ma'anshan Liming Fastener Technology Co ltd
Original Assignee
Ma'anshan Liming Fastener Technology Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Ma'anshan Liming Fastener Technology Co ltd filed Critical Ma'anshan Liming Fastener Technology Co ltd
Priority to CN202021718797.6U priority Critical patent/CN213195532U/en
Application granted granted Critical
Publication of CN213195532U publication Critical patent/CN213195532U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to a check bolt forming die for aviation, including mould shell and section mould, mould shell parcel section mould, the section mould includes left section mould and right section mould, set up into die cavity one in the section mould, the lower extreme that becomes die cavity one sets up into die cavity two, the top that becomes die cavity one sets up the air vent, the air vent runs through the top and the external intercommunication of section mould, a die cavity top sets up pours the passageway, the outer end of section mould just is located and is provided with the installation cover in the mould shell, the installation is sheathe in and is set up and pour the mouth, pour the mouth and pour the passageway intercommunication. The utility model has the characteristics of simple structure, it is reasonable.

Description

Forming die for aviation check bolt
Technical Field
The utility model relates to a mould, concretely relates to check bolt forming die for aviation.
Background
At present, various molds and tools for obtaining required products by injection molding, blow molding, extrusion, die casting or forging forming, smelting, stamping and other methods are used in industrial production of molds. 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 method realizes the processing of the shape of an article mainly by changing the physical state of a formed material, and enables a blank to be a tool of a workpiece with a specific shape and size under the action of external force. The method is widely applied to blanking, die forging, cold heading, extrusion, powder metallurgy part pressing, pressure casting and the forming processing of compression molding or injection molding of products such as engineering plastics, rubber, ceramics and the like. Most of the existing forming dies are designed in an integrated mode, and products are difficult to take out after forming is completed, so that the overall working efficiency is lower.
SUMMERY OF THE UTILITY MODEL
The aforesaid that exists is not enough among the prior art, the utility model provides an anti loosening bolt forming die for aviation to overcome the above-mentioned technical problem that exists among the prior art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides an aviation is with check bolt forming die, includes mould shell and section mould, mould shell parcel section mould, characterized by: the forming die comprises a left forming die and a right forming die, a first forming cavity is arranged in the forming die, a second forming cavity is arranged at the lower end of the first forming cavity, the left forming die and the right forming die respectively account for half of the first forming cavity and the second forming cavity, an air vent is arranged at the top of the first forming cavity, the air vent penetrates through the top of the forming die and is communicated with the outside, a pouring channel is arranged at the top of the first forming cavity, an installation sleeve is arranged at the outer end of the forming die and located in a die shell, a pouring opening is formed in the installation sleeve, and the pouring opening is communicated with the pouring.
The utility model discloses in, the edge that becomes die cavity one sets up the chamfer.
The utility model discloses in, the lower extreme of installation cover and the upper end phase-match of section mould.
The utility model discloses in, left side section mould is unanimous with right side section mould shape, size.
The utility model discloses in, set up the notch of the whole die holding of being convenient for on the mould shell.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. the forming die is composed of a left forming die and a right forming die, so that the formed product can be taken out by separating the left forming die and the right forming die after the product is formed.
2. The edge of the section mould is provided with the chamfer, so that the product can be conveniently demoulded after the forming is finished, and the production efficiency of the product is improved by improving the demoulding efficiency of the product.
Drawings
FIG. 1 is a schematic structural diagram of a preferred embodiment of the present invention;
in the figure: 1-a mould shell; 2, forming a die; 3-left mould; 4-right section mould; 5, forming a first forming cavity; 6, forming a second forming cavity; 7, air vents; 8, pouring a channel; 9, mounting a sleeve; 10, pouring a hole; and 11, chamfering.
Detailed Description
In order to facilitate understanding of the present invention, the present invention will be described more fully hereinafter with reference to the accompanying drawings. The preferred embodiments of the present invention are shown in the drawings. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used herein in the description of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention.
Fig. 1 is a schematic view of a preferred embodiment of the present invention.
The utility model provides an aviation is with check bolt forming die, includes mould shell 1 and section mould 2, mould shell 1 parcel section mould 2, characterized by: the forming die 2 comprises a left forming die 3 and a right forming die 4, a forming cavity I (5) is arranged in the forming die 2, a forming cavity II 6 is arranged at the lower end of the forming cavity I5, the left forming die 3 and the right forming die 4 respectively account for half of the forming cavity I5 and the forming cavity II 6, an air vent 7 is arranged at the top of the forming cavity I5, the air vent 7 penetrates through the top of the forming die 2 to be communicated with the outside, a pouring channel 8 is arranged at the top of the forming cavity I5, the outer end of the forming die 2 is located in a mounting sleeve 9 which is arranged in the die shell 1, a pouring opening 10 is arranged on the mounting sleeve 9, and the pouring opening 10 is communicated with the pouring.
In the present invention, the edge of the forming cavity one 5 is provided with a chamfer 11.
The utility model discloses in, the lower extreme of installation cover 9 and the upper end phase-match of section mould 2.
In the utility model, the left section mould 3 is identical to the right section mould 4 in shape and size.
The utility model discloses in, the last notch that sets up the whole die holding of being convenient for of mould shell 1.
Under the normal working condition, the raw materials flow through the pouring channel from the pouring opening to enter the first molding cavity and the second molding cavity, redundant gas is discharged from the vent hole, after the molding is finished, an operator takes down the mounting sleeve and takes down the shell, so that the left die and the right die are separated to take out a product.
The above examples merely represent a practical way of implementing the present invention, which is described in more detail and in greater detail, but are not to be construed as limiting the scope of the invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.

Claims (5)

1. The utility model provides an aviation is with check bolt forming die, includes mould shell (1) and section mould (2), mould shell (1) parcel section mould (2), characterized by: the forming die (2) comprises a left forming die (3) and a right forming die (4), a forming cavity I (5) is arranged in the forming die (2), a forming cavity II (6) is arranged at the lower end of the forming cavity I (5), the left forming die (3) and the right forming die (4) respectively occupy a half of the forming cavity I (5) and the forming cavity II (6), an air vent (7) is arranged at the top of the forming cavity I (5), the air vent (7) penetrates through the top of the forming die (2) to be communicated with the outside, a pouring channel (8) is arranged at the top of the forming cavity I (5), an installation sleeve (9) is arranged at the outer end of the forming die (2) and is located in the die shell (1), a pouring opening (10) is formed in the installation sleeve (9), and the pouring opening (10) is communicated with the pouring channel (8).
2. The forming die for the aviation check bolt as claimed in claim 1, wherein the forming die comprises: and a chamfer (11) is arranged on the edge of the forming cavity I (5).
3. The forming die for the aviation check bolt as claimed in claim 1, wherein the forming die comprises: the lower end of the mounting sleeve (9) is matched with the upper end of the section mould (2).
4. The forming die for the aviation check bolt as claimed in claim 1, wherein the forming die comprises: the left mould (3) and the right mould (4) are consistent in shape and size.
5. The forming die for the aviation check bolt as claimed in claim 1, wherein the forming die comprises: the shuttering (1) is provided with a notch for facilitating the installation of the whole die.
CN202021718797.6U 2020-08-18 2020-08-18 Forming die for aviation check bolt Expired - Fee Related CN213195532U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021718797.6U CN213195532U (en) 2020-08-18 2020-08-18 Forming die for aviation check bolt

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021718797.6U CN213195532U (en) 2020-08-18 2020-08-18 Forming die for aviation check bolt

Publications (1)

Publication Number Publication Date
CN213195532U true CN213195532U (en) 2021-05-14

Family

ID=75839539

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021718797.6U Expired - Fee Related CN213195532U (en) 2020-08-18 2020-08-18 Forming die for aviation check bolt

Country Status (1)

Country Link
CN (1) CN213195532U (en)

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

Granted publication date: 20210514