CN218744243U - Cold drawing deep die for pure titanium interior trim cover-shaped sheet metal part on airplane - Google Patents
Cold drawing deep die for pure titanium interior trim cover-shaped sheet metal part on airplane Download PDFInfo
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- CN218744243U CN218744243U CN202223144009.9U CN202223144009U CN218744243U CN 218744243 U CN218744243 U CN 218744243U CN 202223144009 U CN202223144009 U CN 202223144009U CN 218744243 U CN218744243 U CN 218744243U
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Abstract
The utility model discloses a cold drawing deep mould of pure titanium interior trim cover shape panel beating part on aircraft belongs to mould technical field, aims at solving the current mode of taking the thermoforming and takes the shaping interior cover shape aircraft panel beating part, and the mould is with high costs to thermoforming part speed is slow, long problem consuming time. The die comprises a female die, a male die, a female die holder and a male die holder, and is characterized in that the female die is connected with the female die holder in a positioning manner through a plurality of cylindrical pins, and the female die is fixedly connected with the female die holder through a plurality of second screws; the male die is fixedly connected with the male die holder through a plurality of cylindrical pins; the male die is externally provided with a blank holder which can move up and down. This mould is the deep-drawing mould, compares with traditional deep-drawing, and this mould does not use the ejector pin structure, but adopts the spring structure, and processing preparation is convenient to very big saving the mould cost, this mould possesses the blank holder structure simultaneously, does not produce the fold when the part takes shape.
Description
Technical Field
The utility model relates to the technical field of mold, specifically be a cold drawing deep die suitable for pure titanium interior trim cover shape panel beating part of the same type.
Background
The industrial pure titanium has good oxidation resistance and heat resistance, has good plasticity and is commonly used on airplane parts. The existing inner cover-shaped airplane sheet metal parts are large in batch, if the parts are formed in a hot forming mode, the cost of a die is high, the hot forming speed of the parts is low, and the consumed time is long.
Disclosure of Invention
In view of the technical deficiencies, the purpose of the present invention is to provide a cold drawing die for pure titanium trim cover sheet metal parts on an airplane, which does not wrinkle when the pure titanium trim cover sheet metal parts are formed, is convenient to take, and has low economic cost; the assembly requirement is met, and the rejection rate of parts is reduced.
In order to solve the technical problem, the utility model adopts the following technical scheme:
a cold drawing die for a pure titanium interior trim cover-shaped sheet metal part on an airplane comprises a female die, a male die, a female die holder and a male die holder, and is characterized in that the female die is connected with the female die holder in a positioning mode through a plurality of cylindrical pins
The female die is fixedly connected with the groove seat through a plurality of second screws;
the male die is fixedly connected with the male die holder through a plurality of cylindrical pins;
a blank holder capable of moving up and down is arranged outside the male die, a plurality of first screws are connected to the male die base, and the male die base and the blank holder are in positioning connection through the first screws; a spring is assembled on the first screw and is positioned between the blank holder and the convex die holder;
a plurality of groups of guide sleeves and guide pillars for butt joint guiding are arranged between the male die base and the female die base, the guide sleeves are fixedly arranged on the male die base, and the guide pillars are fixedly arranged on the female die base;
and a plurality of lifting ring screws are arranged on the outer sides of the male die holder and the female die holder.
The beneficial effects of the utility model reside in that: this mould is the deep-drawing mould, compares with traditional deep-drawing, and this mould does not use the ejector pin structure, but adopts the spring structure, and processing preparation is convenient to very big saving the mould cost, this mould possesses the blank holder structure simultaneously, does not produce the fold when the part takes shape.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings 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 creative efforts.
FIG. 1 isbase:Sub>A schematic sectional structure view in the A-A direction ofbase:Sub>A cold drawing die forbase:Sub>A pure titanium trim cover-shaped sheet metal part on an airplane according to the present invention;
FIG. 2 is a schematic view of a B-B direction cross-sectional structure of a cold drawing die for a pure titanium interior trim cover-shaped sheet metal part on an airplane according to the present invention;
fig. 3 is a top view of a cold drawing die for a pure titanium interior trim cover-shaped sheet metal part on an airplane according to the present invention;
fig. 4 is a schematic perspective view of a cold drawing die for a pure titanium interior trim cover-shaped sheet metal part on an aircraft according to the present invention;
fig. 5 is a schematic structural view of the cold drawing die convex die base of the pure titanium interior trim cover-shaped sheet metal part on the aircraft according to the present invention;
fig. 6 is a schematic structural view of a cold drawing deep die blank holder of a pure titanium trim cover-shaped sheet metal part on an airplane according to the present invention;
fig. 7 is a schematic structural view of a cold drawing die cavity of a pure titanium interior trim cover-shaped sheet metal part on an airplane according to the present invention;
fig. 8 is a schematic structural diagram of a sheet metal part of a conventional inner hood-shaped airplane.
Description of the reference numerals:
the die comprises a female die 1, a female die holder 2, a male die 3, a male die holder 4, a blank holder 5, a guide sleeve 6, a guide pillar 7, a spring 8, a first screw 9, a cylindrical pin 10, a lifting ring screw 11 and a second screw 12.
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.
As shown in fig. 1-7, the cold drawing deep die for the pure titanium interior trim cover-shaped sheet metal part on the airplane comprises a female die 1, a male die 3, a female die holder 2 and a male die holder 4, wherein the female die holder 2 is connected with an upper platform of a press machine and is fixed; the female die 1 is connected to the female die holder 2 through the butt joint positioning effect of the cylindrical pin 10 and the fastening effect of the second screw 12; the convex die holder 4 is connected with the lower platform of the press and is fixed; the male die 3 is connected to the male die holder 4 through the butt joint positioning function of the cylindrical pin 10 and the fastening function of the second screw 12;
a blank holder 5 capable of moving up and down is arranged outside the male die 3, a plurality of first screws 9 are connected to the male die base 4, and the male die base 4 and the blank holder 5 are in positioning connection through the first screws 9; a spring 8 is assembled on the first screw 9, and the spring 8 is positioned between the blank holder 5 and the convex die holder 4; the male die 3 and the blank holder 5 are not fixed, the blank holder 5 can move up and down according to the stroke size of the first screw 9, when the male die 3 and the female die 1 are not matched, the spring 8 is in a loose state without compression, when the male die 3 and the female die 1 are matched, the spring 8 is tightly pressed, the compression is generated, elastic force is generated, and after the parts are matched, when the female die 1 is upward, the spring 8 releases the elastic force to push the blank holder 5 to unload.
A plurality of groups of guide sleeves 6 and guide pillars 7 for butt joint and guiding are arranged between the male die holder 4 and the female die holder 2, the guide sleeves 6 are fixedly arranged on the male die holder 4, and the guide pillars 7 are fixedly arranged on the female die holder 2; the guide sleeve 6 and the guide post 7 play a role in butt joint and guide between the male die and the female die 1;
the outer sides of the male die holder 4 and the female die holder 2 are respectively provided with a plurality of lifting bolts 11, and the lifting bolts 11 play a role in assembling and disassembling the die.
The working principle is as follows:
the die is assembled and installed on a press, and the punch-die base 2 is connected with the upper platform and the lower platform of the press respectively and is fixed. The next blank is placed on the blankholder 5 with the edge of the blank aligned with the edge of the blankholder 5. The upper platform of the press machine drives the female die 1 to move downwards, and when the female die 1 is contacted with the blank holder 5
And the female die 1 continues to move downwards, the blank holder 5 generates blank holding force at the moment, the materials around the blank are dragged to be free from generating wrinkles, and when the male die 3 and the female die 1 are closed, the part forming is finished. The female die 1 moves upwards, the spring 8 releases elasticity to push the blank holder 5 to move upwards, and the part loosens and falls off.
It will be apparent to those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (1)
1. A cold drawing die for a pure titanium interior trim cover-shaped sheet metal part on an airplane comprises a female die, a male die, a female die holder and a male die holder, and is characterized in that the female die is in positioning connection with the female die holder through a plurality of cylindrical pins, and the female die is in fastening connection with a groove holder through a plurality of second screws;
the male die is fixedly connected with the male die holder through a plurality of cylindrical pins;
a blank holder capable of moving up and down is arranged outside the male die, a plurality of first screws are connected on the male die base, and the male die base and the blank holder are positioned and connected through the first screws; a spring is assembled on the first screw and positioned between the blank holder and the convex die holder;
a plurality of groups of guide sleeves and guide pillars for butt joint and guiding are arranged between the male die holder and the female die holder, the guide sleeves are fixedly arranged on the male die holder, and the guide pillars are fixedly arranged on the female die holder;
and a plurality of lifting ring screws are arranged on the outer sides of the male die holder and the female die holder.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202223144009.9U CN218744243U (en) | 2022-11-25 | 2022-11-25 | Cold drawing deep die for pure titanium interior trim cover-shaped sheet metal part on airplane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202223144009.9U CN218744243U (en) | 2022-11-25 | 2022-11-25 | Cold drawing deep die for pure titanium interior trim cover-shaped sheet metal part on airplane |
Publications (1)
Publication Number | Publication Date |
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CN218744243U true CN218744243U (en) | 2023-03-28 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202223144009.9U Active CN218744243U (en) | 2022-11-25 | 2022-11-25 | Cold drawing deep die for pure titanium interior trim cover-shaped sheet metal part on airplane |
Country Status (1)
Country | Link |
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CN (1) | CN218744243U (en) |
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2022
- 2022-11-25 CN CN202223144009.9U patent/CN218744243U/en active Active
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