CN213317188U

CN213317188U - Stamping die for producing airplane mandrel

Info

Publication number: CN213317188U
Application number: CN202021808597.XU
Authority: CN
Inventors: 孙建毅
Original assignee: Guizhou Anshun Longfei Auto Parts Co ltd
Current assignee: Guizhou Anshun Longfei Auto Parts Co ltd
Priority date: 2020-08-26
Filing date: 2020-08-26
Publication date: 2021-06-01
Anticipated expiration: 2030-08-26

Abstract

The utility model discloses an aircraft mandrel production stamping die, comprising a main body, the lower extreme surface of main part is provided with the bed die, the both sides surface of bed die all is provided with protection mechanism, the upper end surface of bed die is provided with cleans the mechanism, the upper end surface that cleans the mechanism is provided with the connecting rod. A aircraft mandrel production stamping die, be equipped with protection mechanism and clean the mechanism, can use the back at stamping die, install the bed die both sides with the protective sheath through link and spread groove, prevent that the bed die from receiving the collision and causing the damage of mould, the mechanism that cleans of setting, can be before stamping die uses, install the mould top with the connecting piece, the inside clean silver of mechanism can clean the dust that the connecting rod surface was gathered, the dust that prevents the connecting rod surface and gathers influences the use of mould, bring better use prospect.

Description

Stamping die for producing airplane mandrel

Technical Field

The utility model relates to a stamping die field, in particular to aircraft mandrel production stamping die.

Background

The stamping die for producing the airplane mandrel is a stamping die for producing parts in an airplane model, can be conveniently used by people, and is simple in structure and convenient to operate.

There is certain drawback when using in current aircraft mandrel production stamping die, at first, in the use, the mould bottom receives the collision easily and damages, has certain inconvenience, and secondly, the connecting rod outer wall gathers the dust easily, and the use of giving people has brought certain adverse effect, for this reason, we provide an aircraft mandrel production stamping die.

SUMMERY OF THE UTILITY MODEL

The utility model discloses a main aim at provides an aircraft mandrel production stamping die can effectively solve the problem among the background art.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an aircraft mandrel production stamping die, includes the main part, the lower extreme surface of main part is provided with the bed die, the both sides surface of bed die all is provided with protection mechanism, the upper end surface of bed die is provided with cleans the mechanism, the upper end surface that cleans the mechanism is provided with the connecting rod, the upper end surface of connecting rod is provided with the mould, protection mechanism's inside is provided with the link, the lower extreme surface of link is provided with the protective sheath, the lower extreme surface of protective sheath is provided with shock pad, the inside that cleans the mechanism is provided with the connecting piece, the upper end surface of connecting piece is provided with connects the shell, the jack has been seted up at the middle part of connecting the shell, the inner wall of jack is.

The protection mechanism is mainly beneficial to protecting the bottom of the mold.

The cleaning mechanism is mainly beneficial to cleaning dust accumulated on the surface of the connecting rod.

Preferably, the outer surface of the lower end of the connecting frame is fixedly connected with the outer surface of the upper end of the protective sleeve, an adhesive is arranged between the protective sleeve and the damping gasket, and the outer surface of the lower end of the protective sleeve is fixedly connected with the outer surface of the upper end of the damping gasket through the adhesive.

Preferably, the outer surface of the upper end of the connecting piece is fixedly connected with the outer surface of the lower end of the connecting shell, a fixing groove is formed between the clean cotton sliver and the jack, and the outer surface of one side of the clean cotton sliver is fixedly connected with the inner wall of the jack through the fixing groove.

Preferably, a fixing hole is formed between the upper die and the connecting rod, and the outer surface of the lower end of the upper die is movably connected with the outer surface of the upper end of the connecting rod through the fixing hole.

Preferably, the outer surface of the lower end of the connecting rod is fixedly connected with the outer surface of the upper end of the lower die, and the outer surfaces of the two ends of the lower die are respectively provided with a connecting groove.

Preferably, the outer surface of one side of the protection mechanism is movably connected with the outer surface of one side of the lower die through the connecting frame and the connecting groove.

Preferably, the outer surface of the lower end of the cleaning mechanism is movably connected with the outer surface of the upper end of the lower die through a connecting piece, and one end of the connecting rod penetrates through the inner wall of the connecting shell.

Compared with the prior art, the utility model discloses following beneficial effect has: this aircraft mandrel produces stamping die, protection mechanism through setting up, use the back at stamping die, the lower mould both sides are installed with the protective sheath to accessible link and spread groove, prevent that the lower mould from receiving the damage that the collision caused the mould, be favorable to improving the life of mould, clean the mechanism through setting up, can be before stamping die uses, mould top is installed to the connecting piece, the inside clean silver of mechanism can clean the dust that the connecting rod surface was gathered, prevent that the dust that the connecting rod surface was gathered from influencing the use of mould, be favorable to people's use, whole aircraft mandrel produces stamping die simple structure, and convenient for operation, the effect of use is better for traditional mode.

Drawings

Fig. 1 is the overall structure schematic diagram of the stamping die for producing the airplane mandrel of the present invention.

Fig. 2 is the overall structure elevation view of the stamping die for producing the airplane mandrel of the present invention.

Fig. 3 is an enlarged view of the protection mechanism 2 of fig. 1 of the aircraft mandrel production stamping die of the present invention.

Fig. 4 is an enlarged view of the cleaning mechanism 4 of fig. 1 of the stamping die for producing the airplane spindle according to the present invention.

In the figure: 1. a main body; 2. a protection mechanism; 3. a lower die; 4. a cleaning mechanism; 5. an upper die; 6. a connecting rod; 201. a shock-absorbing pad; 202. a connecting frame; 203. a protective sleeve; 401. a connecting member; 402. connecting the shell; 403. a jack; 404. and cleaning the cotton sliver.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

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. 1-4, an aircraft mandrel production stamping die comprises a main body 1, a lower die 3 is arranged on the outer surface of the lower end of the main body 1, protection mechanisms 2 are arranged on the outer surfaces of two sides of the lower die 3, a cleaning mechanism 4 is arranged on the outer surface of the upper end of the lower die 3, a connecting rod 6 is arranged on the outer surface of the upper end of the cleaning mechanism 4, an upper die 5 is arranged on the outer surface of the upper end of the connecting rod 6, a connecting frame 202 is arranged inside the protection mechanism 2, a protective sleeve 203 is arranged on the outer surface of the lower end of the connecting frame 202, a shock absorption gasket 201 is arranged on the outer surface of the lower end of the protective sleeve 203, a connecting piece 401 is arranged inside the cleaning mechanism 4, a connecting shell 402 is arranged.

Further, the lower extreme surface of link 202 and the upper end surface fixed connection of protective sheath 203 are provided with the adhesive between protective sheath 203 and the shock attenuation gasket 201, and the lower extreme surface of protective sheath 203 passes through the adhesive and is connected with the upper end surface fixed connection of shock attenuation gasket 201, is favorable to protecting the mould bottom.

Further, the outer surface of the upper end of the connecting piece 401 is fixedly connected with the outer surface of the lower end of the connecting shell 402, a fixing groove is formed between the cleaning cotton sliver 404 and the insertion hole 403, and the outer surface of one side of the cleaning cotton sliver 404 is fixedly connected with the inner wall of the insertion hole 403 through the fixing groove, so that dust accumulated on the surface of the connecting rod can be cleaned conveniently.

Further, be provided with the fixed orifices between last mould 5 and the connecting rod 6, the lower extreme surface of going up mould 5 passes through the upper end surface swing joint of fixed orifices and connecting rod 6, is favorable to the connection stability between the mould.

Further, the lower extreme surface of connecting rod 6 and the upper end outer fixed surface of bed die 3 are connected, and the spread groove has all been seted up to the both ends surface of bed die 3, are favorable to the stable in structure of mould.

Further, the outer surface of one side of the protection mechanism 2 is movably connected with the outer surface of one side of the lower die 3 through the connecting frame 202 and the connecting groove, which is beneficial to the stable connection between the protection mechanism 2 and the main body 1.

Furthermore, the outer surface of the lower end of the cleaning mechanism 4 is movably connected with the outer surface of the upper end of the lower die 3 through a connecting piece 401, and one end of a connecting rod 6 penetrates through the inner wall of the connecting shell 402, so that the stable connection between the cleaning mechanism 4 and the main body 1 is facilitated.

It should be noted that the utility model relates to a stamping die for producing airplane mandrel, before using, the user takes off the protection mechanism 2 from the stamping die, installs the lower die 3 and the upper die 5 on the stamping machine, and then can complete the installation of the whole stamping die, the protection mechanism 2 is arranged, after the stamping die is used, the protection sleeves 203 can be arranged on the two sides of the lower die through the connecting frame 202 and the connecting grooves, the lower die 3 is prevented from being damaged by collision, the service life of the die is prolonged, its setting clean mechanism 4, can be before stamping die uses, install connecting piece 401 mould 5 top, the inside clean silver 404 of mechanism can clean the dust that the connecting rod 6 surface was gathered, prevents that the dust that the connecting rod 6 surface was gathered from influencing the use of mould, is favorable to people's use, and is comparatively practical.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. An aircraft mandrel production stamping die, comprising a main body (1), characterized in that: the outer surface of the lower end of the main body (1) is provided with a lower die (3), the outer surfaces of two sides of the lower die (3) are provided with protection mechanisms (2), the outer surface of the upper end of the lower die (3) is provided with a cleaning mechanism (4), the outer surface of the upper end of the cleaning mechanism (4) is provided with a connecting rod (6), the outer surface of the upper end of the connecting rod (6) is provided with an upper die (5), the inside of the protection mechanism (2) is provided with a connecting frame (202), the outer surface of the lower end of the connecting frame (202) is provided with a protective sleeve (203), the outer surface of the lower end of the protective sleeve (203) is provided with a damping gasket (201), the inside of the cleaning mechanism (4) is provided with a connecting piece (401), the outer surface of the upper end of the connecting piece, the inner wall of the jack (403) is provided with a cleaning cotton sliver (404).

2. The aircraft mandrel production stamping die of claim 1, wherein: the outer surface of the lower end of the connecting frame (202) is fixedly connected with the outer surface of the upper end of the protective sleeve (203), an adhesive is arranged between the protective sleeve (203) and the damping gasket (201), and the outer surface of the lower end of the protective sleeve (203) is fixedly connected with the outer surface of the upper end of the damping gasket (201) through the adhesive.

3. The aircraft mandrel production stamping die of claim 1, wherein: the outer surface of the upper end of the connecting piece (401) is fixedly connected with the outer surface of the lower end of the connecting shell (402), a fixing groove is formed between the cleaning cotton sliver (404) and the jack (403), and the outer surface of one side of the cleaning cotton sliver (404) is fixedly connected with the inner wall of the jack (403) through the fixing groove.

4. The aircraft mandrel production stamping die of claim 1, wherein: a fixing hole is formed between the upper die (5) and the connecting rod (6), and the outer surface of the lower end of the upper die (5) is movably connected with the outer surface of the upper end of the connecting rod (6) through the fixing hole.

5. The aircraft mandrel production stamping die of claim 1, wherein: the outer surface of the lower end of the connecting rod (6) is fixedly connected with the outer surface of the upper end of the lower die (3), and the outer surfaces of the two ends of the lower die (3) are respectively provided with a connecting groove.

6. The aircraft mandrel production stamping die of claim 1, wherein: the outer surface of one side of the protection mechanism (2) is movably connected with the outer surface of one side of the lower die (3) through a connecting frame (202) and a connecting groove.

7. The aircraft mandrel production stamping die of claim 1, wherein: the outer surface of the lower end of the cleaning mechanism (4) is movably connected with the outer surface of the upper end of the lower die (3) through a connecting piece (401), and one end of a connecting rod (6) penetrates through the inner wall of the connecting shell (402).