CN214053384U - Aviation terminal stamping die - Google Patents

Abstract

The utility model discloses an aviation terminal stamping die, including shell, fixed plate, mould piece, last module, stopper and baffle, the lower extreme of shell is provided with the bottom plate, and the upper end of bottom plate is provided with first fixing bolt, the fixed plate sets up in the inside below of shell, and the surface rear of fixed plate is provided with electric telescopic sleeve, and electric telescopic sleeve's surperficial rear is provided with electric telescopic handle simultaneously, the mould piece sets up in the inside below of shell, and is provided with the polyethylene layer above the mould piece surface, and the surface top on polyethylene layer is provided with the screw rod simultaneously, go up the module setting in the upper end of shell, and the lower extreme of going up the module is provided with the electric lift loop bar, the stopper sets up the upper end at the shell. This aviation terminal stamping die through stopper and second fixing bolt's setting, goes up the module and rocks when preventing the punching press, causes the aviation terminal size of punching press to cause the error, can't satisfy user's demand, has improved the result of use of this stamping die utensil.

Description

Aviation terminal stamping die

Technical Field

The utility model relates to an aviation correlation technique field specifically is an aviation terminal stamping die.

Background

Aviation, a complex and strategic human activity, refers to the flight of an aircraft in the earth's atmosphere and many fields related thereto, such as scientific research and education, industrial manufacturing, public transportation, professional operations, aviation, national defense and military, government management, etc., by utilizing air space and aircraft, the aviation activity can be subdivided into many independent industries and fields, typically, aeronautical manufacturing, civil aviation, etc., and it is often seen that people use this term from their respective fields, its connotation and richness and variety.

But the aviation terminal stamping die who uses at present does not possess the setting of stopper, can't carry out effectual limiting displacement to it in the use, leads to the aviation terminal size of punching press to cause the error easily, makes its loss unable use.

Disclosure of Invention

An object of the utility model is to provide an aviation terminal stamping die to the aviation terminal stamping die who provides in solving above-mentioned background art at present uses does not possess the setting of stopper, can't carry out effectual limiting displacement to it in the use, leads to the aviation terminal size of punching press to cause the error easily, makes the unable problem of using of its loss.

In order to achieve the above object, the utility model provides a following technical scheme: an aviation terminal stamping die comprises a shell, a fixing plate, a die block, an upper module, a limiting block and a baffle plate, wherein a bottom plate is arranged at the lower end of the shell, a first fixing bolt is arranged at the upper end of the bottom plate, the fixing plate is arranged below the inner part of the shell, an electric telescopic sleeve is arranged behind the surface of the fixing plate, an electric telescopic rod is arranged behind the surface of the electric telescopic sleeve, the die block is arranged below the inner part of the shell, a polyethylene layer is arranged above the surface of the die block, a screw rod is arranged above the surface of the polyethylene layer, the upper module is arranged at the upper end of the shell, an electric lifting sleeve rod is arranged at the lower end of the upper module, the limiting block is arranged at the upper end of the shell, a second fixing bolt is arranged at the upper end of the limiting block, a fixing block is arranged at the upper end of the second fixing bolt, a limiting groove is formed in the fixing block, the baffle is arranged on the front surface of the shell, and a hinge is arranged at the lower end of the baffle.

Preferably, the shell is in threaded connection with the bottom plate through a first fixing bolt, and the first fixing bolt and the bottom plate are vertically distributed.

Preferably, the electric telescopic rod, the electric telescopic sleeve and the fixed plate form a telescopic structure, and the electric telescopic sleeve is symmetrically arranged with a central axis of the fixed plate.

Preferably, the polyethylene layer is movably connected with the die block through a screw, and the size of the screw is smaller than that of the die block.

Preferably, the upper module, the electric lifting sleeve rod and the shell form a lifting structure, and the electric lifting sleeve rod and the shell are vertically distributed.

Preferably, the limiting block is in threaded connection with the upper module through a second fixing bolt, and the upper module is higher than the limiting block.

Preferably, the baffle, the hinges and the shell form a rotating structure, and the hinges are distributed on the baffle at equal intervals.

Compared with the prior art, the beneficial effects of the utility model are that:

1. according to the aviation terminal stamping die, due to the arrangement of the limiting block and the second fixing bolt, the upper die block is prevented from shaking during stamping, the size of a stamped aviation terminal is prevented from causing errors, the requirements of a user cannot be met, and the using effect of the stamping die is improved;

2. according to the aviation terminal stamping die, the polyethylene layer and the screw rod are arranged, so that the stamping die is more wear-resistant in use, the service life is longer, the use cost of the stamping die is saved, and the utilization rate of the stamping die is improved;

3. this aviation terminal stamping die through the setting of baffle and hinge, can protect the operator when this stamping die is punching press, causes the injury to the operator when preventing the punching press, has improved the rate of utilization of this die utensil.

Drawings

Fig. 1 is a schematic view of the front cross-sectional structure of the present invention;

FIG. 2 is a schematic view of the front view of the present invention;

FIG. 3 is a schematic side view of the present invention;

fig. 4 is an enlarged schematic structural view of a portion a in fig. 1 according to the present invention.

In the figure: 1. a housing; 2. a base plate; 3. a first fixing bolt; 4. a fixing plate; 5. an electric telescopic sleeve; 6. an electric telescopic rod; 7. a mold block; 8. a polyethylene layer; 9. a screw; 10. an upper module; 11. an electric lifting loop bar; 12. a limiting block; 13. a second fixing bolt; 14. a fixed block; 15. a limiting groove; 16. a baffle plate; 17. and (7) a hinge.

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.

Referring to fig. 1-4, the present invention provides a technical solution: an aviation terminal stamping die comprises a shell 1, a fixing plate 4, a die block 7, an upper module 10, a limiting block 12 and a baffle 16, wherein a bottom plate 2 is arranged at the lower end of the shell 1, a first fixing bolt 3 is arranged at the upper end of the bottom plate 2, the fixing plate 4 is arranged below the inner part of the shell 1, an electric telescopic sleeve 5 is arranged behind the surface of the fixing plate 4, an electric telescopic rod 6 is arranged behind the surface of the electric telescopic sleeve 5, the die block 7 is arranged below the inner part of the shell 1, a polyethylene layer 8 is arranged above the surface of the die block 7, a screw 9 is arranged above the surface of the polyethylene layer 8, the upper module 10 is arranged at the upper end of the shell 1, an electric lifting sleeve rod 11 is arranged at the lower end of the upper module 10, the limiting block 12 is arranged at the upper end of the shell 1, a second fixing bolt 13 is arranged at the upper end of the limiting block 12, a fixing block 14 is arranged at the upper end of the second fixing bolt 13, and the inside of fixed block 14 is provided with spacing groove 15, and baffle 16 sets up the surface in the front of shell 1, and the lower extreme of baffle 16 is provided with hinge 17.

Further, shell 1 is through first fixing bolt 3 and 2 threaded connection of bottom plate, and first fixing bolt 3 and bottom plate 2 are the vertical distribution, through first fixing bolt 3 and bottom plate 2's setting, can possess effectual stability to this stamping die when using, and the too big its rocking that leads to of pressure when preventing the punching press has improved the practicality of this die utensil.

Further, electric telescopic handle 6, electric telescopic sleeve 5 and fixed plate 4 constitute extending structure, and electric telescopic sleeve 5 sets up with the axis symmetry of fixed plate 4, through the setting of electric telescopic sleeve 5, electric telescopic handle 6 and fixed plate 4, can release the aviation terminal that the punching press is good through electric telescopic handle 6, and convenient to use person takes, has improved this die's result of use.

Further, polyethylene layer 8 passes through screw rod 9 and mould piece 7 swing joint, and the size of screw rod 9 is less than the size of mould piece 7, through polyethylene layer 8 and screw rod 9's setting, can make this stamping die wear-resisting more when using, and life is longer, has improved the rate of utilization of this stamping die utensil.

Further, go up module 10, electric lift loop bar 11 and shell 1 and constitute elevation structure, and electric lift loop bar 11 and shell 1 are the vertical distribution, through last module 10 and electric lift loop bar 11's setting, make this stamping die can go up and down the punching press automatically when using, be more convenient for save stamping time, improved the practicality of this die stamping utensil.

Further, stopper 12 passes through second fixing bolt 13 and last module 10 threaded connection, and goes up module 10 highly be higher than stopper 12's height, through stopper 12 and second fixing bolt 13's setting, goes up module 10 and rocks during the prevention punching press, causes the aviation terminal size of punching press to cause the error, has improved the result of use of this die utensil.

Further, baffle 16, hinge 17 and shell 1 constitute revolution mechanic, and hinge 17 is equidistant distribution on baffle 16, through baffle 16 and hinge 17's setting, can protect the operator when this stamping die is punching press, causes the injury to the operator when preventing the punching press, has improved the rate of utilization of this die utensil.

The working principle is as follows: for the aviation terminal stamping die, firstly, an external power supply is switched on, the shell 1 is clockwise screwed through the first fixing bolt 3 to be in threaded connection with the bottom plate 2, the stamping die can have effective stability when in use, the phenomenon that the stamping die shakes due to overlarge pressure during stamping is prevented, then the electric telescopic rod 6 is in telescopic connection with the fixing plate 4 through the electric telescopic sleeve 5, the stamped aviation terminal can be pushed out through the electric telescopic rod 6 to be convenient for a user to take, then the polyethylene layer 8 is clockwise rotated through the screw rod 9 to be movably connected with the die block 7, the stamping die can be more wear-resistant during use, the service life is longer, the upper die block 10 is in lifting connection with the shell 1 through the electric lifting sleeve rod 11, the stamping die can be automatically lifted and stamped during use and is more convenient for an operator to use, and then the limiting block 12 is clockwise screwed through the second fixing bolt 13 to be in threaded connection with the upper die block 10, can be through the identical connection of stopper 12 spacing groove 15, module 10 rocks when preventing the punching press, the aviation terminal size that causes the punching press leads to the fact the error, at last pass through hinge 17 and 1 swivelling joint of shell with baffle 16, can protect the operator when this stamping die punching press, prevent that the impulsive force is too big to cause the injury to the operator, wherein the model of electric telescopic sleeve 5 is XC860, electric telescopic handle 6's model is XC860, electric lift loop bar 11's model is XTL100, just so accomplish whole aviation terminal stamping die's use.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. The utility model provides an aviation terminal stamping die, includes shell (1), fixed plate (4), mould piece (7), goes up module (10), stopper (12) and baffle (16), its characterized in that: the lower end of the shell (1) is provided with a bottom plate (2), the upper end of the bottom plate (2) is provided with a first fixing bolt (3), the fixed plate (4) is arranged below the inner part of the shell (1), the surface rear part of the fixed plate (4) is provided with an electric telescopic sleeve (5), the surface rear part of the electric telescopic sleeve (5) is provided with an electric telescopic rod (6), the mold block (7) is arranged below the inner part of the shell (1), the surface upper part of the mold block (7) is provided with a polyethylene layer (8), the surface upper part of the polyethylene layer (8) is provided with a screw rod (9), the upper module (10) is arranged at the upper end of the shell (1), the lower end of the upper module (10) is provided with an electric lifting sleeve rod (11), the limit block (12) is arranged at the upper end of the shell (1), and the upper end of the limit block (12) is provided with a second fixing bolt (13), the upper end of the second fixing bolt (13) is provided with a fixing block (14), a limiting groove (15) is formed in the fixing block (14), the baffle (16) is arranged on the front surface of the shell (1), and a hinge (17) is arranged at the lower end of the baffle (16).

2. The aviation terminal stamping die of claim 1, wherein: the shell (1) is in threaded connection with the bottom plate (2) through the first fixing bolt (3), and the first fixing bolt (3) and the bottom plate (2) are vertically distributed.

3. The aviation terminal stamping die of claim 1, wherein: the electric telescopic rod (6), the electric telescopic sleeve (5) and the fixed plate (4) form a telescopic structure, and the electric telescopic sleeve (5) is symmetrically arranged by the central axis of the fixed plate (4).

4. The aviation terminal stamping die of claim 1, wherein: the polyethylene layer (8) is movably connected with the die block (7) through a screw rod (9), and the size of the screw rod (9) is smaller than that of the die block (7).

5. The aviation terminal stamping die of claim 1, wherein: go up module (10), electric lift loop bar (11) and shell (1) constitution elevation structure, and electric lift loop bar (11) and shell (1) are vertical distribution.

6. The aviation terminal stamping die of claim 1, wherein: the limiting block (12) is in threaded connection with the upper module (10) through a second fixing bolt (13), and the height of the upper module (10) is higher than that of the limiting block (12).

7. The aviation terminal stamping die of claim 1, wherein: the baffle (16), the hinges (17) and the shell (1) form a rotating structure, and the hinges (17) are distributed on the baffle (16) at equal intervals.

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