CN222679238U - Forming die of aircraft cable protection casing - Google Patents

Abstract

The utility model discloses a molding die for an aircraft cable shield, comprising a bottom plate, a fixed die fixedly arranged at the top of the bottom plate, positioning rods fixedly arranged at both sides of the fixed die, positioning rings movably sleeved on the outer side of the positioning rods, a top plate fixedly arranged at the top of the positioning rods, and a hydraulic rod fixedly arranged at the bottom of the top plate. After the punching of the utility model is completed, the hydraulic rod drives the movable die to reset, and at this time, the removal template is driven to move upward by the connecting rod, and the machine cable shield inside the molding groove is squeezed out to be separated from the molding groove, without manual removal work, and mechanical extrusion is performed at the same time to prevent the machine cable shield from being adsorbed inside the molding groove, which is laborious to remove manually; when the movable die is reset, the connecting rod moves upward until the extrusion control switch is pressed, thereby turning off the electromagnet, and the spring instantly releases the elastic force, driving the extrusion block to bounce toward the machine cable shield, and the machine cable shield is completely ejected, thereby completing the complete removal of the machine cable shield.

Description

Forming die of aircraft cable protection casing

Technical Field

The utility model relates to the field of mould equipment, in particular to a forming mould for an aircraft cable protective cover.

Background

The mould is a mould and tool for producing the needed products by injection moulding, blow moulding, extrusion, die casting or forging, smelting, stamping and other methods in industrial production, in short, the mould is a tool for producing molded articles, the tool is composed of various parts, and different moulds are composed of different parts, and the processing of the appearance of the articles is realized mainly by changing the physical state of the molded materials, namely the model is named as the "industrial master".

The cable protection casing of aircraft need utilize stamping die to go on when processing, settle the sheetmetal on the mould, then utilize the punching press to make the sheetmetal at shaping inslot portion shaping, the product is located shaping inslot portion after the shaping, still need the manual work to take out it, has reduced fan cable protection casing's machining efficiency, so need a device to solve above-mentioned problem urgently.

Disclosure of utility model

The utility model aims to provide a forming die for an aircraft cable protective cover, which aims to solve the problems in the background technology.

In order to achieve the purpose, the forming die of the aircraft cable protective cover comprises a bottom plate, wherein the top end of the bottom plate is fixedly provided with a fixed die, two sides of the fixed die are fixedly provided with positioning rods, the outer sides of the positioning rods are movably sleeved with positioning rings, movable dies are fixedly arranged between the positioning rings, the top ends of the positioning rods are fixedly provided with top plates, the bottom ends of the top plates are fixedly provided with hydraulic rods, the lower ends of the hydraulic rods are fixed at the top end positions of the movable dies, when the forming die is used, metal plates are arranged in forming grooves at the bottom ends of the fixed dies, then the hydraulic rods are started, the movable dies are driven to move downwards, stamping forming work is carried out on metal plates in the forming grooves of the fixed dies, meanwhile, the movable dies are positioned along the positioning rods by the positioning rings, accurate stamping work of the movable dies is guaranteed, a die taking mechanism convenient for taking out is arranged in the fixed die, the top end of the bottom plate is provided with an ejecting mechanism for releasing products, the die taking mechanism comprises connecting rods and a die taking plate, the connecting rods are fixed on the hydraulic rods, the die taking plate is fixed at the top end positions of the connecting rods, after the connecting rods are fixed, and after the connecting rods are driven to move downwards, the movable dies are driven to move upwards, the movable dies are driven to take out the metal plates, and the metal plates are required to be extruded out and form the products by the metal plates, and are extruded out of the metal plates, and can be extruded and removed from the forming grooves by the metal plates through the forming grooves through the forming die.

Preferably, the ejection mechanism comprises a vertical plate, a movable rod, a spring, an electromagnet, a control switch and an extrusion block, wherein the vertical plate is fixed at the top end of the bottom plate, the movable rod is movably inserted and arranged on the vertical plate, the electromagnet is embedded and fixed on one side of the vertical plate, the spring is fixed on one side of the electromagnet, the extrusion block is fixed on one side of the movable rod, one side of the extrusion block is fixed on the spring, the control switch is embedded and fixed at the lower end of the hydraulic rod, when the movable die is reset, the connecting rod moves upwards until the control switch is extruded, so that the electromagnet is closed, the spring instantly releases elasticity to drive the extrusion block to stretch towards a product, the product is completely ejected, and the product is completely taken out.

Preferably, the connecting rod movably penetrates into the fixed die.

Preferably, the upper surface of the template is flush with the upper surface of the forming groove inside the fixed die.

Preferably, the movable rods are arranged in two, and are symmetrically inserted in the positions on two sides of the vertical plate.

Preferably, the extrusion block is made of magnetic metal, the control switch is electrically connected with the electromagnet, and the spring is in a compressed state.

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

After the stamping is completed, the hydraulic rod drives the movable die to reset, the die taking plate is driven to move upwards through the connecting rod at the moment, the machine cable protective cover in the forming groove is extruded to be separated from the forming groove, the machine cable protective cover does not need to be manually taken out to work, meanwhile, the machine cable protective cover is prevented from being adsorbed in the forming groove and is manually taken out to be laborious, when the movable die is reset, the connecting rod moves upwards until the control switch is extruded to be closed, the spring instantly releases the elastic force to drive the extrusion block to stretch out the product, and the machine cable protective cover is completely ejected out, so that the machine cable protective cover is completely taken out.

Drawings

FIG. 1 is a schematic diagram of the overall structure of a molding die of an aircraft cable protective cover according to the utility model;

FIG. 2 is a cross-sectional view of a molding die of an aircraft cable protective cover according to the present utility model;

fig. 3 is an enlarged schematic view of a molding die a of an aircraft cable shield according to the present utility model.

The drawing comprises a bottom plate 1, a fixed die 2, a movable die 3, a positioning rod 4, a positioning ring 5, a top plate 6, a hydraulic rod 7, a control switch 8, a connecting rod 9, a connecting rod 10, a die taking plate 11, an extrusion block 12, a vertical plate 13, a movable rod 14, an electromagnet 15 and a spring.

Detailed Description

The following description of the embodiments of the present utility model will be given with reference to the accompanying drawings, which are given by way of example only, and not by way of limitation. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-3, the utility model provides a forming die of an aircraft cable protection cover, which comprises a bottom plate 1, the top of the bottom plate 1 is fixedly provided with a fixed die 2 through a mounting frame, two sides of the fixed die 2 are fixedly welded with positioning rods 4, the outer sides of the positioning rods 4 are movably sleeved with positioning rings 5, a movable die 3 is fixedly welded between the positioning rings 5, a top plate 6 is fixedly welded at the top end of the positioning rods 4, a hydraulic rod 7 is fixedly arranged at the bottom end of the top plate 6 through the mounting frame, the lower end of the hydraulic rod 7 is fixedly arranged at the top end position of the movable die 3 through bolts, a metal plate is arranged in a forming groove at the bottom end of the fixed die 2 in use, then the hydraulic rod 7 is started, the hydraulic rod 7 drives the movable die 3 to move downwards, metal sheets in the forming groove of the fixed die 2 are subjected to stamping forming work, meanwhile, a die taking mechanism convenient for taking the die is arranged in the fixed die 2, the bottom plate 1 is provided with a die taking mechanism for taking out the die, the die taking mechanism is released at the top end of the bottom plate 1, the hydraulic rod 9 is fixedly arranged at the top end of the hydraulic rod 7 through bolts, the connecting rod 9 is fixedly arranged at the top end of the movable die taking plate 10, the connecting rod is fixedly arranged in the forming groove, the forming die is required to be taken out of the forming die by the forming die, the metal sheets are simultaneously, the forming die is required to be removed by taking out the connecting rod is removed from the forming the inside the forming die by taking die, the metal sheets by taking the die, the die into the die by the die, the fixing die is moving the die, the die 9 is released by moving the movable die, the moving the movable die taking plate a die 9, the connecting plate 9 is, the forming plate a drawing plate is conveniently, the drawing a die a drawing plate a product can is, the product can be is conveniently is put.

The ejecting mechanism comprises a vertical plate 12, a movable rod 13, springs 15, electromagnets 14, a control switch 8 and an extrusion block 11, wherein the vertical plate 12 is welded and fixed at the top end of the bottom plate 1, the movable rod 13 is movably inserted on the vertical plate 12, the movable rods 13 are two and symmetrically inserted at two sides of the vertical plate 12, the electromagnets 14 are embedded and fixed on one side of the vertical plate 12, the springs 15 are welded and fixed on one side of the electromagnets 14, the extrusion block 11 is welded and fixed on one side of the movable rod 13, one side of the extrusion block 11 is welded and fixed on the springs 15, the extrusion block 11 is made of magnetic metal materials, the control switch 8 is embedded and fixed at the lower end of the hydraulic rod 7, the control switch 8 is electrically connected with the electromagnets 14, the springs 15 are in a compressed state, and when the movable die 3 is reset, the connecting rod 9 moves upwards until the control switch 8 is extruded, so that the electromagnets 14 are closed, the springs 15 are instantly released, the extrusion block 11 is driven to eject products, and the products are completely ejected, so that the complete product extraction work is completed.

The working principle is that after stamping is completed, the hydraulic rod 7 drives the movable die 3 to reset, at the moment, the die taking plate 10 is driven to move upwards through the connecting rod 9 to extrude a product in the forming groove, the product is separated from the forming groove, manual taking out is not needed, meanwhile, mechanical extrusion is performed, the product is prevented from being adsorbed in the forming groove, manual taking out is laborious, when the movable die 3 resets, the connecting rod 9 moves upwards until the switch 8 is controlled to be extruded, so that the electromagnet 14 is closed, the spring 15 instantly releases elasticity, the extrusion block 11 is driven to eject the product, and the product is completely ejected, so that the complete taking out of the product is completed.

It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

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

Claims (6)

1. The forming die for the aircraft cable protective cover comprises a bottom plate (1) and is characterized in that a fixed die (2) is fixedly arranged at the top end of the bottom plate (1), positioning rods (4) are fixedly arranged at the two sides of the fixed die (2), positioning rings (5) are movably sleeved on the outer sides of the positioning rods (4), movable dies (3) are fixedly arranged between the positioning rings (5), a top plate (6) is fixedly arranged at the top end of the positioning rods (4), a hydraulic rod (7) is fixedly arranged at the bottom end of the top plate (6), a die-taking mechanism convenient for die-taking is arranged in the fixed die (2), an ejecting mechanism for ejecting a product is arranged at the top end of the bottom plate (1), the die-taking mechanism comprises a connecting rod (9) and a die-taking plate (10), the connecting rod (9) is fixedly arranged on the hydraulic rod (7), and the die-taking plate (10) is fixedly arranged at the top end of the connecting rod (9).

2. The molding die of the aircraft cable protecting cover according to claim 1, wherein the ejecting mechanism comprises a vertical plate (12), a movable rod (13), a spring (15), an electromagnet (14), a control switch (8) and an extrusion block (11), wherein the vertical plate (12) is fixed at the top end of the bottom plate (1), the movable rod (13) is movably inserted and arranged on the vertical plate (12), the electromagnet (14) is embedded and fixed on one side of the vertical plate (12), the spring (15) is fixed on one side of the electromagnet (14), the extrusion block (11) is fixed on one side of the movable rod (13), one side of the extrusion block (11) is fixed on the spring (15), and the control switch (8) is embedded and fixed at the lower end of the hydraulic rod (7).

3. The molding die of the aircraft cable protection cover according to claim 2, wherein the connecting rod (9) movably penetrates into the fixed die (2).

4. A molding die for an aircraft cable guard according to claim 3, wherein the upper surface of the take-out plate (10) is flush with the upper surface of the molding groove inside the fixed die (2).

5. The molding die for the aircraft cable protecting cover according to claim 4, wherein two movable rods (13) are symmetrically inserted and arranged at two sides of the vertical plate (12).

6. The molding die of the aircraft cable protecting cover according to claim 5, wherein the extrusion block (11) is made of magnetic metal, the control switch (8) is electrically connected with the electromagnet (14), and the spring (15) is in a compressed state.