CN213944460U

CN213944460U - Device for stamping aircraft parts

Info

Publication number: CN213944460U
Application number: CN202021893935.4U
Authority: CN
Inventors: 王丽
Original assignee: Harbin Aviation Technology Development Co ltd
Current assignee: Harbin Aviation Technology Development Co ltd
Priority date: 2020-09-02
Filing date: 2020-09-02
Publication date: 2021-08-13
Anticipated expiration: 2030-09-02

Abstract

The utility model relates to an aircraft parts processing technology field specifically is a device for being used for carrying out stamping process to aircraft parts, include: the workstation, workstation upper surface four corners department is provided with four support columns perpendicularly, support column top fixedly connected with backup pad, backup pad upper surface central point fixed mounting has the power cylinder, power cylinder one side fixed mounting has controller power cylinder opposite side fixed mounting has control panel, the power cylinder output runs through in the backup pad and is connected with the punching press die head, workstation bottom four corners department is provided with the supporting shoe, the workstation center runs through and is provided with puts the thing platform, set up on the workstation and put thing platform assorted jack, it is provided with two sets of fixture blocks to put thing platform bilateral symmetry, set up two perforation corresponding with the fixture block on the workstation, the utility model discloses can conveniently treat getting of machined part and put, avoid leading to the phenomenon of mechanical pressure hand because of machine fault or misoperation to guarantee operating personnel's safety from this.

Description

Device for stamping aircraft parts

Technical Field

The utility model relates to an aircraft parts processing technology field specifically is a device for being used for carrying out stamping process to aircraft parts.

Background

The stamping processing is a production technology for obtaining product parts with certain shapes, sizes and performances by directly applying deformation force to a plate in a die and deforming the plate by means of the power of conventional or special stamping equipment, has a good stamping forming effect, is low in power consumption and simple to operate, and is widely applied to various fields. '

However, the existing device for stamping parts has certain disadvantages when in use, a worker needs to take and place a workpiece in a stamping die, the work of the punching die is dangerous, the stamped part can splash scraps in the stamping process, if the punched part is easy to cause serious injury to a human face, and meanwhile, the possibility of mechanical hand pressing can be caused when a machine breaks down or operates incorrectly, so that the disadvantages are well solved.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a device for being directed at aircraft parts carries out stamping process to solve the problem that proposes among the above-mentioned background art.

The above utility model discloses an above-mentioned utility model purpose can realize through following technical scheme:

an apparatus for stamping an aircraft component, comprising: the worktable is characterized in that four supporting columns are vertically arranged at four corners of the upper surface of the worktable, a supporting plate is fixedly connected to the top ends of the supporting columns, a power cylinder is fixedly mounted at the central position of the upper surface of the supporting plate, a controller is fixedly mounted at one side of the power cylinder, a control panel is fixedly mounted at the other side of the power cylinder, the output end of the power cylinder penetrates through the supporting plate and is connected with a stamping die head, supporting blocks are arranged at the four corners of the bottom of the worktable, a storage table is arranged at the center of the worktable in a penetrating manner, jacks matched with the storage table are formed in the worktable, two groups of clamping blocks are symmetrically arranged at two sides of the storage table, two through holes corresponding to the clamping blocks are formed in the worktable, two clamping grooves matched with the clamping blocks are formed in the worktable, a workpiece to be machined is placed at the top end of the storage table, and a limiting block is integrally formed in the bottom of the storage table, the limiting block is integrally formed at the bottom of the limiting block and is provided with a handle, and the workbench and the supporting plate are connected with a protection plate through fixing bolts.

Furthermore, a cushion pad is bonded to the bottom of the supporting block, and the cushion pad is made of rubber.

Further, a groove is formed in the top end of the object placing table, and the workpiece to be machined is placed in the groove.

Further, put the thing platform through perforating and sliding connection between the workstation, put the thing platform and inlay through the fixture block and locate in the draw-in groove with workstation fixed connection.

Furthermore, every group fixture block is two, two fixedly connected with telescopic link between the fixture block, and two fixture block vertical arrangement, telescopic link outer wall cover is equipped with the spring, and wherein the fixture block of upper base with put the thing platform welding, lower floor's fixture block with put thing platform sliding connection.

Further, it is a set of lower floor's fixture block in the fixture block is close to the one end integrated into one piece of putting the thing platform and is provided with the forked tail slider, put the thing bench set up with the spout of forked tail slider looks adaptation, the fixture block passes through forked tail slider cooperation spout and puts thing platform sliding connection.

Further, fixing bolt is four, the guard plate is two, and is the transparent plastic material, fixing bolt runs through two guard plates and backup pad and workstation threaded connection, fixing bolt outer wall cover is equipped with buffer spring, buffer spring is located between two guard plates.

Compared with the prior art, the utility model provides a device for being directed at aircraft parts carries out stamping process possesses following beneficial effect:

1. the utility model discloses, when using, hold between the fingers the handle and put the thing platform and rotate 90 degrees after upwards promoting and put thing platform and take out whole from the workstation bottom through the perforation, will wait to add the machined part and place and put thing platform and reset after putting thing platform top and can install on the workstation, this mounting means can conveniently wait to add and put of machined part, avoids the phenomenon of mechanical pressure hand because of machine fault or misoperation, so as to guarantee operating personnel's safety;

2. the utility model discloses, during punching press, because the device openly installs the guard plate, the piece that splashes out in the punching press can effectively be stopped through the guard plate, through set up buffer spring between two guard plates, buffer spring can reduce the impact force that the guard plate received, lengthen the life of guard plate;

3. the utility model discloses, during the punching press, the spring between two fixture blocks can reduce the impact force that the thing platform received, avoids putting thing platform pressurized and damages, prolongs the life who puts the thing platform.

Drawings

Fig. 1 is a schematic view of the structure of the present invention;

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

FIG. 3 is a schematic view of the side structure of the connection between the object placing table and the working table of the present invention;

fig. 4 is an enlarged schematic structural view of a portion a of fig. 3 according to the present invention;

fig. 5 is a schematic side sectional view of the protection plate of the present invention.

In the figure: 1-a workbench; 2-a support column; 3-a support plate; 4-a power cylinder; 5-a controller; 6-control panel; 7-a stamping die head; 8-a support block; 9-placing a table; 10-a jack; 11-a fixture block; 12-perforating; 13-a card slot; 14-a fixing bolt; 15-a workpiece to be machined; 16-a limiting block; 17-a handle; 18-protective plate; 19-a cushion pad; 20-a telescopic rod; 21-a spring; 22-dovetail slide block; 23-a chute; 24-return spring.

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.

Example (b): referring to fig. 1 to 5, the present invention provides a technical solution: an apparatus for stamping an aircraft component, comprising: the automatic cutting machine comprises a workbench 1, four support columns 2 are vertically arranged at four corners of the upper surface of the workbench 1, a support plate 3 is fixedly connected at the top ends of the support columns 2, a power cylinder 4 is fixedly arranged at the central position of the upper surface of the support plate 3, a controller 5 is fixedly arranged at one side of the power cylinder 4, a control panel 6 is fixedly arranged at the other side of the power cylinder 4, the output end of the power cylinder 4 penetrates through the support plate 3 and is connected with a stamping die head 7, a support block 8 is arranged at the four corners of the bottom of the workbench 1, an object placing table 9 is arranged at the center of the workbench 1 in a penetrating manner, a jack 10 matched with the object placing table 9 is arranged on the workbench 1, two groups of fixture blocks 11 are symmetrically arranged at two sides of the object placing table 9, two through holes 12 corresponding to the fixture blocks 11 are arranged on the workbench 1, two clamping grooves 13 matched with the fixture blocks 11 are also arranged on the workbench 1, a workpiece 15 is arranged at the top end of the object placing table 9, and a limit block 16 is integrally formed at the bottom of the object placing table 9, the handle 17 is arranged at the bottom of the limiting block 16 in an integrated forming mode, the protective plate 18 is connected to the front faces of the workbench 1 and the supporting plate 3 through the fixing bolt 14, the cushion pad 19 is bonded to the bottom of the supporting block 8, and the cushion pad 19 is made of rubber.

Wherein, it is provided with a recess to put thing platform 9 top, treat that machined part 15 places in the recess, put thing platform 9 through perforation 12 and workstation 1 between sliding connection, put thing platform 9 and inlay through fixture block 11 and locate draw-in groove 13 in with workstation 1 fixed connection, when using, hold between the fingers the handle will put thing platform 9 and upwards promote the back rotatory 90 degrees rethread perforation 12 will put thing platform 9 and wholly take out from workstation 1 bottom, will treat that machined part 15 places again and will put thing platform 9 and reset after putting thing platform 9 top and can install on workstation 1, this mounting means can conveniently treat getting of machined part 15 and put, avoid leading to the phenomenon of mechanical pressure hand because of machine trouble or misoperation, with this assurance operating personnel's safety.

Wherein, every group fixture block 11 is two, fixedly connected with telescopic link 20 between two fixture blocks 11, and two fixture block 11 vertical arrangements, 20 outer wall covers of telescopic link are equipped with spring 21, wherein the fixture block 11 of upper base with put thing platform 9 welding, lower floor's fixture block 11 with put thing platform 9 sliding connection, lower floor's fixture block 11 in a set of fixture block 11 is close to the one end integrated into one piece who puts thing platform 9 and is provided with forked tail slider 22, put and set up the spout 23 with forked tail slider 22 looks adaptation on the thing platform 9, fixture block 11 cooperates spout 23 and puts thing platform 9 sliding connection through forked tail slider 22, during the punching press, spring 21 between two fixture blocks 11 can reduce the impact force that thing platform 9 received, avoid putting thing platform 9 pressurized damage, the life of thing platform 9 is put in the extension.

Wherein, fixing bolt 14 is four, protection plate 18 is two, and be the transparent plastic material, fixing bolt 14 runs through two protection plates 18 and

backup pad

3 and 1 threaded connection of workstation, fixing bolt 14 outer wall cover is equipped with buffer spring 24, buffer spring 24 is located between two protection plates 18, during the punching press, because protection plate 18 is openly installed to the device, piece accessible protection plate 18 of splashing effectively blocks in the punching press, through set up buffer spring 24 between two protection plates 18, buffer spring 24 can reduce the impact force that protection plate 18 received, the life of extension protection plate 18.

The working principle is as follows: in the use process of the utility model, when in use, the handle is held to push the object placing table 9 upwards and then rotate 90 degrees, and then the object placing table 9 is taken out from the bottom of the workbench 1 through the perforation 12, the workpiece 15 to be processed is placed on the top end of the object placing table 9, and then the object placing table 9 is reset to be installed on the workbench 1, the installation mode can facilitate the taking and placing of the workpiece 15 to be processed, the phenomenon of mechanical hand pressing caused by machine failure or misoperation is avoided, so as to ensure the safety of operators, during punching, the spring 21 between the two clamping blocks 11 can reduce the impact force on the object placing table 9, the object placing table 9 is prevented from being damaged by pressure, the service life of the object placing table 9 is prolonged, because the protection plate 18 is arranged at the front side of the device, the splashed fragments in punching can be effectively blocked by the protection plate 18, through the buffer spring 24 arranged between the two protection plates 18, the buffer spring 24 can reduce the impact force on the protection plate 18, the service life of the guard plate 18 is extended.

It is noted that, herein, relational terms such as first and second, and the like may be 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. Also, 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. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

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

1. An apparatus for stamping an aircraft component, comprising: workstation (1), its characterized in that: four supporting columns (2) are vertically arranged at four corners of the upper surface of the workbench (1), a supporting plate (3) is fixedly connected to the top ends of the supporting columns (2), a power cylinder (4) is fixedly mounted at the center of the upper surface of the supporting plate (3), a controller (5) is fixedly mounted on one side of the power cylinder (4), a control panel (6) is fixedly mounted on the other side of the power cylinder (4), the output end of the power cylinder (4) penetrates through the supporting plate (3) and is connected with a stamping die head (7), supporting blocks (8) are arranged at four corners of the bottom of the workbench (1), an object placing table (9) is arranged in the center of the workbench (1) in a penetrating mode, jacks (10) matched with the object placing table (9) are formed in the workbench (1), two groups of clamping blocks (11) are symmetrically arranged on two sides of the object placing table (9), and two through holes (12) corresponding to the clamping blocks (11) are formed in the workbench (1), still seted up on workstation (1) with two draw-in grooves (13) of fixture block (11) looks adaptation, it places and waits machined part (15) to put thing platform (9) top, it is provided with stopper (16) to put thing platform (9) bottom integrated into one piece, stopper (16) bottom integrated into one piece is provided with handle (17), workstation (1) and backup pad (3) openly are connected with guard plate (18) through fixing bolt (14).

2. An apparatus for stamping an aircraft component as defined in claim 1, wherein: a buffer pad (19) is bonded to the bottom of the supporting block (8), and the buffer pad (19) is made of rubber.

3. An apparatus for stamping an aircraft component as defined in claim 1, wherein: a groove is formed in the top end of the object placing table (9), and the workpiece (15) to be machined is placed in the groove.

4. An apparatus for stamping an aircraft component as defined in claim 1, wherein: put thing platform (9) through perforation (12) and sliding connection between workstation (1), put thing platform (9) and inlay through fixture block (11) and locate in draw-in groove (13) and workstation (1) fixed connection.

5. An apparatus for stamping an aircraft component as defined in claim 1, wherein: every group fixture block (11) are two, two fixedly connected with telescopic link (20) between fixture block (11), and two fixture block (11) vertical range, telescopic link (20) outer wall cover is equipped with spring (21), wherein fixture block (11) at the bottom of the top is with put thing platform (9) welding, lower floor's fixture block (11) with put thing platform (9) sliding connection.

6. An apparatus for stamping an aircraft component as defined in claim 5, wherein: a set of lower floor fixture block (11) in fixture block (11) is close to the one end integrated into one piece of putting thing platform (9) and is provided with forked tail slider (22), put and offer spout (23) with forked tail slider (22) looks adaptation on thing platform (9), fixture block (11) through forked tail slider (22) cooperation spout (23) with put thing platform (9) sliding connection.

7. An apparatus for stamping an aircraft component as defined in claim 1, wherein: fixing bolt (14) four, guard plate (18) are two, and are the transparent plastic material, fixing bolt (14) run through two guard plates (18) and backup pad (3) and workstation (1) threaded connection, fixing bolt (14) outer wall cover is equipped with buffer spring (24), buffer spring (24) are located between two guard plates (18).