CN212043535U

CN212043535U - Machining center for machining aviation parts

Info

Publication number: CN212043535U
Application number: CN202020283613.1U
Authority: CN
Inventors: 王英伟
Original assignee: Liaoning Weilong Technology Co ltd
Current assignee: Liaoning Weilong Technology Co ltd
Priority date: 2020-03-10
Filing date: 2020-03-10
Publication date: 2020-12-01
Anticipated expiration: 2030-03-10

Abstract

The utility model discloses a machining center of aviation spare part processing usefulness, including the processing workstation, the standing groove has been seted up to department in the middle of the upper end of processing workstation, and the front side lower part of processing workstation has seted up the wire guide, first collecting vat and second collecting vat have been seted up to the lateral wall of processing workstation, and first collecting vat and second collecting vat notch department are connected with the clear bits structure, be provided with location clamping structure in the standing groove, first collecting vat and the second collecting vat that the processing workstation was seted up set up with processing workstation lower extreme central line symmetry, and first collecting vat, second collecting vat and standing groove pass through the division board and separate the setting. A machining center of aviation spare part processing usefulness, clear bits structure can realize that collecting vat and outside communicate with each other, conveniently fixes a position the piece collection of clamping structure contact aviation spare part cutting in-process, fix a position clamping structure and utilize electric putter to realize the oscilaltion, the convenience is used according to the demand.

Description

Machining center for machining aviation parts

Technical Field

The utility model relates to a machining center field, in particular to machining center of aviation spare part processing usefulness.

Background

The numerical control milling machine is an automatic processing device developed on the basis of a common milling machine, the processing technologies of the two are basically the same, and the structures are somewhat similar. The numerical control milling machine is divided into two categories, namely a tool magazine without tool magazine and a tool magazine with tool magazine. Wherein the numerical control milling machine with the tool magazine is also called as a machining center; in the machining process of the machining center, the chips are collected more inconveniently, and the chips are accumulated on the workbench to influence the machining of parts on the workbench.

SUMMERY OF THE UTILITY MODEL

The utility model discloses a main aim at provides a machining center of aviation spare part processing usefulness can effectively solve the problem in the background art.

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

the utility model provides a machining center of aviation spare part processing usefulness, includes the machining workbench, the standing groove has been seted up to the department in the middle of the upper end of machining workbench, and the front side lower part of machining workbench has seted up the wire guide, first collecting vat and second collecting vat have been seted up to the lateral wall of machining workbench, and first collecting vat and second collecting vat notch department are connected with the clear bits structure, be provided with location clamping structure in the standing groove.

Preferably, the first collecting groove and the second collecting groove which are formed in the machining workbench are symmetrically arranged on the center line of the lower end of the machining workbench, and the first collecting groove, the second collecting groove and the placing groove are arranged in a separated mode through the partition plate.

Preferably, the chip cleaning structure comprises a first partition plate, a first connecting cover, a second partition plate and a second connecting cover, the upper end of the first partition plate is connected with the first connecting cover through a hinge, the first partition plate is fixed at the position of a groove opening of the side part of the first collecting tank through a bolt, the first connecting cover movably connected with the upper end of the first partition plate is connected with the machining workbench through a lock catch, the upper end of the second partition plate is connected with the second connecting cover through a hinge, the second partition plate is fixed at the position of a groove opening of the side part of the second collecting tank through a bolt, and the second connecting cover is connected with the machining workbench through a lock catch.

Preferably, the location clamping structure includes a location base plate, a mounting hole, a location centre gripping section of thick bamboo, installation piece, through-hole, electric putter, fixed connector, and the department has seted up the mounting hole in the middle of one side of location base plate, the downthehole plug-in connection of mounting hole has a location centre gripping section of thick bamboo, and the opposite side of a location centre gripping section of thick bamboo is provided with and is provided with the installation piece, the through-hole has been seted up to side department around the lower extreme of location base plate, and through-hole lower extreme drill way insert and be provided with electric putter, the upper end drill way of through-hole has inserted fixed connector.

Preferably, electric putter places into the standing groove tank bottom, and electric putter is connected with the processing workstation through the bolt, fixed connector is connected with the location base plate through the bolt.

Compared with the prior art, the utility model discloses following beneficial effect has:

the utility model discloses in, the collection vat can be realized to the clear bits structure and the outside communicates with each other, and the piece that conveniently fixes a position the clamping structure contact aviation industry spare part cutting in-process is collected, and location clamping structure utilizes electric putter to realize the oscilaltion, and the convenience is used according to the demand.

Drawings

Fig. 1 is a schematic view of the overall structure of a machining center for machining aviation parts of the present invention;

fig. 2 is a schematic view of the overall structure of a machining center for machining aviation parts according to the present invention;

FIG. 3 is a schematic diagram showing a chip cleaning structure of a machining center for machining aviation parts;

fig. 4 is the utility model relates to a machining center's that aviation spare part processing was used location clamping structure dissects the sketch map.

In the figure: 1. a machining workbench; 2. a scrap cleaning structure; 201. a first separator; 202. a first connection cover; 203. a second separator; 204. a second connecting cover; 3. positioning and clamping the structure; 301. positioning the substrate; 302. mounting holes; 303. positioning the clamping cylinder; 304. mounting a sheet; 305. a through hole; 306. an electric push rod; 307. fixing the connector; 4. a wire guide hole; 5. a first holding tank; 6. a second holding tank; 7. and (6) placing the groove.

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.

As shown in fig. 1-4, a machining center for machining aviation components and parts comprises a machining workbench 1, a placement groove 7 is formed in the middle of the upper end of the machining workbench 1, a wire guide hole 4 is formed in the lower portion of the front side of the machining workbench 1, a first collecting groove 5 and a second collecting groove 6 are formed in the side wall of the machining workbench 1, chip cleaning structures 2 are connected to the notches of the first collecting groove 5 and the second collecting groove 6, and a positioning clamping structure 3 is arranged in the placement groove 7.

The first collecting groove 5 and the second collecting groove 6 which are arranged on the processing workbench 1 are symmetrically arranged on the center line of the lower end of the processing workbench 1, and the first collecting groove 5, the second collecting groove 6 and the placing groove 7 are arranged in a separated mode through partition plates.

The chip cleaning structure 2 comprises a first partition plate 201, a first connecting cover 202, a second partition plate 203 and a second connecting cover 204, the upper end of the first partition plate 201 is connected with the first connecting cover 202 through a hinge, the first partition plate 201 is fixed at a side groove opening of a first collecting tank 5 through a bolt, the first connecting cover 202 movably connected with the upper end of the first partition plate 201 is connected with the machining workbench 1 through a lock catch, the upper end of the second partition plate 203 is connected with the second connecting cover 204 through a hinge, the second partition plate 203 is fixed at a side groove opening of a second collecting tank 6 through a bolt, and the second connecting cover 204 is connected with the machining workbench 1 through a lock catch; the chip cleaning structure 2 can realize that the collecting groove is communicated with the outside, and the chip collecting in the cutting process of the contact of the positioning and clamping structure 3 and the aeronautical parts is convenient.

The positioning and clamping structure 3 comprises a positioning base plate 301, a mounting hole 302, a positioning and clamping cylinder 303, a mounting piece 304, a through hole 305, an electric push rod 306 and a fixed connector 307, wherein the mounting hole 302 is formed in the middle of one side of the positioning base plate 301, the positioning and clamping cylinder 303 is inserted and connected into the mounting hole 302, the mounting piece 304 is arranged on the other side of the positioning and clamping cylinder 303, the through hole 305 is formed in the front side and the rear side of the lower end of the positioning base plate 301, the electric push rod 306 is inserted and arranged in the lower end hole of the through hole 305, the fixed connector 307 is inserted in the upper end hole of the through hole 305, and the fixed connector 307 is in threaded; the positioning and clamping structure 3 can be lifted up and down by the electric push rod 306, and can be conveniently used according to requirements.

Wherein, the electric putter 306 is placed into the bottom of the placing groove 7, the electric putter 306 is connected with the processing workbench 1 through a bolt, and the fixed connector 307 is connected with the positioning substrate 301 through a bolt.

It should be noted that, the utility model relates to a machining center for machining aviation parts, when assembling the machining workbench 1, the scrap removing structure 2 and the positioning and clamping structure 3, the electric push rod 306 arranged on the positioning and clamping structure 3 is placed in the groove of the placing groove 7, the electric push rod 306 is moved until the screw hole arranged on the upper end edge of the base of the electric push rod 306 is aligned with the screw hole arranged on the bottom of the placing groove 7, the bolt is inserted from the screw hole arranged on the lower end of the machining workbench 1 to fixedly connect the electric push rod 306 and the machining workbench 1, the electric positioning push rod is inserted into the positioning and clamping cylinder 303, the tail wire of the electric positioning push rod sequentially penetrates through the positioning and clamping cylinder 303, the hole arranged on the hole wall of the mounting hole 302 is inserted into the wire hole 4 arranged on the groove wall of the placing groove 7, the tail wire of the electric positioning push rod penetrates through the wire hole 4 arranged on the, the positioning clamping cylinder 303 is inserted into the mounting hole 302, the position of the threaded hole formed on the edge of the end face of the positioning clamping cylinder 303 is adjusted by rotation, the threaded hole formed on the end face of the positioning clamping cylinder 303 is aligned with the positioning base plate 301, the positioning base plate 301 and the positioning clamping cylinder 303 are fixedly connected by inserting a bolt, the mounting plate 304 is placed on the end face of the other end of the positioning clamping cylinder 303, the threaded hole formed on the edge of the end face of the mounting plate 304 is aligned with the threaded hole formed on the positioning base plate 301, the positioning base plate 301 and the mounting plate 304 are fixedly connected by using a bolt, the hole formed in the middle of the end face of the mounting plate 304 is communicated with the hole formed in the middle of the end face of the positioning clamping cylinder 303, the through hole 305 formed on the lower end of the positioning base plate 301 is aligned with the electric push rod 306, the fixed connector 307 is connected with the electric push rod 306 through threads, the upper end disc of the fixed connector 307 is fixedly connected with the positioning base plate 301 through bolts, in the process that the electric push rod 306 extends upwards, the electric push rod 306 pushes the fixed connector 307, the fixed connector 307 drives the positioning base plate 301 to ascend until the positioning clamping barrel 303 is exposed, so that the positioning clamping of aviation parts is facilitated, the first partition plate 201 is connected with the first connecting cover 202 through a hinge, the first partition plate 201 is placed at the notch of the side end of the first collecting tank 5, the first partition plate 201 is fixedly connected with the machining workbench 1 through bolts, the first connecting cover 202 is connected with the machining workbench 1 through a lock catch, the second partition plate 203 is connected with the second connecting cover 204 through a hinge, the connection modes between the second partition plate 203, the second connecting cover 204 and the machining workbench 1 are the same as the connection modes between the first partition plate 201, the first connecting cover 202 and the machining workbench 1, when the connecting cover is used, the connecting cover is obliquely placed into the collecting tank, and chips generated by cutting conveniently enter the collecting tank.

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. The utility model provides a machining center that aviation spare part processing was used which characterized in that: including processing workstation (1), standing groove (7) have been seted up to the department in the middle of the upper end of processing workstation (1), and the front side lower part of processing workstation (1) has seted up wire guide (4), first collecting vat (5) and second collecting vat (6) have been seted up to the lateral wall of processing workstation (1), and first collecting vat (5) and second collecting vat (6) notch department are connected with clear bits structure (2), standing groove (7) inslot is provided with location clamping structure (3).

2. The machining center for machining aviation components and parts as claimed in claim 1, wherein: the processing workbench (1) is provided with a first collecting tank (5) and a second collecting tank (6) which are symmetrically arranged along the central line of the lower end of the processing workbench (1), and the first collecting tank (5), the second collecting tank (6) and the placing tank (7) are separated by partition plates.

3. The machining center for machining aviation components and parts according to claim 2, wherein: clear bits structure (2) include first baffle (201), first connection lid (202), second baffle (203), second connection lid (204), and there is first connection lid (202) first baffle (201) upper end through hinge connection, first baffle (201) pass through the bolt fastening at first collecting vat (5) lateral part notch department, and first baffle (201) upper end swing joint's first connection lid (202) are connected with processing workstation (1) through the hasp, there is second connection lid (204) second baffle (203) upper end through hinge connection, and second baffle (203) pass through the bolt fastening at second collecting vat (6) lateral part notch department, second connection lid (204) are connected with processing workstation (1) through the hasp.

4. The machining center for machining aviation components and parts as claimed in claim 3, wherein: the utility model discloses a fixing device, including location base plate (301), mounting hole (302), location centre gripping structure (3), location centre gripping section of thick bamboo (303), installation piece (304), through-hole (305), electric putter (306), fixed connector (307), and one side middle department of location base plate (301) has seted up mounting hole (302), the downthehole inserted connection of mounting hole (302) has a location centre gripping section of thick bamboo (303), and the opposite side of location centre gripping section of thick bamboo (303) is provided with installation piece (304), rear side department has seted up through-hole (305) before the lower extreme of location base plate (301), and through-hole (305) lower extreme drill way insert and be provided with electric putter (306), the upper end drill way of through-hole (305) has inserted fixed connector (307), and fixed connector (307) and electric putter (306) pass through threaded.

5. The machining center for machining aviation components and parts as claimed in claim 4, wherein: the electric push rod (306) is placed into the bottom of the placing groove (7), the electric push rod (306) is connected with the machining workbench (1) through a bolt, and the fixed connector (307) is connected with the positioning base plate (301) through a bolt.