CN217912378U

CN217912378U - Automatic change aviation part shaping with leftover bits excision equipment

Info

Publication number: CN217912378U
Application number: CN202222003020.7U
Authority: CN
Inventors: 张成江
Original assignee: Sichuan Feihong Sky Technology Co ltd
Current assignee: Sichuan Feihong Sky Technology Co ltd
Priority date: 2022-07-31
Filing date: 2022-07-31
Publication date: 2022-11-29
Anticipated expiration: 2032-07-31

Abstract

The utility model discloses an automatic change aviation part for shaping leftover bits excision equipment, including base, transport mechanism, control panel and revolving stage, the left side of base up end is fixed with the plummer, transport mechanism fixes the bottom at the slider, both sides are fixed with first support and second support respectively around bearing the interior top right side of frame, both sides all are fixed with the electronic flexible post of second around the first support bottom, bear the right side of frame front side and seted up the opening, the revolving stage rotates the top of connecting at the mount, and the front side of mount and the right side of mount are provided with first collection box and second collection box respectively. This automatic change leftover bits excision equipment for aviation part shaping, after every completion material loading operation, revolving stage counter-clockwise turning 90 degrees supports the board downstream after to this supports tightly fixes aviation part, and briquetting downstream afterwards makes things convenient for automatic broken leftover bits, and the leftover bits falls in first collection box thereupon, conveniently concentrates the collection to handle.

Description

Automatic change aviation part for shaping leftover bits excision equipment

Technical Field

The utility model relates to an aviation parts machining technical field specifically is an automatic change leftover bits excision equipment for aviation parts shaping.

Background

The aviation parts are general names of various aviation parts used for manufacturing aircrafts, aeroengines, airborne equipment and the like, the aviation parts are material guarantees for developing and producing aviation products and are technical bases for enabling the aviation products to achieve performance, service life and reliability expected by people.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an automatic change leftover bits excision equipment for aviation part shaping to the degree of automation of solving the current leftover bits excision equipment that proposes in the above-mentioned background art is not enough, is difficult to accomplish material loading and unloading operation voluntarily, and the not enough continuous efficient problem of whole operation.

In order to achieve the above purpose, the utility model provides a following technical scheme: an automatic leftover material cutting device for aviation part forming comprises a base, a transfer mechanism, a control panel and a rotary table,

the device comprises a base, a bearing table, a conveying belt device and a bearing frame, wherein the bearing table is fixed on the left side of the upper end surface of the base, the upper end surface of the bearing table is rotatably connected with the conveying belt device, and the bearing frame is fixed in the middle of the upper end surface of the base;

the transfer mechanism is fixed at the bottom of the sliding block, the sliding block is connected to the left side of the inner top of the bearing frame in a sliding mode, a first support and a second support are fixed to the front side and the rear side of the right side of the inner top of the bearing frame respectively, a second electric telescopic rod is fixed to the right side of the bottom of the second support, second electric telescopic columns are fixed to the front side and the rear side of the bottom of the first support respectively, the bottom of the second electric telescopic column on the front side is connected with the pressing block, the bottom of the second electric telescopic column on the rear side is connected with the abutting plate, an opening is formed in the right side of the front side of the bearing frame, a fixing frame is arranged on the inner side of the bearing frame, and the fixing frame is fixed on the base;

the rotary table is rotatably connected to the top of the fixing frame, a first collecting box and a second collecting box are respectively arranged on the front side of the fixing frame and the right side of the fixing frame, and the first collecting box and the second collecting box are placed on the base.

Preferably, the top of the bearing frame is internally fixed with a first electric telescopic rod, and the right end of the first electric telescopic rod is connected with the sliding block.

Preferably, the sliding block is connected in the sliding groove in a sliding mode, and the sliding groove is formed in the inner top of the bearing frame.

Preferably, the transport mechanism includes first electronic flexible post, motor box, first motor shaft, suction pump and sucking disc, and first electronic flexible post is fixed in the bottom of slider, and the bottom of first electronic flexible post is connected with the motor box simultaneously, the motor box internal fixation has first motor, and the downside of first motor is connected with the suction pump through first motor shaft, and the bottom of suction pump is fixed with the sucking disc simultaneously.

Preferably, the pressing block and the first support frame form a telescopic structure through the corresponding second electric telescopic column.

Preferably, the abutting plate and the first support frame form a telescopic structure through the corresponding second electric telescopic column.

Preferably, the control panel is fixed on the front end face of the bearing frame, a transparent plate is arranged on the upper side of the control panel, and the transparent plate is inlaid on the bearing frame.

Preferably, a second motor is fixed in the fixing frame, and the upper side of the second motor is rotatably connected with the rotary table through a second motor shaft.

Preferably, the upper end face of the rotary table is fixed on four limit frames, and the four limit frames are circumferentially and uniformly distributed.

Compared with the prior art, the beneficial effects of the utility model are that: the automatic leftover material cutting equipment for aviation part forming,

(1) The aviation part unloading device is provided with a conveying belt device, a sliding block, a suction pump, a sucking disc and a rotary table, after a molded aviation part is placed on the conveying belt device, the aviation part can move rightwards under the operation effect of the conveying belt device, when the aviation part reaches the position right below the suction pump, the suction pump moves downwards, the suction pump and the sucking disc are matched to suck the aviation part, the suction pump moves upwards, then the sliding block moves rightwards, the aviation part is conveniently transferred to the upper part of the rotary table, the aviation part is released after being lowered onto the rotary table, the loading operation is conveniently and automatically completed, and in the process of lowering the aviation part, the suction pump can rotate, the angle of the aviation part is conveniently adjusted, and the aviation part can be landed on the rotary table in a complete manner;

(2) The device is provided with a pressing block, a supporting plate, a rotary table and a first collecting box, after each feeding operation is finished, the rotary table rotates 90 degrees anticlockwise, then the supporting plate moves downwards to tightly fix the aviation part in a supporting mode, then the pressing block moves downwards, leftover materials can be conveniently and automatically pressed and broken, and the leftover materials fall into the first collecting box, so that centralized collecting and processing are facilitated;

(3) The second electric telescopic rod, the rotary table and the second collecting box are arranged, after the leftover material cutting operation is completed, the rotary table continues to rotate 90 degrees anticlockwise, and then the second electric telescopic rod extends to push the processed aviation parts into the second collecting box, so that the blanking operation can be conveniently and automatically completed;

(4) Be provided with the revolving stage, can transport next aviation part to the revolving stage on the in-process that carries out leftover bits excision processing to previous aviation part, later revolving stage intermittent type formula rotates, and convenient orderly efficient accomplishes transportation, leftover bits excision and the uninstallation operation of every aviation part.

Drawings

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

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

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

FIG. 4 is a schematic diagram of the right-side cross-sectional structure of the present invention;

FIG. 5 is a schematic top view of the cross-sectional structure of the present invention;

fig. 6 is a schematic top view of the present invention.

In the figure: 1. the base, 2, plummer, 3, conveyer belt device, 4, bear the frame, 5, the spout, 6, first electric telescopic handle, 7, the slider, 8, transport mechanism, 801, first electric telescopic column, 802, the motor box, 803, first motor, 804, first motor shaft, 805, the suction pump, 806, the sucking disc, 9, first support, 10, the second support, 11, the second electric telescopic handle, 12, the second electric telescopic column, 13, the briquetting, 14, the butt plate, 15, control panel, 16, the transparent plate, 17, the opening, 18, the mount, 19, the second motor, 20, the second motor shaft, 21, the revolving stage, 22, spacing frame, 23, first collection box, 24, the second collection box.

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. 1-6, the present invention provides a technical solution: the utility model provides an automatic change aviation part for shaping leftover bits excision equipment, it is shown according to fig. 1 and fig. 2, the left side of base 1 up end is fixed with plummer 2, and the up end of plummer 2 rotates and is connected with conveyer device 3, the centre department of base 1 up end is fixed with bears frame 4 simultaneously, bear the top internal fixation of frame 4 and have first electric telescopic handle 6, and the right-hand member of first electric telescopic handle 6 is connected with slider 7, the collocation uses first electric telescopic column 801, after sucking pump 805 and sucking disc 806 suck-up aviation part, first electric telescopic handle 6 extension, slide right with this promotion slider 7, conveniently transport the processing to aviation part.

According to fig. 1, 2 and 3, the transfer mechanism 8 is fixed at the bottom of the slider 7, the slider 7 is slidably connected to the left side of the inner top of the bearing frame 4, the slider 7 is slidably connected in the chute 5, the chute 5 is arranged at the inner top of the bearing frame 4, the chute 5 plays a role in assisting to limit in the process of sliding the slider 7 left and right, so that the slider 7 can slide left and right more stably, the transfer mechanism 8 comprises a first electric telescopic column 801, a motor box 802, a first motor 803, a first motor shaft 804, a suction pump 805 and a suction cup 806, the first electric telescopic column 801 is fixed at the bottom of the slider 7, meanwhile, the bottom of the first electric telescopic column 801 is connected with the motor box 802, the first motor 803 is fixed in the motor box 802, the lower side of the first motor 803 is connected with the suction pump 805 through the first motor shaft 804, the bottom of the suction pump 805 is fixed with the suction cup 806, after the aviation part is transferred to the upper side of the turntable 21, the first electric telescopic column 801 extends, the suction pump 803 and the aviation part can rotate under the action of the first motor shaft 804, so that the whole aviation part 21 can be adjusted conveniently on the whole turntable 21.

As shown in fig. 1, 2, 3 and 4, a first support 9 and a second support 10 are fixed to the front side and the rear side of the right side of the top in the bearing frame 4, a second electric telescopic rod 11 is fixed to the right side of the bottom of the second support 10, second electric telescopic columns 12 are fixed to the front side and the rear side of the bottom of the first support 9, the bottom of the front second electric telescopic column 12 is connected to a pressing block 13, the bottom of the rear second electric telescopic column 12 is connected to a supporting plate 14, the pressing block 13 forms a telescopic structure with the first support 9 through the corresponding second electric telescopic column 12, after the processing of the aerial parts is completed, the turntable 21 rotates 90 degrees counterclockwise, after the aerial parts are tightly fixed by the supporting plate 14, the pressing block 13 moves downward under the stretching action of the corresponding second electric telescopic column 12, so as to break the leftover bits, the supporting plate 14 forms a telescopic structure with the first support 9 through the corresponding second electric telescopic column 12, before the cutting-off work of the leftover bits is performed, the supporting plate 14 needs to move downward under the stretching action of the corresponding second electric telescopic column 12, the supporting frame 12, the whole transparent plate 15 controls the operation of the upper panel, and the operation of the whole aerial parts, the transparent plate 15 is controlled by the manual control panel, and the operation of the whole panel 15, and the manual control panel is controlled by the manual work.

According to fig. 1, 2, 3, 4 and 5, an opening 17 is formed in the right side of the front side of the bearing frame 4, a fixing frame 18 is arranged on the inner side of the bearing frame 4, the fixing frame 18 is fixed on the base 1, a second motor 19 is fixed in the fixing frame 18, a rotary table 21 is rotatably connected to the upper side of the second motor 19 through a second motor shaft 20, the rotary table 21 can rotate anticlockwise and intermittently under the action of the second motor 19 and the second motor shaft 20, and the leftover material cutting and unloading operation of each aviation part can be completed orderly.

According to fig. 1, fig. 2, fig. 3, fig. 4 and fig. 6, the revolving stage 21 rotates and connects the top at the mount 18, and the front side of mount 18 and the right side of mount 18 are provided with first collection box 23 and second collection box 24 respectively, first collection box 23 and second collection box 24 all place on base 1 simultaneously, the up end of revolving stage 21 is fixed with on spacing frame 22, and spacing frame 22 is provided with four, four spacing frame 22 circumference evenly distributed simultaneously, spacing frame 22 plays spacing effect to aviation part, guarantee aviation part's work degree with this, the convenient smooth excision work of accomplishing every aviation part leftover bits.

The working principle of the embodiment is as follows: when the automatic leftover material cutting equipment for aviation part molding is used, the external power supply is connected, the operation of the whole device is controlled by operating the control panel 15, firstly, aviation parts are placed on the conveyor belt device 3, the conveyor belt device 3 is started, the conveyor belt device 3 operates to drive the aviation parts to move rightwards, after the aviation parts reach the position right below the suction pump 805, the first electric telescopic column 801 is started, the first electric telescopic column 801 extends, the motor box 802, the suction pump 805 and the suction cup 806 integrally move downwards, after the aviation parts are sucked by the suction pump 805 and the suction cup 806, the first electric telescopic column 801 contracts, the suction pump 805 moves upwards, then the first electric telescopic rod 6 is started, the first electric telescopic rod 6 extends, the slide block 7 slides rightwards under the action of the chute 5, so that the aviation parts of the rotary table are conveyed to the position above the rotary table 21, and then the aviation parts are lowered, simultaneously starting the first motor 803, the first motor 803 drives the first motor shaft 804 to rotate so as to drive the suction pump 805 to rotate, so as to adjust the angle of the aviation part, so that the aviation part can be completely landed on the rotary table 21, the limit frame 22 has a limit function on the aviation part, the aviation part is loosened after the aviation part is landed, then the motor box 802, the suction pump 805 and the suction cup 806 are integrally returned to the original position, then the second motor 19 is started, the second motor 19 drives the second motor shaft 20 to rotate so as to drive the rotary table 21 to rotate 90 degrees anticlockwise, then the second electric telescopic column 12 at the rear side of the bottom of the first bracket 9 is started, the second electric telescopic column 121 is extended so as to drive the abutting plate 14 to move downwards so as to abut and fix the aviation part, then the second electric telescopic column 12 at the front side of the bottom of the first bracket 9 is started, and the second electric telescopic column 12 is extended, the pressing block 13 is driven to move downwards to press off the leftover materials, the leftover materials fall into the first collecting box 23, then the rotary table 21 continues to rotate anticlockwise for 90 degrees, then the second electric telescopic rod 11 is started to extend, the second electric telescopic rod 11 pushes the processed aviation parts down into the second collecting box 24, blanking operation is completed, the next aviation part can be transferred onto the rotary table 21 in the process of carrying out leftover material cutting processing on the previous aviation part, then the rotary table 21 rotates intermittently, transferring, leftover material cutting and unloading operation of each aviation part can be completed conveniently, orderly and efficiently, the whole operation process can be observed through the transparent plate 16, and the content which is not described in detail in the specification belongs to the prior art known by professional technicians in the field.

According to the above embodiment, alright realize the utility model discloses well. It is worth to say that, on the premise of the above structural design, in order to solve the same technical problem, even if some insubstantial changes or retouching are made in the utility model, the essence of the adopted technical scheme is still the same as the utility model, so it should be in the protection scope of the utility model.

Claims

1. The utility model provides an automatic change aviation part for shaping leftover bits excision equipment, includes base (1), transport mechanism (8), control panel (15) and revolving stage (21), its characterized in that:

the conveying device comprises a base (1), wherein a bearing table (2) is fixed on the left side of the upper end face of the base (1), the upper end face of the bearing table (2) is rotatably connected with a conveying belt device (3), and a bearing frame (4) is fixed in the middle of the upper end face of the base (1);

the transfer mechanism (8) is fixed to the bottom of the sliding block (7), the sliding block (7) is connected to the left side of the inner top of the bearing frame (4) in a sliding mode, a first support (9) and a second support (10) are fixed to the front side and the rear side of the right side of the inner top of the bearing frame (4) respectively, a second electric telescopic rod (11) is fixed to the right side of the bottom of the second support (10), second electric telescopic columns (12) are fixed to the front side and the rear side of the bottom of the first support (9), the bottom of the front second electric telescopic column (12) is connected with the pressing block (13), meanwhile the bottom of the rear second electric telescopic column (12) is connected with the abutting plate (14), an opening (17) is formed in the right side of the front side of the bearing frame (4), a fixing frame (18) is arranged on the inner side of the bearing frame (4), and the fixing frame (18) is fixed to the base (1);

the rotary table (21) is rotatably connected to the top of the fixing frame (18), a first collecting box (23) and a second collecting box (24) are respectively arranged on the front side of the fixing frame (18) and the right side of the fixing frame (18), and the first collecting box (23) and the second collecting box (24) are both placed on the base (1).

2. The automatic change aviation part shaping with leftover bits excision equipment of claim 1 characterized in that: bear the top internal fixation of frame (4) and have first electric telescopic handle (6), and the right-hand member of first electric telescopic handle (6) is connected with slider (7).

3. The automatic change leftover bits and pieces excision equipment for aviation part shaping of claim 1, characterized in that: the sliding block (7) is connected in the sliding groove (5) in a sliding mode, and the sliding groove (5) is formed in the inner top of the bearing frame (4).

4. The automatic change leftover bits and pieces excision equipment for aviation part shaping of claim 1, characterized in that: transport mechanism (8) include first electric telescopic column (801), motor box (802), first motor (803), first motor shaft (804), suction pump (805) and sucking disc (806), and first electric telescopic column (801) are fixed in the bottom of slider (7), and the bottom of first electric telescopic column (801) is connected with motor box (802) simultaneously, motor box (802) internal fixation has first motor (803), and the downside of first motor (803) is connected with suction pump (805) through first motor shaft (804), and the bottom of suction pump (805) is fixed with sucking disc (806) simultaneously.

5. The automatic change leftover bits and pieces excision equipment for aviation part shaping of claim 1, characterized in that: the pressing block (13) and the first support (9) form a telescopic structure through the corresponding second electric telescopic column (12).

6. The automatic change leftover bits and pieces excision equipment for aviation part shaping of claim 1, characterized in that: the supporting plate (14) and the first support (9) form a telescopic structure through the corresponding second electric telescopic column (12).

7. The automatic change leftover bits and pieces excision equipment for aviation part shaping of claim 1, characterized in that: the control panel (15) is fixed on the front end face of the bearing frame (4), a transparent plate (16) is arranged on the upper side of the control panel (15), and the transparent plate (16) is inlaid on the bearing frame (4).

8. The automatic change leftover bits and pieces excision equipment for aviation part shaping of claim 1, characterized in that: a second motor (19) is fixed in the fixing frame (18), and the upper side of the second motor (19) is rotatably connected with a rotary table (21) through a second motor shaft (20).

9. The automatic change leftover bits and pieces excision equipment for aviation part shaping of claim 1, characterized in that: the upper end face of the rotary table (21) is fixed on four limiting frames (22), and the four limiting frames (22) are uniformly distributed in the circumferential direction.