CN221517199U - Deburring mechanism for aviation parts - Google Patents

Abstract

The application belongs to the technical field of deburring and polishing, and discloses an aircraft part deburring mechanism, which comprises an operation table, wherein symmetrical sliding grooves are formed in the operation table, pulleys are arranged in the sliding grooves, a portal frame is arranged at the top of each pulley, a movable mechanism is arranged in the middle position of the inner top of the portal frame, a fixed mechanism is arranged on the side wall of the operation table far away from the portal frame, and a dust collection mechanism is arranged at the center position of the bottom of the operation table; the screw rod is screwed to the carousel that rotates relatively is fixed and cooperates the rubber clamp pad when screwing fixedly to aviation part, and protection aviation part can not damaged, can make the movable mechanism carry out the processing burr of multi-angle through first movable arm and second movable arm and cooperation pivot seat to cooperation reset spring can reset the movable block in the movable slot and drive the second movable arm to reset when accomplishing aviation part processing, reduces the damage that machinery used.

Description

Deburring mechanism for aviation parts

Technical Field

The application relates to the technical field of deburring and polishing, in particular to a deburring mechanism for aviation parts.

Background

The aviation part mainly refers to various spare and accessory parts of an aviation aircraft, including aircraft body parts, aeroengine parts, instruments, airborne equipment, hydraulic systems, accessories and the like, burrs are easy to be generated at a sprue, a die parting surface and a die insert of the aviation part when the aviation part is produced and injection molded, so that deburring treatment is needed to be carried out on the aviation part by using deburring equipment.

Via search disclosure (bulletin) number: CN218927217U discloses a deburring equipment for aviation part processing, including multiaspect rotation type clearance mechanism of polishing, multiaspect rotation type clearance mechanism of polishing includes rotation driving component and multiaspect rotation adjustable clearance subassembly of polishing, multiaspect rotation adjustable clearance subassembly of polishing includes main pole circular mount pad, main pole, the fastener, vice pole, fine hair cloth strip and dull polish piece, main pole circular mount pad top links to each other with rotation driving component bottom, main pole circular mount pad's the outer disc of upper slope towards outside direction equipartition has two main poles at least, main pole lower part is opened and is connected the mounting groove with vice pole, vice pole is equipped with in the mounting groove with the pole that connects, and form detachable connection through the fastener between main pole and the vice pole, at least the equipartition has a fine hair cloth strip and a dull polish piece on the free end outer wall of vice pole, vice pole connecting end is opened at least and is connected a vice pole fastener installation through-hole. The utility model can rotationally polish and remove burrs and rotationally brush and remove cleaning scraps.

The machine is carrying out burring and polishing processing in-process to aviation section part corner, often has the piece dust of polishing and can not in time clear up to lead to the problem that the piece dust splashes of polishing in-process, thereby lead to the piece to fall into other positions of section bar, can influence subsequent handling, and the piece dust that on the other hand splashes can cause the injury to the human body after inhaling.

In order to solve the problems, the application provides an aircraft part deburring mechanism.

Disclosure of utility model

The application provides an aircraft part deburring mechanism which adopts the following technical scheme:

The utility model provides an aircraft part deburring mechanism, includes the operation panel, the spout of symmetry has been seted up on the operation panel, all be equipped with the pulley in the spout, the pulley top is equipped with the portal frame, top intermediate position is equipped with movable mechanism in the portal frame, the operation panel is kept away from the lateral wall of portal frame and all is equipped with fixed establishment, operation panel bottom central point puts and is equipped with dust extraction mechanism.

Through above-mentioned technical scheme, carry out fixed clamp through fixed establishment with the aeronautical part that needs burring to polish, be fixed in well and carry out burring processing on the operation panel, can extend a plurality of angles of the aeronautical part of polishing through the machine of movable mechanism with the burring, carry out the dust absorption mechanism and clear up the piece dust that will produce and suck away when polishing the burring.

Further, a grid is arranged at the bottom in the operation table, a driving motor is arranged at one end, far away from the portal frame, of the movable mechanism, and a deburring device is arranged at one end, far away from the movable mechanism, of the driving motor.

Through above-mentioned technical scheme, drive the deburring ware through driving motor and work and carry out the burring to the aviation part and handle to reduce the aviation part through the grid and fall into dust extraction and can let the piece dust pass through.

Furthermore, support columns are arranged at four corners of the bottom of the operation table, and bottom pads are arranged at the bottoms of the support columns.

Through above-mentioned technical scheme, can the steady operation of the whole equipment of steady support through the support column to the area of contact of cooperation base cushion increase equipment and ground makes the operation of equipment more firm.

Further, the movable mechanism comprises a rotating shaft seat, a first movable arm is arranged on one side of the outer wall of the rotating shaft seat, a second movable arm is arranged at one end, away from the rotating shaft seat, of the first movable arm, a movable groove is formed in one side of the first movable arm, a reset spring is arranged on one side, close to the rotating shaft seat, of the movable groove, a movable block is arranged on one side, away from the rotating shaft seat, of the movable groove, a second mounting seat is arranged on one side, close to the movable groove, of the second movable arm, an auxiliary rod is arranged in the second mounting seat, a first mounting seat is arranged at one end, close to the movable groove, of the auxiliary rod, and a movable block is arranged at the top of the first mounting seat.

Through above-mentioned technical scheme, can make the movable mechanism carry out the processing burr of multi-angle through first movable arm and second movable arm and cooperation pivot seat to cooperation reset spring can reset the movable block in the movable tank and drive the second movable arm and reset when handling the aviation part, reduce the damage that machinery was used.

Further, the number of the reset springs is two, the reset springs and the movable blocks are both located in the movable groove, and the first installation seat is connected with the second installation seat through the auxiliary rod.

Through the technical scheme, the first movable arm and the second movable arm are matched with the reset spring, when the aviation part is processed, the movable block in the movable groove can be reset, the second movable arm is driven to reset, and damage of mechanical use is reduced.

Further, fixed establishment includes the threaded rod, the one end that the operation panel was kept away from to the threaded rod all is equipped with the carousel, the one end that the carousel was kept away from to the threaded rod all is equipped with the rubber and presss from both sides the pad, the threaded rod all runs through the operation panel.

Through above-mentioned technical scheme, screw the threaded rod through rotating relative carousel and fix and cooperate the rubber clamp pad to screw when fixing the aviation part, protection aviation part can not damaged.

Further, the dust collection mechanism comprises a shell, a coarse mesh net is arranged in the shell, a fine mesh net is arranged in the shell, the fine mesh net is positioned below the coarse mesh net, an exhaust pipe is arranged at the bottom of the shell, and an air suction pump is arranged at the top of the exhaust pipe.

Through above-mentioned technical scheme, in the time of the burring of aircraft part was handled, inhale the shell with the piece dust that the burring produced through the aspirator pump, filter the piece dust through coarse mesh number net cooperation fine mesh number net, discharge through the blast pipe after filtering.

In summary, the application has the following beneficial technical effects:

Rotating relative carousel screw threaded rod and fixing and cooperation rubber clamp pad are screwing fixedly the aircraft part, protection aircraft part can not damaged, can make the movable mechanism carry out the processing burr of multi-angle through first movable arm and second movable arm and cooperation pivot seat, and cooperation reset spring can reset the movable block in the movable slot and drive the second movable arm and reset when accomplishing the aircraft part processing, reduce the damage that machinery was used, in the debris dust suction shell that the deburring produced through the aspirator pump when aircraft part deburring was handled, filter the debris dust through coarse mesh number net cooperation fine mesh number net, discharge through the blast pipe after filtering, debris and dust that produces when reducing deburring to human injury, and the clearance that can be timely produces the piece, prevent that the piece from falling into other section bars.

Drawings

FIG. 1 is a schematic diagram of the overall structure of the present application;

FIG. 2 is a schematic view of the movable mechanism structure of the present application;

FIG. 3 is an enlarged schematic view of the structure of FIG. 2A according to the present application;

Fig. 4 is a schematic structural view of a dust suction mechanism of the present application.

The reference numerals in the figures illustrate:

1. An operation table; 2. a support column; 3. a bottom pad; 4. a portal frame; 5. a movable mechanism; 501. a rotating shaft seat; 502. a first movable arm; 503. a second movable arm; 504. a second mounting base; 505. an auxiliary lever; 506. a first mount; 507. a movable groove; 508. a movable block; 509. a return spring; 6. a fixing mechanism; 601. a turntable; 602. a threaded rod; 603. a rubber clamping pad; 7. a chute; 8. a grille; 9. a dust collection mechanism; 901. a housing; 902. coarse mesh number net; 903. a fine mesh number net; 904. an exhaust pipe; 905. a getter pump; 10. a pulley; 11. a deburring device; 12. and driving the motor.

Detailed Description

The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application; it is apparent that the described embodiments are only some embodiments of the present application, not all embodiments, and that all other embodiments obtained by persons of ordinary skill in the art without making creative efforts based on the embodiments in the present application are within the protection scope of the present application.

In the description of the present application, it should be noted that the positional or positional relationship indicated by the terms such as "upper", "lower", "inner", "outer", "top/bottom", etc. are based on the positional or positional relationship shown in the drawings, are merely for convenience of describing the present application and simplifying the description, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present application. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present application, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "configured to," "engaged with," "connected to," and the like are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present application will be understood in specific cases by those of ordinary skill in the art.

Examples:

The embodiment of the application discloses an aircraft part deburring mechanism, referring to fig. 1 and 2, which comprises an operation table 1, wherein symmetrical sliding grooves 7 are formed in the operation table 1, pulleys 10 are arranged in the sliding grooves 7, a portal frame 4 is arranged at the top of each pulley 10, a movable mechanism 5 is arranged in the middle position of the top of each portal frame 4, a fixed mechanism 6 is arranged on the side wall, far away from the portal frame 4, of the operation table 1, a dust collection mechanism 9 is arranged in the center of the bottom of the operation table 1, the aircraft part needing deburring and polishing is fixedly clamped through the fixed mechanism 6, the aircraft part is well fixed on the operation table 1 for deburring, the movable mechanism 5 can carry out extension polishing on the aircraft part for a plurality of angles, and generated dust is cleaned and sucked through the dust collection mechanism 9 when deburring and deburring are carried out.

Referring to fig. 1 and 2, a grille 8 is arranged at the bottom in the operation table 1, a driving motor 12 is arranged at one end of the movable mechanism 5 away from the portal frame 4, a deburring device 11 is arranged at one end of the driving motor 12 away from the movable mechanism 5, the deburring device 11 is driven to work by the driving motor 12 to perform deburring treatment on aviation parts, and the aviation parts are reduced to fall into a dust collection mechanism 9 through the grille 8 and can pass through dust.

Referring to fig. 1, support columns 2 are respectively arranged at four corners of the bottom of the operation table 1, bottom pads 3 are respectively arranged at the bottoms of the support columns 2, and the support columns 2 can stably support the stable operation of the whole equipment, and the contact area between the equipment and the ground is increased by matching with the bottom pads 3, so that the operation of the equipment is more stable.

Referring to fig. 2 and 3, the movable mechanism 5 includes a rotating shaft seat 501, a first movable arm 502 is disposed on one side of an outer wall of the rotating shaft seat 501, a second movable arm 503 is disposed at one end of the first movable arm 502 away from the rotating shaft seat 501, a movable groove 507 is disposed in one side of the first movable arm 502, a return spring 509 is disposed on one side of the movable groove 507 close to the rotating shaft seat 501, a movable block 508 is disposed on one side of the movable groove 507 away from the rotating shaft seat 501, a second mounting seat 504 is disposed on one side of the second movable arm 503 close to the movable groove 507, an auxiliary rod 505 is disposed in the second mounting seat 504, a first mounting seat 506 is disposed at one end of the auxiliary rod 505 close to the movable groove 507, a movable block 508 is disposed at the top of the first mounting seat 506, the movable mechanism 5 can be used for multi-angle burr treatment by the first movable arm 502 and the second movable arm 503 in cooperation with the rotating shaft seat 501, and the movable block 508 can be reset and drive the second movable arm 503 to reset when the treatment of the aviation parts is completed by cooperation of the return spring 509.

Referring to fig. 2 and 3, the number of the restoring springs 509 is two, the restoring springs 509 and the movable blocks 508 are both located in the movable groove 507, the first mounting seat 506 is connected with the second mounting seat 504 through the auxiliary rod 505, the first movable arm 502 and the second movable arm 503 cooperate with the restoring springs 509 to restore the movable blocks 508 in the movable groove 507 and drive the second movable arm 503 to restore when the processing of the aviation parts is completed, so that the damage of mechanical use is reduced.

Referring to fig. 1, the fixing mechanism 6 includes a threaded rod 602, one end of the threaded rod 602 away from the operation platform 1 is provided with a turntable 601, one end of the threaded rod 602 away from the turntable 601 is provided with a rubber clamping pad 603, the threaded rod 602 penetrates through the operation platform 1, the threaded rod 602 is screwed by rotating the opposite turntable 601 to fix the aviation part and cooperate with the rubber clamping pad 603, and the aviation part is protected from being damaged while being screwed and fixed.

Referring to fig. 1 and 4, the dust suction mechanism 9 includes a housing 901, a coarse mesh net 902 is disposed in the housing 901, a fine mesh net 903 is disposed in the housing 901, the fine mesh net 903 is located below the coarse mesh net 902, an exhaust pipe 904 is disposed at the bottom of the housing 901, a suction pump 905 is disposed at the top of the exhaust pipe 904, and when the air-craft part is subjected to deburring, the dust generated by deburring is sucked into the housing 901 by the suction pump 905, and is filtered by the coarse mesh net 902 and the fine mesh net 903, and is discharged through the exhaust pipe 904 after being filtered.

The implementation principle of the embodiment is as follows: the rotating disc 601 is used for rotating the threaded rod 602 to fix the aviation part and matched with the rubber clamping pad 603, the aviation part is protected from being damaged when the aviation part is screwed and fixed, the movable mechanism 5 can be used for multi-angle burr treatment through the first movable arm 502 and the second movable arm 503 and matched with the rotating shaft seat 501, the movable block 508 in the movable groove 507 can be reset and the second movable arm 503 is driven to reset when the aviation part is processed, the damage of mechanical use is reduced, the chip dust generated by deburring is sucked into the shell 901 through the suction pump 905 when the aviation part is subjected to deburring, the chip dust is filtered through the coarse mesh net 902 and the fine mesh net 903, and the chip dust is discharged through the exhaust pipe 904 after the filtration.

The above embodiments are not intended to limit the scope of the present application, so: all equivalent changes in structure, shape and principle of the application should be covered in the scope of protection of the application.

Claims (7)

1. The utility model provides an aircraft part deburring mechanism, includes operation panel (1), its characterized in that: symmetrical sliding grooves (7) are formed in the operation table (1), pulleys (10) are arranged in the sliding grooves (7), a portal frame (4) is arranged at the top of each pulley (10), a movable mechanism (5) is arranged at the middle position of the top in the portal frame (4), a fixing mechanism (6) is arranged on the side wall, far away from the portal frame (4), of the operation table (1), and a dust collection mechanism (9) is arranged at the central position of the bottom of the operation table (1).

2. An aircraft part deburring mechanism as claimed in claim 1, wherein: the novel deburring device is characterized in that a grid (8) is arranged at the inner bottom of the operation table (1), a driving motor (12) is arranged at one end, far away from the portal frame (4), of the movable mechanism (5), and a deburring device (11) is arranged at one end, far away from the movable mechanism (5), of the driving motor (12).

3. An aircraft part deburring mechanism as claimed in claim 1, wherein: support columns (2) are arranged at four corners of the bottom of the operating platform (1), and bottom pads (3) are arranged at the bottoms of the support columns (2).

4. An aircraft part deburring mechanism as claimed in claim 1, wherein: the movable mechanism (5) comprises a rotating shaft seat (501), a first movable arm (502) is arranged on one side of the outer wall of the rotating shaft seat (501), a second movable arm (503) is arranged at one end, far away from the rotating shaft seat (501), of the first movable arm (502), a movable groove (507) is formed in one side of the first movable arm (502), a reset spring (509) is arranged on one side, close to the rotating shaft seat (501), of the movable groove (507), a movable block (508) is arranged on one side, far away from the rotating shaft seat (501), of the movable groove (507), a second mounting seat (504) is arranged on one side, close to the movable groove (507), of the second movable arm (503), an auxiliary rod (505) is arranged in the second mounting seat (504), a first mounting seat (506) is arranged at one end, close to the movable groove (507), and the top of the first mounting seat (506) is provided with a movable block (508).

5. An aircraft part deburring mechanism as claimed in claim 4, wherein: the number of the reset springs (509) is two, the reset springs (509) and the movable blocks (508) are both positioned in the movable grooves (507), and the first mounting seats (506) are mutually connected with the second mounting seats (504) through the auxiliary rods (505).

6. An aircraft part deburring mechanism as claimed in claim 1, wherein: the fixing mechanism (6) comprises a threaded rod (602), one end, away from the operation platform (1), of the threaded rod (602) is provided with a rotary table (601), one end, away from the rotary table (601), of the threaded rod (602) is provided with a rubber clamp pad (603), and the threaded rod (602) penetrates through the operation platform (1).

7. An aircraft part deburring mechanism as claimed in claim 1, wherein: the dust collection mechanism (9) comprises a shell (901), a coarse mesh net (902) is arranged in the shell (901), a fine mesh net (903) is arranged in the shell (901), the fine mesh net (903) is located below the coarse mesh net (902), an exhaust pipe (904) is arranged at the bottom of the shell (901), and an air suction pump (905) is arranged at the top of the exhaust pipe (904).