CN220295897U - Perforating device is used in processing of aviation spare part - Google Patents

Abstract

The utility model discloses a perforating device for processing aviation parts, which comprises a workbench, wherein a drilling mechanism is fixedly arranged on the top surface of the workbench, a bottom plate is fixedly arranged on the surface of the drilling mechanism, a clamping assembly is fixedly arranged on the top surface of the workbench, and cleaning assemblies are fixedly arranged on two sides of the top surface of the workbench. In the above-mentioned scheme, set up the clamping assembly, place aviation spare part on placing the board during the use, change the sliding plate position through adjusting screw and nut, make splint press from both sides tight aviation spare part, when reaching punching to aviation spare part, make the more accurate effect of punching, start the motor before punching, the motor can drive the axis of rotation and rotate, and the axis of rotation drives the flabellum and rotate, thereby blow the suction box with the piece, and the fan then can inhale the dust collection box with the piece in, the filter screen can prevent piece entering fan, make piece stay in the dust collection box, reach the condition emergence that prevents that the piece exists influencing the punching precision.

Description

Perforating device is used in processing of aviation spare part

Technical Field

The utility model relates to the technical field of punching devices, in particular to a punching device for processing aviation parts.

Background

Aviation components are a generic term for various components of an aircraft, and punching is an indispensable part in the processing of components, and usually, a puncher is used to punch the aviation components, but in practical use, there are still some disadvantages, such as: aviation spare part is used for in the aspect of the aircraft manufacturing, generally to the requirement of machining precision higher, and when using the puncher to punch, need the manual work to support, but the manual work supports and can't accomplish to fix completely, then can appear certain error, can produce some piece when secondly punching to the spare part, the piece can scatter the surface of spare part and wait to punch the position, can make the drill point touch of puncher piece, the existence of piece can make the position and the size that beat the hole take place the skew to the precision to drilling causes certain influence, leads to can't satisfy the demand to aviation spare part high accuracy processing.

Disclosure of Invention

In order to overcome the defects in the prior art, the utility model provides the punching device for processing the aviation parts, so as to solve the problems that in the prior art, the aviation parts are generally used in the aspect of airplane manufacture, the requirement on processing precision is high, when a punching machine is used for punching, the punching machine is required to manually support, but the manual support cannot be completely fixed, certain errors can occur, some fragments can be generated when the parts are punched, the fragments can be scattered to the surfaces of the parts and the positions to be punched, the drill points of the punching machine can touch the fragments, the positions and the sizes of holes can be offset due to the existence of the fragments, so that the precision of the punching is influenced to a certain extent, and the requirement on high-precision processing of the aviation parts cannot be met.

In order to solve the technical problems, the utility model provides the following technical scheme: the utility model provides an aviation spare part processing is with perforating device, includes the workstation, the top surface fixed mounting of workstation has drilling mechanism, drilling mechanism's fixed surface installs the bottom plate, the fixed surface of bottom plate installs a spring, the bottom fixed mounting of a spring has the clamp plate, the top surface fixed mounting of workstation has clamping assembly, the both sides fixed mounting of workstation top surface has cleaning assembly.

The clamping assembly comprises a placing plate, a screw is installed on the internal thread of the placing plate, a nut is installed on the surface thread of the screw, and a sliding block is fixedly installed in the placing plate.

The sliding plate is characterized in that a sliding rod is movably arranged in the sliding plate, a second spring is fixedly arranged on the surface of the sliding plate, a clamping plate is fixedly arranged at one end of the second spring, and the clamping assembly is matched with the bottom plate, the first spring, the pressing plate and the clamping assembly, so that a better fixing effect can be achieved.

The cleaning assembly comprises a first supporting frame and a second supporting frame, wherein a motor is fixedly arranged on the surface of the first supporting frame, a rotating shaft is fixedly arranged on a driving shaft of the motor, fan blades are fixedly arranged on the surface of the rotating shaft, a bearing is fixedly arranged on the surface of the rotating shaft, a supporting column is fixedly arranged on the surface of the bearing, a fan box is fixedly arranged at one end of the supporting column, and a protective fence is fixedly arranged on the surface of the fan box.

Wherein, one end of the second supporting frame is fixedly provided with a dust collection box, the surface of the dust collection box is fixedly provided with a dust collection box, the surface of the dust collection box is fixedly provided with a fan, and the air outlet of the fan is fixedly provided with a filter screen.

The technical scheme of the utility model has the following beneficial effects:

in the above-mentioned scheme, set up the clamping assembly, place aviation spare part on placing the board during the use, change the sliding plate position through adjusting screw and nut, make the sliding plate slide on the slider, finally make splint press from both sides tight aviation spare part, start drilling mechanism and begin punching to aviation spare part, when the drilling machine descends to certain altitude, can drive the clamp plate and touch aviation spare part, under the effect of spring No. one, can extrude aviation spare part, play the fixed action again, when reaching punching to aviation spare part, can keep it relatively stable, make the effect that punches more accurate, start the motor before punching, the motor can drive the axis of rotation and rotate, and the axis of rotation drives the flabellum and rotate, thereby blow the piece to the dust box, and the fan then can inhale the dust box with the piece, the filter screen can prevent the piece entering fan, make the piece stay in the dust box, reach the piece that will punch the production in time clear away, prevent that the piece exists influencing the condition emergence of punching precision.

Drawings

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

FIG. 2 is a diagram of the overall internal architecture of the present utility model;

FIG. 3 is a schematic view of a clamping assembly according to the present utility model;

FIG. 4 is a schematic view of a cleaning assembly according to the present utility model.

[ reference numerals ]

1. A work table; 2. a drilling mechanism; 3. a bottom plate; 4. a first spring; 5. a pressing plate; 6. a clamping assembly; 7. cleaning the assembly; 61. placing a plate; 62. a screw; 63. a nut; 64. a slide block; 65. a sliding plate; 66. a slide rod; 67. a second spring; 68. a clamping plate; 71. a first support frame; 72. a motor; 73. a rotating shaft; 74. a fan blade; 75. a bearing; 76. a support column; 77. a fan case; 78. a guard rail; 79. a second support frame; 710. a dust suction box; 711. a dust collection box; 712. a blower; 713. and (3) a filter screen.

Detailed Description

In order to make the technical problems, technical solutions and advantages to be solved more apparent, the following detailed description will be given with reference to the accompanying drawings and specific embodiments.

As shown in fig. 1 to fig. 4, the embodiment of the utility model provides a punching device for processing aviation parts, which comprises a workbench 1, wherein a drilling mechanism 2 is fixedly arranged on the top surface of the workbench 1, a bottom plate 3 is fixedly arranged on the surface of the drilling mechanism 2, a first spring 4 is fixedly arranged on the surface of the bottom plate 3, a pressing plate 5 is fixedly arranged at the bottom end of the first spring 4, a clamping assembly 6 is fixedly arranged on the top surface of the workbench 1, and cleaning assemblies 7 are fixedly arranged on two sides of the top surface of the workbench 1; the drilling mechanism 2 is an existing device, the drill point starts to rotate after being started, and the aviation parts are drilled through the up-and-down movement of the electric telescopic rod.

As shown in fig. 3, the clamping assembly 6 includes a placing plate 61, a screw 62 is mounted on an internal thread of the placing plate 61, a nut 63 is mounted on a surface thread of the screw 62, a sliding block 64 is fixedly mounted in the placing plate 61, a sliding plate 65 is movably mounted on a surface of the sliding block 64, a sliding rod 66 is movably mounted in the sliding plate 65, a second spring 67 is fixedly mounted on a surface of the sliding plate 65, a clamping plate 68 is fixedly mounted at one end of the second spring 67, and the clamping assembly 6 is matched with the bottom plate 3, the first spring 4 and the clamping assembly 6, so that a better fixing effect can be achieved; the surfaces of the placing plate 61 and the clamping plate 68 are covered with rubber pads, the rubber pads and the second spring 67 can effectively protect aviation components from being damaged, the sliding block 64 is shaped into a T shape, the sliding plate 65 cannot be separated from the workbench 1, and the sliding plate 65 and the clamping plate 68 are kept relatively stable due to the sliding rod 66.

As shown in fig. 4, the cleaning assembly 7 includes a first support frame 71 and a second support frame 79, a motor 72 is fixedly installed on a surface of the first support frame 71, a rotating shaft 73 is fixedly installed on a driving shaft of the motor 72, fan blades 74 are fixedly installed on a surface of the rotating shaft 73, a bearing 75 is fixedly installed on a surface of the rotating shaft 73, a supporting column 76 is fixedly installed on a surface of the bearing 75, a fan case 77 is fixedly installed at one end of the supporting column 76, a guard rail 78 is fixedly installed on a surface of the fan case 77, a dust box 710 is fixedly installed at one end of the second support frame 79, a dust box 711 is fixedly installed on a surface of the dust box 710, a fan 712 is fixedly installed on a surface of the dust box 711, and a filter screen 713 is fixedly installed at an air outlet of the fan 712; the guard rail 78 prevents the operator from being scratched by the fan blades 74 when working, and the filter screen 713 can block debris out of the air opening of the fan 712.

The working process of the utility model is as follows: the aviation part is placed on the placement plate 61, the position of the sliding plate 65 is changed through the adjusting screw 62 and the nut 63, the sliding plate 65 slides on the sliding block 64, finally the clamping plate 68 clamps the aviation part, the drilling mechanism 2 is started to start to punch the aviation part, when the aviation part descends to a certain height, the pressing plate 5 can touch the aviation part, the aviation part can be extruded under the action of the first spring 4, the motor 72 is started before punching, the motor 72 can drive the rotating shaft 73 to rotate, the rotating shaft 73 drives the fan blade 74 to rotate, chips are blown to the dust collection box 710, and the fan 712 can suck the chips into the dust collection box 711.

The last points to be described are: first, in the description of the present application, it should be noted that, unless otherwise specified and defined, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be mechanical or electrical, or may be a direct connection between two elements, and "upper," "lower," "left," "right," etc. are merely used to indicate relative positional relationships, which may be changed when the absolute position of the object being described is changed;

secondly: in the drawings of the disclosed embodiments, only the structures related to the embodiments of the present disclosure are referred to, and other structures can refer to the common design, so that the same embodiment and different embodiments of the present disclosure can be combined with each other under the condition of no conflict;

finally: the foregoing description of the preferred embodiments of the utility model is not intended to limit the utility model to the precise form disclosed, and any such modifications, equivalents, and alternatives falling within the spirit and principles of the utility model are intended to be included within the scope of the utility model.

Claims (5)

1. The utility model provides an aviation spare part processing is with perforating device, includes the workstation, its characterized in that, the top surface fixed mounting of workstation has drilling mechanism, drilling mechanism's fixed surface installs the bottom plate, the fixed surface of bottom plate installs a spring, the bottom fixed mounting of a spring has the clamp plate, the top surface fixed mounting of workstation has clamping assembly, the both sides fixed mounting of workstation top surface has the clearance subassembly.

2. The aircraft component machining perforating device of claim 1, wherein the clamping assembly comprises a placement plate, a screw is mounted on an internal thread of the placement plate, a nut is mounted on a surface thread of the screw, and a slider is fixedly mounted inside the placement plate.

3. The perforating device for machining aviation components of claim 2, wherein the sliding plate is movably arranged on the surface of the sliding block, the sliding rod is movably arranged in the sliding plate, the second spring is fixedly arranged on the surface of the sliding plate, the clamping plate is fixedly arranged at one end of the second spring, and the clamping assembly is matched with the bottom plate, the first spring and the clamping assembly, so that a better fixing effect can be achieved.

4. The perforating device for machining aviation components of claim 1, wherein the cleaning assembly comprises a first support frame and a second support frame, a motor is fixedly arranged on the surface of the first support frame, a rotating shaft is fixedly arranged on a driving shaft of the motor, fan blades are fixedly arranged on the surface of the rotating shaft, a bearing is fixedly arranged on the surface of the rotating shaft, a supporting column is fixedly arranged on the surface of the bearing, a fan box is fixedly arranged at one end of the supporting column, and a protective guard is fixedly arranged on the surface of the fan box.

5. The perforating device for processing aviation components of claim 4, wherein a dust box is fixedly arranged at one end of the second supporting frame, a dust box is fixedly arranged on the surface of the dust box, a fan is fixedly arranged on the surface of the dust box, and a filter screen is fixedly arranged at an air outlet of the fan.