Aircraft part grinding equipment
By using hydraulic cylinders and dust collectors to clean up dust, and screen plates to collect iron filings, and combining electric push rods and limit plates to limit the movement of parts, the problem of dust and iron filings cleaning is solved, improving the quality of aircraft parts grinding and operator safety.
Patent Information
- Application Number
- CN202520017068.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-06
- Publication Date
- 2025-12-26
- Estimated Expiration
- 2035-01-06
AI Technical Summary
Existing aircraft parts grinding equipment produces dust and small iron filings during the grinding process, which are difficult to clean effectively, affecting processing quality and operator health.
The system employs a combination of hydraulic cylinders, fixed rods, mounting rods, a grinder, a sieve plate, and a dust collector. The hydraulic cylinders drive the grinder to move and activate the dust collector to handle dust. The sieve plate collects small iron filings. Combined with electric push rods, clamps, and limit plates, the system achieves limited positioning and stable grinding of parts of different shapes.
It effectively removes dust and small iron filings, improves the quality of parts, reduces the health impact on operators, and ensures the stability and efficiency of the grinding process.
Smart Images
Figure CN223719144U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the field of aircraft parts polishing, specifically, an aircraft parts polishing device. BACKGROUND
[0002] The aircraft parts polishing device is crucial in the aviation manufacturing industry, mainly used for fine machining and surface treatment of aircraft parts. The parts to be polished are fixed on the workbench to ensure stability. The polishing speed, feed amount and polishing time are input through the control panel. The device is started, the polishing tool contacts the parts, and the surface is treated by rotating or reciprocating. After polishing, cleaning and inspection are performed to ensure that the parts meet the technical standards, thereby achieving polishing of the parts.
[0003] In the process of polishing aircraft parts, the usual device is to limit the parts. After limiting, the parts are polished directly using a polisher. Although this method can polish the parts, dust may be generated during polishing. If not cleaned in time, it will not only affect the processing quality of the parts, but also affect the operator, making it inconvenient for the operator to use. UTILITY MODEL CONTENT
[0004] To make up for the above shortcomings, the utility model provides an aircraft parts polishing device that overcomes the above technical problems or at least partially solves the above problems.
[0005] The utility model is implemented as follows:
[0006] The utility model provides an aircraft parts polishing device, which comprises a fixing frame,
[0007] The top of the fixing frame is provided with a mounting frame, the inside of the mounting frame is provided with two groups of hydraulic cylinders, the bottom of the two groups of hydraulic cylinders is respectively provided with a fixing rod and a mounting rod, the bottom of the fixing rod and the bottom of the mounting rod are both provided with a polisher, and the rear part of the mounting frame is provided with two groups of dust collectors.
[0008] The top of the fixing frame is provided with two groups of sieve plates, and the top of the two groups of sieve plates is respectively provided with a polishing table and a polishing ring.
[0009] In one preferred scheme, the top of one group of sieve plates is provided with two groups of electric push rods, and the polishing table is arranged between the two groups of electric push rods.
[0010] In one preferred scheme, the side of the two groups of electric push rods facing each other is provided with a clamp, and the side of the two groups of clamps facing each other is provided with an anti-skid pad.
[0011] In a preferred scheme, the top of the other group of the screen plate is provided with an electric telescopic rod, and the output end of the electric telescopic rod is provided with a limiting plate.
[0012] In a preferred scheme, the limiting plate is arranged above the polishing ring, and the front part of the fixing frame is provided with a mounting door.
[0013] In a preferred scheme, the inner part of the two groups of the mounting frame is provided with a mounting hole, and the dust collector is arranged in the inner part of the mounting hole.
[0014] In a preferred scheme, the two groups of the dust collector are arranged obliquely above the polishing table and the polishing ring respectively, and the four corners of the polishing table are arranged in a slope shape.
[0015] In a preferred scheme, the front part of the fixing frame is provided with a PLC controller, and the bottom of the fixing frame is provided with a supporting leg.
[0016] The aircraft part polishing equipment has the following beneficial effects:
[0017] 1. Through the cooperation of the hydraulic cylinder, the fixed rod, the mounting rod, the polisher, the screen plate and the dust collector, two groups of hydraulic cylinders can be started to drive the fixed rod or the mounting rod to move downward according to the needs, the polisher moves synchronously when moving, the dust collector is started to process the dust generated during polishing when the polishing disc on the polisher moves to the aircraft part, the small iron filings and the like generated during polishing of the aircraft part can fall into the bottom of the fixing frame for collection through the screen plate, so that the dust generated during polishing of the aircraft part can be processed, thereby not only the quality of the aircraft part can be improved, but also the influence of the operator can be reduced.
[0018] 2. Through the cooperation of the polishing ring, the polishing table, the electric push rod, the clamp, the electric telescopic rod and the limiting plate, when the operator needs to limit the aircraft part, the operator can place the aircraft part on the top of the polishing ring or the polishing table according to the needs, then the operator can control the two groups of electric push rods to drive the clamps to move towards each other or start the electric telescopic rod to drive the limiting plate to move downward according to the needs, so that the circular or square aircraft part can be limited, and the polishing operation is performed subsequently after the limiting is completed. BRIEF DESCRIPTION OF DRAWINGS
[0019] In order to more clearly illustrate the technical scheme of the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiments, and it should be understood that the following drawings only show some embodiments of the present application, and should not be regarded as a limitation to the scope, and for those skilled in the art, other related drawings can be obtained without creative labor on the basis of the drawings.
[0020] Figure 1 is a whole perspective view provided by the embodiment of the present application;
[0021] Figure 2 is a top structure schematic view of the fixing frame provided by the embodiment of the present application;
[0022] Figure 3 is a rear structure schematic view of the fixing frame provided by the embodiment of the present application;
[0023] Figure 4 is a top structure schematic view of the fixing frame provided by the embodiment of the present application;
[0024] In the figure: 11, fixing frame; 12, mounting frame; 13, hydraulic cylinder; 14, fixed rod; 15, sander; 16, polishing table; 17, mounting rod; 18, electric push rod; 19, clamp; 2, sieve plate; 21, mounting door; 22, dust collector; 23, electric telescopic rod; 24, non-slip pad; 25, limiting plate; 26, polishing ring. DETAILED DESCRIPTION
[0025] In order to make the purpose, technical scheme and advantages of the embodiment of the present application clearer, the technical scheme in the embodiment of the present application will be described clearly and completely below in combination with the drawings in the embodiment of the present application. Obviously, the described embodiment is a part of the embodiments of the present application, rather than all the embodiments of the present application. Based on the embodiments in the present application, all the other embodiments obtained by the person skilled in the art without making creative labor belong to the scope of protection of the present application.
[0026] Reference Figures 1-4The utility model provides a technical scheme: an airplane spare part polishing equipment, including fixed frame 11, the top of fixed frame 11 is provided with mounting frame 12, the inside of mounting frame 12 is provided with two groups of hydraulic cylinder 13, the bottom of two groups of hydraulic cylinder 13 is provided with fixed rod 14 and mounting rod 17 respectively, the bottom of fixed rod 14 and the bottom of mounting rod 17 all are provided with polisher 15, the rear portion of mounting frame 12 is provided with two groups of dust collector 22, the top of fixed frame 11 is provided with two groups of sieve plate 2, the top of two groups of sieve plate 2 is provided with polishing table 16 and polishing ring 26 respectively, through the mutual matching of hydraulic cylinder 13, fixed rod 14, mounting rod 17, polisher 15, sieve plate 2 and dust collector 22, when the operator needs to polish the airplane spare part, the operator can first start two groups of hydraulic cylinder 13 to drive fixed rod 14 or mounting rod 17 to move downwards according to the need, when moving, can drive polisher 15 to move synchronously, when the polishing disc on polisher 15 moves to the airplane spare part, the operator can start dust collector 22 to process the dust generated when polishing, and through the setting of sieve plate 2, can make other small iron filings generated during the polishing of airplane spare part fall into the bottom of fixed frame 11 and be collected, thereby the dust generated during the polishing of airplane spare part can be processed, thereby not only can improve the quality of airplane spare part, but also can reduce the influence of operator, convenient for the operator to use.
[0027] Refer to Figures 1-4 In a preferred embodiment, the top of one group of sieve plates 2 is provided with two groups of electric push rods 18, the polishing table 16 is arranged between the two groups of electric push rods 18, the side facing each other of the two groups of electric push rods 18 is provided with a clamp 19, the side facing each other of the two groups of clamps 19 is provided with an anti-skid pad 24, the anti-skid pad 24 is arranged, thereby the limiting effect of the clamp 19 can be improved, the top of the other group of sieve plates 2 is provided with an electric telescopic rod 23, the output end of the electric telescopic rod 23 is provided with a limiting plate 25, through the mutual cooperation of the polishing ring 26, the polishing table 16, the electric push rod 18, the clamp 19, the electric telescopic rod 23 and the limiting plate 25, when the operator needs to limit the airplane spare part, the operator can place the airplane spare part on the top of the polishing ring 26 or the polishing table 16 according to the demand, then the operator can control the two groups of electric push rods 18 to drive the clamps 19 to move towards each other or start the electric telescopic rod 23 to drive the limiting plate 25 to move downwards according to the need, thereby the circular or square airplane spare part can be limited, and the polishing operation is carried out subsequently after the limiting is completed.
[0028] Refer to Figures 1-4In a preferred embodiment, the limiting plate 25 is arranged above the polishing ring 26, the front of the fixing frame 11 is provided with a mounting door 21, by arranging the mounting door 21, the concentrated small iron filings and the like can be treated, the installation holes are arranged in the interiors of the two groups of installation frames 12, the dust collectors 22 are arranged in the interiors of the installation holes, the two groups of dust collectors 22 are arranged obliquely above the polishing table 16 and obliquely above the polishing ring 26 respectively, the four corners of the polishing table 16 are arranged in a slope shape, so that the collection effect of the small iron filings can be improved, the front of the fixing frame 11 is provided with a PLC controller, the PLC controller is arranged to control the hydraulic cylinder 13, the polisher 15, the electric push rod 18, the dust collector 22 and the electric telescopic rod 23, and the bottom of the fixing frame 11 is provided with supporting legs, so that the stability of the fixing frame 11 can be improved.
[0029] Specifically, the working process or working principle of the aircraft part polishing equipment is as follows: in the process of polishing the aircraft parts, the conventional device is to position the parts, and after positioning, the polisher 15 is directly used to polish the parts. Although this method can polish the parts, dust may be generated during polishing. If it is not cleaned in time, it will not only affect the processing quality of the parts, but also affect the operator, and it is not convenient for the operator to use. Therefore, the technical scheme can solve the above problems. When the operator needs to position the aircraft parts, the operator can place the aircraft parts on the top of the polishing ring 26 or the polishing table 16 according to the needs, and then the operator can control the two groups of electric push rods 18 to move the clamps 19 towards each other or start the electric telescopic rod 23 to move the limiting plate 25 downward according to the needs, so that the circular or square aircraft parts can be positioned. After positioning, the subsequent polishing operation is carried out. When the operator needs to polish the aircraft parts, the operator can first start the two groups of hydraulic cylinders 13 to move the fixed rod 14 or the mounting rod 17 downward according to the needs. When moving, the polisher 15 can be moved synchronously. When the polishing disc on the polisher 15 moves to the position of the aircraft parts, the operator can start the dust collector 22 to treat the dust generated during polishing. By arranging the sieve plate 2, the small iron filings and the like generated during polishing of the aircraft parts can fall into the bottom of the fixing frame 11 for collection, so that the dust generated during polishing of the aircraft parts can be treated, thereby improving the quality of the aircraft parts, reducing the influence on the operator, and facilitating the operator to use. Thus, all processes are completed.
[0030] It should be noted that the hydraulic cylinder 13, the grinder 15, the electric push rod 18, the dust collector 22 and the electric telescopic rod 23 are all connected with an external power supply and are devices or equipment existing in the prior art or devices or equipment that can be realized in the prior art, and the power supply, specific components and principles thereof are clear to those skilled in the art, and thus will not be described in detail.
Claims
1. An aircraft component sanding apparatus, characterized by: Including fixed frame (11), The top of the fixed frame (11) is provided with a mounting frame (12), the inside of the mounting frame (12) is provided with two groups of hydraulic cylinders (13), the bottom of the two groups of hydraulic cylinders (13) is respectively provided with a fixed rod (14) and a mounting rod (17), the bottom of the fixed rod (14) and the bottom of the mounting rod (17) are provided with a sander (15), and the rear of the mounting frame (12) is provided with two groups of dust collectors (22). The top of the fixed frame (11) is provided with two groups of sieve plates (2), and the top of the two groups of sieve plates (2) is respectively provided with a polishing table (16) and a polishing ring (26).
2. An aircraft part sanding apparatus as defined in claim 1, wherein, The top of one group of the sieve plates (2) is provided with two groups of electric push rods (18), and the polishing table (16) is arranged between the two groups of electric push rods (18).
3. An aircraft part sanding apparatus as defined in claim 2, wherein, Opposite sides of the two groups of electric push rods (18) are provided with clamps (19), and opposite sides of the two groups of clamps (19) are provided with anti-skid pads (24).
4. An aircraft part sanding apparatus as defined in claim 3, wherein, The top of the other group of the sieve plates (2) is provided with an electric telescopic rod (23), and the output end of the electric telescopic rod (23) is provided with a limiting plate (25).
5. An aircraft part sanding apparatus as defined in claim 4, wherein, The limiting plate (25) is arranged above the polishing ring (26), and the front of the fixed frame (11) is provided with a mounting door (21).
6. An aircraft part sanding apparatus as defined in claim 5, wherein, The inside of the two groups of mounting frames (12) is provided with mounting holes, and the dust collectors (22) are arranged in the mounting holes.
7. An aircraft part sanding apparatus as defined in claim 6, wherein, The two groups of dust collectors (22) are arranged obliquely above the polishing table (16) and the polishing ring (26) respectively, and the four corners of the polishing table (16) are provided in a slope shape.
8. An aircraft part sanding apparatus as defined in claim 7, wherein, The front of the fixed frame (11) is provided with a PLC controller, and the bottom of the fixed frame (11) is provided with supporting legs.