Permeation device for nondestructive testing of airplane part liquid permeation

By designing a permeation device including stirring blades and a tilting device, the problem of uneven material penetration is solved, the uniform flow rate and concentration of the permeate are achieved, the detection error is reduced, and it is ensured that the bottom of the material can also be penetrated.

CN120651760APending Publication Date: 2025-09-16GUIZHOU AEROSPACE PRECISION PRODS
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Patent Information

Application Number
CN202510867903.8
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-06-26
Publication Date
2025-09-16

AI Technical Summary

Technical Problem

The existing permeation device causes uneven penetration of the material, especially the place where the bottom of the material contacts the material plate cannot be penetrated by the permeate, resulting in large errors in the test results.

Method used

An infiltration device including a box, a support frame, a lifting device, a motor, a lifting device and a stirring device is designed. Through the cooperation of stirring blades and a tilting device, uniform infiltration of the material is achieved, ensuring that the bottom of the material can also be penetrated by the permeate.

Benefits of technology

The uniform flow rate and concentration of the penetrant are achieved, which reduces the detection error caused by poor penetration effect, ensures uniform penetration of the material everywhere, and avoids the problem that the bottom of the material cannot be penetrated due to adhesion with the material plate.

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Abstract

The invention provides a permeation device for nondestructive testing of airplane part liquid permeation. The permeation device comprises a box body, a support frame, a lifting device, a motor and a jacking device, the support frame is mounted above the box body; the lifting device is installed above the supporting frame and connected with the jacking device. The motor is mounted on one side of the box body; one end of the rotating rod is connected with the output end of the motor, and the other end extends into the box body; the stirring device is arranged in the box body and is connected with one end of the rotating rod in the box body; inclined devices are arranged on the two sides of the stirring device; the jacking device is arranged above the stirring device; according to the invention, the flow velocity of the penetrating fluid in the box body is faster, the concentration of each part is uniform, the material permeation is more uniform, and the detection result error caused by poor permeation effect due to uneven concentration of each part of the penetrating fluid is reduced; the phenomenon that the bottom of the material is attached to the material plate and cannot permeate is avoided.
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Description

Technical Field

[0001] The invention belongs to the technical field of liquid penetrant nondestructive testing equipment for aircraft parts, and in particular relates to a penetrant device for liquid penetrant nondestructive testing of aircraft parts. Background Art

[0002] Liquid penetrant nondestructive testing is a surface nondestructive testing method that mainly uses the wetting and capillary effects of liquids to penetrate the open defects on the surface of solid materials. The infiltrated liquid is then precipitated onto the surface through a developer, indicating the presence of defects. The liquid penetrant testing process can be divided into pre-cleaning, penetration, cleaning, drying, imaging, observation and other steps, among which the penetration device is indispensable.

[0003] The existing infiltration device has a relatively simple structure. The material is placed on the material plate to start infiltration, which makes the material infiltration uneven. The place where the bottom of the material contacts the material plate cannot be penetrated by the infiltration liquid, resulting in large errors in the subsequent imaging process. Summary of the Invention

[0004] In view of the above problems, the object of the present invention is to provide a liquid penetrant nondestructive testing device for aircraft parts that can be uniformly penetrated by materials.

[0005] The present invention is achieved through the following technical solutions: A penetrant device for liquid penetrant nondestructive testing of aircraft parts, comprising a housing, a support frame, a lifting device, a motor, and a lifting device; the support frame is mounted above the housing; the lifting device is mounted above the support frame, and the lifting device is connected to the lifting device; the motor is mounted on one side of the housing; one end of the rotating rod is connected to the output end of the motor, and the other end extends into the housing; the stirring device is disposed in the housing and connected to one end of the rotating rod in the housing; tilting devices are provided on both sides of the stirring device; the lifting device is disposed above the stirring device; the lifting device comprises a fixing seat, a crane, and a lifting cable; The fixing seat is installed above the support frame; the crane is installed above the fixing seat; one end of the lifting cable is connected to the output end of the crane, and the other end is branched into a "Y" shape and connected to the two ends of the top of the lifting device; the connection between the lifting cable and the lifting device is hinged with a hinge block; the stirring device includes a sliding spring, a stirring blade, a limit column, a rotating block and a fixed block; a plurality of stirring blades are mounted on the rotating rod inside the box; the stirring blade can slide along the rotating rod; a rotating block is fixed to the right side of the stirring blade; a fixed block is provided on the inner wall of the right side of the box; an inclined surface is provided on the rotating block; The cam is provided with an inclined surface that matches the rotating block; the sliding spring is sleeved in the rotating rod, and one end is fixed to the inner wall of the box body, and the other end is fixed to the left side of the stirring blade; the stirring blade is cross-shaped; the stirring device also includes a limit column; a notch is provided on the stirring blade; the limit column is installed on the rotating rod in the notch of the stirring blade; the tilting device includes a limit rod, a top plate, a limit spring, a top block, a support column and a support block; the top plate is symmetrically installed at the left and right ends of the stirring blade, and a hole is provided in the center to make way for the rotating rod; the limit rod passes through the box body horizontally and is slidably installed on the box body; the limit rod The right end is installed on the top plate; the limit spring is installed on the limit rod; a top block with a wedge-shaped surface is installed on the left side of the top plate; the support column is vertically slidably installed in the groove on the inner wall of the box; the upper end of the support column is installed with a support block, and the lower end cooperates with the wedge-shaped surface of the top block; the lifting device includes a material plate, a T-bar, an extrusion plate and a top column; the material plate is provided with a mezzanine; the hinge block is installed at both ends of the top of the material plate; the T-bar is vertically slidably installed on the material plate; the extrusion plate is installed at the lower end of the T-bar; one end of the top column is symmetrically installed on the left and right ends of the extrusion plate, and the other end is vertically slidably installed in the interlayer of the material plate.

[0006] Beneficial effects of the present invention: The present invention can make the flow rate of the permeate in the box faster, the concentration is uniform everywhere, and the material is penetrated more evenly, reducing the poor penetration effect caused by uneven concentration of the permeate in various places, which will cause errors in the detection results; and avoid the bottom of the material being unable to penetrate due to adhesion with the material plate. BRIEF DESCRIPTION OF THE DRAWINGS

[0007] The present invention will be further described in detail below with reference to the accompanying drawings.

[0008] Figure 1 This is a schematic diagram of the structure of the present invention Figure 1 .

[0009] Figure 2 This is a schematic diagram of the structure of the present invention Figure 2 .

[0010] Figure 3 It is a half-planed diagram of the present invention.

[0011] Figure 4 It is a partial schematic diagram of the stirring device in the present invention.

[0012] Figure 5 It is a partial schematic diagram of the tilting device in the present invention.

[0013] Figure 6 It is a partial schematic diagram of the lifting device described in the present invention. As shown in the figure: 1-box; 2-support frame; 3-fixed seat; 4-crane; 5-cable; 6-hinge block; 7-motor; 8-rotating rod; 9-stirring device; 901-sliding spring; 902-stirring blade; 903-limiting column; 904-rotating block; 905-fixed block; 10-tilting device; 1001-limiting rod; 1002-top plate; 1003-limiting spring; 1004-top block; 1005-support column; 1006-support block; 11-lifting device; 1101-material plate; 1102-T-rod; 1103-extrusion plate; 1104-top column. DETAILED DESCRIPTION

[0014] The following describes the implementation of the present invention through specific embodiments. People skilled in the art can easily understand other advantages and effects of the present invention from the contents disclosed in this specification.

[0015] It should be noted that the structures, proportions, sizes, etc. depicted in the drawings of this specification are only used to match the contents disclosed in the specification for people familiar with this technology to understand and read, and are not used to limit the conditions for the implementation of the present invention. Therefore, they have no substantial technical significance. Any modification of the structure, change in the proportional relationship, or adjustment of the size should still fall within the scope of the technical content disclosed by the present invention without affecting the efficacy and purpose of the present invention. At the same time, the terms such as "upper", "lower", "left", "right", "middle", etc. quoted in this specification are only for the convenience of description and are not used to limit the scope of the implementation of the present invention. Changes or adjustments in their relative relationships should also be regarded as the scope of the implementation of the present invention without substantially changing the technical content.

[0016] In the description of the present invention, it should be noted that, unless otherwise expressly specified and limited, the terms "connected" and "connected" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to the specific circumstances. It should be noted that the terms "include", "comprise" or any other variants are intended to cover non-exclusive inclusion, so that a process, method, article or device that includes a series of elements includes not only those elements, but also other elements that are not explicitly listed, or also includes elements that are inherent to such process, method, article or device.

[0017] like Figures 1-6 The device for liquid penetrant nondestructive testing of aircraft parts includes a housing 1, a support frame 2, a fixing base 3, a crane 4, a suspension cable 5, a hinge block 6, a motor 7, a rotating rod 8, a stirring device 9, a tilting device 10, and a lifting device 11. The support frame 2 is installed above the box 1; The lifting device is installed above the support frame 2, and the lifting device is connected to the jacking device 11; the lifting device includes a fixed seat 3, a crane 4 and a lifting cable 5; the fixed seat 3 is installed above the support frame 2; the crane 4 is installed above the fixed seat 3; one end of the lifting cable 5 is connected to the output end of the crane 4, and the other end is branched into a "Y" shape and connected to the two ends of the top of the jacking device 11; the connection between the lifting cable 5 and the jacking device 11 is hinged with a hinge block 6.

[0018] The motor 7 is installed on one side of the box 1; One end of the rotating rod 8 is connected to the output end of the motor 7, and the other end extends into the box body 1; The stirring device 9 is arranged in the box body 1 and is connected to one end of the rotating rod 8 in the box body 1; the stirring device 9 includes a sliding spring 901, a stirring blade 902, a limiting column 903, a rotating block 904 and a fixed block 905; a plurality of stirring blades 902 are set on the rotating rod 8 inside the box body 1; the stirring blades 902 can slide along the rotating rod 8; a rotating block 904 is fixed to the right side of the stirring blade 902; a fixed block 905 is provided on the inner wall of the right side of the box body 1; The rotating block 904 is provided with an inclined surface; the fixed block 905 is provided with an inclined surface matching the rotating block 904; the sliding spring 901 is sleeved in the rotating rod 8, and one end is fixed to the inner wall of the box body 1, and the other end is fixed on the left side of the stirring blade 902; the stirring blade 902 is cross-shaped; the stirring device 9 also includes a limiting column 903; a notch is provided on the stirring blade 902; the limiting column 903 is installed on the rotating rod 8 in the notch of the stirring blade 902.

[0019] The tilting device 10 is arranged on both sides of the stirring device 9; the tilting device 10 includes a limit rod 1001, a top plate 1002, a limit spring 1003, a top block 1004, a support column 1005 and a support block 1006; the top plate 1002 is symmetrically installed at the left and right ends of the stirring blade 902, and a hole is provided in the center to make way for the rotating rod 8; the limit rod 1001 passes through the box body 1 horizontally and is slidably installed on the box body 1; the right end of the limit rod 1001 is installed on the top plate 1002; the limit spring 1003 is installed on the limit rod 1001; a top block 1004 with a wedge surface is installed on the left side of the top plate 1002; the support column 1005 is vertically slidably installed in the groove on the inner wall of the box body 1; the upper end of the support column 1005 is installed with a support block 1006, and the lower end cooperates with the wedge surface of the top block 1004.

[0020] The lifting device 11 is arranged above the stirring device 9: the lifting device 11 includes a material plate 1101, a T-shaped rod 1102, an extrusion plate 1103 and a top column 1104; the material plate 1101 is provided with a mezzanine; the hinge block 6 is installed at both ends of the top of the material plate 1101; the T-shaped rod 1102 is vertically slidably installed on the material plate 1101; the lower end of the T-shaped rod 1102 is installed with an extrusion plate 1103, and when the stirring blade 902 rotates to the highest point, its blade end contacts the extrusion plate 1103; one end of the top column 1104 is symmetrically installed at the left and right ends of the extrusion plate 1103, and the other end is vertically slidably installed in the mezzanine of the material plate 1101.

[0021] Working principle: After the motor 7 is started, the motor 7 rotates with the rotating rod 8. Under the limiting action of the limiting column 903, the rotating rod 8 rotates with the stirring blade 902, and the stirring blade 902 rotates with the rotating block 904. When the rotating block 904 rotates and contacts the fixed block 905, the rotating block 904 is squeezed by the fixed block 905, causing the rotating block 904 to move to the left with the stirring blade 902, and the stirring blade 902 squeezes the sliding spring 901. When the rotating block 904 rotates away from the fixed block 905, the sliding spring 901, the stirring blade 902 and the rotating block 904 reset, the rotating rod 8 drives the stirring blade 902 to rotate, and the rotating block 904 periodically contacts the fixed block 905. The fixed block 905 pushes the stirring blade 902 to slide axially along the rotating rod 8, squeezing the sliding spring 901; the spring resets when it is out of contact, and when the stirring device 9 moves to the left, the stirring blade 902 squeezes the top plate 1002 in the left tilting device 10, causing the top plate 1002 to move to the left, and the top plate 1002 moves to the left with the top block 1004 moving to the left, and the top block 1004 moves to the left. The wedge-shaped surface of the top block 1004 squeezes the support column 1005, causing the support column 1005 to move upward, and the support column 1005 moves upward with the support block 1006 moving upward, and the support block 1006 moves upward to lift one side of the lifting device 11, so that the lifting device 11 tilts, and when the stirring blade 902 is reset, the top plate 1002, the top block 1004, the support column 1005 and the support block 1006 in the left tilting device 10 are reset, and the left side of the lifting device 11 is reset. The top plate 1002 and the top block 1004 in the right tilting device 10 move to the right, and the top block 1004 squeezes the support column 1005, so that the support column 1005 and the support block 1006 move upward, and the right side of the lifting device 11 is lifted. As the stirring blade 902 moves left and right, the lifting device 11 tilts left and right, allowing the material on the material plate 1101 to move left and right, and the holes on the material plate 1101 can contact the bottom of the material more. The bottom of the material can also be penetrated by the permeate, preventing the bottom of the material from being unable to penetrate due to the fit with the material plate 1101; when the end point of the rotating blade of the stirring blade 902 contacts the extrusion plate 1103, the extrusion plate 1103 is forced to move upward, and the upward displacement of the extrusion plate 1103 brings the top column 1104 upward to lift the material. When the stirring blade 902 moves away from the extrusion plate 1103, the extrusion plate 1103 brings the top column 1104 to reset. As the stirring blade 902 rotates, the extrusion plate 1103 brings the top column 1104 up and down, and the material is regularly lifted up and down by the top column 1104, so that the bottom of the material contacts the permeate more fully, and the permeate penetrates more evenly.

[0022] The protection scope of the present invention is not limited to the technical solutions disclosed in the specific implementation methods. Any modifications, equivalent replacements, improvements, etc. made to the above embodiments based on the technical essence of the present invention fall within the protection scope of the present invention.

Claims

1. A penetrant device for liquid penetrant nondestructive testing of aircraft parts, characterized by: The invention comprises a box body (1), a support frame (2), a lifting device, a motor (7), a tilting device (10) and a lifting device (11); the support frame (2) is installed above the box body (1); the lifting device is installed above the support frame (2), and the lifting device is connected to the lifting device (11); the motor (7) is installed on one side of the box body (1); one end of the rotating rod (8) is connected to the output end of the motor (7), and the other end extends into the box body (1); the stirring device (9) is arranged in the box body (1) and connected to one end of the rotating rod (8) in the box body (1); the tilting device (10) is arranged on both sides of the stirring device (9); and the lifting device (11) is arranged above the stirring device (9).

2. The liquid penetrant nondestructive testing device for aircraft parts according to claim 1, characterized in that: The lifting device comprises a fixed seat (3), a crane (4) and a lifting cable (5); the fixed seat (3) is installed above the support frame (2); the crane (4) is installed above the fixed seat (3); one end of the lifting cable (5) is connected to the output end of the crane (4), and the other end is branched into a "Y" shape and connected to the two ends of the top of the lifting device (11); the connection between the lifting cable (5) and the lifting device (11) is hinged with a hinge block (6).

3. The liquid penetrant nondestructive testing device for aircraft parts according to claim 2, characterized in that: The lifting device (11) comprises a material plate (1101), a T-shaped rod (1102), an extrusion plate (1103) and a top column (1104); the material plate (1101) is provided with a sandwich layer; the hinge block (6) is mounted on both ends of the top of the material plate (1101); the T-shaped rod (1102) is vertically slidably mounted on the material plate (1101); the extrusion plate (1103) is mounted on the lower end of the T-shaped rod (1102); one end of the top column (1104) is symmetrically mounted on the left and right ends of the extrusion plate (1103), and the other end is vertically slidably mounted in the sandwich layer of the material plate (1101).

4. The liquid penetrant nondestructive testing device for aircraft parts according to claim 1, characterized in that: The stirring device (9) comprises a sliding spring (901), a stirring blade (902), a limiting column (903), a rotating block (904) and a fixed block (905); a plurality of stirring blades (902) are mounted on a rotating rod (8) on the inner side of the housing (1); the stirring blades (902) can slide along the rotating rod (8); a rotating block (904) is fixed to the right side of the stirring blade (902); a fixed block (905) is provided on the inner wall of the right side of the housing (1); an inclined surface is provided on the rotating block (904); and an inclined surface matching the rotating block (904) is provided on the fixed block (905); the sliding spring (901) is mounted in the rotating rod (8), and one end is fixed to the inner wall of the housing (1), and the other end is fixed to the left side of the stirring blade (902).

5. The liquid penetrant nondestructive testing device for aircraft parts according to claim 4, characterized in that: The stirring blade (902) is cross-shaped.

6. The liquid penetrant nondestructive testing device for aircraft parts according to claim 4, characterized in that: The stirring blade (902) is provided with a notch; the limiting column (903) is installed on the rotating rod (8) in the notch of the stirring blade (902).

7. The liquid penetrant nondestructive testing device for aircraft parts according to claim 1, characterized in that: The tilting device (10) comprises a limiting rod (1001), a top plate (1002), a limiting spring (1003), a top block (1004), a support column (1005) and a support block (1006); the top plate (1002) is symmetrically mounted on the left and right ends of the stirring blade (902), and a hole is provided in the center to make way for the rotating rod (8); the limiting rod (1001) passes through the box body (1) horizontally and is slidably mounted on the box body (1); The right end of the limiting rod (1001) is mounted on the top plate (1002); a limiting spring (1003) is sleeved on the limiting rod (1001); a top block (1004) with a wedge-shaped surface is mounted on the left side of the top plate (1002); the support column (1005) is vertically slidably mounted on the inner wall notch of the box body (1); a support block (1006) is mounted on the upper end of the support column (1005), and the lower end cooperates with the wedge-shaped surface of the top block (1004).