A testing method for aviation parts based on intelligent sensing system

Abstract

The present invention relates to the technical field of quality testing, and discloses an aviation component testing method based on an intelligent sensing system, comprising: obtaining the lower contour and width of the aviation component to produce a mold that can fit the lower contour of the aviation component, placing the mold and pressing the aviation component multiple times, using a circular light source to illuminate the gap between the mold and the aviation component each time, adjusting multiple illumination angles and obtaining the illumination image formed on the light source baffle, and filtering out the target image position to calculate the maximum value of the gap between the mold and the aviation component, thereby avoiding the problem of no target image on the light source baffle due to the illumination angle problem.

Description

Technical Field

[0001] The invention relates to the technical field of quality testing, and in particular to an aviation component testing method based on an intelligent sensor system. Background Art

[0002] Quality inspection of aviation parts is crucial to ensuring the safety and quality of aviation operations. With the continuous advancement of science and technology, the quality requirements for aviation parts are becoming higher and higher, and the quality inspection technology in production is also constantly innovating and optimizing to ensure the reliability and practicality of parts.

[0003] At present, the mainstream quality monitoring technologies on the market are mainly divided into manual and high-precision instruments. Manual and high-precision instruments are used to detect whether the overall shape of aviation parts meets the standards of standard aviation parts. However, such quality inspection methods are too single and can only mechanically give qualified or unqualified results. Detailed reasons for failure cannot be given, and thus, aviation parts cannot be repaired again, resulting in a waste of resources. At the same time, manual inspection relies on experience and has detection errors. High-precision instrument testing costs are too high and are not universal.

[0004] In summary, there is an urgent need for a testing method for aviation parts to solve the above problems. Summary of the invention

[0005] The present invention provides an aviation component testing method based on an intelligent sensing system, which is used to promote the solution of the problems mentioned in the above background technology.

[0006] The present invention provides the following technical solution: an aviation component testing method based on an intelligent sensing system,

[0007] Optionally, a method for testing aviation components based on an intelligent sensing system, comprising:

[0008] S1 obtains the lower profile and thickness of a standard aviation component, and manufactures a mold that can fit the profile of the standard aviation component according to the lower profile and thickness;

[0009] S2 places the mold and fits the lower contour of the aviation component to form a cutting gap between the mold and the aviation component, and selects two ends of the cutting gap as the first pressure test point and the second pressure test point;

[0010] S3 performs the first pressure test, and uses the first pressure test point as the starting point, uses a circular light source to perform a lighting test along the interception gap, and sets a light source baffle in the direction perpendicular to the light source. If a target image is formed on the light source baffle, adjust the light source angle;

[0011] S4 performs a second pressure test, and uses the second pressure test point as the starting point, uses a circular light source to perform a lighting test along the interception gap, and sets a light source baffle vertically in the direction of the light source. If a target image is formed on the light source baffle, adjust the light source angle.

[0012] Optionally, the first pressure test is performed, and the first pressure test point is used as the starting point, a circular light source is used to perform a lighting test along the interception gap, a light source baffle is set in a direction perpendicular to the light source, and if a target image is formed on the light source baffle, the light source angle is adjusted, specifically including:

[0013] Respectively obtain the positions of the mold placed corresponding to the first pressure test point and the second pressure test point, and record them as the first position plane and the second position plane respectively;

[0014] Applying pressure to the aviation component along a direction perpendicular to the first position plane through a first pressure test point;

[0015] Connecting the first pressure test point and the second pressure test point to form a pressure test line segment;

[0016] On one side of the mold, a circular light source is arranged at a horizontal distance i from the first pressure test point, and on the other side of the mold, a light source baffle is arranged at a horizontal distance 3i from the mold. When the circular light source is illuminated without obstacles, the illumination image formed on the light source baffle is circular. The circular light source is adjusted to be horizontal and aligned with the pressure test section so that the light source illuminates from the first pressure test point to the second pressure test point along the interception gap;

[0017] Adjust the circular light source to be horizontal and the angle between it and the pressure test section to 120 degrees. The angle between the circular light source and the pressure test section is recorded as the initial angle. Adjust the initial angle to the right along the horizontal direction in 10 degrees. When the cumulative adjustment angle is 120 degrees, end the angle adjustment.

[0018] Move the circular light source and the light source baffle from the first pressure test point to the second pressure test point along the interception gap, and obtain all light images on the light source baffle in real time through the light sensor;

[0019] Set the light image distance threshold P;

[0020] Take the circular light source as the starting point and draw a ray along the illumination direction of the circular light source. The ray intersects with the light source baffle at point c.

[0021] The illumination sensor acquires all illumination images, and the illumination image closest to point c is selected as the pre-selected target image. If the distance between the pre-selected target image and point c is greater than P, the pre-selected target image is marked as a non-target image.

[0022] If the distance between the pre-selected target image and point c is less than or equal to P, the pre-selected target image is marked as the target image, the current target image position is marked by the light measuring instrument, and the first target position set is recorded, and the lighting angle is adjusted;

[0023] Mark the current position of the circular light source, adjust the lighting angle of the circular light source, and calculate the size of the intersection area between the circular lighting direction and the interception gap through the position change of the target image on the light source baffle.

[0024] Optionally, the circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0025] Keep the initial angle of the current circular light source and adjust the vertical lighting angle;

[0026] Take the current circular light source's illumination direction as the horizontal line, keep the circular light source position unchanged, adjust the illumination angle upwards along the vertical direction until the angle between the circular light source's illumination direction and the horizontal line is 15 degrees for illumination testing, and adjust the illumination angle vertically downwards along the illumination direction with an adjustment range of 1 degree;

[0027] Determine whether all illumination images of the light source baffle are target images;

[0028] If it is a non-target image, adjust the lighting angle;

[0029] If it is a target image, the current target image position is marked by a light meter, and the second target position set is recorded to adjust the lighting angle;

[0030] If the cumulative adjustment of the illumination angle of the circular light source is 30 degrees, the vertical illumination angle adjustment is stopped.

[0031] Optionally, the circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0032] Calculate the distance between any two elements in the first target position set, and select the largest distance value as the first adjustment theoretical value;

[0033] Calculate the distance between any two elements in the second target position set, and select the largest distance value as the second adjustment theoretical value;

[0034] If the first adjustment theoretical value is greater than or equal to the second adjustment theoretical value, the first adjustment theoretical value is used as the final adjustment theoretical value;

[0035] If the first adjustment theoretical value is less than the second adjustment theoretical value, the second adjustment theoretical value is used as the final adjustment theoretical value;

[0036] Set the gap pass threshold;

[0037] If the final adjusted theoretical value is greater than the gap qualified threshold, the tested aviation component fails;

[0038] If the final adjusted theoretical value is less than or equal to the qualified gap threshold, the aviation component under test is qualified.

[0039] Optionally, the second pressure test is performed, and the second pressure test point is used as the starting point, a circular light source is used to perform a lighting test along the interception gap, and a light source baffle is vertically arranged in the direction of the light source. If a target image is formed on the light source baffle, the light source angle is adjusted, which specifically includes:

[0040] Respectively obtain the positions of the mold placed corresponding to the first pressure test point and the second pressure test point, and record them as the first position plane and the second position plane respectively;

[0041] Applying pressure to the aviation component along a direction perpendicular to the second position plane through the second pressure test point;

[0042] Connecting the first pressure test point and the second pressure test point to form a pressure test line segment;

[0043] On one side of the mold, a circular light source is arranged at a horizontal distance i from the first pressure test point, and on the other side of the mold, a light source baffle is arranged at a horizontal distance 3i from the mold. When the circular light source is illuminated without obstacles, the illumination image formed on the light source baffle is circular. The circular light source is adjusted to be horizontal and aligned with the pressure test section so that the light source illuminates from the second pressure test point to the first pressure test point along the interception gap;

[0044] Adjust the circular light source to be horizontal and the angle between it and the pressure test section to 120 degrees. The angle between the circular light source and the pressure test section is recorded as the initial angle. Adjust the initial angle to the right along the horizontal direction in 10 degrees. When the cumulative adjustment angle is 120 degrees, end the angle adjustment.

[0045] Move the circular light source and the light source baffle from the second pressure test point to the first pressure test point along the interception gap, and obtain all light images on the light source baffle in real time through the light sensor;

[0046] Set the light image distance threshold P;

[0047] Take the circular light source as the starting point and draw a ray along the illumination direction of the circular light source. The ray intersects with the light source baffle at point c.

[0048] The illumination sensor acquires all illumination images, and the illumination image closest to point c is selected as the pre-selected target image. If the distance between the pre-selected target image and point c is greater than P, the pre-selected target image is marked as a non-target image.

[0049] If the distance between the pre-selected target image and point c is less than or equal to P, the pre-selected target image is marked as the target image, the current target image position is marked by the light measuring instrument, and the first target position set is recorded, and the lighting angle is adjusted;

[0050] Mark the current position of the circular light source, adjust the lighting angle of the circular light source, and calculate the size of the intersection area between the circular lighting direction and the interception gap through the position change of the target image on the light source baffle.

[0051] Optionally, the circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0052] Keep the initial angle of the current circular light source and adjust the vertical lighting angle;

[0053] Take the current circular light source's illumination direction as the horizontal line, keep the circular light source position unchanged, adjust the illumination angle upwards along the vertical direction until the angle between the circular light source's illumination direction and the horizontal line is 15 degrees for illumination testing, and adjust the illumination angle vertically downwards along the illumination direction with an adjustment range of 1 degree;

[0054] Determine whether all illumination images of the light source baffle are target images;

[0055] If it is a non-target image, adjust the lighting angle;

[0056] If it is a target image, the current target image position is marked by a light meter, and the second target position set is recorded to adjust the lighting angle;

[0057] If the cumulative adjustment of the illumination angle of the circular light source is 30 degrees, the vertical illumination angle adjustment is stopped.

[0058] Optionally, the circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0059] Calculate the distance between any two elements in the first target position set, and select the largest distance value as the first adjustment theoretical value;

[0060] Calculate the distance between any two elements in the second target position set, and select the largest distance value as the second adjustment theoretical value;

[0061] If the first adjustment theoretical value is greater than or equal to the second adjustment theoretical value, the first adjustment theoretical value is used as the final adjustment theoretical value;

[0062] If the first adjustment theoretical value is less than the second adjustment theoretical value, the second adjustment theoretical value is used as the final adjustment theoretical value;

[0063] Set the gap pass threshold;

[0064] If the final adjusted theoretical value is greater than the gap qualified threshold, the tested aviation component fails;

[0065] If the final adjusted theoretical value is less than or equal to the qualified gap threshold, the aviation component under test is qualified.

[0066] Optionally, the intelligent sensing system consists of a light sensor and a light measuring instrument.

[0067] The present invention has the following beneficial effects:

[0068] 1. This is an aviation component testing method based on an intelligent sensing system. The method places a mold and an aviation component for fitting, respectively sets a circular light source and a light source baffle on both sides of the mold, selects a pressure point, applies pressure to the aviation component, sets the illumination angle of the circular light source according to the gap position between the mold and the aviation component, and moves the circular light source along the gap track to perform illumination testing on the entire gap. This can reduce manual operations, reduce the rate of manual mismeasurement, and improve test efficiency.

[0069] 2. The invention discloses an aviation component testing method based on an intelligent sensing system. The method adjusts the horizontal angle of the circular light source illumination direction. Each time the horizontal angle is adjusted, all illumination images on the light source baffle are obtained through the illumination sensor. A ray is made along the illumination direction with the light source position as the starting point. The intersection of the ray and the light source baffle is used as the base point. The distance between all illumination images and the base point is determined according to the illumination meter. All distances are compared with the light image distance threshold. The image with the smallest distance less than the light image distance threshold is selected as the target image. The position of the target image is recorded and entered into a set. After each horizontal angle adjustment, the current horizontal angle is kept unchanged. The illumination angle is adjusted along the vertical direction. The target image is selected. The position of the target image is recorded and entered into a set. The maximum value of the horizontal position set and the maximum value of the vertical position set are calculated. The maximum value is compared with the qualified gap threshold to determine the maximum gap direction. The gap is illuminated at multiple angles to improve the comprehensiveness of the test, avoid the problem of not forming a target image due to angle problems, and further reduce the false detection rate.

[0070] 3. This aviation parts testing method based on an intelligent sensing system can accurately measure the size of the gap through a large amount of target position data, providing a basis for subsequent maintenance. This not only improves the accuracy of the data, but also reduces the detection cost and detection randomness, avoiding waste of resources.

[0071] 4. This is an aviation component testing method based on an intelligent sensing system. The testing method can be adjusted according to different test points and position planes, is applicable to aviation components of different shapes and sizes, and is universal.

[0072] 5. This is an aviation component testing method based on an intelligent sensing system. The standardized testing process and automated equipment settings ensure the repeatability of each test and help obtain reliable test results. BRIEF DESCRIPTION OF THE DRAWINGS

[0073] Figure 1 It is a schematic diagram of the structure of the present invention;

[0074] Figure 2 This is a diagram of adjusting the angle of a circular light source in the horizontal direction;

[0075] Figure 3 This is a diagram of adjusting the angle of a circular light source in the vertical direction. DETAILED DESCRIPTION

[0076] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0077] Example 1, see Figures 1 to 3 , an aviation component testing method based on an intelligent sensing system, comprising:

[0078] S1 obtains the lower profile and thickness of a standard aviation component, and manufactures a mold that can fit the profile of the standard aviation component according to the lower profile and thickness;

[0079] S2 places the mold and fits the lower contour of the aviation component to form a cutting gap between the mold and the aviation component, and selects two ends of the cutting gap as the first pressure test point and the second pressure test point;

[0080] This test method can be adjusted according to different test points and position planes, and is applicable to aviation parts of different shapes and sizes, and is universal.

[0081] S3 performs the first pressure test, and uses the first pressure test point as the starting point, uses a circular light source to perform a lighting test along the interception gap, and sets a light source baffle in the direction perpendicular to the light source. If a target image is formed on the light source baffle, adjust the light source angle;

[0082] S4 performs a second pressure test, and uses the second pressure test point as the starting point, uses a circular light source to perform a lighting test along the interception gap, and sets a light source baffle vertically in the direction of the light source. If a target image is formed on the light source baffle, adjust the light source angle.

[0083] See also Figure 2 The first pressure test is performed, and the first pressure test point is used as the starting point, a circular light source is used to perform a lighting test along the interception gap, and a light source baffle is set in the direction perpendicular to the light source. If a target image is formed on the light source baffle, the light source angle is adjusted, which specifically includes:

[0084] Respectively obtain the positions of the mold placed corresponding to the first pressure test point and the second pressure test point, and record them as the first position plane and the second position plane respectively;

[0085] Applying pressure to the aviation component along a direction perpendicular to the first position plane through a first pressure test point;

[0086] Connecting the first pressure test point and the second pressure test point to form a pressure test line segment;

[0087] On one side of the mold, a circular light source is arranged at a horizontal distance i from the first pressure test point, and on the other side of the mold, a light source baffle is arranged at a horizontal distance 3i from the mold. When the circular light source is illuminated without obstacles, the illumination image formed on the light source baffle is circular. The circular light source is adjusted to be horizontal and aligned with the pressure test section so that the light source illuminates from the first pressure test point to the second pressure test point along the interception gap;

[0088] iIt can be adjusted according to the size of aviation parts and actual conditions;

[0089] By placing the mold and the aviation parts for bonding, circular light sources and light source baffles are set on both sides of the mold, and the pressure points are selected to apply pressure to the aviation parts. According to the position of the gap between the mold and the aviation parts, the lighting angle of the circular light source is set, and the circular light source is moved along the gap track to perform lighting test on the entire gap. This can reduce manual operations, reduce the rate of manual misdetection, and improve test efficiency.

[0090] Adjust the circular light source to be horizontal and the angle between it and the pressure test section to 120 degrees. The angle between the circular light source and the pressure test section is recorded as the initial angle. Adjust the initial angle to the right along the horizontal direction in 10 degrees. When the cumulative adjustment angle is 120 degrees, end the angle adjustment.

[0091] Move the circular light source and the light source baffle from the first pressure test point to the second pressure test point along the interception gap, and obtain all light images on the light source baffle in real time through the light sensor;

[0092] Set the light image distance threshold P;

[0093] The light image distance threshold P is used for subsequent determination of the target image;

[0094] Take the circular light source as the starting point and draw a ray along the illumination direction of the circular light source. The ray intersects with the light source baffle at point c.

[0095] The illumination sensor acquires all illumination images, and the illumination image closest to point c is selected as the pre-selected target image. If the distance between the pre-selected target image and point c is greater than P, the pre-selected target image is marked as a non-target image.

[0096] If the distance between the pre-selected target image and point c is less than or equal to P, the pre-selected target image is marked as the target image, the current target image position is marked by the light measuring instrument, and the first target position set is recorded, and the lighting angle is adjusted;

[0097] Mark the current position of the circular light source, adjust the lighting angle of the circular light source, and calculate the size of the intersection area between the circular lighting direction and the interception gap through the position change of the target image on the light source baffle.

[0098] See also Figure 3 , the circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0099] Keep the initial angle of the current circular light source and adjust the vertical lighting angle;

[0100] Take the current circular light source's illumination direction as the horizontal line, keep the circular light source position unchanged, adjust the illumination angle upwards along the vertical direction until the angle between the circular light source's illumination direction and the horizontal line is 15 degrees for illumination testing, and adjust the illumination angle vertically downwards along the illumination direction with an adjustment range of 1 degree;

[0101] Determine whether all illumination images of the light source baffle are target images;

[0102] If it is a non-target image, adjust the lighting angle;

[0103] If it is a target image, the current target image position is marked by a light meter, and the second target position set is recorded to adjust the lighting angle;

[0104] Through a large amount of target position data, the size of the gap can be accurately measured to provide a basis for subsequent maintenance. This not only improves the accuracy of the data, but also reduces the detection cost and detection randomness, avoiding waste of resources.

[0105] If the cumulative adjustment of the illumination angle of the circular light source is 30 degrees, the vertical illumination angle adjustment is stopped.

[0106] The circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0107] Calculate the distance between any two elements in the first target position set, and select the largest distance value as the first adjustment theoretical value;

[0108] Calculate the distance between any two elements in the second target position set, and select the largest distance value as the second adjustment theoretical value;

[0109] If the first adjustment theoretical value is greater than or equal to the second adjustment theoretical value, the first adjustment theoretical value is used as the final adjustment theoretical value;

[0110] If the first adjustment theoretical value is less than the second adjustment theoretical value, the second adjustment theoretical value is used as the final adjustment theoretical value;

[0111] Set the gap pass threshold;

[0112] The gap qualified threshold is used to subsequently determine whether the gap size of the current illumination test point is qualified;

[0113] If the final adjusted theoretical value is greater than the gap qualified threshold, the tested aviation component fails;

[0114] If the final adjusted theoretical value is less than or equal to the qualified gap threshold, the aviation component under test is qualified.

[0115] By adjusting the horizontal angle of the circular light source, each time the horizontal angle is adjusted, all the light images on the light source baffle are obtained through the light sensor, and rays are made along the light direction with the light source position as the starting point, and the intersection of the rays and the light source baffle is used as the base point. The distance between all the light images and the base point is judged according to the light meter, and by comparing all distances with the light image distance threshold, the one that is less than the light image distance threshold and has the smallest distance is selected as the target image, and the target image position is recorded and entered into the set. After each horizontal angle adjustment, the current horizontal angle is kept unchanged, and the illumination angle is adjusted along the vertical direction to filter out the target image, and the target image position is recorded and entered into the set. By calculating the maximum value of the horizontal position set and the maximum value of the vertical position set, the maximum value is compared with the qualified gap threshold to determine the maximum gap direction, and the gap is tested for illumination at multiple angles to improve the comprehensiveness of the test, avoid the problem of not forming the target image due to angle problems, and further reduce the false detection rate.

[0116] The second pressure test is performed, and the second pressure test point is used as the starting point, a circular light source is used to perform a lighting test along the interception gap, and a light source baffle is vertically set in the direction of the light source. If a target image is formed on the light source baffle, the light source angle is adjusted, specifically including:

[0117] Respectively obtain the positions of the mold placed corresponding to the first pressure test point and the second pressure test point, and record them as the first position plane and the second position plane respectively;

[0118] Applying pressure to the aviation component along a direction perpendicular to the second position plane through the second pressure test point;

[0119] Connecting the first pressure test point and the second pressure test point to form a pressure test line segment;

[0120] On one side of the mold, a circular light source is arranged at a horizontal distance i from the first pressure test point, and on the other side of the mold, a light source baffle is arranged at a horizontal distance 3i from the mold. When the circular light source is illuminated without obstacles, the illumination image formed on the light source baffle is circular. The circular light source is adjusted to be horizontal and aligned with the pressure test section so that the light source illuminates from the second pressure test point to the first pressure test point along the interception gap;

[0121] Adjust the circular light source to be horizontal and the angle between it and the pressure test section to 120 degrees. The angle between the circular light source and the pressure test section is recorded as the initial angle. Adjust the initial angle to the right along the horizontal direction in 10 degrees. When the cumulative adjustment angle is 120 degrees, end the angle adjustment.

[0122] Move the circular light source and the light source baffle from the second pressure test point to the first pressure test point along the interception gap, and obtain all light images on the light source baffle in real time through the light sensor;

[0123] Set the light image distance threshold P;

[0124] Take the circular light source as the starting point and draw a ray along the illumination direction of the circular light source. The ray intersects with the light source baffle at point c.

[0125] The illumination sensor acquires all illumination images, and the illumination image closest to point c is selected as the pre-selected target image. If the distance between the pre-selected target image and point c is greater than P, the pre-selected target image is marked as a non-target image.

[0126] If the distance between the pre-selected target image and point c is less than or equal to P, the pre-selected target image is marked as the target image, the current target image position is marked by the light measuring instrument, and the first target position set is recorded, and the lighting angle is adjusted;

[0127] Mark the current position of the circular light source, adjust the lighting angle of the circular light source, and calculate the size of the intersection area between the circular lighting direction and the interception gap through the position change of the target image on the light source baffle.

[0128] The circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0129] Keep the initial angle of the current circular light source and adjust the vertical lighting angle;

[0130] Take the current circular light source's illumination direction as the horizontal line, keep the circular light source position unchanged, adjust the illumination angle upwards along the vertical direction until the angle between the circular light source's illumination direction and the horizontal line is 15 degrees for illumination testing, and adjust the illumination angle vertically downwards along the illumination direction with an adjustment range of 1 degree;

[0131] Determine whether all illumination images of the light source baffle are target images;

[0132] If it is a non-target image, adjust the lighting angle;

[0133] If it is a target image, the current target image position is marked by a light meter, and the second target position set is recorded to adjust the lighting angle;

[0134] If the cumulative adjustment of the illumination angle of the circular light source is 30 degrees, the vertical illumination angle adjustment is stopped.

[0135] The circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle:

[0136] Calculate the distance between any two elements in the first target position set, and select the largest distance value as the first adjustment theoretical value;

[0137] Calculate the distance between any two elements in the second target position set, and select the largest distance value as the second adjustment theoretical value;

[0138] If the first adjustment theoretical value is greater than or equal to the second adjustment theoretical value, the first adjustment theoretical value is used as the final adjustment theoretical value;

[0139] If the first adjustment theoretical value is less than the second adjustment theoretical value, the second adjustment theoretical value is used as the final adjustment theoretical value;

[0140] Set the gap pass threshold;

[0141] If the final adjusted theoretical value is greater than the gap qualified threshold, the tested aviation component fails;

[0142] If the final adjusted theoretical value is less than or equal to the qualified gap threshold, the aviation component under test is qualified.

[0143] The intelligent sensing system consists of a light sensor and a light measuring instrument.

[0144] Standardized test procedures and automated equipment setup ensure repeatability of each test, helping to obtain reliable test results.

[0145] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0146] The above is only a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the technical principles of the present invention. These improvements and modifications should also be regarded as the scope of protection of the present invention.

Claims

1. An aviation component testing method based on an intelligent sensing system, characterized in that: include, S1 obtains the lower profile and thickness of a standard aviation component, and manufactures a mold that can fit the profile of the standard aviation component according to the lower profile and thickness; S2 places the mold and fits the lower contour of the aviation component to form a cutting gap between the mold and the aviation component, and selects two ends of the cutting gap as the first pressure test point and the second pressure test point; S3 performs the first pressure test, and uses the first pressure test point as the starting point, uses a circular light source to perform a lighting test along the interception gap, and sets a light source baffle in the direction perpendicular to the light source. If a target image is formed on the light source baffle, the light source angle is adjusted, which specifically includes the following steps: Respectively obtain the positions of the mold placed corresponding to the first pressure test point and the second pressure test point, and record them as the first position plane and the second position plane respectively; Applying pressure to the aviation component along a direction perpendicular to the first position plane through a first pressure test point; Connecting the first pressure test point and the second pressure test point to form a pressure test line segment; On one side of the mold, a circular light source is arranged at a horizontal distance i from the first pressure test point, and on the other side of the mold, a light source baffle is arranged at a horizontal distance 3i from the mold. When the circular light source is illuminated without obstacles, the illumination image formed on the light source baffle is circular. The circular light source is adjusted to be level with the pressure test section so that the light source illuminates from the first pressure test point to the second pressure test point along the interception gap; Adjust the circular light source to be level with the pressure test section and adjust the angle between the circular light source and the pressure test section to 120 degrees. The circular light source and the pressure test section are level with each other and the angle between the circular light source and the pressure test section is recorded as the initial angle. Adjust the initial angle to the right along the horizontal direction in 10 degrees. When the cumulative adjustment angle is 120 degrees, end the angle adjustment. Move the circular light source and the light source baffle from the first pressure test point to the second pressure test point along the interception gap, and obtain all light images on the light source baffle in real time through the light sensor; The first pressure test is performed, and the first pressure test point is used as the starting point, a circular light source is used to perform a lighting test along the interception gap, a light source baffle is set in the direction perpendicular to the light source, and if a target image is formed on the light source baffle, the light source angle is adjusted, and the following further includes: Set the light image distance threshold P; Take the circular light source as the starting point and draw a ray along the illumination direction of the circular light source. The ray intersects with the light source baffle at point c. The illumination sensor acquires all illumination images, and the illumination image closest to point c is selected as the pre-selected target image. If the distance between the pre-selected target image and point c is greater than P, the pre-selected target image is marked as a non-target image. If the distance between the pre-selected target image and point c is less than or equal to P, the pre-selected target image is marked as the target image, the current target image position is marked by the light measuring instrument, and the first target position set is recorded, and the lighting angle is adjusted; Mark the current position of the circular light source, adjust the illumination angle of the circular light source in the vertical direction, and calculate the size of the intersection area between the circular illumination direction and the interception gap through the position change of the target image on the light source baffle; S4 performs a second pressure test, and uses the second pressure test point as the starting point, uses a circular light source to perform a lighting test along the interception gap, and sets a light source baffle vertically in the direction of the light source. If a target image is formed on the light source baffle, adjust the light source angle.

2. The aviation component testing method based on the intelligent sensor system according to claim 1 is characterized in that: The illumination angle of the circular light source is adjusted in the vertical direction, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle: Maintain the initial angle of the current circular light source; Take the current circular light source's illumination direction as the horizontal line, keep the circular light source position unchanged, adjust the illumination angle upwards along the vertical direction until the angle between the circular light source's illumination direction and the horizontal line is 15 degrees for illumination testing, and adjust the illumination angle vertically downwards along the illumination direction with an adjustment range of 1 degree; Determine whether all illumination images of the light source baffle are target images; If it is a non-target image, adjust the lighting angle; If it is a target image, the current target image position is marked by a light meter, and the second target position set is recorded to adjust the lighting angle; If the cumulative adjustment of the illumination angle of the circular light source reaches 30 degrees, the vertical illumination angle adjustment is stopped.

3. The aviation component testing method based on the intelligent sensor system according to claim 2 is characterized in that: The circular light source illumination angle is adjusted, and the size of the intersection area between the circular illumination direction and the interception gap is calculated by the position change of the target image on the light source baffle: Calculate the distance between any two elements in the first target position set, and select the largest distance value as the first adjustment theoretical value; Calculate the distance between any two elements in the second target position set, and select the largest distance value as the second adjustment theoretical value; If the first adjustment theoretical value is greater than or equal to the second adjustment theoretical value, the first adjustment theoretical value is used as the final adjustment theoretical value; If the first adjustment theoretical value is less than the second adjustment theoretical value, the second adjustment theoretical value is used as the final adjustment theoretical value; Set the gap pass threshold; If the final adjusted theoretical value is greater than the gap qualified threshold, the tested aviation component fails; If the final adjusted theoretical value is less than or equal to the qualified gap threshold, the aviation component under test is qualified.

4. The aviation component testing method based on the intelligent sensor system according to claim 1 is characterized in that: The second pressure test is performed, and the second pressure test point is used as the starting point, a circular light source is used to perform a lighting test along the interception gap, and a light source baffle is vertically set in the direction of the light source. If a target image is formed on the light source baffle, the light source angle is adjusted, specifically including: Respectively obtain the positions of the mold placed corresponding to the first pressure test point and the second pressure test point, and record them as the first position plane and the second position plane respectively; Applying pressure to the aviation component along a direction perpendicular to the second position plane through the second pressure test point; Connecting the first pressure test point and the second pressure test point to form a pressure test line segment; On one side of the mold, a circular light source is arranged at a horizontal distance i from the second pressure test point, and on the other side of the mold, a light source baffle is arranged at a horizontal distance 3i from the mold. When the circular light source is illuminated without obstacles, the illumination image formed on the light source baffle is circular. The circular light source is adjusted to be level with the pressure test section so that the light source illuminates from the second pressure test point to the first pressure test point along the interception gap; Adjust the circular light source to be level with the pressure test section and adjust the angle between the circular light source and the pressure test section to 120 degrees. Adjust the circular light source to be level with the pressure test section and record the angle between the circular light source and the pressure test section as the initial angle. Adjust the initial angle to the right along the horizontal direction by 10 degrees. When the cumulative adjustment angle is 120 degrees, end the angle adjustment. Move the circular light source and the light source baffle from the second pressure test point to the first pressure test point along the interception gap, and obtain all light images on the light source baffle in real time through the light sensor; Set the light image distance threshold P; Take the circular light source as the starting point and draw a ray along the illumination direction of the circular light source. The ray intersects with the light source baffle at point c. The illumination sensor acquires all illumination images, and the illumination image closest to point c is selected as the pre-selected target image. If the distance between the pre-selected target image and point c is greater than P, the pre-selected target image is marked as a non-target image. If the distance between the pre-selected target image and point c is less than or equal to P, the pre-selected target image is marked as the target image, the current target image position is marked by the light measuring instrument, and the first target position set is recorded, and the lighting angle is adjusted; Mark the current position of the circular light source, adjust the vertical angle of the circular light source, and calculate the size of the intersection area between the circular lighting direction and the interception gap through the position change of the target image on the light source baffle.

5. The aviation component testing method based on the intelligent sensor system according to claim 1 is characterized in that: The intelligent sensing system consists of a light sensor and a light measuring instrument.

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