Device for detecting position defects of aircraft assembly parts

Abstract

The invention relates to the technical field of assembly position detection of aviation product component assembly, in particular to a device for detecting position defects of aircraft assembly components, which can be used for quickly detecting the accuracy of the assembly positions of the components and avoiding the influence of human factors.

Description

Technical Field

[0001] This invention relates to the field of assembly position detection technology for aerospace product components, specifically to a detection device for positional defects in aircraft assembly components. This method and device can quickly detect the accuracy of component assembly positions, avoiding the influence of human factors. Background Technology

[0002] With the development of aviation technology, the positional accuracy requirements for the assembly of aviation product components are becoming increasingly stringent. However, during actual assembly, due to the inherent tolerances of the parts, positioning deviations, and manufacturing deviations of the tooling fixtures, the assembled components may deviate from their theoretical positions, affecting the aircraft's strength, shape, and overall performance. Therefore, the detection of the correct assembly position of components in aviation products is becoming increasingly important. Currently, in actual production, the detection of component positions mainly relies on tooling locators and shape clamps. The correctness of the installation position is determined by measuring the relative relationship between the product and the locator / clamp. This process is cumbersome, labor-intensive, and heavily dependent on the experience of process designers, workers, and inspectors. Factors such as the accuracy of the tooling locators and clamps, the selection of measurement points, changes in workers and inspectors, and deformation of the locators and clamps due to long-term use are unavoidable. These factors lead to incomplete detection, insufficient reliability, and low accuracy. Therefore, to facilitate operators and inspectors in quickly detecting the assembly position of components while ensuring accurate and reliable results, a digital and intelligent method and device for detecting component assembly positions is urgently needed. Summary of the Invention

[0003] The present invention provides a detection device for detecting the relative position of aircraft components after assembly, for detecting defects in the assembly position of aircraft components, so as to solve the problems in the above-mentioned technical background.

[0004] The technical problem solved by this invention is achieved by the following technical solution:

[0005] This invention designs a device for detecting positional defects in aircraft assembly components. Using this device, operators and inspectors can be replaced to detect relative positional defects in aircraft components after assembly. By using deep learning technology to replace traditional manual inspection, the influence of human factors can be avoided and efficiency can be improved.

[0006] This invention employs a deep learning data acquisition module to collect and record the position information of the assembly to be inspected, and automatically transmits this information to a position calculation module. The position calculation module analyzes and processes the data, then feeds the results back to a microcontroller module. The microcontroller module processes the data and sends commands to a controller. The microcontroller and controller then display the inspection results on a screen for intuitive visualization (e.g., green for a successful inspection, red for a failed inspection). This allows the operator to quickly obtain the results. Simultaneously, if an inspection fails, an automatic buzzer and alarm light provide corresponding indications (the buzzer sounds and the alarm light flashes) for multi-directional alerts.

[0007] According to one aspect of this application, a detection device for positional defects in aircraft assembly components is provided, comprising a mechanical structure, an electric control section, and a data acquisition and processing section;

[0008] The mechanical structure consists of a threaded rod 1, an operating rod 2, a movable clamping block 3, a support component 4, a connecting screw 10, an upper cover 11, a display screen 12, bolts 15, hexagonal nuts 16, washers 17, a connecting body 19, a foot support rod 20, a threaded connector 21, a support body 29, a system box 35, and a red-green light starter 38.

[0009] The electric control unit consists of a red signal light 5, a double-headed stud 6, a green signal light 7, an electric telescopic rod 13, an electric telescopic device 14, a distance sensor 18, a telescopic device 22, and a blue signal light 36.

[0010] The data acquisition and processing section consists of a sound alarm 8, a light alarm 9, a switch button 23, an HTTP interface 24, an HDMI interface 25, a camera connector 26, an adaptive flexible connector 27, a camera 28, a data acquisition unit 30, an edge processing unit 31, a data processing unit 32, a data control unit 33, a power module 34, and a detection button 37.

[0011] The threaded rod 1, operating rod 2, movable clamping block 3, support member 4 and red and green light starter 38 constitute a positioning and locking component;

[0012] The threaded rod 1 is a transmission component of the positioning and locking part. The bottom of the threaded rod 1 is in the form of a ball joint, which facilitates connection with the movable clamping block 3. The threaded rod 1 can be screwed in and out by the interaction of the external thread and the internal thread of the support component 4.

[0013] The operating lever 2 is the actuating component of the positioning and locking part. The operating lever 2 can be turned by hand force, and the threaded rod 1 is driven by the operating lever 2 to realize the screwing in and out of the support component 4.

[0014] The movable clamping block 3 is a functional component of the positioning and locking part. Its structure adopts a ball joint. The bottom of the threaded rod 1 is placed inside the movable clamping block 3, which can realize multi-directional rotation. It is used to adjust the positioning and locking part to work in different positions and structures. It can be realized by rotating the operating rod 2 by hand to drive the threaded rod 1 to rotate in and out, thereby driving the movable clamping block 3 to press.

[0015] The support member 4 contains a support member for the positioning and locking component. The positioning and locking component can be fixed to the surface of the selected component through the support member 4, thus completing the fixing of the positioning and locking component and facilitating subsequent measurement needs.

[0016] The red and green light starter 38 is the light start button for the positioning and locking component. When in use, it turns on the red light signal light 5 and the green light signal light 7, which emit red and green light respectively for detection.

[0017] The connecting screw 10, the upper cover 11, and the system box 35 are supporting and load-bearing components;

[0018] The connecting screw 10 is a positioning, clamping and fixing component for supporting and bearing the components. It can fix the upper cover 11 to the top of the system box 35, play a positioning and fixing role, and the screw connection facilitates maintenance personnel to repair and maintain.

[0019] The upper cover 11 is a closed component that supports and carries the components. It is fixed to the system box 35 by connecting screws 10 to prevent foreign objects from entering the system box 35 and to prevent external damage to the electronic components inside the system box 35.

[0020] The system box 35 is a functional component that supports and carries the components. Various components are connected inside and on its surface. The system box 35 plays a supporting and carrying role.

[0021] The display screen 12 is a display component that can display the test results on the display screen 12. When the testing device malfunctions, the fault code will also be displayed on the display screen 12 to help maintenance personnel diagnose the fault.

[0022] The bolt 15, hexagonal nut 16, washer 17 and connector 19 are the main load-bearing components;

[0023] The bolts 15, hexagonal nuts 16 and washers 17 are used for fastening to prevent the components from shifting.

[0024] The upper surface of the connector 19 is bolted to the electric expansion joint 14 using bolts 15, hexagonal nuts 16 and washers 17, and the lower surface of the connector 19 is bolted to the expansion joint 22 using bolts 15, hexagonal nuts 16 and washers 17, for bearing components such as the electric expansion joint 14 and the system box 35.

[0025] The foot support rod 20 and the threaded connector 21 are the main support components;

[0026] The foot support rod 20 is a load-bearing component of the main support component. One end has an internal thread structure for easy connection. The three foot support rods 20 are placed at an angle of 120° on the ground to effectively improve the support effect.

[0027] The threaded connector 21 is a connecting component of the main support component. Both ends are externally threaded and can be screwed into the foot support rod 20 and the telescopic device 22 respectively, thus connecting the foot support rod 20 and the telescopic device 22.

[0028] The support 29 is a support component with a triangular structure, which makes the structural connection more secure. It has three bolt holes, which facilitates bolt connection with the system box 35 and provides support for the system box 35 and its internal and surface components.

[0029] The red light signal lamp 5, the double-headed stud 6, and the green light signal lamp 7 are all connected to the positioning and locking component to form the large positioning and locking component.

[0030] The red light signal lamp 5 is a sensing signal component for positioning and locking large components. The red light signal lamp 5 is a sensing signal lamp for the detection device, which is used to adjust the vertical height of the detection device.

[0031] The green light signal lamp 7 is an auxiliary positioning component for positioning and locking large components. The green light emitted by the green light signal lamp 7 is used for positioning the detection device.

[0032] The blue light signal lamp 36 is located at the center of the detection device, and the blue light emitted should be in the same position on the ground as the green light emitted by the green light signal lamp 7 to ensure the stability and reliability of the measurement results.

[0033] The double-ended stud 6 is a connecting component for positioning and locking large parts. The double-ended stud 6 is used to connect the support component 4 to the green light signal lamp 7 to ensure the reliability of the connection.

[0034] The electric telescopic rod 13, electric telescopic device 14, and telescopic device 22 are motion execution components;

[0035] The electric telescopic rod 13 is the actuator of the motion actuator, which is placed inside the electric telescopic device 14 and the telescopic device 22. It can extend and retract with the electric telescopic device 14 and the telescopic device 22, and play the role of motion actuator of the detection device.

[0036] The electric telescopic device 14 is the active force component of the motion execution part, used to ensure that the height of the detection device matches the position of the red light emitted by the red light signal lamp 5;

[0037] The telescopic device 22 is a secondary power component of the motion execution component, used to ensure that the height of the detection device matches the position of the red light emitted by the red light signal lamp 5, to prevent instability of the electric telescopic device 14 due to vibration and other problems, and to make the detection system more reliable.

[0038] The distance sensor 18 is a sensing component that can receive the red light emitted by the red light signal lamp 5. After receiving the red light emitted by the red light signal lamp 5, it can feed back a signal to the control system to ensure that the height of the detection device is consistent with the setting.

[0039] The sound alarm 8 and the light alarm 9 are warning components;

[0040] The sound alarm 8 will issue a warning after receiving an unqualified command, so as to promptly remind the operator and inspector.

[0041] The light alarm 9 will flash red light after receiving an unqualified command, so as to promptly remind the operator and inspector.

[0042] The switch button 23 and the record button 37 are control buttons;

[0043] The switch button 23 is used to start and stop the detection device;

[0044] The recording button 37 is used to record the results of the detection device, and is used to record unqualified detection results;

[0045] The HTTP interface 24 is a data interaction interface that can be used to detect system maintenance and upgrades.

[0046] The HDMI interface 25 is a display interaction interface that can be connected to smart screens, large-size displays, etc., to realize remote display and interaction of the detection structure.

[0047] The camera connector 26, the adaptive flexible connector 27, the camera 28, and the data acquisition unit 30 are data acquisition components;

[0048] The camera connector 26 is used to achieve the connection function, which can reliably connect the data acquisition component to the system box 35;

[0049] The adaptive flexible connector 27 is a fine-tuning and connecting component for the data acquisition component. It can connect the camera connector 26 and the camera 28. Furthermore, the function of the adaptive flexible connector 27 can be used to fine-tune the focal length of the camera 28, making the acquired video image clearer.

[0050] The camera 28 is an execution component of the data acquisition unit and works in conjunction with the data acquisition unit 30 to acquire data video images.

[0051] The edge processing unit 31, data processing unit 32, data control unit 33, and power module 34 are processing and control components;

[0052] The edge processing unit 31 is a video data processing and detection component. It works in conjunction with the data processing unit 32 to detect video data and realize the function of the detection device.

[0053] The data control unit 33 is a control component of the processing and control unit, and issues control commands.

[0054] The sound alarm 8 and light alarm 9 are controlled to issue an alarm;

[0055] The electric telescopic device 14 and telescopic device 22 enable the telescopic adjustment of the detection device;

[0056] The power module 34 is a power supply component that can be charged and discharged to meet the power requirements of the detection device.

[0057] This inspection method is more efficient, strictly adheres to pre-set unified inspection standards, and utilizes the coordinated and comparative effects of multiple inspection modules. It can intelligently and quickly inspect the position of assemblies. During the inspection process, mechanical and automated program control replaces the existing manual visual inspection and measurement, which can improve inspection efficiency and achieve visualized, standardized, and comprehensive inspection results.

[0058] The advantages of this application are as follows: Through analysis of existing methods for detecting the position of assembled parts, it is found that existing methods are cumbersome and complex. They not only require process engineers to select accurate and reasonable measurement positions during the design phase, but also require operators to have relevant experience, stable and accurate tooling without deformation, and are subject to many constraints and significant human factors. For complex assemblies, only a few positions can be checked, resulting in arbitrary and incomplete inspection results. The inspection relies heavily on human experience, lacks versatility, and is not accurate enough, leading to incomplete detection, low detection efficiency, and wasting time and effort.

[0059] To address the aforementioned issues, a simple and easy-to-operate method is needed for the detection of assembly positions of components. This method should be highly efficient and comprehensive, unaffected by the process design level of the process engineers or the skill level of the operators, and should provide clearer, more accurate, and faster results. This technical solution aims to provide operators with an adaptive assembly position detection device for components. Composed of mechanical and electrical control components, this solution features a simple structure, low cost, small size, portability, easy operation, and strong versatility, unaffected by the shape or size of the components. Its ingenious design enables precise detection. For various complex components, it allows for distance adjustments to meet different detection needs, demonstrating strong adaptability and high versatility. Multiple detection modules are used for automated intelligent detection, and the results are displayed using buzzers and warning lights. The results can also be directly output to a display screen, achieving efficient and intuitive detection.

[0060] During the assembly position inspection process, the implementation of the above-mentioned assembly position detection method improves the efficiency of assembly position detection, reduces complex manual operations, enhances operator comfort, boosts the confidence of inspectors in judging the correctness of assembly positions, and prevents products with undetected errors from entering the next stage of work due to various oversights. It enables rapid identification of the correctness of assembly positions, facilitates quick identification of poorly positioned assemblies, and allows for rapid troubleshooting, ensuring the stable and reliable position of the entire component assembly, meeting design requirements, and thus guaranteeing the realization of overall aircraft performance. This contributes to improved assembly accuracy and efficiency. Attached Figure Description

[0061] Figure 1 It is an isometric drawing of the positioning and locking components used in the aircraft assembly component position defect detection device;

[0062] Figure 2 Top view of a device for detecting location defects in aircraft assembly components;

[0063] Figure 3 This is a bottom view of a device used for detecting positional defects in aircraft assembly components.

[0064] Figure 4 It is an isometric drawing used in an aircraft assembly component position defect detection device;

[0065] Figure 5 This is a left view of a device used for detecting positional defects in aircraft assembly components.

[0066] Figure 6 This is a schematic diagram of a method for detecting positional defects in aircraft assembly components.

[0067] The components include: 1. Threaded rod, 2. Operating rod, 3. Movable clamping block, 4. Support component, 5. Red light signal light, 6. Double-ended stud, 7. Green light signal light, 8. Sound alarm, 9. Light alarm, 10. Connecting screw, 11. Top cover, 12. Display screen, 13. Electric telescopic rod, 14. Electric telescopic device, 15. Bolt, 16. Hex nut, 17. Washer, 18. Distance sensor, 19. Connector, 20. Support rod, 21. Threaded connector, 22. Telescopic device, 23. Switch button, 24. HTTP interface, 25. HDMI interface, 26. Camera connector, 27. Adaptive flexible connector, 28. Camera, 29. Support body, 30. Data acquisition unit, 31. Edge processing unit, 32. Data processing unit, 33. Data control unit, 34. Power module, 35. System box, 36. Blue light signal light, 37. Detection button, and 38. Red and green light starter. Detailed Implementation

[0068] The present application is described in detail below with reference to the embodiments, but the present application is not limited to these embodiments.

[0069] Example 1

[0070] A device for detecting positional defects in aircraft assembly components comprises a mechanical structure, an electric control system, and a data acquisition and processing system.

[0071] The mechanical structure consists of a threaded rod 1, an operating rod 2, a movable clamping block 3, a support component 4, a connecting screw 10, an upper cover 11, a display screen 12, bolts 15, a hexagonal nut 16, a washer 17, a connecting body 19, a foot support rod 20, a threaded connector 21, a support body 29, a system box 35, and a red and green light starter 38.

[0072] The electric control unit consists of a red signal light 5, a double-headed stud 6, a green signal light 7, an electric telescopic rod 13, an electric telescopic device 14, a distance sensor 18, a telescopic device 22, and a blue signal light 36.

[0073] The data acquisition and processing section consists of a sound alarm 8, a light alarm 9, a switch button 23, an HTTP interface 24, an HDMI interface 25, a camera connector 26, an adaptive flexible connector 27, a camera 28, a data acquisition unit 30, an edge processing unit 31, a data processing unit 32, a data control unit 33, a power module 34, and a detection button 37.

[0074] The threaded rod 1, operating rod 2, movable clamping block 3, support member 4 and red and green light starter 38 constitute a positioning and locking component;

[0075] The threaded rod 1 is a transmission component of the positioning and locking part. The bottom of the threaded rod 1 is in the form of a ball joint, which facilitates connection with the movable clamping block 3. The threaded rod 1 can be screwed in and out by the interaction of the external thread and the internal thread of the support component 4.

[0076] The operating lever 2 is the actuating component of the positioning and locking part. The operating lever 2 can be turned by hand force, and the threaded rod 1 is driven by the operating lever 2 to realize the screwing in and out of the support component 4.

[0077] The movable clamping block 3 is a functional component of the positioning and locking part. Its structure adopts a ball joint. The bottom of the threaded rod 1 is placed inside the movable clamping block 3, which can realize multi-directional rotation. It is used to adjust the positioning and locking part to work in different positions and structures. It can be realized by rotating the operating rod 2 by hand to drive the threaded rod 1 to rotate in and out, thereby driving the movable clamping block 3 to press.

[0078] The support member 4 contains a support member for the positioning and locking component. The positioning and locking component can be fixed to the surface of the selected component through the support member 4, thus completing the fixing of the positioning and locking component and facilitating subsequent measurement needs.

[0079] The red and green light starter 38 is the light start button for the positioning and locking component. When in use, it turns on the red light signal light 5 and the green light signal light 7, which emit red and green light respectively for detection.

[0080] The connecting screw 10, the upper cover 11, and the system box 35 are supporting and load-bearing components;

[0081] The connecting screw 10 is a positioning, clamping and fixing component for supporting and bearing the components. It can fix the upper cover 11 to the top of the system box 35, play a positioning and fixing role, and the screw connection facilitates maintenance personnel to repair and maintain.

[0082] The upper cover 11 is a closed component that supports and carries the components. It is fixed to the system box 35 by connecting screws 10 to prevent foreign objects from entering the system box 35 and to prevent external damage to the electronic components inside the system box 35.

[0083] The system box 35 is a functional component that supports and carries the components. Various components are connected inside and on its surface. The system box 35 plays a supporting and carrying role.

[0084] The display screen 12 is a display component that can display the test results on the display screen 12. When the testing device malfunctions, the fault code will also be displayed on the display screen 12 to help maintenance personnel diagnose the fault.

[0085] The bolt 15, hexagonal nut 16, washer 17 and connector 19 are the main load-bearing components;

[0086] The bolts 15, hexagonal nuts 16 and washers 17 are used for fastening to prevent the components from shifting.

[0087] The upper surface of the connector 19 is bolted to the electric expansion joint 14 using bolts 15, hexagonal nuts 16 and washers 17, and the lower surface of the connector 19 is bolted to the expansion joint 22 using bolts 15, hexagonal nuts 16 and washers 17, for bearing components such as the electric expansion joint 14 and the system box 35.

[0088] The foot support rod 20 and the threaded connector 21 are the main support components;

[0089] The foot support rod 20 is a load-bearing component of the main support component. One end has an internal thread structure for easy connection. The three foot support rods 20 are placed at an angle of 120° on the ground to effectively improve the support effect.

[0090] The threaded connector 21 is a connecting component of the main support component. Both ends are externally threaded and can be screwed into the foot support rod 20 and the telescopic device 22 respectively, thus connecting the foot support rod 20 and the telescopic device 22.

[0091] The support 29 is a support component with a triangular structure, which makes the structural connection more secure. It has three bolt holes, which facilitates bolt connection with the system box 35 and provides support for the system box 35 and its internal and surface components.

[0092] The red light signal lamp 5, the double-headed stud 6, and the green light signal lamp 7 are all connected to the positioning and locking component to form the large positioning and locking component.

[0093] The red light signal lamp 5 is a sensing signal component for positioning and locking large components. The red light signal lamp 5 is a sensing signal lamp for the detection device, which is used to adjust the vertical height of the detection device.

[0094] The green light signal lamp 7 is an auxiliary positioning component for positioning and locking large components. The green light emitted by the green light signal lamp 7 is used for positioning the detection device.

[0095] The blue light signal lamp 36 is located at the center of the detection device, and the blue light emitted should be in the same position on the ground as the green light emitted by the green light signal lamp 7 to ensure the stability and reliability of the measurement results.

[0096] The double-ended stud 6 is a connecting component for positioning and locking large parts. The double-ended stud 6 is used to connect the support component 4 to the green light signal lamp 7 to ensure the reliability of the connection.

[0097] The electric telescopic rod 13, electric telescopic device 14, and telescopic device 22 are motion execution components;

[0098] The electric telescopic rod 13 is the actuator of the motion actuator, which is placed inside the electric telescopic device 14 and the telescopic device 22. It can extend and retract with the electric telescopic device 14 and the telescopic device 22, and play the role of motion actuator of the detection device.

[0099] The electric telescopic device 14 is the active force component of the motion execution part, used to ensure that the height of the detection device matches the position of the red light emitted by the red light signal lamp 5;

[0100] The telescopic device 22 is a secondary power component of the motion execution component, used to ensure that the height of the detection device matches the position of the red light emitted by the red light signal lamp 5, to prevent instability of the electric telescopic device 14 due to vibration and other problems, and to make the detection system more reliable.

[0101] The distance sensor 18 is a sensing component that can receive the red light emitted by the red light signal lamp 5. After receiving the red light emitted by the red light signal lamp 5, it can feed back a signal to the control system to ensure that the height of the detection device is consistent with the setting.

[0102] The sound alarm 8 and the light alarm 9 are warning components;

[0103] The sound alarm 8 will issue a warning after receiving an unqualified command, so as to promptly remind the operator and inspector.

[0104] The light alarm 9 will flash red light after receiving an unqualified command, so as to promptly remind the operator and inspector.

[0105] The switch button 23 and the record button 37 are control buttons;

[0106] The switch button 23 is used to start and stop the detection device;

[0107] The recording button 37 is used to record the results of the detection device, and is used to record unqualified detection results;

[0108] The HTTP interface 24 is a data interaction interface that can be used to detect system maintenance and upgrades.

[0109] The HDMI interface 25 is a display interaction interface that can be connected to smart screens, large-size displays, etc., to realize remote display and interaction of the detection structure.

[0110] The camera connector 26, the adaptive flexible connector 27, the camera 28, and the data acquisition unit 30 are data acquisition components;

[0111] The camera connector 26 is used to achieve the connection function, which can reliably connect the data acquisition component to the system box 35;

[0112] The adaptive flexible connector 27 is a fine-tuning and connecting component for the data acquisition component. It can connect the camera connector 26 and the camera 28. Furthermore, the function of the adaptive flexible connector 27 can be used to fine-tune the focal length of the camera 28, making the acquired video image clearer.

[0113] The camera 28 is an execution component of the data acquisition unit and works in conjunction with the data acquisition unit 30 to acquire data video images.

[0114] The edge processing unit 31, data processing unit 32, data control unit 33, and power module 34 are processing and control components;

[0115] The edge processing unit 31 is a video data processing and detection component. It works in conjunction with the data processing unit 32 to detect video data and realize the function of the detection device.

[0116] The data control unit 33 is a control component of the processing and control unit, and issues control commands.

[0117] The sound alarm 8 and light alarm 9 are controlled to issue an alarm;

[0118] The electric telescopic device 14 and telescopic device 22 enable the telescopic adjustment of the detection device;

[0119] The power module 34 is a power supply component that can be charged and discharged to meet the power requirements of the detection device.

[0120] The specific work process is as follows:

[0121] Step 1: Before use, check the appearance of the aircraft assembly component defect detection device, and check whether the device label is complete and the appearance is intact. If it is complete and intact, proceed to the next step.

[0122] Step Two: Secure the positioning and locking component horizontally onto the test piece as required, ensuring alignment with one end of the test piece. Press the red-green light starter 38 of the positioning and locking component to illuminate the red indicator light 5 and the green indicator light 7. Check for any abnormalities. If no abnormalities are found, proceed to the next step.

[0123] Step 3: Press the defect detection device switch button 23, check if the display screen 12 is intact and if the blue light indicator 36 is lit. If there are no problems, proceed to the next step.

[0124] Step 4: Place the defect detection device on a level surface, ensuring that the blue light emitted by the blue light indicator 36 of the defect detection device intersects with the green light emitted by the green light indicator 7 of the positioning and locking component on the ground, thus completing the positioning of the defect detection device and the positioning and locking component.

[0125] Step 5: Press the detection button 23 of the defect detection device to start the detection work. The display screen 12 shows the real-time results of the defect detection. When a location defect is found, the data control unit 33 will control the sound alarm 8 to emit a "beep beep" warning and the light alarm 9 to emit a "red light" flashing to remind the operator and inspector of the location defect. Five seconds later, the video image data of the defect location fault will be automatically recorded.

[0126] Step Six: After the location information to be detected is completed in sequence, press the switch button 23 and the red and green light starter 38 of the aircraft assembly component location defect detection device to turn off the aircraft assembly component location defect detection device. Disconnect the mechanical connection in the reverse order of connection and put the flexible adaptive adapter of the smart camera back to its original position.

[0127] The above description is merely a specific embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any modifications or substitutions made by those skilled in the art within the technical scope disclosed in the present invention should be included within the scope of protection of the present invention. Therefore, the scope of protection of the present invention should be determined by the scope of the claims.

Claims

1. A device for detecting positional defects in aircraft assembly components, characterized in that, It consists of a mechanical structure, an electric control system, and a data acquisition and processing system. The mechanical structure consists of a threaded rod (1), an operating rod (2), a movable clamping block (3), a support component (4), a connecting screw (10), an upper cover (11), a display screen (12), bolts (15), hexagonal nuts (16), washers (17), a connector (19), a foot support rod (20), a threaded connector (21), a support body (29), a system box (35), and a red and green light starter (38). The electric control unit consists of a red light signal lamp (5), a double-headed stud (6), a green light signal lamp (7), an electric telescopic rod (13), an electric telescopic device (14), a distance sensor (18), a telescopic device (22), and a blue light signal lamp (36). The data acquisition and processing section consists of a sound alarm (8), a light alarm (9), a switch button (23), an HTTP interface (24), an HDMI interface (25), a camera connector (26), an adaptive flexible connector (27), a camera (28), a data acquisition unit (30), an edge processing unit (31), a data processing unit (32), a data control unit (33), a power module (34), and a detection button (37).

2. The detection device for positional defects in aircraft assembly components according to claim 1, characterized in that, The threaded rod (1), operating rod (2), movable clamping block (3), support member (4) and red and green light starter (38) constitute a positioning and locking component; The threaded rod (1) is a transmission component of the positioning and locking component. The bottom of the threaded rod (1) is in the form of a ball joint, which facilitates connection with the movable clamping block (3). The threaded rod (1) can be screwed in and out by using the external thread and the internal thread of the support component (4) to cooperate with each other. The operating lever (2) is the actuator of the positioning and locking component. The operating lever (2) can be turned by hand force, and the threaded rod (1) is driven by the operating lever (2) to realize the screwing in and out of the support component (4); The movable clamping block (3) is a functional component of the positioning and locking component. Its structure adopts a ball joint. The bottom of the threaded rod (1) is placed inside the movable clamping block (3), which can achieve multi-directional rotation. It is used to adjust the positioning and locking component to work in different positions and structures. It can be realized by rotating the operating rod (2) by hand to drive the threaded rod (1) to rotate in and out, thereby driving the movable clamping block (3) to press. The support member (4) contains the support member for the positioning and locking component. The positioning and locking component can be fixed to the surface of the selected component through the support member (4), thus completing the fixing of the positioning and locking component and facilitating subsequent measurement needs. The red and green light starter (38) is the light start button for the positioning and locking component. When in use, the red light signal lamp (5) and the green light signal lamp (7) are turned on to emit red light and green light respectively for detection.

3. The detection device for positional defects in aircraft assembly components according to claim 2, characterized in that, The connecting screw (10), the upper cover (11), and the system box (35) are supporting and load-bearing components; The connecting screw (10) is a positioning, clamping and fixing component for supporting and bearing components. It can fix the upper cover (11) to the top of the system box (35) to play a positioning and fixing role. The screw connection is convenient for maintenance personnel to repair and maintain. The upper cover (11) is a closed component that supports and carries the components. It is fixed to the system box (35) by connecting screws (10) to prevent foreign objects from entering the system box (35) and to prevent external damage to the electronic components inside the system box (35). The system box (35) is a functional component that supports and bears the components. Various components are connected inside and on its surface. The system box (35) plays a supporting and bearing role. The display screen (12) is a display component that can display the test results on the display screen (12). When the testing device malfunctions, the fault code will also be displayed on the display screen (12), which will help maintenance personnel diagnose the fault.

4. The detection device for positional defects in aircraft assembly components according to claim 3, characterized in that, The bolt (15), hexagonal nut (16), washer (17), and connector (19) are the main load-bearing components; The bolts (15), hexagonal nuts (16) and washers (17) are used for fastening and can prevent the components from shifting. The upper surface of the connector (19) is bolted to the electric expansion joint (14) using bolts (15), hexagonal nuts (16) and washers (17), and the lower surface of the connector (19) is bolted to the expansion joint (22) using bolts (15), hexagonal nuts (16) and washers (17), for bearing components such as the electric expansion joint (14) and the system box (35).

5. The detection device for positional defects in aircraft assembly components according to claim 4, characterized in that, The foot support rod (20) and threaded connector (21) are the main support components; The foot support rod (20) is the load-bearing component of the main support component. One end has an internal thread structure, which is convenient for connection. The three foot support rods (20) are placed at an angle of 120° on the ground, which can effectively improve the support effect. The threaded connector (21) is a connecting component of the main support component. Both ends are external threads, which can be screwed into the foot support rod (20) and the telescopic device (22) respectively, and serve to connect the foot support rod (20) and the telescopic device (22). The support (29) is a support component with a triangular structure, which makes the structural connection more secure. It has three bolt holes, which facilitates bolt connection with the system box (35) and provides support for the system box (35) and its internal and surface components.

6. The detection device for positional defects in aircraft assembly components according to claim 5, characterized in that, The red light signal lamp (5), the double-headed stud (6) and the green light signal lamp (7) are all connected to the positioning and locking component to form a large positioning and locking component; The red light signal lamp (5) is a sensing signal component for positioning and locking large components. The red light signal lamp (5) is a sensing signal lamp for the detection device, which is used to adjust the vertical height of the detection device. The green light signal lamp (7) is an auxiliary positioning component for positioning and locking large components. The green light emitted by the green light signal lamp (7) is used for positioning of the detection device. The blue light signal lamp (36) is located at the center of the detection device. The blue light emitted should be in the same position on the ground as the green light emitted by the green light signal lamp (7) to ensure the stability and reliability of the measurement results. The double-ended stud (6) is a connecting component for positioning and locking large components. The double-ended stud (6) is used to connect the support component (4) to the green light signal lamp (7) to ensure the reliability of the connection.

7. The detection device for positional defects in aircraft assembly components according to claim 6, characterized in that, The electric telescopic rod (13), electric telescopic device (14), and telescopic device (22) are motion execution components; The electric telescopic rod (13) is the actuator of the motion actuator, which is placed inside the electric telescopic device (14) and the telescopic device (22). It can extend and retract with the electric telescopic device (14) and the telescopic device (22) to play the role of motion actuator of the detection device. The electric telescopic device (14) is the active force component of the motion execution component, used to ensure that the height of the detection device matches the position of the red light emitted by the red light signal lamp (5); The telescopic device (22) is a secondary power component of the motion execution component, used to ensure that the height of the detection device matches the position of the red light emitted by the red light signal lamp (5), and to prevent the electric telescopic device (14) from becoming unstable due to vibration and other problems, so as to make the detection system more reliable. The distance sensor (18) is a sensing component that can receive the red light emitted by the red light signal lamp (5). After receiving the red light emitted by the red light signal lamp (5), it can feed back a signal to the control system to ensure that the height of the detection device is consistent with the setting.

8. The detection device for positional defects in aircraft assembly components according to claim 7, characterized in that, The sound alarm (8) and the light alarm (9) are warning components; The sound alarm (8) will issue a warning after receiving a non-compliant instruction, so as to promptly remind the operator and the inspector. The light alarm (9) will flash red light after receiving an unqualified command, so as to promptly remind the operator and inspector. The switch button (23) and the record button 37 are control buttons; The switch button (23) is used to start and stop the detection device; The recording button 37 is used to record the results of the detection device, and is used to record unqualified detection results; The HTTP interface (24) is a data interaction interface that can be used to detect system maintenance and upgrades; The HDMI interface (25) is a display interaction interface that can be connected to smart screens, large-size displays, etc., to realize remote display and interaction of the detection structure.

9. The detection device for positional defects in aircraft assembly components according to claim 8, characterized in that, The camera connector (26), the adaptive flexible connector (27), the camera (28), and the data acquisition unit (30) are data acquisition components; The camera connector (26) is used to achieve the connection function, which can reliably connect the data acquisition component to the system box (35); The adaptive flexible connector (27) is a fine-tuning and connecting component for the data acquisition component. It can connect the camera connector (26) and the camera (28). Furthermore, the function of the adaptive flexible connector (27) can be used to fine-tune the focal length of the camera (28), making the acquired video image clearer. The camera (28) is a data acquisition component execution component and works in conjunction with the data acquisition unit (30) to acquire data video images.

10. The detection device for positional defects in aircraft assembly components according to claim 9, characterized in that, The edge processing unit (31), data processing unit (32), data control unit (33), and power module (34) are processing and control components; The edge processing unit (31) is a video data processing and detection component. It works in conjunction with the data processing unit (32) to detect video data and realize the function of the detection device. The data control unit (33) is a control component of the processing and control unit, which issues control commands; The control sound alarm (8) and light alarm (9) are activated to sound an alarm; The electric telescopic device (14) and telescopic device (22) enable the telescopic adjustment of the detection device; The power module (34) is a power supply component that can be charged and discharged to meet the power requirements of the detection device.

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