15 results about "Patch repair" patented technology

The invention relates to the field of intelligent medical treatment, in particular to a colposcope image-based data processing and segmentation method, equipment and a program product. The method includes: acquiring a vagina vinegar white image; performing mirror surface area detection on the vagina vinegar white image to obtain a mirror surface area; in the mirror surface area detection, a vagina vinegar white image is converted into an HIS color space to obtain a low-saturation S, high-brightness I and gradient GR three-channel vagina vinegar white image, and a mirror surface area is marked based on the three-channel vagina vinegar white image; and performing priority calculation on each pixel point in the mirror surface area, and performing patch repair processing based on a priority sequence to obtain a processed vagina vinegar white image. The application has good clinical value.

The application provides an anti-UAV display control training method and system, which can directly use the software interface of the actual system to directly cover, without copying the software interface and process, with low cost and short development cycle; since the actual system software is adopted, the software interface and operation process are 100% consistent with the actual system, a small design problem does not affect the core function, the design fault tolerance is high, and the operation experience is realistic; if patch repair type software upgrading of the actual system is encountered, the application can automatically adapt to realize the capture operation, and solves the problem of the current anti-UAV display control training system, which realizes the construction means of the UAV display control training system through one-to-one copying, and the practicality is poor.

This application discloses a mobile terminal automated testing method and apparatus, relating to the field of automated testing. It retrieves test knowledge related to test requirements from a pre-built knowledge base. Based on the test requirements and test knowledge, it generates automated test scripts executable at the mobile terminal automation driver layer using a large language model. The automated test scripts are then run to execute the tests. If a test fails, a patch script is generated based on the failure evidence package collected during script execution. This patch script is then used as a temporary script to re-execute the test until the test termination condition is met. If the test passes when the termination condition is met, the passed patch script is compared with the automated test script, and the comparison result is submitted for manual review. If the review is successful, the passed patch script is updated in the knowledge base. This application achieves intelligent script generation and automatic patch repair while ensuring script standardization and executability.

UV patch repair device UV patch repair device (6) for repairing damaged pipelines (7), comprising an outer layer (6a) as fabric impregnated with resin, a middle layer (6b) as one foil and an inner layer (6c) as an inflatable hose; sealing in a start section (8b) of the hose; a cable (3) attached to an UV head (5) placed inside the hose; characterised by that the device comprising an end section (8a) of the hose as a closure, a rod (1) attached to the UV head (5) with a string (2) and placed inside the hose, the string further attached to the end section (8a) of the hose and the cable (3) is an electrical cable electrically connected to the UV head (5) and a flow channel for feeding air to the UV head (5) and is placed inside of the UV patch repair device (6).

The invention provides a software repair method and device, equipment, a medium and a product, and relates to the technical field of software engineering.The method comprises the steps that a to-be-repaired code snippet and multi-modal context information and a reference repair case associated with the to-be-repaired code snippet are obtained; according to the to-be-repaired code snippets, the multi-modal context information and the reference repair case, utilizing a generative model to generate at least one candidate repair patch; for each candidate repair patch, performing formalized verification and solution to obtain a verification result corresponding to the candidate repair patch; under the condition that the verification result indicates that the candidate repair patch passes verification, the to-be-repaired code snippets are repaired through the candidate repair patch; and under the condition that the verification result indicates that the candidate repair patch does not pass the verification, feeding back prompt information for triggering the generative model to optimize the candidate repair patch to the generative model according to the path information or the error state code corresponding to the candidate repair patch.

This invention discloses a method for patching and repairing fiber-reinforced composite material components, integrating self-resistance heating and curing process monitoring. The method includes: processing the damaged fiber-reinforced composite material component to form stepped patch holes; fabricating a thin-film element integrating heating and monitoring functions; constructing a composite material electrothermal curing repair platform with embedded thin-film elements; performing electrothermal curing repair and bonding the patch structure with embedded thin-film elements; obtaining a resin curing history curve; comparing the resistance change curve of the thin-film element with the resin curing history curve to determine the resin curing process and achieve in-situ monitoring of molding quality. This invention enables efficient and uniform heating and real-time monitoring of the in-situ curing process of damaged areas in fiber-reinforced composite material components, laying a theoretical foundation and providing technical guidance for researching low-cost, high-efficiency, and intelligent repair methods for composite materials.

The invention provides a function patch repair method and electronic equipment, relates to the technical field of terminals, and aims to solve the problems of repair omission and repair abnormity caused by incomplete information in a function repair process. The method is applied to the electronic equipment and comprises the steps of obtaining a software service pack of software; the software service pack comprises a patch of a target function and a first relation, the target function is a function needing to be repaired, and the first relation is a calling relation of functions in the software; determining a second relationship according to the stack frame information and the first relationship, wherein the second relationship is a calling relationship of a function currently operated in the software; and repairing the function patch according to the second relationship and the patch of the target function.

This utility model relates to the field of pipeline maintenance technology and discloses a patch repair structure for trenchless pipeline local repair. It includes a pipe body and an elastic airbag fixed to the outside of the pipe body. A connecting pipe is provided inside the elastic airbag, and an internal thread is provided at the lower part of the connecting pipe. An end cap is provided at the end of the connecting pipe, and a second external thread is provided on the surface of the end cap to cooperate with the internal thread. This utility model involves placing this structure at the damaged area of ​​the pipeline, opening the end cap, and inflating the elastic airbag through the connecting pipe to make the airbag bulge and fit tightly against the inner wall of the pipeline, thus fixing the structure. Then, by opening the threaded cap and using a connecting cylinder, cement grout is injected into the gap between the pipe body and the inner wall of the pipeline, thereby completing the local repair of the pipeline. This method is lower in cost and suitable for use in pipelines with small-scale damage.

The utility model discloses a die cutting material supplementing module. The die cutting material supplementing module comprises an x-axis moving assembly, a y-axis moving assembly and a material supplementing assembly. The y-axis moving assembly is arranged on the x-axis moving assembly, and the y-axis moving assembly can slide on the x-axis moving assembly; the material supplementing assembly is arranged on the y-axis moving assembly and can slide on the y-axis moving assembly; the material supplementing assembly comprises a z-axis moving assembly, and the z-axis moving assembly is arranged on the y-axis moving assembly; the rotating assembly is arranged on the z-axis moving assembly and can slide on the z-axis moving assembly; the suction head assembly is connected to the rotating assembly and used for adsorbing the die cutting material supplementing product, and the rotating assembly can drive the suction head assembly to rotate circumferentially; and the vacuum device is arranged on the z-axis moving assembly and can be connected with the suction head assembly through a pipeline. Automatic equipment is adopted to replace manual patch repairing, the patch repairing efficiency is improved, pollution and waste of products are avoided, and finally the yield of product material belts can be improved.

The invention provides an online binary optimization method and system, and relates to the technical field of online binary optimization. The running environment of the processor is determined according to the hardware architecture type of the current processor, and when the running environment is qualified, all the processes related to the target service are obtained, and the process PID list is constructed. And then generating a function replacement list according to the original binary file and the process PID list. Verifying whether the function replacement list meets a replacement requirement or not by using a sentry process; and when the function replacement list meets the replacement requirement, the function replacement list is applied to each process according to a patch repair strategy to replace the byte order of the corresponding function symbol in each process, and a final optimized process is obtained. On the basis, the method can be compatible with a hardware architecture of multiple processors, the problem that bottom detail processing is complex and prone to errors is avoided on the basis of reducing development complexity, and the risk that a server is interrupted in the online optimization processing process is overcome.

The utility model provides a kind of automatic boat type spare part repair production line of wood defect, belong to wood mechanical processing technical field. Including feed inlet, spare part processing unit, spare part transport unit, repair wood feed inlet and defect repair unit, the spare part processing unit is located in the side of feed inlet, the spare part transport unit is located below spare part processing unit, the defect repair unit is located above repair wood feed inlet. The utility model can realize the automatic processing and transportation of boat type spare part, and can repair boat type spare part at wood defect, form multiple function integrated production line, reduce labor cost, realize automation.

A method for repairing composite material structures using an I-shaped patch design includes the following steps: Step 1: After determining the number of layers to be removed from the damaged area, the damaged area is processed into an "I-shaped" structure; Step 2: Based on the patch repair layer with the smallest diameter or area, the lower patch with a larger diameter or area is cut into N (N≥2) parts according to the process separation surface; Step 3: Under pre-compaction temperature, the splicing area between the parts of the cut patch in Step 2 is pressed under high pressure to complete the overall splicing process of the patch; Step 4: After sequentially stacking the upper patches, the structure is sealed and cured to complete the repair process. This method can improve the mechanical properties of the composite material structure after damage repair and is applicable to the repair process of laminated structures such as composite skins and sandwich composite panels.

The application discloses a patch method and related equipment. The method comprises the following steps: calculating, in a server, coincidence degrees of each software module in a first patch for upgrading a first application program of a first electronic device and each software module of a first application program of a third electronic device, selecting each part with the maximum coincidence degree to combine into an integral whole, and generating difference data by differentiating the integral whole from the first patch. The second electronic device can obtain the difference data and restore the first patch package. The first electronic device can receive the first patch package from the second device and upgrade the first application program thereon. The technical scheme of the application can avoid the server from issuing large data patches multiple times, reduce the consumption of network bandwidth, greatly improve the efficiency of patch repair, and bring better use experience to users.

The high-temperature and high-pressure casing patching and repairing tool comprises a lifting connector, the inner side face of the lifting connector is connected with a pressure transmitting pipe through a screw thread, the outer side face of the lifting connector is connected with a hanger through a screw thread, and the hanger is connected with a hydraulic cylinder hook in a hooked mode through a piston connecting rod hook; a shock absorption lifting short section penetrates through the pressure transmission pipe and the hanger, one end of the hydraulic cylinder hook is connected with a first-stage hydraulic cylinder in a screwed mode, one end of the first-stage hydraulic cylinder is connected with a second-stage hydraulic cylinder, a first-stage piston connecting rod penetrates through the first-stage hydraulic cylinder, one end of the first-stage piston connecting rod is connected with the shock absorption lifting short section in a screwed mode, and the other end of the first-stage piston connecting rod is connected with the second-stage hydraulic cylinder in a screwed mode. The high-temperature and high-pressure casing patching and repairing tool can work in a high-temperature and high-pressure environment under a deep well, meanwhile, the pressure resistance is high, colloidal cement can be injected into the high-temperature and high-pressure casing patching and repairing tool for well cementation, and the deep well repairing capacity is greatly improved.

The application discloses a kind of aviation engine silicon carbide ceramic matrix composite material part patch repair methods, comprising: using CMC-SiC patch as the structure of patch repair part crack, corrosion pit or fiber crack, surface texture is prepared on the contact surface of CMC-SiC patch and part with pulse laser, brazing material is coated on the contact surface of CMC-SiC patch and part, CMC-SiC patch and part surface are pressed tightly, after vacuum brazing, polishing, cleaning and drying, environmental barrier coating recovery, annealing, the patch repair of aviation engine silicon carbide ceramic matrix composite material part is completed.The application adopts patch technology, reconstructs the force transmission path of crack, corrosion pit or fiber fracture, restores the strength of part, solves the repair problem of relatively wide crack, corrosion pit or fiber fracture and other more serious damage on silicon carbide ceramic matrix composite material part.In addition, specific texture, appearance is prepared on the contact surface of CMC-SiC patch and part with pulse laser, and the optimal combination effect and joint strength of brazing material and patch, part base material are accurately realized.