68 results about "Borescope" patented technology

An object pose prediction system includes a training system and an imaging system. The training system is configured to repeatedly receive a plurality of training image sets and to train a machine learning model to learn a plurality of different poses associated with the test target object in response to repeatedly receiving the plurality of training image sets. The imaging system is configured to receive a 2D test image of a test object, process the 2D test image using the trained machine learning model to predict a pose of the test object, and output a 3D test image including a rendering of the 2D test image having the predicted pose.

The invention relates to the technical field of complex equipment fault identification processing, in particular to a two-way decoupling and gated memory fused borescope image damage detection method, which is characterized in that a two-way decoupling and gated memory fused borescope image damage detection model is established, and training is performed only by adopting a normal image without a label; establishment of the two-way decoupling and gated memory fused borescope image damage detection model comprises feature decoupling, feature fusion and feature reconstruction, and in the feature decoupling stage, double-trunk encoders are adopted to serve as an effective information encoding branch and a redundant information encoding branch respectively; in the feature fusion stage, an adaptive gating and memory guiding feature fusion module is arranged, a structure perception reconstruction decoder is established in the feature reconstruction stage, fused representation features are sent to the structure perception reconstruction decoder for image reconstruction, and the structure perception reconstruction decoder adopts a joint optimization loss function.

According to the intelligent borescope detection system for the aero-engine, in the system, an image acquisition module is arranged in a shell and used for acquiring image data of blade damage of the aero-engine; the image processing module is arranged in the shell and is connected with the image acquisition module so as to perform model reasoning and judge the type of blade damage based on the image data to obtain a detection result and a state; the display module is arranged on the shell and is connected with the image processing module to display the detection result and state in real time; the power supply module is arranged in the shell and is connected with and supplies power to the image processing module, the image acquisition module and the display equipment; the detection interface realizes real-time borescope inspection of the aero-engine in a man-machine cooperative interaction manner, and the specific functions comprise checking, storing, photographing, video recording, detecting and the like; and the detection unit is mainly used for reasoning and identifying the image data of the damage of the aero-engine blade acquired by the image acquisition module.

A defect depth estimation system includes a training system and an imaging system that performs defect depth estimation from a monocular 2D image without using a depth sensor. The training system repeatedly receives a first type of image having a defect, and a second type of image that captures the target object having the defect and provides ground truth data indicating an actual depth of the defect. The training system transforms the first domain and the second domain into a target third domain that reduces a domain gap and trains a machine learning model to learn the actual depth of the defect using the target third domain. The imaging system receives a 2D test image in the first forma and uses the trained machine learning model to determine an estimation of the actual depth of the actual defect and to output estimated the estimation of the actual depth.

Medical imaging camera head attachment devices and methods are provided using light captured by an endoscope system or other medical scope or borescope. Various camera head attachments are provided with a camera head design and system allowing recognition of the attachments and enabling processing algorithms associated with each. The camera head optics are designed to work with a variety of attachments. Several attachments optical designs are provided.

1. The name of the design product: Pipeline endoscope (F2510DJKW). 2. The use of the design product: For detecting the inside of pipeline. 3. The design points of the design product: In the shape of the product. 4. The picture or photo that best shows the design points: In use state Fig. 5.

1. A borescope inspection device comprising: a probe for capturing images of at least a portion of an environment surrounding the probe, display means for displaying images captured by the probe, and an insertion tube connected to the probe and the display means, the insertion tube comprising coupling means extending through the insertion tube and configured to transmit images captured by the probe to the display means, 2. A borescope inspection device comprising: a probe for capturing images of at least a portion of an environment surrounding the probe, display means for displaying images captured by the probe, and an insertion tube coupled to the probe and the display means, the insertion tube comprising coupling means extending through the insertion tube and configured to transmit images captured by the probe to the display means, 3. A borescope inspection device comprising: a probe for capturing images of at least a portion of an environment surrounding the probe, the insertion tube comprising coupling means extending through the insertion tube and configured to transmit images captured by the probe to the display means, the insertion tube further comprising a photonic spectrometer for generating spectroscopic data of at least a portion of the environment surrounding the probe for display by the display means.

The utility model provides an endoscopic camera device for a boiler. The endoscopic camera device comprises an outer tube, an inner tube, a mirror tube and a connecting device, a cold air cavity communicated with the outside is formed in the outer pipe; the inner pipe comprises a first part and a second part; an imaging cavity is formed in the first part, and a containing cavity is formed in the second part; two ends of the mirror tube are respectively connected with a boiler combustion chamber and a camera, and an air inlet of the first part is detachably connected with an air filter through a connecting device; in the shooting process of the camera, compressed air in the cold air cavity flows to cause an air suction effect to promote external air to enter the boiler combustion chamber through the imaging cavity to be output, and therefore the mirror tube is cooled. According to the utility model, the inner tube not communicated with the outer tube continuously extracts air from the outside to cool the mirror tube and the camera in the inner tube through the air suction effect generated by outputting compressed air into the boiler combustion chamber after the compressed air is introduced into the outer tube, so that the problem that the camera is polluted by directly inputting the compressed air is avoided.

1. Name of the designed product: wire reel (box 9DX). 2. Use of the designed product: wire reel for underwater borescope conduit. 3. Design points of the designed product: combination of shape and pattern. 4. Picture or photo best indicating the design points: design 1 perspective view 1. 5. Design 1 is designated as the basic design.

A method of adaptive inspection includes receiving data characterizing one or more images of an inspection region of an industrial machine acquired by an inspection system operating based on a first set of operating parameters. The inspection region includes a site feature. The method also includes determining, by an analytical model, one or more characteristics of the inspection region from the received data characterizing the one or more images of the inspection region. The method further includes generating a control signal based on the one or more characteristics of the inspection region and / or a user input. The inspection system is configured to perform a new inspection of the inspection region based on the control signal.

The present application relates to a kind of tool devices for guiding head lens assembly measurement, belong to lens assembly measurement technical field;Including guiding head lens measuring device, the bottom of guiding head lens measuring device is equipped with support leg, the top of support leg is equipped with first box, the top of first box is equipped with second box, the top of first box is equipped with electric sliding rail, the side of electric sliding rail is equipped with sliding seat, the side of sliding seat is equipped with clip by connecting rod, the bottom of clip is equipped with measuring instrument by connecting rod.The present application is rotated by linkage clamping and double base synchronously, full-process automatic detection, positioning accuracy is high, efficiency is high;Liquid storage cavity fills dimethyl silicone oil, temperature stability is good, flexible clamping does not hurt lens, maintenance is simple;Double base cooperates two times 90 degree displacement, once clamping completes full-dimension optical detection, reference is unified, adapts to multiple specifications lenses, and universality is strong.

A borescope feedback system with haptic feedback includes a borescope cable, a containment device, a cable sensor that is configured to detect motion of the borescope cable and output cable sensor data indicative of the motion of the borescope cable, a feedback device that is configured to controllably apply friction to the borescope cable, and a computing device configured to output a graphical user interface of a virtual reality representation of the borescope cable in a virtual environment; determine at least one of a direction of axial motion, a direction of circumferential motion, or a magnitude of the motion of the borescope cable; determine a collision of the virtual reality representation of the distal portion of the borescope cable with an obstruction in the virtual environment; and output a feedback signal to the feedback device that causes the feedback device to apply an amount of friction to the borescope cable.

The invention discloses a self-adaptive cooling and visual hearth thermal imaging intelligent monitoring system. The system is characterized by comprising a camera lens tube system, a cooling gas source and a flow regulating valve, the camera lens tube system comprises an infrared thermal imaging camera, a lens tube cooling protective cover, a cooling air series pipeline, a lens group and a temperature transmitter; the cooling air source is connected to the cooling air series-connection pipeline through a cooling air pipeline, and the temperature transmitter is installed in the mirror tube cooling protective cover; the system further comprises a controller, when the camera lens tube system extends into the furnace for monitoring, the temperature transmitter collects the temperature in the lens tube cooling protective cover, and the controller adjusts the opening degree of the flow adjusting valve in real time according to the temperature fed back by the temperature transmitter, so that the cooling air intensity is controlled. The working temperature is monitored through the temperature sensor, data are transmitted to the controller, the controller adjusts the rotating speed of the draught fan or the opening degree of the air valve according to a preset cooling strategy, and therefore dynamic adjustment of the cooling air intensity is achieved.

The present invention provides an engine blade detection system and method based on image feature similarity matching, which belongs to the field of engine detection technology. The detection system includes a borescope video acquisition unit for acquiring video frame images of rotating engine blades; a blade zero position positioning unit for marking a zero point in the blade; an image extraction unit for extracting the video frame images frame by frame into pictures, numbering each picture, and marking the zero point picture with zero position; a counting unit for determining the number of blades based on the similarity of the pictures, and the total number of similarity peaks is the number of blades captured by the video frame image. The present invention only needs to use the borescope video frame image and the similarity of the coordinate-based video frame image of the blade rotation process to accurately count the number of detected blades, and can also combine with the defect judgment unit to perform defect judgment, killing two birds with one stone, thereby greatly reducing the error rate and missed detection rate of manual counting.

In one aspect a system and method for merging inspections from multiple borescope inspections into a single inspection and report include receiving, within a graphical user interface (GUI) of a borescope device, a selection of a first inspection file including first data characterizing a first inspection of an asset, receiving, within the GUI, a selection of a second inspection file including second data characterizing a second inspection of the asset, determining that the first inspection file and the second inspection file may be compatible to be merged and generating, automatically, a merged inspection file the merged inspection file that includes the first data and the second data.

The application discloses a kind of optical fiber multi-parameter logging devices, it is related to marine engineering equipment technical field, cable winch, logging cable, guide wheel and logging unit for downhole optical scanning and parameter measurement;Cable winch is used to wind and release logging cable;One end of the logging cable is connected to the cable winch, and the other end is guided by the guide wheel and connected to the logging unit;The logging unit is provided with a gasbag one sealed on the outside of the borescope and a gasbag two for fixing the detection position, which can isolate drilling fluid by inflating to achieve accurate detection and fixation of the detection position and maintain pressure balance;It can realize the technical effects of improving the stability of fixation, improving environmental adaptability, reducing signal interference and flexibly maintaining the pressure balance in the well.

The invention relates to a device and a method for coating hard-to-reach surfaces of a gas turbine (20), in particular an aircraft engine. The device (1) comprises a guide tube (2) that can be inserted through a borescope opening (22) and a repeatedly plastically deformable support element (3) for guiding a borescope head (7) arranged at one end (3') of the support element (3), wherein the guide tube (2) is designed to deform the support element (3) when the support element (3) is passed through the guide tube (2), so that the final shape of the support element (3) when inserted into the gas turbine (20) is determined by the guide tube (2) arranged on the gas turbine (20), and wherein the support element (3) and the borescope head (7) have a working channel (15) for carrying out a slurry (30), the discharge opening (13) of which is arranged on the borescope head (7) such that the discharged slurry (30) enters the image area (8) of the borescope head (7). In the process, a slurry is applied, for example, by a device (1) according to the invention and onto a surface before the slurry (30) is heated so that a coating is formed.

A tool stabilization mechanism is disclosed including a stabilizing device connected to a tool and movable between a deployed position and a non-deployed position, and an actuator for actuating the stabilizing device to move between the deployed position and the non-deployed position. In some forms the tool stabilization mechanism is integrated into a borescope unit, while in other forms it may be an accessory attachable to conventional borescope units. Related methods to the above are also disclosed herein.

The invention relates to a hyperspectral borescope system, and discloses a method and apparatus for inspecting a structure. Electromagnetic radiation is transmitted from an electromagnetic radiation emission system to a surface on a structure. The response to electromagnetic radiation is filtered using a filter located within the borescope inspection housing. The filter is configured to pass several wavelengths in a response to electromagnetic radiation directed toward the surface on the structure. Data from a number of wavelengths passed through a filter is generated using a sensor array. A two-dimensional image of a surface on a structure is generated with a set of graphical indicators that indicate a set of inconsistencies that are not visible to the naked eye. The two-dimensional image is generated using data from the sensor array.

An apparatus investigates a technical device using a borescope. The apparatus has: a guide tube which is introducible through a borescope opening on the technical device to be inspected using the borescope; and a repeatedly plastically deformable carrier configured to guide a borescope head arranged at one end of the carrier. The guide tube is designed to deform the carrier during the passage of the carrier through the guide tube.

The invention discloses a borescope calibration method and a matched portable calibration device, and belongs to the technical field of nondestructive testing and metering testing. The device comprises a base, a sliding block, a sliding base, a transmission mechanism, a line pattern standard ruler, a test line locking device and a standard block set (a two-dimensional resolution plate and a height and depth step gauge), can realize precise control of relative positions of a probe and a standard block, and supports field and outfield use. The calibration method comprises the steps of preparation before calibration, implementation of ten calibration items and data recording and analysis, and coverage of core parameters such as X / Y / Z three-axis indication error, depth of field, probe illumination and field angle through standardized processes such as environment quantitative control and multi-point repeated measurement. The borescope calibration method fills the blank of borescope calibration standards in China, reduces manual operation errors, improves the comprehensiveness, repeatability and traceability of calibration, is compatible with various borescopes, is suitable for the industries of aerospace, precision machinery and the like, and also can be referenced and implemented in the medical field.

The utility model discloses an endoscope assembly for pipeline inner wall inspection, which relates to the technical field of pipeline inner wall inspection and comprises a groove body, and a hollow long pipe is communicated with the middle of the bottom of the groove body. Rotating shafts are arranged on the two sides of the inner wall of the groove body respectively, and an endoscope is rotatably arranged between the rotating shafts on the two sides; a probe is arranged on the front side of the endoscope, and the endoscope is communicated with external display equipment through a wireless network; the endoscope is further provided with a rotation driving assembly. According to the assembly, the endoscope can be overturned back and forth by 180 degrees towards the rear side of the endoscope in the groove body, especially for a long pipeline with many inspection points, the whole endoscope assembly does not need to be repeatedly rotated by 360 degrees and only rotates within the semicircular range in the pipeline, and the inner wall of the whole pipeline can be inspected by overturning the endoscope through the rotation driving assembly; the device reduces labor intensity, can avoid collision or friction with the inner wall of the pipeline, effectively improves the inspection efficiency of the inner wall of the pipeline, and reduces the production cost.

The invention relates to a device and a method for coating hard-to-reach surfaces of a gas turbine (20), in particular of an aircraft engine. The device (1) comprises a guide tube (2), which can be inserted through a borescope opening (22), and a repeatedly plastically deformable support element (3) for guiding a borescope head (7) positioned at one end (3') of the support element (3), wherein the guide tube (2) is designed to deform the support element (3) when the support element (3) is guided through the guide tube (2), such that the final shaping of the support element (3) when the latter is inserted into the gas turbine (20) is defined by the guide tube (2) positioned on the gas turbine (20), and wherein the support element (3) and the borescope head (7) have a working channel (15) for the passage of a slurry (30), the discharge opening (13) of which is positioned on the borescope head (7) in such a way that the slurry (30) discharged therefrom passes into the image region (8) of the borescope head (7). In the method, a slurry is discharged, for example, by a device (1) according to the invention and applied to a surface before the slurry (30) is heated such that a coating is formed.

The invention discloses an optical fiber multi-parameter logging device, and relates to the technical field of ocean engineering equipment. The optical fiber multi-parameter logging device comprises a cable winch, a logging cable, a guide wheel and a logging unit used for underground optical scanning and parameter measurement. The cable winch is used for winding and releasing a logging cable; one end of the logging cable is connected with the cable winch, and the other end of the logging cable is guided and connected to the logging unit through the guide wheel; the well logging unit is provided with a first air bag wrapping the outer side of the pipeline endoscope in a sealed mode and a second air bag used for fixing a detection position, and drilling fluid is isolated through inflation expansion so that accurate detection and fixing of the detection position can be conducted, and pressure balance can be maintained. The technical effects that the fixing stability is improved, the environmental adaptability is improved, signal interference is reduced, and pressure balance in a well is flexibly maintained can be achieved.

This application belongs to the technical field of aeroengine maintenance, and particularly relates to a dismounting and mounting tool for a split anti-drop borescope plug of an aeroengine. The dismounting and mounting tool includes: a first limiting groove and a second limiting groove are respectively arranged at two ends of a wrench adapter; one end of an inner tube is connected to an inner tube end, and the other end is connected to an end nut; the end nut is threadedly connected to a borescope plug screw; an outer sleeve is sleeved outside an inner core, one end of an outer tube is connected to an outer sleeve adapter, and the other end is connected to a socket head; a limiting outer profile surface matching with the second limiting groove is arranged on the outer sleeve adapter; a tightening part is arranged on the outer tube, and the tightening part can be limited by the inner tube end and the end nut to prevent the outer tube from being disconnected from the inner tube; inner sleeve teeth are arranged on the socket head, and the socket head is meshed with a self-locking nut of the borescope plug through the sleeve teeth; a retaining ring is sleeved on the outer tube, and the retaining ring can be limited by the outer sleeve adapter and the socket head to prevent the retaining ring from being disconnected from the outer tube.

In one embodiment, systems and methods include using an inspection system to remove or seal foreign object debris. An inspection system comprises a borescope; wherein a plurality of optical fibers is disposed within the borescope; a mounting system; an articulation system; and a controller, wherein the controller comprises a display; wherein a proximal end of the borescope is coupled to the mounting system, wherein the mounting system is configured to secure the inspection system to an external surface, wherein the mounting system is coupled to the articulation system, wherein the articulation system is configured to actuate the borescope, wherein the articulation system is communicatively coupled to the controller.

A tool stabilization mechanism is disclosed including a stabilizing device connected to a tool and movable between a deployed position and a non-deployed position, and an actuator for actuating the stabilizing device to move between the deployed position and the non-deployed position. In some forms the tool stabilization mechanism is integrated into a borescope unit, while in other forms it may be an accessory attachable to conventional borescope units. Related methods to the above are also disclosed herein.

An augmented reality inspection system for inspecting features within a component includes a camera system that is configured to capture images of a component and a controller that is configured to receive images from the camera system. The controller is further programmed to utilize the received images to determine a location of the camera system and the captured images on the component, and utilize the determined location to generate graphic images relating to features of the component at the determined location. The system further includes a display that is configured to generate a real-time display of the component based in the captured images. The controller is further configured to superimpose the graphic images relating to features of the component onto the real-time display of the component.

The invention discloses an aero-engine abnormal borescope image screening method based on multi-stage generative adversarial, and relates to the field of intelligent detection and machine vision, in particular to the aero-engine abnormal borescope image screening method. The invention aims to solve the problem of low screening accuracy of the abnormal borescope image of the aero-engine due to the fact that the characteristics of weak texture, small abnormal area, high background redundancy and the like in the borescope image are difficult to process in the prior art. The method comprises the following steps: 1, acquiring a healthy aero-engine borescope image data set; 2, constructing a BiGenAD network model, and obtaining a trained BiGenAD network model based on the data set; the BiGenAD network model comprises a random simulator, a pixel restorer and a restoration discriminator; and 3, performing category prediction on the aero-engine borescope image data to be detected based on the trained BiGenAD network model to obtain whether the aero-engine borescope image data to be detected is a healthy image or an abnormal image.

The utility model relates to the technical field of borescopes, and provides a borescope device with a rotating head, which comprises a support, the top of the support is fixedly connected with a supporting rod, the side surface of the supporting rod is provided with an automatic rotating component, the automatic rotating component comprises a round rod, one end of the round rod is fixedly connected to the side surface of the supporting rod, and the other end of the round rod is fixedly connected with the rotating head. A round rod is fixedly connected to one end of the supporting rod, a detector is fixedly connected to one end of the round rod, a cylindrical rod is fixedly connected to the side face of the supporting rod, and a connecting line is arranged on the circumferential face of the cylindrical rod. The borescope can rotate as required, so that the time and energy for manually adjusting the lens are saved, the working efficiency is improved, the damage to equipment caused by strenuous movement or improper operation during manual adjustment can be reduced, and the service life of the borescope device is prolonged.