General Electric Company

Gregory Alan Mohr

Clifford Bueno

Brian W Lasiuk

Elizabeth Lokenberg Dixon

Walter Vincent Dixon, Iii

Michael Robert Hopple

Ronald Cecil McFarland

August David Matula

Forrest Frank Hopkins

Thomas William Birdwell

Thomas James Batzinger

Robert S Gilmore

Michael Kent Cueman

Robert J Mitchell, Jr

Kevin Layne Moermond

Gerald B Nightingale

Dale M Brown

Michael Evans Graham

Kenneth Gordon Herd

Yanfeng Du

Dean Michael Robinson

John Dennis Jackson

Peter S Allison

Elizabeth Lockenberg Dixon

Paul Francis Fitzgerald

Suneel Tumkur Shankarappa

Mysore Siddu Dinesh

Olalekan Solomon Odesanya

Kelly Mark Doyle

Dennis Michael Walsh

Kenneth Gordan Herd

Mark S Conradi

A method, system and apparatus for processing a radiographic image of a scanned object is disclosed. A pixel offset correction is performed in integer format on the radiographic image using saturation arithmetic to produce an image in integer format with any negative corrected values clipped to a value of zero. The resulting pixels are converted to floating point format and the converted pixels are multiplied by a gain factor. Optionally the resulting pixels are recursively averaged with previous results. The resulting pixels are converted to integer format and the converted pixel values are clamped to a maximum value using saturation arithmetic. Non-functional pixel correction is performed in integer format and the resulting pixel values are clamped to a maximum value using saturation arithmetic. An optional processing path replaces the recursive average by a linear average. The resulting pixel values are optionally filtered to enhance features of interest. The resulting pixel value is mapped in integer format to a palette index to establish an output pixel intensity having one of many intensity levels. The optional processing is controlled through the hardware interface of a real-time image controller as images are acquired.

Method, system and apparatus for processing radiographic images of scanned objects

A method and program product for real-time correction of non-functioning pixels in digital radiography, where the method comprises: receiving a list of non-functioning pixels; determining which neighboring functioning pixels are needed to correct the non-functioning pixels; organizing those neighboring functioning pixels and corresponding non-functioning pixels into a plurality of groups by a number of pixels used to perform correction; and performing correction of data from non-functioning pixels within one of the plurality of groups and subsequently performing correction of data from non-functioning pixels within another one of the plurality of groups. Also, a method and program product for producing an accurate real-time map of non-functioning pixels in a detector panel for digital radiography, where the method comprises: determining a first list of non-functioning pixels found using an extended exposure mode of the detector panel; determining a second list of non-functioning pixels found using a real-time mode of the detector panel; and merging the first and second lists into a merged list of non-functioning pixels for the detector panel.

Method of real-time correction of non-functioning pixels in digital radiography

A system and method for identifying flaws in a part being inspected includes generating a 3-d representation of the part, the 3-d representation comprising 3-d spatial coordinates corresponding to different locations on the part, and registering the 3-d spatial coordinates with corresponding locations of a part being inspected. An image of the part being inspected is generated, and a flaw in the part being inspected is identified from the generated image. A location of the flaw is correlated to a corresponding 3-d spatial coordinate, and a device is controlled to perform an operation on the part being inspected at the flaw location using information of the corresponding 3-d spatial coordinate.

System and method for analyzing and identifying flaws in a manufactured part

An energy discrimination radiography system includes at least one radiation source configured to alternately irradiate a component with radiation characterized by at least two energy spectra, where the component has a number of constituents. At least one radiation detector is configured to receive radiation passing through the component and a computer is operationally coupled to the detector. The computer is configured to receive data corresponding to each of the energy spectra for a scan of the component, process the data to generate a multi-energy data set, and decompose the multi-energy data set to generate material characterization images in substantially real time. A method for inspecting the component includes irradiating the component, receiving a data stream of energy discriminated data, processing the energy discriminated data, to generate a multi-energy data set, and decomposing the multi-energy data set, to generate material characterization images in substantially real time.

Energy discrimination radiography systems and methods for inspecting industrial components

A system and method for high-speed radiographic inspection of fluid transport vessels in which a radiation source and a radiation detector are positioned on opposite sides of the outside surface of the vessel. A positioning system is provided for moving and locating the radiation source and radiation detector longitudinally with respect to the vessel and for moving the radiation source and radiation detector circumferentially with respect to the vessel. In operation, the positioning system causes the radiation source and radiation detector to spiral along the vessel in a coordinated manner while the radiation source illuminates an adjacent region of the vessel with radiation. The radiation is converted into corresponding electrical signals used to generate images of objects in the radiation path. Finally, an operator inspects the images for defects.

High speed digital radiographic inspection of piping

A method ( ) for manufacturing a precision part ( ) utilizing a non-precision fixture ( ). The non-precision fixture is precisely measured ( ) and modeled in a CAD program ( ) together with a model of the part ( ). The part model is nested ( ) into the fixture model, and a transformation matrix describing the movement of a coordinate system of the part during the step of nesting is recorded ( ). The transformation matrix may then be used to transform ( ) a tool path that had been developed for the originally designed shape of the fixture. Accordingly, imprecision in the location of a part within an imprecisely measured fixture may be accounted for during subsequent manufacturing operations.

Method of manufacturing precision parts with non-precision fixtures

A method for inspecting an aircraft fuselage using an inspection system including a movable detector, wherein the method includes coupling a collision avoidance system to the inspection system detector, monitoring the collision avoidance system during operation of the inspection system, and controlling operation of the inspection system with the collision avoidance system.

Methods and systems for inspecting aircraft fuselage frames

An image identification and quality indication system for radiographic inspection includes a flexible substrate, for positioning on a surface of an object to be inspected, and a number of locators and image quality indicators arranged on the flexible substrate. Each locator is configured for indicating a position on the object's surface in a respective radiographic image (image). Each image quality indicator is configured to indicate an image quality of the respective image. An image identification and quality indication method for radiographic inspection includes positioning the flexible substrate on the object's surface, including aligning the locators with a number of visible features on object's surface. The method further includes forming at least one reference mark and image quality mark in each of a number of images of the object, using a locator and image quality indicator, respectively. Each reference mark correlates the respective image with a position on the object.

System and method for image identification and quality indication for radiographic inspection

An x-ray shielding system includes a beam controller configured to surround an x-ray source and includes a detector shield configured to position behind an x-ray detector. The beam controller includes a source shield and an aperture. The source shield and the detector shield are adapted to block x-rays, and the aperture is adapted to transmit x-rays. A shielded digital radiographic inspection system includes the x-ray source and the beam controller surrounding the x-ray source. The beam controller includes the source shield and the aperture. The aperture is configured to rotate around the x-ray source. The inspection system further includes a digital x-ray detector positioned radially outward from the x-ray source and facing the aperture. The digital x-ray detector is configured to be movable along an orbit around the x-ray source. The inspection system further includes the detector shield configured to be movable with and positioned behind the digital x-ray detector.

X-ray shielding system and shielded digital radiographic inspection system and method

A system and method for radiographic inspection of airfoil structure on aircraft includes a radiation source located on one side of the airfoil structure and an X-Y scanning device located on an opposing side of the airfoil structure. The X-Y scanning device is positioned to receive radiation from the radiation source. A radiation detector is mounted on the X-Y scanning device so as to be moveable relative to the airfoil structure along t two mutually orthogonal axes. In operation, the radiation detector is moved in a predetermined raster pattern while the radiation source is emitting radiation. This allows a large area to be inspected with single positioning of the X-Y scanning device, thereby improving throughput. The radiation detector converts impinging radiation into electrical signals, and a computer system processes the signals to generate radiographic images of the airfoil structure.

Method and apparatus for localized digital radiographic inspection

A system and method for radiographic inspection of aircraft fuselages includes a radiation source preferably located inside of the fuselage and a radiation detector preferably located outside of the fuselage. A source positioning system is provided for moving the radiation source longitudinally with respect to the fuselage, and a detector positioning system is provided for positioning the radiation detector in longitudinal alignment with the radiation source. The detector positioning system also moves the radiation detector circumferentially with respect to the fuselage. In operation, the radiation detector is moved over the fuselage in a circumferential direction while the radiation source illuminates an adjacent region of the fuselage with radiation.

High speed digital radiographic inspection of aircraft fuselages

A system and method for using the detector to differentiate neutron attenuating material from high x-ray attenuating material in an object. The inspection system is used to detect the presence of nitride in titanium sponge nuggets or residual core material in a hollow-cast turbine engine blades. The inspection system uses a dual radiation source to alternately emit neutrons and x-rays or gamma rays at the object under inspection. A dual modality gas ionization detector detects the radiation passing through the object and sends the detected radiation to a processing means for image generation. The generated image is displayed on a display, enabling objects formed with low and high attenuating material to be distinguished.

System and method for using a dual modality detector for inspecting

A dual modality gas ionization detector for differentiating neutron attenuating material from high x-ray attenuating material in an object. The dual modality gas ionization detector uses .sup.3 He and Xe gases pressurized in an ionization chamber to detect neutrons x-rays or gamma rays. The dual modality gas ionization detector is used in an inspection system for detecting, characterizing, or differentiating small amounts of neutron attenuating materials in objects composed primarily of materials of large attenuating x-ray material.

Dual modality detector

Methods and apparatus for monitoring and controlling cure cycles of composite structures utilize specialized NMR sensor (14) embedded into critical regions in the interior of composite structures (18) to provide in-situ cure state information. Signals developed by the NMR sensors (14) during the curing cycle are processed by an NMR spectrometer (30) to determine selected NMR parameters including T.sub.1, T.sub.2, T.sub.1D, and T.sub.2 * of the materials in the vicinity of the sensor, from which the rigidity of the materials are deduced. Experimental data show clear trends in values of particular NMR parameters taken as time series during cure cycles. Cure cycle control is accomplished using output data from an enhanced NMR spectrometer (30*) to drive temperature and pressure controllers (38, 42) of a curing oven (20*) for real time process control.

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Scotia, NY, United States of America

Gregory Alan Mohr