Browse Topic: X-ray inspections

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Lithium-ion batteries now in widespread use for everything from mobile electronics to electric vehicles rely on a liquid electrolyte to carry ions back and forth between electrodes within the battery during charge and discharge cycles. The liquid uniformly coats the electrodes, allowing free movement of the ions.
Scientists have demonstrated the use of artificial intelligence (AI) to speed up the process of reconstructing images from coherent X-ray scattering data. Traditional X-ray imaging techniques (like medical X-ray images) are limited in the amount of detail they can provide. This has led to the development of coherent X-ray imaging methods that are capable of providing images from deep within materials at a few nanometer resolution or less. These techniques generate X-ray images without the need for lenses by diffracting or scattering the beam off of samples and directly onto detectors.
In the circuit board industry, an increasing number of parts and boards are proving to be difficult to inspect with automated optical inspection (AOI) because the solder is invisible. Furthermore, high-quality requirements such as bonding strength of the automobile industry and full surface inspection of the solder are increasing. To address these needs, Omron has introduced new technology for accomplishing inspections within the required inline take time (the rate at which a product must be completed to meet customer demand). This has been one of the most challenging requirements for computed tomography (CT) X-ray automatic inspection equipment. For continuous imaging technology, highly accurate positioning control and high-speed image sensing are required.
Composite materials for aerospace & defense continue on a path of market growth fueled by tightening environmental and economic targets. This trend is occurring alongside rapid innovations in design, manufacturing, automation and cost reduction. Although slowed by the global pandemic, the increasing role of composites for many industries is, in fact, a foregone conclusion. More and more, composites performance-expressed in the elegant functionality of a curved wingtip on an airliner or in the fewer, thinner, winding fan blades of a GE9X engine-demonstrate an accelerating freedom-of-form and utility that makes composites essential to the future.
This standard defines general requirements for spherical, radial-journal, conical, and thrust bearings which are of laminated elastomeric construction. These bearings are for use in an environment having a temperature spectrum of -65 to +160 °F while reacting steady state loads in addition to oscillating loads and motions. The operating temperature range of -65 to +160 °F reflects the current temperature range for existing parts, but allows for expansion in the future.
ACBG Plain Bearing Committee
This document establishes the requirements for screening, qualification, and lot acceptance testing of Plastic Encapsulated Discrete Semiconductors (PEDS) for use in space application environments. The scope of this document is intended for standard silicon based technology only, but the process and methodology described within can be adopted for other technologies such as Silicon Carbide, Gallium Nitride, and Gallium Arsenide. However, when non-silicon based technology parts are being used, the device characterization shall be modified, and it is recommended to use available industry standards based upon published research/testing reports for those technology to address applicable physics of failure.
CE-12 Solid State Devices
This document contains information and guidance on the use of Pb-free ball grid arrays (BGAs) in an aerospace, defense, and high performance (ADHP) product, or other products which demand a high reliability.
G-24 Pb-free Risk Management Committee for ADHP
This document establishes common industry practices and recommended screening, qualification, and lot acceptance testing of Plastic Encapsulated Microcircuits (PEMs) for use in space application environments.
CE-12 Solid State Devices
This specification covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.
AMS G Titanium and Refractory Metals Committee
This SAE Aerospace Standard standardizes practices to: a identify reliable sources to procure parts, b assess and mitigate risk of distributing fraudulent/counterfeit parts, c control suspect or confirmed fraudulent/counterfeit parts, d and report suspect and confirmed fraudulent/counterfeit parts to other potential users and Authority Having Jurisdiction.
G-19 Counterfeit Electronic Parts Committee
This document provides background information on the design, application, repair and inspection of composite structures, including metal bonding, used on civil transport aircraft. The objective of this document is to assist inspectors to know where to expect composite and metal bonded parts on the aircraft, to understand the capabilities of current NDT methods and to aid interpretation of inspection results. This document does not contain inspection procedures. It is intended to be informative and should not be used singularly, that is, it does not override any instructions that may be issued within a manufacturer's or operator's published documentation.
AMS CACRC Commercial Aircraft Composite Repair Committee
Production Uses of Computed Tomography - Samples in an Aluminum Foundry2006-01-05104/3/2006
Cast parts are traditionally inspected prior to initial production runs and subsequently in support of high volume production to ensure consistent quality and accurate dimensions that match the “as designed” part within specified tolerances. Classical methods for dimensional measurements are CMM systems using touch probes, laser sensors, or optical techniques. Flaw conditions such as cracks, porosity and inclusions can be detected with “real-time” x-ray inspection. These techniques are quite effective on simple parts with two dimensional geometry and non-complicated structures. Specialized x-ray inspection systems for alloy wheel production are examples of such systems. Complex three dimensional castings such as cylinder heads and engine blocks have functional internal structures with close tolerances and morphology that cannot be verified by CMM systems externally or by real-time x-ray. Computed Tomography (CT) has developed as an industrial measurement and quality assurance tool that simultaneously captures surface information and flaw conditions in complex three dimensional castings. The CT process is described for a typical industrial part examination in support of First Article Inspection. A stack of slices is collected in a process that requires 4 to 15 hours using automated system operation. The resulting stack of hundreds of grey level images is converted to an STL surface model of the part containing all dimensions and flaw information. The STL model of the actual part is then registered with the CAD model of the same part to produce a variance map showing the difference between the two as a colour coded model that can be viewed at any angle or sectioned to see internal details. The total analysis time ranges between one to three hours, depending on the type of part, but can be reduced for repetitive inspection of production parts. The CT technology described here is used successfully in Volkswagen foundry Hanover for inspection of prototypes, modified ingot molds, cores and modification of shooting tools in core shooting machines.
Smith, Charles R.Bischoff, UweGeorgi, BerndHansen, FerdinandJeltsch, FrankVoigt, Patrick
Two-stage shot peening was performed on engine valve spring prototypes in order to increase their fatigue strength, thereby decreasing the percentage of fatigue failures originating on valve spring surfaces. The two-stage shot peening comprises a high-arc-height shot peening as the first stage and a low arc height shot peening as the second one. Two types of prototypes were prepared, those processed by ordinary one-stage shot peening and those processed by the two-stage shot peening. The residual stress distribution of each of the prototypes was measured by the X-ray inspection, the fatigue testing was carried out on each of them. It is confirmed that an effective residual stress distribution provided by the two-stage shot peening improves the fatigue strength of engine valve springs. The performance of the two-stage shot peening allows high residual compression stress distribution not only on the surfaces but also on the insides. The effect of residual stresses in such distribution provides fatigue strength higher than that obtained by the use of the ordinary one-stage shot peening, which prevents the failures from originating on the surfaces, thereby prolonging the lives.
KURIHARA, Yoshiaki
This specification covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.
AMS G Titanium and Refractory Metals Committee
The figure depicts an apparatus for measuring x-ray diffraction (XRD) and/or x-ray fluorescence (XRF) in a specimen of material. The specimen could be, for example, a standard XRD powder sample of a mineral, the elemental composition of which one seeks to identify. It is common practice to characterize samples in terms of both XRD and XRF, but heretofore, it has been necessary to use separate XRD and XRF apparatuses.
X-ray-based Computed Tomography (CT) has been linked with finite-element analysis to provide a capability for structural characterization of as-manufactured parts— especially for the nondestructive evaluation of metal-matrix composite (MMC) material parts. In some cases, this capability might eventually obviate costly experiments, including destructive experiments that are traditionally performed to determine mechanical responses. Though developed primarily for MMCs, this capability could also be applied to other types of composites, metal forgings and castings, and plastic components.
This specification covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.
AMS G Titanium and Refractory Metals Committee
AMS K Non Destructive Methods and Processes Committee
AMS K Non Destructive Methods and Processes Committee
This specification establishes the requirements for the (TBS) jet fuel starter for the (TBS) gas turbine engine used in the (TBS) aircraft.
AE-6 Starting Systems and Auxiliary Power Committee
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