REG NASA-LLIS-0801--2000 Lessons Learned Advanced Computed X-Ray Tomography.pdf
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1、Best Practices Entry: Best Practice Info:a71 Committee Approval Date: 2000-04-17a71 Center Point of Contact: MSFCa71 Submitted by: Wil HarkinsSubject: Advanced Computed X-Ray Tomography Practice: Use advanced computed X-ray tomography as a precision method of materials characterization and defect lo
2、cation to ensure high reliability of aerospace hardware and conformance to design requirements. Employ this sophisticated and proven technology for nondestructive evaluation (NDE) of materials and structures. Assure the adherence to established precautionary measures during tomography operations.Pro
3、grams that Certify Usage: This practice has been used on Solid Rocket Motor (SRM), Space Shuttle Main Engine (SSME), Solid Propulsion Integrity Program (SPIP), Modified NASA Motor Program, Sub-Scale Solid Rocket Combustion Simulator, other aerospace and aerospace-related applications.Center to Conta
4、ct for Information: MSFCImplementation Method: This Lesson Learned is based on Reliability Practice number PT-TE-1436 from NASA Technical Memorandum 4322A, NASA Reliability Preferred Practices for Design and Test.Benefit:Advanced computed X-ray tomography can be used to produce both two-dimensional
5、and three-dimensional images of structures, materials, parts, and components. These images are providing Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-information that is useful for inspection, evaluation, and diagnostics of complex hardware.Implem
6、entation Method:1. General Description of the Process:Advanced computed X-ray tomography uses high intensity X-ray sources, sensitive electronic detectors, sophisticated computer control and analysis techniques, and automated manipulation systems capable of translating and rotating test objects, to
7、produce cross-sectional images of precision aerospace components. A system block diagram is shown on Figure 1. This test method can be used to verify tolerances, to determine relative material densities, to locate inclusions or defects, and to measure the extent of erosion and ablation in composite
8、materials. The equipment and procedure is applicable to metals (up to 10 inches thick) composites, or combination metal/composite structures varying from 2 inches to 50 inches in diameter (depending on the material density) and weighing up to 3700 pounds.refer to D descriptionD Figure 1: Advanced Co
9、mputed X-ray Tomography Basic System Block Diagram Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Cross-sectional images, generated by rotating and translating test objects slowly in an X-ray source, produce accurate representations of thin slices o
10、f the test object. It takes 20 minutes to produce an image of a thin slice for a typical SRM nozzle. To form a three-dimensional image of the internal structure of the nozzle, 150 to 250 slice images are acquired and stacked. The entire process is controlled remotely by computer. Operational personn
11、el are located external to the test cell. To prevent personnel contact with harmful X-radiation sources or environment, there are safety precautions that include constant dosage monitoring of stray/exposure radiation.A principal use of advanced computed X-ray tomography at MSFC has been evaluation o
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