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ASTM E2662-2009

宇航设备中使用的平板复合物和夹层芯材放射性检查规程

Standard Practice for Radiologic Examination of Flat Panel Composites and Sandwich Core Materials Used in Aerospace Applications

适用范围:<p>Radiologic examination may be used during product and process design optimization, on line process control, after manufacture inspection, and in service inspection. In addition to verifying structural placement, radiologic examination can be used in the case of honeycomb core materials to detect node bonds, core-to-core splices, and core-to-structure splices. Radiologic examination is especially well suited for detecting sub-surface flaws. The general types of defects detected by radiologic examination include blown core, core corrosion, damaged filaments, density variation, entrapped fluid, fiber debonding, fiber misalignment, foreign material, fractures, inclusions, microcracks, node bond failure, porosity/voids, and thickness variation.</p> <p>Factors that influence image formation and X-ray attenuation in radiologic examination , and which are relevant to interpreting the images for the conditions of interest, should be included in the examination request. Examples are, but not limited to, the following: laminate (matrix and fiber) material, lay-up geometry, fiber volume fraction (flat panels); facing material, core material, facing stack sequence, core geometry (cell size); core density, facing void content, adhesive void content, and facing volume percent reinforcement (sandwich core materials); overall thickness, specimen alignment, specimen geometry relative to the beam (flat panels and sandwich core materials).</p><p id="s00002">1.1 This practice is intended to be used as a supplement to Practices E 1742<astmref rid="a00013">, E 1255<astmref rid="a00009">, and E 2033<astmref rid="a00017">.</p> <p id="s00003">1.2 This practice describes procedures for radiologic examination of flat panel composites and sandwich core materials made entirely or in part from fiber-reinforced polymer matrix composites. Radiologic examination is: <span class="italic">a</span>) radiographic (RT) with film, <span class="italic">b</span>) Computed Radiography (CR) with Imaging Plate, <span class="italic">c</span>) Digital Radiology (DR) with Digital Detector Array<span class=''unicode''>x2019;</span>s (DDA), and <span class="italic">d</span>) Radioscopic (RTR) Real Time Radiology with a detection system such as an Image Intensifier. The composite materials under consideration typically contain continuous high modulus fibers (> 20 GPa), such as those listed in 1.4.</p> <p id="s00004">1.3 This practice describes established radiological examination methods that are currently used by industry that have demonstrated utility in quality assurance of flat panel composites and sandwich core materials during product process design and optimization, process control, after manufacture inspection, in service examination, and health monitoring.</p> <p id="s00005">1.4 This practice has utility for examination of flat panel composites and sandwich constructions containing but not limited to bismaleimide, epoxy, phenolic, poly(amide imide), polybenzimidazole, polyester (thermosetting and thermoplastic), poly(ether ether ketone), poly(ether imide), polyimide (thermosetting and thermoplastic), poly(phenylene sulfide), or polysulfone matrices; and alumina, aramid, boron, carbon, glass, quartz, or silicon carbide fibers. Typical as-fabricated geometries include uniaxial, cross ply and angle ply laminates; as well as honeycomb core sandwich constructions.</p> <p id="s00006">1.5 This practice does not specify accept-reject criteria and is not intended to be used as a means for approving flat panel composites or sandwich core materials for service.</p> <p id="s00007">1.6 To ensure proper use of the referenced standards, there are recognized nondestructive testing (NDT) specialists that are certified according to industry and company NDT specifications. It is recommended that a NDT specialist be a part of any composite component design, quality assurance, in service maintenance or damage examination.</p> <p id="s00008">1.7 <span class="italic">Thi......

实施日期: 2009-06-01

中标分类号: V15 - 航空、航天 - 复合材料与固体燃料

ICS分类号: 49.025.01 - 航空器和航天器工程 - 航空航天制造用材料综合

标准组织: ASTM - 美国材料与试验协会标准

全文来源: WF

英文关键词: aerospace composites, Computed Radiology (CR) digital detector array (DDA) digital radiology (DR) fiber-reinforced polymer matrix composites flat panels high modulus fibers high performance composites honeycomb core laminates nondestructive evaluation (NDE) nondestructive inspection (NDI) nondestructive testing (NDT) polymeric matrix composites (PMC) radiography (RT) radioscopy (RTR) sandwich core materials sandwich constructions structural sandwich constructions

语种: 汉语

页数: 5

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