ASTM F2156-2011 Standard Test Method for Measuring Optical Distortion in Transparent Parts Using Grid Line Slope《利用坐标线斜率测量透明部件中光学失真的标准试验方法》.pdf
《ASTM F2156-2011 Standard Test Method for Measuring Optical Distortion in Transparent Parts Using Grid Line Slope《利用坐标线斜率测量透明部件中光学失真的标准试验方法》.pdf》由会员分享,可在线阅读,更多相关《ASTM F2156-2011 Standard Test Method for Measuring Optical Distortion in Transparent Parts Using Grid Line Slope《利用坐标线斜率测量透明部件中光学失真的标准试验方法》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: F2156 11Standard Test Method forMeasuring Optical Distortion in Transparent Parts UsingGrid Line Slope1This standard is issued under the fixed designation F2156; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year
2、 of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 When an observer looks through an aerospace transpar-ency, relative optical distortion results, specifically in th
3、ick,highly angled, multilayered plastic parts. Distortion occurs inall transparencies but is especially critical to aerospace appli-cations such as combat and commercial aircraft windscreens,canopies, or cabin windows. This is especially true duringoperations such as takeoff, landing, and aerial ref
4、ueling. It iscritical to be able to quantify optical distortion for procurementactivities.1.2 This test method covers the apparatus and proceduresthat are suitable for measuring the grid line slope (GLS) oftransparent parts, including those that are small or large, thin orthick, flat or curved, or a
5、lready installed. This test method isnot recommended for raw material.1.3 The values stated in SI units are to be regarded asstandard. No other units of measurement are included in thisstandard.1.3.1 ExceptionThe values given in parentheses are forinformation only.1.4 This standard does not purport
6、to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:2E177 Pr
7、actice for Use of the Terms Precision and Bias inASTM Test MethodsE691 Practice for Conducting an Interlaboratory Study toDetermine the Precision of a Test MethodF733 Practice for Optical Distortion and Deviation ofTransparent Parts Using the Double-Exposure MethodF801 Test Method for Measuring Opti
8、calAngular Deviationof Transparent Parts3. Terminology3.1 Definitions of Terms Specific to This Standard:3.1.1 design eye, nthe reference point in aircraft designfrom which all anthropometrical design considerations aretaken.3.1.2 distortion, nthe rate of change of deviation resultingfrom an irregul
9、arity in a transparent part.3.1.2.1 DiscussionDistortion shall be expressed as theslope of the angle of localized grid line bending, for example,1 in 5 (see Fig. 1).3.1.3 grid board, nan optical evaluation tool used todetect the presence of distortion in transparent parts.3.1.3.1 DiscussionThe grid
10、board is usually, but notalways, a vertical rectangular backboard with horizontal andvertical intersecting lines with maximum contrast between thewhite lines and the black background.3.1.4 grid line slope, nan optical distortion evaluationparameter that compares the slope of a deviated grid line to
11、thatof a nondeviated grid line.3.1.4.1 DiscussionThe degree of deviation shall be indi-cated by a ratio, for example, 1 in 2, 1 in 8, or 1 in 20 (thevisual optical quality improves as the second number getslarger.)3.1.5 installed angle, nthe transparency orientation asinstalled in the aircraft, defi
12、ned by the angle between ahorizontal line (line of sight) and a plane tangent to the surfaceof the transparency (see Fig. 2).3.1.6 repeatability limit (rL), nfrom Practice E177,27.3.2, “approximately 95 % of individual test results fromlaboratories similar to those in an Inter-laboratory Study (ILS)
13、can be expected to differ in absolute value from their averagevalue by less than 1.96s (about 2s).”3.1.6.1 Discussionin terms of this test method, approxi-mately 95 % of all pairs of replications from the sameevaluator and the same photo differ in absolute value by lessthan the rL.1This test method
14、is under the jurisdiction of ASTM Committee F07 onAerospace and Aircraft , and is the direct responsibility of Subcommittee F07.08 onTransparent Enclosures and Materials.Current edition approved Dec. 1, 2011. Published January 2012. Originallyapproved in 2001. Last previous edition approved in 2006
15、as F2156 - 06. DOI:10.1520/F2156-11.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.1Copyright ASTM Internati
16、onal, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.3.1.7 reproducibility limit (RL), nfrom Practice E177,27.3.3, “approximately 95 % of all pairs of test results fromlaboratories similar to those in the study can be expected todiffer in absolute value by less t
17、han 1.960=2s (about 2.0=2s)= 2.77s (or about 2.8s). This index is also known as the 95 %limit on the difference between two test results.”FIG. 1 Optical Distortion Represented By TangentFIG. 2 Schematic Diagrams of GLS Photographic Recording DistancesF2156 1123.1.7.1 Discussionin terms of this test
18、method, approxi-mately 95 % of all pairs of replications from different evalua-tors and the same photo differ in absolute value by less than theRL.4. Summary of Test Method4.1 The transparent part shall be mounted, preferably at theinstalled angle, at a specified distance from a grid board testpatte
19、rn. A photographic camera shall be placed so as to recordthe grid pattern as viewed through the part from the design eye(or other specified) viewing position. If the viewing position isnot defined, the values in Table 1 may be used as photographictest geometry. The image is then analyzed to assess t
20、he level ofoptical distortion as measured by grid line slope.4.2 Distortion shall be recorded using either a single-exposure photograph or a double-exposure photograph. Thephotographed grid shall then be measured using either adrafting machine procedure or a manual procedure. Eachprocedure has its o
21、wn level of precision.5. Significance and Use5.1 Transparent parts, such as aircraft windshields, cano-pies, cabin windows, and visors, shall be measured for com-pliance with optical distortion specifications using this testmethod. This test method is suitable for assessing opticaldistortion of tran
22、sparent parts as it relates to the visualperception of distortion. It is not suitable for assessing distor-tion as it relates to pure angular deviation of light as it passesthrough the part. Either Test Method F801 or Practice F733 isappropriate and shall be used for this latter application. Thistes
23、t method is not recommended for raw material.6. Apparatus6.1 Test RoomThe test room shall be large enough tolocate the required testing equipment properly.6.1.1 Setup A requires a room approximately 12 m (40 ft)long.6.1.2 Setup B requires a room approximately 7 m (23 ft)long.6.1.3 Setup C: other dis
24、tances shall be used if desired. GLSresults will vary with different distances, which means thatmeasurements of different parts taken at different distancescannot be compared.6.1.4 The walls, ceiling, and floor shall have low reflec-tance. A flat black paint or coating is preferred though notrequire
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