ASTM G124-1995(2003) Standard Test Method for Determining the Combustion Behavior of Metallic Materials in Oxygen-Enriched Atmospheres《在富氧环境中金属材料燃烧特性的测定标准试验方法》.pdf
《ASTM G124-1995(2003) Standard Test Method for Determining the Combustion Behavior of Metallic Materials in Oxygen-Enriched Atmospheres《在富氧环境中金属材料燃烧特性的测定标准试验方法》.pdf》由会员分享,可在线阅读,更多相关《ASTM G124-1995(2003) Standard Test Method for Determining the Combustion Behavior of Metallic Materials in Oxygen-Enriched Atmospheres《在富氧环境中金属材料燃烧特性的测定标准试验方法》.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: G 124 95 (Reapproved 2003)Standard Test Method forDetermining the Combustion Behavior of Metallic Materialsin Oxygen-Enriched Atmospheres1This standard is issued under the fixed designation G 124; the number immediately following the designation indicates the year oforiginal adoption or
2、, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.1. Scope1.1 This test method covers a test apparatus and techniqueto determine the minimum
3、 test gas pressure that supportsself-sustained combustion (the threshold pressure) and theaverage regression rate (apparent burn rate) of a standardizedsample of a metallic material that has been ignited using astrong promoter.1.2 The data obtained from this test method are dependenton the precise t
4、est sample configuration and provide a basis forcomparing the combustion behavior of materials. No criteriaare implied for relating these data to the suitability of amaterials use in any actual system. The application of dataobtained from this test method is discussed in Guides G 88 andG 94.1.3 Requ
5、irements for an apparatus suitable for this testmethod are given, as well as an example of such an apparatus.The example, however, is not required to be used.1.4 This test method is for gaseous oxygen or any mixtureof oxygen with diluents that will support combustion, at anypressure within the capab
6、ilities of the apparatus.1.5 The values stated in SI units are to be regarded as thestandard. The values given in parentheses are for informationonly.1.6 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this
7、standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use. Specific hazardsstatements are given in Section 9.2. Referenced Documents2.1 ASTM Standards:G 88 Guide for Designing Systems for Oxygen Service2G 93 Practice for Cl
8、eaning Methods for Material andEquipment Used in Oxygen-Enriched Environments2G 94 Guide for Evaluating Metals for Oxygen Service22.2 Federal Specification:BB-0-925 Oxygen, Technical, Gas and Liquid32.3 Military Standard:MIL-0-27210E Amendment 1Oxygen, Aviators Breath-ing, Liquid and Gas33. Terminol
9、ogy3.1 Definitions of Terms Specific to This Standard:3.1.1 average regression rate (apparent burn rate)theaverage rate at which the burning/solid-metal interface ad-vances along the test sample length.3.1.2 ignitera material to ignite the promoter that canburn under an electrical influence, such as
10、 a small-diameterwire.3.1.3 promotera material that can add supplemental heatand increase the temperature to start combustion of the materialbeing tested.3.1.4 self-sustained combustioncombustion that con-sumes a sample to the point at which the sample holder affectsfurther combustion (assuming suff
11、icient oxygen).3.1.5 threshold pressurethe minimum gas pressure (at aspecified oxygen concentration and ambient temperature) thatsupports self-sustained combustion of the entire standardsample.4. Summary of Test Method4.1 A small rod of the material is suspended in a chamberfilled with pressurized t
12、est gas. The chamber contains sufficientoxygen so that not more than 10 % of the oxygen will beconsumed when the material combusts completely. A promoter(typically aluminum or magnesium) applied to the bottom ofthe rod starts combustion of the material. The test pressure is1This test method is under
13、 the jurisdiction of ASTM Committee G4 onCompatibility and Sensitivity of Material in Oxygen Enriched Atmospheres and isthe direct responsibility of Subcommittee G04.01 on Test Methods.Current edition approved Feb. 15, 1995. Published August 1995. Originallypublished as G 124 94. Last previous editi
14、on G 124 94.2Annual Book of ASTM Standards, Vol 14.02.3Available from Standardization Documents Order Desk, Bldg 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5094, Attn: NPODS.TABLE 1 Example Data Set for Type 316 Stainless SteelAMaterial Pressure, MPaNumber of SamplesPartial Burn Complete B
15、urnUNS 31600 1.75 10 03.45 8 26.90 0 10AThese data were produced at NASA White Sands Test Facility, New Mexico,880041Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.reduced and another rod is tested if combustion of the entirerod occu
16、rs. This continues until self-sustained combustion ofthe rod does not occur for at least five tests at one pressure. Thelowest pressure at which self-sustained combustion occurred isthe threshold pressure for the material, and the differencebetween it and the highest pressure level that produced onl
17、yincomplete combustion is the margin of potential error. Astuteinitial estimates of the threshold can reduce the amount oftesting necessary to demonstrate the threshold to within therequired uncertainty.5. Significance and Use5.1 This test method will allow comparisons of the combus-tion characteris
18、tics of various metallic materials. The combus-tion characteristics that can be evaluated include (1) thresholdpressure and (2) average regression rate (apparent burn rate) ofthe sample.6. Interferences6.1 Any internal materials that may bake out or vaporizeduring the combustion process at test temp
19、erature/pressuremay interfere with the chemistry of the fire propagation.6.2 The specific atmosphere in the test chamber can have asevere effect. Therefore, alien air, argon, nitrogen, carbondioxide, moisture, and others can be important interferinggases.6.3 The test is conducted under stagnant cond
20、itions. Aflowing system or one that facilitates buoyant convectivecurrents may be a significantly more severe climate.6.4 The specific temperature of the test sample prior toignition can have an important effect.NOTE 1The promoters discussed in this test method have producedfavorable results over a
21、wide range of metal test specimens with thedegree of precision sought to date. As the threshold is approached or wheninteraction between promoter and metal occur promoter can thwart theignition process. Hence the prospect that future work may refine thepromoter and enable the measurement of lower th
22、resholds than aremeasurable today cannot be ruled out.7. Apparatus7.1 A schematic of a typical system is shown in Fig. 1.Other designs may also be used, if they fulfill the requirementsbelow.7.2 Test ChamberA cross-section of a typical stainlesssteel test chamber is shown in Fig. 2. No more than 10
23、% of theavailable oxygen should be consumed during a test. AppendixX1 provides criteria for establishing the lowest test pressuresthat meet this criterion for various vessel volumes. If thechamber cannot be made sufficiently large, an accumulator canbe attached that contains more test gas if the cha
24、mber cannot bemade sufficiently large; however, this is not as severe a testenvironment as in the larger vessel. The test chamber shall notcontribute any chemical interference to testing.NOTE 2The addition of an accumulator can act as a snubber tosuppress pressure rises that occur due to temperature
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