ASD-STAN PREN 3976-1999 Aerospace Series Titanium and Titanium Alloys Test Method Chemical Analysis for the Determination of Hydrogen Content (Edition P 1)《航空航天系列 钛和钛合金试验方法 氢含量测定的化.pdf
《ASD-STAN PREN 3976-1999 Aerospace Series Titanium and Titanium Alloys Test Method Chemical Analysis for the Determination of Hydrogen Content (Edition P 1)《航空航天系列 钛和钛合金试验方法 氢含量测定的化.pdf》由会员分享,可在线阅读,更多相关《ASD-STAN PREN 3976-1999 Aerospace Series Titanium and Titanium Alloys Test Method Chemical Analysis for the Determination of Hydrogen Content (Edition P 1)《航空航天系列 钛和钛合金试验方法 氢含量测定的化.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 1999-04-30 prEN 3976 Edition P 1 April 1999 Comments should be sent within six months after the date of publication to AECMA Gu!ledelle 94 8-1200 BRUXELLES PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gul
2、ledelle 94 - 8-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 11 ICs: Descriptors: ENGLISH VERSION Aerospace series Titanium and titanium alloys Test method Chemical analysis for the determination of hydrogen content Srie arospatiale Titane et alliages de titane Mthode dessai Analyse
3、 chimique pour dtermination de la teneur en hydrogne Luft- und Raumfahrt Titan und Titanlegierungen Versuchsmethode Chemische Analyse zur Bestimmung des Wasserstoffanteils This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace I
4、ndustries). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to
5、an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft Euro
6、pean Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra cooies can be suoolied bv B.N.A.E. - TechnoDolic 54 - 199. rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX C5 Chairman Mr Evetts aecma 1999 STD-AECMA PREFI 377b-ENGL 1799 S LO123Ll OOLbL04 IT3 S P
7、age 2 prEN 3976: 1999 Contents Page O Introduction I Scope 2 Normative references 3 Definitions 4 Health and safety 5 Principle 6 Testing requirements 7 Test report Annex A (informative) STD-AECMA PREN 397b-ENGL 1999 LOL23Ll 001bL05 D3T I Page 3 prEN 3976: 1999 O Introduction This standard is part o
8、f the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. 1 Scope This standard specifies the requirements for chemical analysis using Inert Gas Fusion Thermal Conductivity Method for the determination of the hydrogen
9、content of titanium and titanium alloys for aerospace applications. The method applies to hydrogen contents ranging from several micrograms per gram to several hundreds of micrograms per gram. It shall be applied when referred to in the EN technical specification or material standard unless otherwis
10、e specified on the drawing, order or inspection schedule. The absolute method not used in routine inspection is solid state hot extraction under vacuum NOTE 1 followed by measurement of volume and pressure. Due to its complexity, it is only summarized in Annex A. 2 Normative references This European
11、 standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated reference, subsequent amendments to or revisions of any of these publications apply
12、 to this European standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 Guide 30: 1992 IS0 Guide 31: 1981 IS0 Guide 35: 1989 EN 2003-1 O EN 4258 EN 4259 Terms and Definitions Used in Connection with Refer
13、ence Materials Contents of certificates of reference materials Certification of reference materials - General and statistical principles Aerospace series - Titanium and titanium alloys - Test methods - Part IO: Sampling for determination of hydrogen content 1) Aerospace series - Metallic materials -
14、 General organization of standardization - Links between types of EN standards and their use Aerospace series - Metallic materials - Definition of general terms 2) 3 Definitions For the purposes of this standard, the following definitions apply: Definition of general terms: see EN 4259. Definition o
15、f certified reference material (C.R.M.): see IS0 Guide 30. 1) Published as AECMA Prestandard at the date of publication of this standard 2) In preparation at the date of publication of this standard Page 4 prEN 3976: 1999 Method 1 2 4 Health and safety Extraction Mode Temperatu re Supporting Gas Wit
16、h flux 1800 “C Nitrogen or Argon 2 100 “C Argon Without flux Resources, test pieces, test samples, test materials, test equipment and test procedures shall comply with the current health and safety regulations/laws of the countries where the test is to be carried out. Where materials and/or reagents
17、 which may be hazardous to health are specified, appropriate precautions in conformity with local regulations and/or laws shall be taken. 5 Principle The test consists of thermally decomposing the hydrogenated compounds (mostly as metallic hydrides) present in the titanium or titanium alloys. The de
18、gassed hydrogen is sent, in a stream of supporting inert gas, into the detection system (thermal conductivity cell) which allows a quantitative measurement of hydrogen content (comparative). Two extraction modes are considered, with respect to the use (or not) of a melting flux. (Table 1). 5.1 Metho
19、d 1 The role of melting flux is to liquefy the mixture (thus facilitating the gas extraction) and to avoid an eventual formation of nitrides. Fusion is performed in a graphite crucible at a temperature of around 1 800 OC: - either in a nitrogen supporting gas which allows the nitrogen in the sample
20、to be disregarded with the carbon monoxyde which, with the nitrogen, has a very small difference in conductivity. (The excess of carbon and the temperature at which melting is performed prevents any carbon dioxyde from forming; it is necessary, however, to foresee a way of trapping small quantities
21、of this gas eventually present by using, for example, a molecular sieve); - or in an argon supporting gas which prevents nitrides forming and results in a better sensitivity since argon has a greater difference in conductivity compared to hydrogen. A separation of nitrogen and carbon oxides is neces
22、sary as well as, in the case of using a high frequency furnace, an adapted frequency to avoid discharges by ionization. 5.2 Method 2 Fusion is performed in a graphite crucible at a temperature of around 2 100 “C and shall be carried out in an argon supporting gas (nitrogen in this case would cause f
23、ormation of nitrides). 6 Testing requirements 6.1 Resources 6.1.1 Equipment There are numerous models of apparatus but they all generally include the following elements: - Device for introducing samples; - Heating device (induction furnace or resistance furnace); - Sweeping system using supporting g
24、as; Page 5 prEN 3976: 1999 - System for separating gases (if necessary); - Thermal conductivity cell. Where a high frequency furnace is used with an argon supporting gas, the frequency shall be adapted to avoid discharges by ionization. 6.1.2 MateriaMReagents 6.1.2.1 According to IS0 Guides 31 and 3
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