ASD-STAN PREN 2002-16-2000 Aerospace Series Metallic Materials Test Methods Part 16 Non-Destructive Testing Penetrant Testing (Edition P 1)《航空航天系列 金属材料试验方法 第16部分 无损检验 渗透检验 第P1版》.pdf

1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 2000-01-31 prEN 2002-16 Edition P I January 2000 Comments should be sent within six months after the date of publication to AECMA Guiledelle 94 8-1200 BRUXELLES PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA

2、) Gulledelle 94 - 8-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 11 ICs: Descriptors: ENGLISH VERSION Aerospace series Metallic materials Test methods Part 16: Non-destructive testing Penetrant testing Srie arospatiale Matriaux mtalliques Mthodes dessais Partie 16: Essais non destr

3、uctifs Examen par ressuage Luft- und Raumfahrt Metallische Werkstoffe Prfverfahren Teil 16: Zerstrungsfreie Prfung Eindringprfung This “Aerospace Series Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper

4、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 an extent that interchangeability is affec

5、ted, physically or functionally, without re-identification of the standard. Affer 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 European Standard to CEN (European Committee f

6、or Standardization) for formal vote. Nota - Extra cooies can be SUDOlkd bv B.N.A.E. - Technooolis 54 - 199. rue Jean-Jacaues Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX C5 Chairman Mr Evetts I I aecma 2000 COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information

7、 Handling ServicesSTD-AECMA PREN 2flOZ-Lb-ENLL 2CllIO m 1012311 LlUd74L3 371 M Page 2 prEN 2002-16: 2000 Contents O Introduction . v) C Ln ._ 30 20 10 O 400 450 500 550 600 650 700 750 800 Wavelength (nml Figure IA - CIE photocopic luminosity curve COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling Services