1、STDSAECMA PRE! 2407-ENGL 1778 W LL7123Ll 0015L87 872 E AECMA STANDARD NORME AECMA AECMA NORM prEN 2407 Edition 2 December 1998 ICs: Descriptors: PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 8-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 AL
2、LIAGE RSISTANT A CHAUD MIS EN SOLUTION ET PRCIPIT TLES ET BANDES a I3 mm A BASE DE NICKEL NI-P1 00-HT SRIE AROSPATIALE Supersedes edition 1 May 1980 ENGLISH VERSION HEAT RESISTING NICKEL SOLUTION TREATED AND PRECIPITATION TREATED SHEETS AND STRIPS a I3 mm AEROSPACE SERIES BASE ALLOY NI-P100-HT LUFT-
3、 UND RAUMFAHRT HOCHWARMFESTE NICKELBASISLEGIERUNG NI-PI 00-HT AUSGEHRTET BLECHE UND BNDER a I3 mm This “Aerospace series“ Standard has been drawn up under the European Associa tion of A erospa ce In dus tries). It is published on yell0 w paper in three equivalen It will be submitted as a draft Europ
4、ean Stan for formal vote. of AECMA (The an). Standardization) I Replace page 1 of the previous edition by this page I Declassification approved 1998-12-31 The equivalent versions in French and German languages can be supplied by B.N.A.E. - Technopolis 54 - ISS, rue Jean-Jacques Rousseau 921 38 ISSY
5、- LES - MOULINEAUX CEDEX - FRANCE - aecrna 1998 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN2qO 80 = 1012311 00031L11 O m-, DRAFT ECIRWEA
6、N STANISUHU- AEROSPACE SEDSIES- HEAT RESISTING NICKEL BASE ALLOY NI-PlOO-HT Solution treated and precipitation treated Sheets and strips a 6 3 nun prEN2407 Page 3 Element Chemical omp position“) min. 1 I 2 3 4 L 5 - 6 - 7 8 I 9 10 11 12 13 14 15 16 19 L - - I- - s L is 19 20 21 22 23 24 26 26 1 I I
7、- - - - - n 1 2 I 3 I 4 Air xelt and vacum refine or Vacuum melt or ConsabILe electrode refiel5 Method Qf melting Farm Method of production Liinit dimensions 5.1 Lcceotance standards 5.2 Dieensional standarh Condition and Heat treatment Deliwy Solution treated and descaled Solution treated and preci
8、pitation treated Condition and Heat treatment uso DeliveZ=y condition i- 720 iO0C/t = 8 h/furnaee CQGL at 50*C/h to 620 f moc/ Bolding t r+ 8 h/A.r coo Delivery condftfom Condition of use d3 0,654 a53 Tost piece Heat treatment Sampling Dinmsions concerned Thlcknsss of claddinn on each face Direction
9、 of sample I Temperature Proof u, Stress c (0 Strength Elongation Reduction lof area E -c 795 3 1035 1 2 825 A % x .? HV Hardness ,Z 260 1- -I -I- RC u_ k K I_ MPa* I_ - J Shear Strength 88 nd i ng Impact - I 1 - tJ I 65 0 I r b 23 - _I_- - Tlme O. Stres L?I w U u Elongation h MPfP 5% _II Ruptura Is
10、tres MPe I 690 % _ Elongation 1 Notes 1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECIA PREN2407 80 m 3032333 0003342 2 m ; prEN2407 Page 4 ;rain
11、 size /dm lm Notes Typical use 2 3 4 .verage of 0,065 or iner with a maximum I f 0,125. 2 3 1) Bracketed figures ii?dl.cate composition expressed as parts per rclllicn (ppm). The method of analysis for lead, bisnuth and silver shall be agreed between manufacturer, arid purchaser. The method of melcing required shall be agreed between :nanufacturer arid parchaser. Ir1 prepara t ion. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
