AECMA PREN 2408-1980 Heat Resisting Nickel Base Alloy NI-P100-HT Solution Treated and Precipitation Treated Plates a Greater Than 3 mm Aerospace Series Edition 1《航空航天系列.镍基合金 NI-P10.pdf

《AECMA PREN 2408-1980 Heat Resisting Nickel Base Alloy NI-P100-HT Solution Treated and Precipitation Treated Plates a Greater Than 3 mm Aerospace Series Edition 1《航空航天系列.镍基合金 NI-P10.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2408-1980 Heat Resisting Nickel Base Alloy NI-P100-HT Solution Treated and Precipitation Treated Plates a Greater Than 3 mm Aerospace Series Edition 1《航空航天系列.镍基合金 NI-P10.pdf（3页珍藏版）》请在麦多课文档分享上搜索。

1、A.E.C.M.A. STANDARD NORME A.E.C.M.A. A.E.C.M.A. NORM DRAFT prEN2408 Edition 1 May 1980 ENGLISH VERSION HEAT RESISTING NICKEL SOLUTION TREATED AND PRECIPITATION TREATED PLATES a 3 mm AEROSPACE SERIES BASE ALLOY NI-P100-HT ALLIAGE RESISTANT A CHAUD MIS EN SOLUTION ET PRECIPITE PLAQUES a 3 rnrn SERIE A

2、EROSPATIALE A BASE DE NICKEL NI-P100-HT LUFT-UND RAUMFAHRT HOCHWARMFESTE NICKE LBASISL EGI ER U NG NI -P 100-Hf AUSGEHRTET PLATTEN a 3 mrn The text of this standard, which exists in three equivalent versions (English, French, German) has been drawn up under the responsibility of A ECMA (Association

3、Europenne des Constructeurs de Matriel Arospatial) and has been circulated to Official Services. Any reservations expressed by Official Services and not resolved in this issuefi have been incorporated in the history sheet which has accompanied this prEN to CEN. It ispublished on yellowpaper as a dra

4、ft European Standar intended to receive, under the same presentation and according to its own rules, the approval of CEN (European Committee for Standardization). Approvad by The eqillvalent versions in French and German langiiages can G.N.A.E., 8, rue Moreau-Vauthier 92100 BOULOGNE-BILLANCOURT - FR

5、ANCE. -Ip_ I_ 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-,-,-AE-CMA PRENZ?Cl!_ampling Delivery condition 9 720 & lGC/C = 8 h/Pd-rnace cool at 5GC/h to

6、 620ir EOC/ _. Holding t x 8 h/AAir cool Condition of use Delivery condition 73 Iimensians :onCerncd rhicknocs of :Idding on ech face Xrection of sample x L _I_. . Room temperature I Room temperature I 650 2 1Q35 3 825 Proof Rediictisn lardneas Shear Strength 3ening I - 3 1240 3 1000 - 3 12 55 4 268

7、 3 350 - -I- - kl- Impact I Temperature I P stress o Elongation w 21 Rupture b 4 Votes -_ 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-,-,-prEN2408 Page

8、 4 AECMA PREN2408 80 3032333 0003345 i Notes Typical us9 .verage o 0,065 or iner with a maxi- um of 0,125, 4 1) Bracketed figures indicate composition expressed as parts per millicn (Fin). The nethod of analysis for lead, Disrmth and silver chal? be agreed betkteen ir.anuacturer and pur-haser. The methoci of me1sir.g require6 shall be agreed betcieen manufacturer and purchaser. In rreparat 1c.n. a 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-,-,-