AECMA PREN 2167-1999 Heat Resisting Steel FE-PA91-HT Solution Treated Bars Aerospace Series Edition 2 [Refer To ASD-STAN PREN 4263 ASD-STAN PREN 4571]《航空航天系列.耐热钢 FE-PA91-HT溶液处理棒材》.pdf

《AECMA PREN 2167-1999 Heat Resisting Steel FE-PA91-HT Solution Treated Bars Aerospace Series Edition 2 [Refer To ASD-STAN PREN 4263 ASD-STAN PREN 4571]《航空航天系列.耐热钢 FE-PA91-HT溶液处理棒材》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2167-1999 Heat Resisting Steel FE-PA91-HT Solution Treated Bars Aerospace Series Edition 2 [Refer To ASD-STAN PREN 4263 ASD-STAN PREN 4571]《航空航天系列.耐热钢 FE-PA91-HT溶液处理棒材》.pdf（3页珍藏版）》请在麦多课文档分享上搜索。

1、STD=AECMA PREN 2Lb7-ENGL 1999 LOL23LL 0037438 LLb = Declassification approved 1999-1 2-31 AECMA STANDARD NORME AECMA AECMA NORM The equivalent versions in French and German languages can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau 92138 ISSY - LES - MOULINEAUX CEDEX - F

2、RANCE prEN 2167 Edition 2 December 1999 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 1 I ICs: Supersedes edition I January 1979 Descriptors: ENGLISH VERSION HEAT RESISTING STEEL FE-PASI-HT SOLUTI

3、ON TREATED BARS AEROSPACE SERIES ACIER RSISTANT CHAUD MIS EN SOLUTION BARRES FE-PA91-HT SRIE AROSPATIALE HOCHWARMFESTER STAHL FE-PA91 -HT LSUNGSGEGLHT STANGEN LUFT- UND RAUMFAHRT This “Aerospace series“ Standard has been drawn up under the European Association of Aerospace Industries). It will be su

4、bmitted as a draft European Standa formal vote. f AECMA (The Standardization) for I Replace page 1 of the previous edition by this page I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking perm

5、itted without license from IHS-,-,-AECMA PREN2367 i7 m 3032333 0002363 9 m DRAFT EUROPEAN STANDARD - AEROSPACE SERIES So lut ion treated Bars prEN2167 Page 3 HEAT RESISTING STEEL FE-PA91-HT Element Chemical Composition min. c si K P S Co Cr Mo N2 Ni NbtTa W Fe G,08 - 1,Ci - - i8,5 20,o 2,50 o,io i9,

6、 0,75 2,o o,i6 1,o 2,o 0,040 0,030 21,O 22,5 3,5G 0,20 21,O 1,25 3,O T(e ain %!er 1 Xrnensions 100 :oncerned 2 - 3 Hard ness Shear Strength tlethod of melting 1 HB - 229 - R, MPa) Air or vacuum melt or Air melt and vacuum refine or Consumable electrode remelt Notes :arm dethod of production .mit dim

7、ensions *i IMP=IN/ i) The method of melting required shall be agreed between manufacturer Bars for machining De 100 IIUII Bars for forging “ qcceptance Standards 2069-1 and EN2069-3 2, :ondition ind deat treatment Delivery Solution treated 1180 l5V/t = lhfiiater quench :ondition ind +eat treatment J

8、se Solution treated Delivery condition I rest piece +eat treatment jampiing Not heat treated Machined or descaled Solution treated 1180 f l5V/t lhfiater quench Condition of use I Xrection of sample -. Temperature I 6 1 “c 1 Room temperature 2 305 Proof Stress II Strongti1 690 Rin 880 2 35 Bending ir

9、 = k x a) I4 I Impact I4 J I an purcha 12) Ih preparaEti; 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 PREN2167 79 m 1012311 O002362 O m prEM2167 Page 4 1 Notes Typical use 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-,-,-