ASD-STAN PREN 4088-1997 Aerospace Series Steel FE-PL5101 (13MoCrNiV4-4-3-1) Vacuum Induction Melted and Vacuum Arc Remelted Carburized Hardened Sub-Zero Treated and Tempered Bar fo.pdf
《ASD-STAN PREN 4088-1997 Aerospace Series Steel FE-PL5101 (13MoCrNiV4-4-3-1) Vacuum Induction Melted and Vacuum Arc Remelted Carburized Hardened Sub-Zero Treated and Tempered Bar fo.pdf》由会员分享,可在线阅读,更多相关《ASD-STAN PREN 4088-1997 Aerospace Series Steel FE-PL5101 (13MoCrNiV4-4-3-1) Vacuum Induction Melted and Vacuum Arc Remelted Carburized Hardened Sub-Zero Treated and Tempered Bar fo.pdf(5页珍藏版)》请在麦多课文档分享上搜索。
1、AECMA STANDARD NORME AECMA AECMA NORM prEN 4088 Edition P 1 November 7997 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 ICs: Descriptors: ENGLISH VERSION Aerospace series Steel FE-PL51 O1 (1 3M
2、oCrNiV4-4-3-1) Vacuum induction melted and vacuum arc remelted Carburized, hardened, sub-zero treated and tempered Bar for machining De I 30 mm 1 315 MPa 5 Rm I1 650 MPa Srie arospatiale Acier FE-PL5 1 O 1 (1 3MoCrNiV4-4-3-1) Fusion par induction sous vide et par arc sous vide Cment, durci par tremp
3、e, trait par le froid et revenu Barres pour usinage De 5 30 mm 1 315 MPa I Rm I 1 650 MPa Luft- und Raumfahrt Stahl FE-PL5101 (13MoCrNiV4-4-3-11 Vakuurninduktionserschmolzen und vakuumbogenerschmolzen Aufgekohlt, gehrtet, tieftemperatrbehandelt und angelassen Stangen zur spanabhebenden Formgebung De
4、 I 30 mm 1 315 MPa I R, Il 650 MPa 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 for the needs of AECMA-Members. It has been technically approved by the experts of the concern
5、ed 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 affected, physically or functionally, without re-identification of the standard. After examination a
6、nd signature of the AECMA Standard Checking Centre INPSI and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopo
7、lis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX I Comments should be sent within six months after the date of publication to I Edition approved for publication 1997-1 1-28 AECMA Gulledelle 94 B-1200 BRUXELLES C5 Chairman Mr Odorico aecrna 199 STD*AECMA PREN 4OBB-ENGL 1777
8、LO32322 0034240 230 M Page 3 prEN 4088: 1997 O Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-5. 1 Scope This st
9、andard specifies the requirements relating to: Steel FE-PL51 O1 (1 3MoCrNiV4-4-3-1) Vacuum induction melted and vacuum arc remelted Carburized, hardened, sub-zero treated and tempered Bar for machining De I 30 mm 1 315 MPa 2 Rm I1 650 MPa for aerospace applications. 2 Normative references This Europ
10、ean 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 references, subsequent amendments to or revisions of any of these publications a
11、pply 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. EN 2002-22 Aerospace series - Test methods for metallic materials - Part 22: Plane strain fracture toughness test 1) EN 2043 Aerospa
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- ASDSTANPREN40881997AEROSPACESERIESSTEELFEPL510113MOCRNIV4431VACUUMINDUCTIONMELTEDANDVACUUMARCREMELTEDCARBURIZEDHARDENEDSUBZEROTREATEDANDTEMPEREDBARFOPDF
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