AECMA PREN 2305-1999 Nickel Base Alloy NI-P11 540 MPa Less Than or Equal to Rm Less Than or Equal to 620 MPa Bars and Wires for Rivets Aerospace Series Edition 2 [Refer To ASD-STAN.pdf

1、STDmAECMA PREN 2305-ENGL 1999 1012311 0037445 356 W AECMA STANDARD NORME AECMA AECMA NORM prEN 2305 Edition 2 December 1999 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 ICs: Supersedes edition

2、 I May 1980 Descriptors: ENGLISH VERSION NICKEL BASE ALLOY NI-PI I 540 MPa I Rm I 620 MPa BARS AND WIRES FOR RIVETS AEROSPACE SERIES ALLIAGE BASE DE NICKEL NI-PI 1 540 MPa I Rm I 620 MPa BARRES ET FILS POUR RIVETS SRIE AROSPATIALE LUFT- UND RAUMFAHRT NICKELBASISLEGIERUNG NI-PI 1 540 MPa 5 R, 5 620 M

3、Pa STANGEN UND DRAHT FR NIETE It is published on yellow paper in three equivalent v It will be submitted as a dmff European Standard to formal vote. I Replace page 1 of the previous edition by this page I Declassification approved 1999-12-31 - The equivalent versions in French and German languages c

4、an be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau 92138 ISSY - LES - MOULINEAUX CEDEX - FRANCE 0 aecma 1999 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitt

5、ed without license from IHS-,-,-prEN2305 Page 3 O e a O I Chemical Element 1 2 3 4 - 5 I 6 7 I 8 9 10 11 12 13 14 15 16 17 - - - P - I - - is - 19 Composition min. 55 1 max. - - - - 28 - O ,O8 Bas e 0,16 0,5 2,0 0,024 0,5 34 2 lethod of melting Air melt Bars and wires for rivets DC10m EN2038-1) and

6、EN20984 1 :orm nethod of production .mit dimensions .1 Acceptance standards .2 Dinensional standards :ondition ind eat treatment 3elivery - Cold drawn ondition ind Delivery Condition ieat treatment Jse rest piece +eat treatment iampling Delivery condition mrn ,c 10 limensions :oncerned % rhicknecs o

7、f :Iudding on each fact. Xrectien of carnplo -_. Room temperature I- R, /MPa*) 540 Rm 4 620 3 25 t- I- - Hardness Shear Strength Bending I mpact -i- Time Temperature b Stress o Elongation Rupture Strsss Elongation et rupture I- - -I- Al I Notes Copyright Association Europeene des Constructeurs de Ma

8、teriel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECIA PREN2305 80 M LO12311 0002851 4 prEN2305 Page 4 1 porcion test Notas Typical us8 2 s 8 mm : 10 revolutions in each direction 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-,-,-