AECMA PREN 2404-1999 Heat Resisting Nickel Base Alloy NI-P100-HT Solution Treated and Precipitation Treated Bars Aerospace Series Edition 2 Supersedes Edition 1 May 1980 [Refer To .pdf

1、1- 5 AECMA STANDARD prEN 2404 Edition 2 NORME AECMA AECMA NORM December 1999 - PUBUSHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Guiledalle 94 - 51200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 811 1 Supersedes edition 1 May 1980 ICs: Descriptors: ENGLISH VERSION HEAT R

2、ESISTING NICKEL SOLUTION TREATED AND PRECIPITATION TREATED BARS AEROSPACE SERIES BASE ALLOY NI-PI 00-HT ALLIAGE RSISTANT A CHAUD A BASE DE NICKEL NI-Pl00-HT, MIS EN SOLUTION ET PRCIPITE BARRES SERIE AROSPATIALE LUFT- UND RAUMFAHRT HOCHWARMFESTE , NICKELBASISLEGIERUNG NI-PIOO-HT AUSGEHARTET STANGEN T

3、his “Aerospace senes Standard has been drawn up under the re European Association of Aerospace Industries). It is published on yellow paper in three equivalent v It will be submitted as a drafi European Standa formal vote. f AECMA (The Standardization) for Replace page 1 of the previous edition by t

4、his page Declassification I The eauivaleni venions in French and German bneueges 1 approved 1999-1 2-31 I .- can be supplied by B.N.A.E. - Technopolii 54 - 1 Q9, rue Jean-Jacques Rousseau I 92138 ICSY - LES - MOUUNEAUX CEDM - FRANCE aecma 1999 COPYRIGRT Association Buropeene Des Constructeurs de Mat

5、eriel Aerospace . _ Lfc-ensed by Information Handling Services . 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-,-,-I DRAFT EUHOPEAN SIANOAHO - AEHOSFAGk

6、scntiis Solution treated and precipitation treated Bars prENZ404 Page 3 HEAT RESISTIhG NICKEL BASE ALLOY NI-P100-HT Chemical 1 lement 1 -arm Method of production ,mit dimensions Ucceptance standards !j,2 Di9rn;ional standards Condition ind Heat treatment Delivery Condition and Heat treatment us3 Tes

7、t piece Heat treatment Sampling Dimensions concerned Thickness of cladding on each face I Direction of sample ShearStrength i R, MPa*) lkL Bendina impact K.J Temperature 8 OC The th - - Stress Elongation et rupture A X Notes I 3 I 4 2 Air melt, vacuum refine and consumable electrode remelt or vacum

8、melt and consumable electrode remelt Bars for machining I Bars for forging De4 100 mm I - EEJ2098-i 3, and EN2095-3 I I Untreated Fti2368 Solution treated end . I orecioltation treated Bachined or &scaled Solution treated I l coolat50Wh . I to 620 f 10 fc 4- t = 8 hlalr cool I Soiution treated and I

9、 . I Solutlon treated and precipitation treated ! ! precioitatlon treated i 950S:O980OC/t=l hl 8 htfurnace Delivery condition I Delivery condition , air cool orweterquench +720 2 10 Wt 4-720 f 10 %It =8 hlfurnece I o 620 2 10aC+t =B Mair coolt cool at 50 Wh I I cool at W Wh to 620 t 10 OC+t =I3 h/ai

10、r coo! Condition of use L loom teniperature 3 1035 b 1270 2, 13 t 20 LT L LT Room temperature 650 65 O 3 1035 9 8 60 3 860 5 1240 3 1000 3 960 95 13 35 88 * 20 a8 - I 1 - - 3 331 r, 331 650 690 35 *) 1MPa = 1Ntmm2 11, 7), 31, see line 98 Copyright Association Europeene des Constructeurs de Materiel

11、Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN2404 Page 4 1 zzxq+ dotes ypical um I I I 3 I 4 2 0,090 or finer with occasional 0,18 permitted 1) Bracketed figures indicate composition expressed as parts per

12、million (ppm). The method of analysis fcr lead, bisnuth and silver shall Se agreed between manufacturer and purchaser. manufacturer and purchaser. 2) The method of melting required shall be agreed between 3 ) In preparation. 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-,-,-