AECMA PREN 3500-1995 Aerospace Series Titanium Alloy TI-P11 Annealed 540 Less Than or Equal to Rm Less Than or Equal to 700 MPa Sheet and Strip a Less Than or Equal to 6 mm Edition.pdf

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1、UDC : AECMA STANDARD prEN 3500 NORME AECMA Edition P 2 AECMA NORM May 1995 EDITE PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATERIEL AEROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1) 47.36.98.76 Supersedes issue P1 March 1988 Descriptors : E

2、NGLISH VERSION Aerospace series Titanium alloy TI-P1 1 Annealed 540 I Rm I700 MPa Sheet and strip a I6 mm Srie arospatiale Alliage de titane TI-P1 1 Recuit 540 I Rm I 700 MPa Tles et bandes a 5 6mm Luft- und Raumfahrt Titanlegierung TI-P1 1 geglht 540 I Rm I700 MPa Bleche und Bnder a 5 6 mm This “Ae

3、rospace Series” Prestandard has bee for the needs concerned Tec all not be changed to an extent that thout re-identification of the standa After examina Standard Checking Centre (NPS) and formal agreement of the Offici the Member countries it will be submitted as a draft European Standa mmittee for

4、Standardization) for formal vote. Replace page 1 of the previous issue by this page Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX Declassification approved 1995-05-31 Comments should be sent within six months afte

5、r the date of publication to AECMA Technopolis - 175, rue Jean-Jacques Rousseau 921 38 Issy-les-Moulineaux Cedex - FRANCE C5 Chairman M. Odorico aecma 1995 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction

6、or networking permitted without license from IHS-,-,- AECMA PREN3.500 88 1101i2311i prEN 3500 Page 3 1 This standard specifies for the aerospace application, the mechanical properties for sheet and strip a 6 mm, annealed, in titanium alloy Scope and field of application TI-P11. Unless otherwise spec

7、ified by the drawing, the order or the inspection schedule, the present standard shall be used in conjunction with the referenced EN standards. 2 References EN 2032-1, EN 2032-2, EN 2098-2, EN 2338, EN 2339, EN 2500-4, EN 2600, Aerospace series - Conventional designation for metallic materials Aeros

8、pace series - Metallic materials - Part 2 - Coding of material in delivery heat treatment conditions Aerospace series - Inspection and testing requirements for titanium and heat resisting alloys wrought product - Part 2 - Inspection and testing requirements for sheets, strips and plates Aerospace se

9、ries - Sheets - Titanium and titanium alloys - Cold rolled - Thickness 0,2 5 a 5 3 mm - Dimensions Aerospace series - Sheets - Titanium and titanium alloys - Hot rolled - Thickness 0,8 5 a 6 mm - Dimensions Aerospace series - Guidelines for the preparation ana use of standards for metallic materials

10、 - Part 4 - Titanium and titanium alloys 1) Aerospace series - Designation of metal 1 ic semi -finished products - Rules 1). i) in preparation Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking

11、 permitted without license from IHS-,-,-AECMA PREN3500 BA W LOL23Ll 0005733 b prEN 3500 Page 4 O 8 e Ti Others O2 N2 HZ Each I Total Fe C Cu I Element Chem ka1 Composltlon 3,O 0,20 0,08 0,20 0,05 I ! (125) I i 0,lO ) I0,40 ) I Rem. 1 2 Multlple melting, At least the final. melt shall be in vacuum us

12、ing consumable electrode procesa. If agreed with purchaser, preliminary melting stages may use non-consumable electrode Wethod of melting Sheet and strip a(6mm - =om Wethod of productlon Llmlt dlmensions 5.1 Technical speclflcatlon EN 2098-2 5.2 Dimensional standard EN 2338 I EN 2339 5.3 Dimensional

13、 standard code 34 35 Annealed 5.1 Condition and heat treatment delivery 780 5 8 5 800C / t 20 min Cooled in air or inert atmosphere II 5.2 Dellverv condition code :ondition ind -i eat treatm ent Jw As delivered rest plece teat treatment am pl I ng In the delivery condition a mm 3 lmenslo ns :oncerne

14、d rhlcknoas o :ladding on each lace L or LT 3irectlon of sample Temperature 6 % Room temperature 460 Ru0.2 570 - Strength R, MPa *I - Elongation A, % 540 & Rm 5 700 2 15 Reduction of area IHB I - Hardness Shear Strength R, MPa - Bending k r(=msc Impact K - _- Temperature I 6 I % Time 1 t I h Stress

15、U, MPe *I - Elongation a % - Rupture stress UR MPa *: Eiongatlon st rupture BI lins 98 1 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-,-,-1 Designati

16、on Notes Typical use 2 The rules governing the designation of semi-finished products are indicated in standari EN 2600. When the codified designation is used, the identification code shall be a follows : LEN 35Q I LXX I I- 1 I I I 1 Material standard number Il /Letter code (see 6.2) Appropriate dime

17、nsional standard code (see 5.3) Data concerning dimension (see EN 2600) I i) Determination not required for routine acceptance -1 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-,-,-