ASD-STAN PREN 6071-1998 Aerospace Series Aluminium and Aluminium Alloy Wrought Products Technical Specification Plate (Edition P 1)《航空航天系列 铝和铝合金压力加工制品 技术规范 厚板材 第P1版》.pdf
《ASD-STAN PREN 6071-1998 Aerospace Series Aluminium and Aluminium Alloy Wrought Products Technical Specification Plate (Edition P 1)《航空航天系列 铝和铝合金压力加工制品 技术规范 厚板材 第P1版》.pdf》由会员分享,可在线阅读,更多相关《ASD-STAN PREN 6071-1998 Aerospace Series Aluminium and Aluminium Alloy Wrought Products Technical Specification Plate (Edition P 1)《航空航天系列 铝和铝合金压力加工制品 技术规范 厚板材 第P1版》.pdf(19页珍藏版)》请在麦多课文档分享上搜索。
1、STD-AECMA PREN b07L-ENGL 1778 .I 1OL23LL 0015b07 IT2 AECMA STANDARD NORME AECMA AECMA NORM prEN 6071 Edition P 1 November 1998 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: Descriptors: EN
2、GLISH VERSION Aerospace series Aluminium and aluminium alloy wrought products Technical specification Plate Srie arospatiale Demi-produits corroys en aluminium et alliages daluminium Spcification technique Plaques Luft- und Raumfahrt Aluminium und Aluminium Knetlegierungen Technische Lieferbedingung
3、en Platte 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 concerned Technical Committee fo
4、llowing 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 and signature of the AECMA
5、 Standard Checking Centre (NPS) 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. aecma 1998 Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199,
6、rue Jean-Jacques Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX Edition approved for publication Comments should be sent within six months after the date of publication to 1998-1 1-30 AECMA Gulledelle 94 B-1200 BRUXELLES AIBITFG Chairman Mr W. Lampa STD-AECMA PREN bD71-ENGL 1998 1012311 00LSbLO 014 Pag
7、e 2 prEN 6071 : 1998 Contents list 1 Scope 2 Normative references 3 Definitions 4 Requirements 5 Qualification testing 6 Release testing 7 Marking Annex A (normativ) Qualification testing and inspection/test frequency Annex B (normativ) Release testing and inspection/test frequency 1 Scope This stan
8、dard defines the specific requirements for aluminium and aluminium alloy plate. The plate may be clad or unclad supplied in the as-rolled or machined condition. It shall be applied in conjunction with EN 6070. 2 Normative references This European Standard incorporates by dated or undated reference p
9、rovisions 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 apply to this European Standard only when incorporated in
10、it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 1880 EN 2002-1 EN 2004-1 EN 4500-1 EN 6018 EN 6070 EN 6072 EN 6073 ASTM-B 557 ASTM B 769-94 ASTM-E 3 ASTM-E 9 ASTM-E 11 1 ASTM-E 238 Instruments for the measurement of surface roughness
11、 by the profile method; Con- tact (stylus) instruments of progressive profile transformation; Profile recording instruments Aerospace Series - Test methods for metallic materials - Part 1 - Tensile testing at ambient temperature ) Aerospace Series - Test methods for aluminium and aluminium alloy pro
12、ducts Part 1 - Determination of electrical conductivity of wrought aluminium and aluminium alloys Aerospace Series - Metallic materials - Rules for drafting and presentation of material standards- Part 1 - General rules I Aerospace series - Test methods for metallic materials - Determination of dens
13、ity according to displacement method ) Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - General requirements) Aerospace series - Metallic materials - Test methods - Constant amplitude fatigue testing I Aerospace series - Metallic materials - Aluminium and
14、 aluminium alloys - Test me- thods - Drop test ) Standard Test Methods of Tension Testing Wrought and Cast Aluminium- and Magnesium-Alloy products 2 Standard Method for Shear Testing of Aluminium Alloys ) Standard Practice for preparation of Metallographic Specimens 2, Standard Test Methods of Compr
15、ession Testing of Metallic Materials at Room Temper- ature 2, Standard Test Method for Youngs Modulus, Tangent Modulus and Chord Modulus Standard Test Method for Pin-Type Bearing Test of Metallic Materials ) 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published b
16、y: American Society for Testing and Materials (ASTM). 1916 Race Street, Philadelphia, PAI 91 03. USA Page 4 prEN 607 1 : 1998 I i ASTM-E 399 ASTM-E 561 ASTM-E 602 ASTM-E 647 ASTM G 34-86 ASTM-G 47 MIL-H-6088 MIL-STD-2154 Standard Test Method for Plane-Strain Fracture Toughness of Metallic Materials
17、Standardpractice for R-Curve Determination Standard Test Method for Sharp-Notch Tension Testing with Cylindrical Specimens 2, Test Method for Constant-Load-Amplitude Fatigue Crack Growth Rates Above 1 O-8miCycle Standard Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Al
18、uminium Alloys (EXCO test) Standard Test Method for Determining Susceptibility to Stress Corrosion Cracking of High-Strength Aluminum Alloy Products Heat Treatment of Aluminum Alloys 31 Inspection, Ultrasonic, Wrought Metals, Process for 3, 3 Definitions For the purposes of this standard the followi
19、ng definitons apply: General definitions see EN 6070. 3.1 Parent plate Plate undergoing the same operations over its whole length (including solution heat treatment, controlled stretching, ageing) before being cut. 3.2 plate Flat rolled product of rectangular cross-section and uniform thickness over
20、 6 mm. 3.3 Machined plate Product produced from a plate completely machined over one or two faces. 3.4 Controlled stretching Stretching performed after solution heat treatment and quenching for the purpose of reducing internal stresses. The stretching is defined by a minimum permanent elongation and
21、 if necessary by a maximum permanent elongation indicated in the material specification. 2) Published by: American Society for Testing and Materials (ASTM). 1916 Race Street, Philadelphia, PA19103, USA 3) Published by: Department of Defense (DoD), the Pentagon, Washington D.C. 20301, USA STD-AECMA P
22、REN b07L-ENGL 1998 = ltOL232L 0015b13 823 E Page 5 prEN 607 1 : 1998 Number of parent plates per batch 1 to 2 4 Requirements Number of parent plates to be tested 1 4.1 General Requirements See EN 6070 3 to 4 4.2 Technical Requirements 2 4.2.1 General 5 to 6 6 The plate shall satisfy the requirements
23、 of the relevant material standard and the related Individual Product Specification (IPS). Unless otherwise specified in the relevant material standard or IPS, the test method and test frequency are given in Annex A for qualification testing and in Annex B for release testing. 3 4 Manufacturer must
24、ensure a consistent material as far as structure, chemical composition and strength are concerned. 4.2.1.1 Controlled stretching Controlled stretched plate shall be largely free from residual stresses to minimize distortion during machining. Straightening and dressing operations following either sol
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