AECMA PREN 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf

上传人:jobexamine331 文档编号:421234 上传时间:2018-11-06 格式:PDF 页数:5 大小:136.06KB
下载 相关 举报
AECMA PREN 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf_第1页
第1页 / 共5页
AECMA PREN 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf_第2页
第2页 / 共5页
AECMA PREN 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf_第3页
第3页 / 共5页
AECMA PREN 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf_第4页
第4页 / 共5页
AECMA PREN 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf_第5页
第5页 / 共5页
亲,该文档总共5页,全部预览完了,如果喜欢就下载吧!
资源描述

1、STD*AECMA PREN Li289-ENGL 1998 10LZ311 0014559 05T Edition approved for publication AECMA STANDARD NORME AECMA AECMA NORM Comments should be sent within six months after the date of Dublication to C5 Chairman prEN 4289 Edition P 1 April 1998 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTR

2、IES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. +32) 2 775 81 11 ICs: Descriptors: ENGLISH VERSION Aerospace series Aluminium alloy AL-P7 1 75- Forging stock Srie arospatiale Alliage daluminium AL-P7175- Produits destins la forge Luft- und Raumfahrt Aluminiumlegierung AL

3、P7175- Schmiedevormaterial 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 Tech

4、nical 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 and sign

5、ature of the AECMA 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 Cornmittee for Standardization) for formal vote. 1998-04-30 AECMA Gulledelle 94 Mr Evetts I B-1200 BRUXELLES I ae

6、cma 1998 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-,-,-Page 3 prEN 4289: 1998 O Introduction This standard is part of the series of EN metallic mater

7、ial standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-2. 1 Scope This standard specifies the requirements relating to: Aluminium alloy AL-P7175- Forging stock for aerospace applications. 2

8、 Normative references This European 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 revision

9、s of any of these publications apply 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 2043 EN 2070-3 EN 2070-7 EN 2082-2 EN 4258 EN 4500-2 Aerospace series - Metallic materials - Gene

10、ral requirements for semi-finished product qualification (excluding forgings and castings) 1) Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - Part 3: Bar and section Aerospace series - Aluminium and aluminium alloy wrought products - Technical specificat

11、ion - Part 7: Wrought forging stock Aerospace series - Aluminium alloy forging stock and forgings - Technical specification - Part 2: Forging stock Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use 1) Aerospace series

12、 Metallic materials - Rules for drafting and presentation of material standards - Part 2: Specific rules for aluminium, aluminium alloys and magnesium alloys 1) 1) Published as AECMA Prestandard at the date of publication of this standard Previouc page is blank Copyright Association Europeene des C

13、onstructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Material designation 6.1 Aluminium alloy AL-P7175 Delivery condition 03 F Heat treatment - - Form Ingot or billet Rod, bar or section Method

14、 of production Cast Extruded Limit dimension(s) mm al I O00 a I 400 Technical specification EN 2082-2 EN 2070-7 6.2 7 Delivery condition code U U Use condition 03 F Heat treatment Delivery condition Delivery condition 8.1 8.2 8.3 9 Characteristics Test sample(s) See EN 2082-2 See EN 2070-7 Test piec

15、e(s) See EN 2082-2 See EN 2070-7 Heat treatment T73 (see line 29) T73 (see line 29) Dimensions concerned mm See EN 2082-3 a or D s 400 Thickness of cladding on lo I each face - % - 1 I 12 13 14 15 16 - - - - I 17 I Hardness I - Direction of test piece L L Temperature e OC Ambient Ambient Proof stres

16、s %,2 MPa 2385 2385 l) T Strength R, MPa 2455 1) 2455 1) Elongation A% 27 1) 27 1) Reductionofarea Z % - I18 I Shearstrength I R, IMPal - Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking perm

17、itted without license from IHS-,-,-eference heat treatment - - xternal defects See EN 2070-7 or EN 2082-2 See EN 2070-7 or EN 2082-2 lacrostructure iternal defects Marking inspection Dimensional inspection Notes Typical use Page 5 prEN 4289: 1998 Forged test pieces (cast stock) or delivery condition

18、 (extruded section) + 460 “C 5 8s 480 “C / WQ Os 80 “C 2, + 100 “C c Oc 120 “C I6 h 5 t 5 24 h + 170 “C c Oc 182 “C I6 h 5 t 5 18 h See EN 2070-7 or EN 2082-2 See EN 2070-7 51 Extruded forging stock Back end defects : see EN 2070-7 Peripheral coarse grain : level A (as per EN 2070-3) See EN 2070-7 o

19、r EN 2082-2 1) The “capability clause“ applies. 2) The use of quench additives or higher quenchant temperature shall be subject to agreement between manufacturer and purchaser. - -I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot

20、for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 prEN 4289: 1998 Product qualification See EN 2043 Qualification programme to be agreed between manufacturer and purchaser. 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-,-,-

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 4134-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Long Thread in Heat Resisting Nickel Base Alloy Aluminium IVD Coated Classification .pdf AECMA PREN 4134-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Long Thread in Heat Resisting Nickel Base Alloy Aluminium IVD Coated Classification .pdf
  • AECMA PREN 4135-1994 Aerospace Series Bolts Normal Bi-Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Titanium Alloy Anodized MoS2 Lubricated Classification 1 .pdf AECMA PREN 4135-1994 Aerospace Series Bolts Normal Bi-Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Titanium Alloy Anodized MoS2 Lubricated Classification 1 .pdf
  • AECMA PREN 4136-1994 Aerospace Series Bolts Normal Bi-Hexagonal Head Coarse Tolerance Normal Shank Long Thread in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambient Te.pdf AECMA PREN 4136-1994 Aerospace Series Bolts Normal Bi-Hexagonal Head Coarse Tolerance Normal Shank Long Thread in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambient Te.pdf
  • AECMA PREN 4137-1994 Aerospace Series Bolts Normal Bi-Hexagonal Head Stepped Shank Long Thread in Titanium Alloy Anodized MoS2 Lubricated Classification 1 100 MPa (at Ambient Tempe.pdf AECMA PREN 4137-1994 Aerospace Series Bolts Normal Bi-Hexagonal Head Stepped Shank Long Thread in Titanium Alloy Anodized MoS2 Lubricated Classification 1 100 MPa (at Ambient Tempe.pdf
  • AECMA PREN 4138-1994 Aerospace Series Screws Pan Head Offset Cruciform Recess Coarse Tolerance Normal Shank Medium Length Thread in Alloy Steel Cadmium Plated Classification 1 100 .pdf AECMA PREN 4138-1994 Aerospace Series Screws Pan Head Offset Cruciform Recess Coarse Tolerance Normal Shank Medium Length Thread in Alloy Steel Cadmium Plated Classification 1 100 .pdf
  • AECMA PREN 4139-1993 Aerospace Series Screws Pan Head Offset Cruciform Recess Threaded to Head in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambient Temperature) 235 D.pdf AECMA PREN 4139-1993 Aerospace Series Screws Pan Head Offset Cruciform Recess Threaded to Head in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambient Temperature) 235 D.pdf
  • AECMA PREN 4139-1994 Aerospace Series Screws Pan Head Offset Cruciform Recess Threaded to Head in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambient Temperature) 235 D.pdf AECMA PREN 4139-1994 Aerospace Series Screws Pan Head Offset Cruciform Recess Threaded to Head in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambient Temperature) 235 D.pdf
  • AECMA PREN 4153-2009 Aerospace series Rivets solid universal head in aluminium alloy 2219 anodized or chromated metric series Edition P 1《航空航天系列.铝合金2219 万能头实心铆钉 阳极氧化或铬酸盐处理 公制系列.版本P.pdf AECMA PREN 4153-2009 Aerospace series Rivets solid universal head in aluminium alloy 2219 anodized or chromated metric series Edition P 1《航空航天系列.铝合金2219 万能头实心铆钉 阳极氧化或铬酸盐处理 公制系列.版本P.pdf
  • AECMA PREN 4154-2009 Aerospace series Rivet solid 100 degrees countersunk normal head in aluminium alloy 2219 anodized or chromated metric series Edition P1《航空航天系列.铝合金2219 100°标称埋头.pdf AECMA PREN 4154-2009 Aerospace series Rivet solid 100 degrees countersunk normal head in aluminium alloy 2219 anodized or chromated metric series Edition P1《航空航天系列.铝合金2219 100°标称埋头.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1