AECMA PREN 2070-7-1987 Aerospace Series Aluminium and Aluminium Alloy Wrought Products - Technical Specification - Part 7 - Wrought Forging Stock Edition 1《航空系列.铝和铝合金锻制品的检验和试验要求.第7.pdf

《AECMA PREN 2070-7-1987 Aerospace Series Aluminium and Aluminium Alloy Wrought Products - Technical Specification - Part 7 - Wrought Forging Stock Edition 1《航空系列.铝和铝合金锻制品的检验和试验要求.第7.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2070-7-1987 Aerospace Series Aluminium and Aluminium Alloy Wrought Products - Technical Specification - Part 7 - Wrought Forging Stock Edition 1《航空系列.铝和铝合金锻制品的检验和试验要求.第7.pdf（6页珍藏版）》请在麦多课文档分享上搜索。

1、A. E .C .M .A. STAN DARD NORME A.E.C.M.A. A.E.C.M.A. NORM prEN2070 Part 7 Edition 1 February 1987 ENGLISH VERSION Aerospace series Aluminium and aluminium alloy wrought products - Technical specification - Part 7 - Wrought forging stock Srie arospatiale Demi-produits corroys en aluminium et alliages

2、 daluminium - Spcification technique - Partie 7 - Produits corroys destins la forge Luft- und Raumfahrt Halbzeug aus Aluminium und Aluminium- Knetlegierungen - Technische Lieferbedingungen - Teil 7 - Schmiedevormaterial This industrial standard for the aerospace sector has been drawn up under the re

3、sponsibility of AECMA (Associa tion Europenne des Constructeurs de Matriel Arospatial). It is published on yellow paper in three equivalent versions (English, French, German). It will be submitted to CEN (European Committee for Standardization) as a draft European Standard. . b !A ; - U a C c U ! 5

4、U u E U L c $ i E C O O U F L Approved by The eqoivaient versions in French and German languages COMITE DE NORMALISATION can be supplied by 6.NA.E 8, rue Moreau-Vauthier Of A.E.C.M.A. 1987-02-01 92100 BOULOGNE-BILLANCOURT -FRANCE. I Copyright Association Europeene des Constructeurs de Materiel Aeros

5、patial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN2070-07 7 W 1012311 0007638 7 Page 2 Contents 9 10 Scope and field of application References Batch size Dimensions External defects Internal defects Tensile tes

6、t Back end defect and peripheral coarse grain zone Special tests Mark in g r 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-,-,-AECMA PREN2070-07 87 9 L

7、OL23LL O007637 7 E 1 Scope anc field of application prEN2070-7 Page 3 The present standard specifies the particular requirements of wrought products for the production of forgings in aluminium and aluminium alloys, This standard shall be used in conjunction with EN207-1. 2 References Aerospace serie

8、s - Test methods for m Tensile tests at ambient temperature allic materials - Part 1 - Pf EN2002-1, EN2004-2, Aerospace series - Test methods for aluminium and aluminium alloys products - Part 2 - Ultrasonic testing of plates, forgings and extrusions EN2070-1, Aerospace series - Aluminium and alumin

9、ium alloy wrought products - Technical Specification - Part 1 - General requirements EN2070-2, Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - Part 2 - Sheet, strip, formed profiles and plate . Aerospace series - Aluminium and aluminium alloy wrought pro

10、ducts - Technical specification - Part 3 - Bars and extrucions EN2C7-3, 1) EN2715, Aerospace series - Macrographic examination of aluminium and aluminium alloy forging stock - Forging and wrought products . 3 Batch size A batch of forging stock shall consist of material of the same cross-section fro

11、m Che same cast. A cast is defined in EN2070-1. 1) 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-,-,-AECIA PREN2070-07 7 = LOL23LL 0007640

12、 5 prEN2070-7 Page 4 4 Dimensions Dimensions and tolerances shall be agreed between the manufacturer and the purchaser and shall be specified on the order or on the inspection schedule. The frequency of examination adopted by the manufacturer shall be sufficient to permit him to certify compliance w

13、ith the requirements, 5 External defects Visual surface inspection shall be carried out in the delivery condition. The surface of the forging stock shall be clean and free from defects such as cracks, laps, scratches, corrosion, considered harmful to its use. Surface defects may be removed provided

14、the forging stock dimensions remain within any tolerances that may be specified. 6 Internal defects If required by the order or the inspection schedule products having dimensions in accordance with table 1 shall be ultrasonically tested in accordance with EN2004-2 and shall, unless otherwise specifi

15、ed, meet the requirements of class A. If the material is ultrasonically testedin o condition different from the condition of supply, this shall be subject to agreement between rcanufacturer and purchaser and shall be specified on the order, inspection or manufacturing schedule. 7 Tensile test The co

16、ndition of the material shall comply with the relevant material standard. The tensile test shall be carried out in accordance with Eh2002-1 on test samples heat treated in full section or after forging to 3G mm diameter. Tests shall be performed OE proportional round test pieces of the form and one

17、of the sizes indicated in EK2002-1. ;.- ea 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-,-,-Th AECMA PREN2070-07 7 L0123LL dire ti n of t material stand

18、ard. st ample shall b in prEN2070-7 Page 5 f th quir emen t ordance with the r SamplSng frequency shall be in accordance with table 1. The test results shall comply with the relevant material standard. 8 Back end defect and peripheral coarse grain zone If the product is obtained by extrusion macrogr

19、aphic examination shall be carried out on a cross section cut from the back end of the extrusion at a frequency sufficient to ensure that the entire batch meets the requirement of this standard. The material shall be tested in accordance with EN2715 and the samples shall be solution heat treated pri

20、or to testing. The extrusion shall be free from back end defect and unless otherwise agreed between the manufacturer and the purchaser the maximum thickness of the peripheral coarse grain zone.shal1 be as specified by the material standard, the order or the inspection schedule. Where necessary, the

21、product may be machined to meet the requirements. 9 Special tests Special tests and inspections may be required by the purchaser. In such cases, after agreement between purchaser and manufacturer, the nature of test, method, number and acceptance standards shall be specified on the order or the insp

22、ection schedule. 10 Marking Marking shall be in accordance with EN2070-1 and EN2070-2 or EE2070-3 as appropriate. If special tests in accordance with clause 9 are required the marking shall be defined an.d shall reflect these extra requirements. The frequency of examination adopted by the manufactur

23、er shall be sufficient to permit him to certify compliance with the requirements. 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-,-,-AECMA PREN2070-07 7 =

24、 LO12311 0007642 9 E .- prEN2070-7 Page 6 O a, v) 3 m o al al v) f - al v) 3 m o a, a, - v, I - I s O O ? m S +i v) al S O o o) UJ c .- t .- +i n - I - - m 3 v) 5 zu w +- u 3 U O Q U a, U X W L 2 +- v) o 3 U a +- E - v) o 3 U O i- L n - I (D v) u al al U 4- Lc Y (o al E 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-,-,-