AECMA PREN 4800-2-2001 Aerospace Series Titanium and Titanium Alloys Technical Specification Part 2 Bar and Section Edition P1《航空航天系列.钛和钛合金 技术规范.第2部分 棒材和型材.P1版》.pdf

《AECMA PREN 4800-2-2001 Aerospace Series Titanium and Titanium Alloys Technical Specification Part 2 Bar and Section Edition P1《航空航天系列.钛和钛合金 技术规范.第2部分 棒材和型材.P1版》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 4800-2-2001 Aerospace Series Titanium and Titanium Alloys Technical Specification Part 2 Bar and Section Edition P1《航空航天系列.钛和钛合金 技术规范.第2部分 棒材和型材.P1版》.pdf（23页珍藏版）》请在麦多课文档分享上搜索。

1、 AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 31 Decem ber 2002 prEN 4800-1 Edition P 1 December 2002 Comments should be sent within six months after the date of publication to AECMA-STAN PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION AEEbsT

2、Am Gulledeile 94 - 8-1200 BfUSSelS - Tel. + 32 2 775 81 10 - Fax. + 32 2 775 81 11 - www.aecma-stan.org ICs: Descriptors: Supersedes prEN 3544-2 dated April 1994 and relevant part of prEN 3544-1 ENGLISH VERSION Aerospace series Titanium and titanium alloys Technical specification Part 1: Plate, shee

3、t and strip Srie arospatiale Titane et alliages de titane Spcification technique Partie 1: Plaques, tles et bandes Luft- und Raumfahrt Titan und Titanlegierungen Kneterzeugnisse Technische Lieferbedingungen Teil i: Platten, Bleche und Bnder This Herospace Series“ Prestandard ha been drawn up under t

4、he responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published on green paper for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the

5、publication of this Prestandard, the technical content shall not be changed to an exfent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of AECMA-STAN if will be submitted as a draf

6、t European Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX Material Domain Copyright 2002 O by AECMA-STAN Copyright Association Europeene des

7、Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 prEN 4800-1 : 2002 Contents Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . O 1 2 Normative

8、 references 3 Definitions . , . _ . . ._ . . 4 Wording of order 5 Health and safety . . . . . . 6 Technical requirements ,._._._t.,.,.,., Table 1 -Technical requirements for lines 1 to 29, where appropriate. Table 2 - Technical requirements for lines 30 onwards, where appropriate Page 3 3 3 5 5 5 5

9、8 17 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 4800-1 : 2002 O Introduction This standard is part of the series of EN metallic materi

10、al standards for aerospace applications. The general organisation of this series is described in EN 4258. 1 Scope This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy plate, sheet and strip. It shall be applied when ref

11、erred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule. 2 Normative references This European Standard incorporates by dated or undated reference, provisions from other publications. These normative references are cited at the

12、 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 it by amendment or revision. For undated references the latest edition of the

13、publication referred to applies. IS0 4288 EN 2000 EN 2002-1 EN 2002-2 EN 2002-5 EN 2002-6 EN 2002-8 EN 2002-22 EN 2003-9 EN 2032-1 EN 2032-2 EN 2078 EN 2955 Geometrical Product Specifications (GPS) - Surface texture: Profile method - Rules and Procedures for the Assessment of surface texture. Aerosp

14、ace series - Quality assurance - EN aerospace products - Approval of the quality system of manufacturers Aerospace series - Test methods for metallic materials - Part 1: Tensile testing at ambient temperature 1) Aerospace series - Test methods for metallic materials - Part 2: Tensile testing at elev

15、ated temperature 1) Aerospace series - Test methods for metallic materials - Part 5: Uninterrupted creep and stress-rupture testing 1) Aerospace series - Metallic materials - Test methods - Part 6: Bend testing 1) Aerospace series - Metallic materials - Test methods - Part 8: Micrographic determinat

16、ion of grain size 1) Aerospace series - Metallic materials - Test methods - Part 22: Plane strain fracture toughness test 2) Aerospace series - Test methods - Titanium and titanium alloys - Part 9 : Determination of surface contamination 1) Aerospace series - Metallic materials - Part 1 : Convention

17、al designation Aerospace series - Metallic materials - Part 2: Coding of metallurgical condition in delivery condition Aerospace series - Metallic materials - Manufacturing schedule, inspection schedule, inspection and test report - Definition, general principles, preparation and approval Aerospace

18、series - Recycling of titanium and titanium alloy scrap 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 4 prEN 4800-1 : 2002 EN 31 14-1 EN 31 14-3

19、 EN 31 14-4 EN 3683 EN 3684 EN 3873 EN 3874 EN 3976 EN 3987 EN 3988 EN 4050-1 EN 4050-4 EN 4258 EN 4259 EN 4268 TR 2410 Aerospace series - Test method - Microstructure of (a + ) titanium alloy wrought products - Part 1 : General requirements 1) Aerospace series - Test method - Microstructure of (a +

20、 ) titanium alloy wrought products - Part 3: Microstructure of plate 1) Aerospace series - Test method - Microstructure of (a + ) titanium alloy wrought products - Part 4: Microstructure of sheet for superplastic forming 1) Aerospace series - Test methods - Titanium alloy wrought products - Determin

21、ation of primary alpha content - Point count method and line intercept method 1) Aerospace series - Test methods - Titanium alloy wrought products - Determination of beta transus temperature - Metallographic method 1) Aerospace series - Test methods for metallic materials - Crack propagation test 2)

22、 Aerospace series - Test methods for metallic materials - Constant amplitude force- controlled low cycle fatigue testing 1) Aerospace series - Titanium and titanium alloys - Test method - Chemical analysis for the determination of hydrogen content 1) Aerospace series - Test method for metallic mater

23、ials - Constant amplitude force- controlled high cycle fatigue testing 2) Aerospace series - Test methods for metallic materials - Constant amplitude strain- controlled low cycle fatigue testing 1) Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging

24、 stock and forgings - Part 1: General requirements 1) Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria 1) Aerospace series - Metallic materials - General organization of standardization - Links bet

25、ween types of EN standards and their use Aerospace series - Metallic materials - Definitions of general terms 1) Aerospace series - Metallic materials - Heat treatment facilities - General requirements 2) Aerospace series - Metallic materials - Relationship between dimensional standards and material

26、 standards 3) 1) Published as AECMA Prestandard at the date of publication of this standard 2) In preparation at the date of publication of this standard 3) Published as AECMA Technical Report at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel A

27、erospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 4800-1: 2002 3 Definitions General definition, see EN 4259. 4 Wording of order The order shall clearly indicate: quantities to be supplied; dates of deliv

28、ery; material standard number; delivery condition and metallurgical code of products; dimensions and tolerances or reference to an appropriate dimensional standard; product designation, when required; forwarding address; nature and type of packing, if required; definition and frequency of any specia

29、l tests and their retest procedures, if required. 5 Health and safety Products in the delivery condition shall fulfil the health and safety laws of the area of the country when and where it is to be delivered. A product safety data sheet shall be available. 6 Tech n i cal req u i remen ts 6.1 Genera

30、l The product shall be manufactured in accordance with the requirements of the relevant material standard and the applicable requirements of this specification. A manufacturing schedule shall be established and applied in accordance with EN 2078. Product shall satisfy the requirements of the materia

31、l standard andlor order and shall be free from irregularities prejudicial to the subsequent manufacture or use of this product. Not with standing previous acceptance complying with this material standard, any product that is found, at a later stage, to contain such defects shall be rejected. Unless

32、otherwise specified, the requirements in tables 1 and 2 shall apply in conjunction with those of the relevant material standard. Table 1 relates to lines 1 to 29 (inclusive) of the material standard and table 2 relates to lines 30 onwards in which the sub-line format is also used. Lines 2 to 98 may

33、also be opened in line 100 if the material standard details specific qualification requirements. If a specific line number is not shown in tables 1 and 2, the requirement is stated in the material standard and/or order. The requirements of the order andlor material standard shall over-ride the requi

34、rements of the technical specification. 6.2 Qualification requirements Qualification requirements when invoked by the material standard and/or order are detailed in tables 1 and 2. Unless otherwise agreed between the manufacturer and purchaser the qualification phase shall be run on the first 3 batc

35、hes coming from 3 ingots. 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 6 prEN 4800-1 : 2002 6.3 Release requirements 6.3.1 Release tests Releas

36、e testing shall be the responsibility of the manufacturer. The purchaser reserves the right to perform any of the inspections andlor tests required by the material standard andlor order. The test samples shall be representative of the product. When required the manufacturer shall inform the purchase

37、r of the planned dates for extraction of samples and release testing in order that these operations may be witnessed. Tables 1 and 2 detail the requirements for each line of the material standard. Unless otherwise specifically requested by the purchaser, a particular inspection and/or test for relea

38、se shall be carried out if corresponding acceptance criteria andlor values are stated in the applicable material standard, but see also section 6.3.5 “Capability clause“. 6.3.2 Retests If the test procedure or test piece preparation is faulty, testing shall be re-applied at the original frequency af

39、ter rectification of the original cause of failure. When failure cannot be attributed to faulty testing, or test piece preparation, further test samples shall be selected at twice the original frequency from the product, one of which shall be that on which the original results were obtained unless a

40、lready withdrawn by the manufacturer after suitable identification of the cause of failure. If all retest results are satisfactory, the batch shall be accepted. If one or more tests are unsatisfactory, the batch shall be: - rejected, or - 1 O0 % retested and the conforming products accepted, or - pa

41、rtially or fully re-heat treated if heat treatment can rectify the cause of the failure and tested as a completely new batch except for chemical composition, for which redetermination of hydrogen content is required. No product or test sample shall be re-heat treated more than twice. 6.3.3 Rejection

42、 Any failure to meet the requirements of the material standard shall be cause for rejection. 6.3.4 Special tests Special tests may be required by the purchaser. In such cases, the nature of the test, method, frequency and technical requirements shall be specified on the order or inspection schedule

43、and shall be mutually agreed by the manufacturer and purchaser. 6.3.5 Capability clause Where this is invoked and where sufficient evidence exists, the test shall not be carried out (unless specifically requested by the purchaser). However, this in no way reduces the obligations of the manufacturer

44、to fulfil the requirements, If subsequent testing indicates that the product does not comply with the requirements, the batch shall be rejected. If sufficient statistical evidence does not exist, the test shall be carried out at a frequency agreed between the manufacturer and the purchaser. 6.3.6 St

45、atistical process control Reduction in the extent of release testing, other than that defined in 6.3.5 above, may be negotiated with the purchaser on the basis of appropriate statistical process control andlor statistical data. Copyright Association Europeene des Constructeurs de Materiel Aerospatia

46、l Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 7 prEN 4800-1 : 2002 6.3.7 Inspection and test report The manufacturer shall furnish, with each delivery, a report conforming to the requirements of EN 2078 stating the f

47、ollowing: manufacturers name and address and, if appropriate, identification of the plant; order number; material standard number; method of melting; delivery condition and metallurgical code of the product; quantity and dimensions; manufacturing and inspection schedule reference; cast and batch num

48、ber; batch and/or test samples heat treatment condition; results of the tests and retests if any. Traceability Each product shall be traceable to the cast, production batch and/or heat treatment batch at ali stages of manufacture, testing and delivery. Copyright Association Europeene des Constructeu

49、rs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 8 prEN 4800-1: 2002 I CI UJ m o Q N 8 t o m c) n 8 a v- s m Q 8 i Y- 5 5 8 2 u c m o m C C O U C .- .- c .- u f a U al K t o m a r o m al K O .- - 5 .- e N I I C U al u) a U C m .- 2 p! c .- Li L! b9 3 o 3 C e E a 2. a U 5 5 .g Q m a P Q S UJ r .- - E 2. K O - 2 - m 3 U a C 5 5 .-