AECMA PREN 4800-3-2001 Aerospace Series Titanium and Titanium Alloys Technical Specification Part 3 Tube Edition P1《航空航天系列.钛和钛合金 技术规范.第3部分 管子.P1版》.pdf

1、AECMA STANDARDNORME AECMAAECMA NORMprEN 4800-2Edition P 1April 2002PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION (AECMA-STAN)Gulledelle 94 B-1200 BRUXELLES Tel. (+32) 2 775 8110 Fax. (+32) 2 775 8111ENGLISH VERSIONAerospace seriesTitanium and titanium alloysTechnica

2、l specificationPart 2: Bar and sectionSrie arospatialeTitane et alliages de titaneSpcification techniquePartie 2: Barres et profilsLuft- und RaumfahrtTitan und Titanlegierungen KneterzeugnisseTechnische LieferbedingungenTeil 2: Stangen und ProfileThis “Aerospace Series“ Prestandard has been drawn up

3、 under the responsibility of AECMA-STAN (TheEuropean Association of Aerospace Industries - Standardization). It is published on green paper for theneeds of the European Aerospace Industry. It has been technically approved by the experts of theconcerned Domain following member comments.Subsequent to

4、the publication of this Prestandard, the technical content shall not be changed to anextent that interchangeability is affected, physically or functionally, without re-identification of thestandard.After examination and review by users and formal agreement of AECMA-STAN it will be submitted as adraf

5、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 CEDEXEdition approved for publication2002-04-30Comments should be sent within six monthsafter

6、the date of publication toAECMA-STANGulledelle 94B-1200 BRUXELLESMaterial DomainMr Evetts aecma 2002Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Pag

7、e 2prEN 4800-2: 2002ContentsPage0 Introduction. 31 Scope 32 Normative references. 33 Definitions. 44 Wording of order . 45 Health and safety 46 Technical requirements. 5Table 1 Technical requirements for lines 1 to 29, where appropriate. 7Table 2 Technical requirements for lines 30 onwards, where ap

8、propriate . 16Copyright 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 3prEN 4800-2: 20020 IntroductionThis standard is part of the series of EN metallic m

9、aterial standards for aerospace applications. The generalorganization of this series is described in EN 4258.1 ScopeThis standard defines the requirements for the ordering, manufacture, testing, inspection and delivery oftitanium and titanium alloy bar and section. It shall be applied when referred

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

11、e places in the text and the publications are listedhereafter. For dated references, subsequent amendments to or revisions of any of these publications applyto this European Standard only when incorporated in it by amendment or revision. For undated referencesthe latest edition of the publication re

12、ferred to applies.EN 2000 Aerospace series Quality assurance EN aerospace products Approval of the qualitysystem of manufacturersEN 2002-1 Aerospace series Test methods for metallic materials Part 1: Tensile testing at ambienttemperature 1)EN 2002-2 Aerospace series Test methods for metallic materia

13、ls Part 2: Tensile testing at elevatedtemperature 1)EN 2002-5 Aerospace series Test methods for metallic materials Part 5: Uninterrupted creep andstress-rupture testing 1)EN 2002-8 Aerospace series Metallic materials Test methods Part 8: Micrographic determinationof grain size 1)EN 2002-16 Aerospace

14、 series Metallic materials Test methods Part 16: Non-destructive testing Penetrant testing 1)EN 2003-9 Aerospace series Test methods Titanium and titanium alloys Part 9 : Determination ofsurface contamination 1)EN 2032-1 Aerospace series Metallic materials Part 1: Conventional designationEN 2032-2 A

15、erospace series Metallic materials Part 2: Coding of metallurgical condition in deliveryconditionEN 2078 Aerospace series Metallic materials Manufacturing schedule, inspection schedule,inspection and test report Definition, general principles, preparation and approvalEN 2954 Aerospace series Macrost

16、ructural examination of titanium and titanium alloy wroughtproducts 2)EN 2955 Aerospace series Recycling of titanium and titanium alloy scrapEN 3042 Aerospace series Quality assurance EN aerospace products Qualification procedureEN 3114-1 Aerospace series Test method Microstructure of ( + ) titanium

17、 alloy wrought products Part 1: General requirements 1)EN 3114-2 Aerospace series Test method - Microstructure of ( + ) titanium alloy wrought products Part 2: Microstructure of bars, sections, forging stock and forgings 1)EN 3238 Aerospace series Test methods for metallic materials Shear test for r

18、ivet wires andrivets in metallic material except aluminium and aluminium alloys 2)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 4prEN 4800-2: 20

19、02EN 3683 Aerospace series Test methods Titanium alloy wrought products Determination ofprimary content Point count method and line intercept method 1)EN 3684 Aerospace series Test methods Titanium alloy wrought products Determination of transus temperature Metallographic method 1)EN 3874 Aerospace

20、series Test methods for metallic materials Constant amplitude force-controlled low cycle fatigue testing 1)EN 3976 Aerospace series Titanium and titanium alloys Test method Chemical analysis for thedetermination of hydrogen content 1)EN 3987 Aerospace series Test method for metallic materials Consta

21、nt amplitude force-controlled high cycle fatigue testing 2)EN 3988 Aerospace series Test methods for metallic materials Constant amplitude strain-controlled low cycle fatigue testing 1)EN 4050-1 Aerospace series Test method for metallic materials Ultrasonic inspection of bars,plates, forging stock a

22、nd forgings Part 1: General requirements 1)EN 4050-4 Aerospace series Test method for metallic materials Ultrasonic inspection of bars,plates, forging stock and forgings Part 4: Acceptance criteria 1)EN 4258 Aerospace series Metallic materials General organization of standardization Linksbetween typ

23、es of EN standards and their useEN 4259 Aerospace series Metallic materials Definition of general terms 1)EN 4268 Aerospace series Metallic materials Heat treatment facilities General requirements 2)TR 2410 Aerospace series Metallic materials Relationship between dimensional standards andmaterial st

24、andards 3)3 DefinitionsGeneral definition, see EN 4259.4 Wording of orderThe order shall clearly indicate: quantities to be supplied; dates of delivery; material standard number; delivery condition and metallurgical code of products; dimensions and tolerances or reference to an appropriate dimension

25、al standard; product designation, when required; forwarding address; nature and type of packing, if required; definition and frequency of any special tests and their retest procedures, if required.5 Health and safetyProducts in the delivery condition shall fulfil the health and safety laws of the ar

26、ea of the country when andwhere it is to be delivered.A product safety data sheet shall be available.1) Published as AECMA Prestandard at the date of publication of this standard2) In preparation at the date of publication of this standard3) Published as AECMA Technical Report at the date of publica

27、tion of this standardCopyright 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 5prEN 4800-2: 20026 Technical requirements6.1 GeneralThe product shall be man

28、ufactured in accordance with the requirements of the relevant material standardand the applicable requirements of this specification. A manufacturing schedule shall be established andapplied in accordance with EN 2078.Product shall satisfy the requirements of the material standard and/or order and s

29、hall be free fromirregularities 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 alater stage, to contain such defects shall be rejected.Unless otherwise specified, the requirem

30、ents in tables 1 and 2 shall apply in conjunction with those of therelevant material standard. Table 1 relates to lines 1 to 29 (inclusive) of the material standard and table 2relates to lines 30 onwards in which the sub-line format is also used. Lines 2 to 98 may also be opened inline 100 if the ma

31、terial standard details specific qualification requirements. If a specific line number is notshown in tables 1 and 2, the requirement is stated in the material standard and/or order.The requirements of the order and/or material standard shall over-ride the requirements of the technicalspecification.

32、6.2 Qualification requirementsQualification 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 onthe first 3 batches, coming from 3 different ingots.6.3 Rel

33、ease requirements6.3.1 Release testsRelease testing shall be the responsibility of the manufacturer.The purchaser reserves the right to perform any of the inspections and/or tests required by the materialstandard and/or order.The test samples shall be representative of the product.When required the

34、manufacturer shall inform the purchaser of the planned dates for extraction of samplesand 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 specificallyrequested by the purchaser, a particul

35、ar inspection and/or test for release shall be carried out ifcorresponding acceptance criteria and/or values are stated in the applicable material standard, but see also6.3.5 “Capability clause“.6.3.2 RetestsIf the test procedure or test piece preparation is faulty, testing shall be re-applied at th

36、e original frequencyafter rectification of the original cause of failure.When failure cannot be attributed to faulty testing, or test piece preparation, further test samples shall beselected at twice the original frequency from the product, one of which shall be that on which the originalresults wer

37、e obtained unless already withdrawn by the manufacturer after suitable identification of the causeof failure. If all retest results are satisfactory, the batch shall be accepted. If one or more tests areunsatisfactory, the batch shall be: rejected, or 100 % retested and the conforming products accep

38、ted, or partially or fully re-heat treated if heat treatment can rectify the cause of the failure and tested as acompletely new batch except for chemical composition, for which redetermination of hydrogen contentis required. No product or test sample shall be re-heat treated more than twice.Copyrigh

39、t 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 6prEN 4800-2: 20026.3.3 RejectionAny failure to meet the requirements of the material standard shall be ca

40、use for rejection.6.3.4 Special testsSpecial tests may be required by the purchaser. In such cases, the nature of the test, method, frequency andtechnical requirements shall be specified on the order or inspection schedule and shall be mutually agreedby the manufacturer and purchaser.6.3.5 Capabilit

41、y clauseWhere capability clause is invoked and where sufficient statistical evidence exists, the test shall not becarried out (unless specifically requested by the purchaser). However, this in no way reduces the obligationsof the manufacturer to fulfil the requirements. If subsequent testing indicat

42、es that the product does notcomply 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 betweenthe manufacturer and the purchaser.6.3.6 Statistical process controlReduction in the extent of release t

43、esting, other than that defined in 6.3.5 above, may be negotiated with thepurchaser on the basis of appropriate statistical process control and/or statistical data.6.3.7 Inspection and test reportThe manufacturer shall furnish, with each delivery, a report conforming to the requirements of EN 2078st

44、ating the following: manufacturers name and address and, if appropriate, identification of the plant; order number; material standard number; delivery condition and metallurgical code of the product; quantity and dimensions; manufacturing and inspection schedule reference; cast and batch number; bat

45、ch and/or test samples heat treatment condition; results of the tests and retests if any.6.4 TraceabilityEach product shall be traceable to the cast, production batch and/or heat treatment batch at all stages ofmanufacture, testing and delivery.Copyright Association Europeene des Constructeurs de Ma

46、teriel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 7prEN 4800-2: 2002Table 1 Technical requirements for lines 1 to 29, where appropriateFrequency of testingMaterial standard linereferenceNo TitleRequireme

47、ntsQualification Release1 Material designation See EN 2032-1. The test samples used for chemical analysis shall be representative of the product and shall be taken fromlocation corresponding to top and bottom of each ingot produced after the final melting stage. The methodof chemical analysis shall

48、be at the discretion of the manufacturer unless otherwise stated in the materialstandard or order. In cases of dispute, the method of chemical analysis shall be agreed between themanufacturer and purchaser preferably using existing chemical analysis standards. The measuredchemical composition shall be stated on the certificate of conformance.2 per cast 2 per cast2 Chemical compositionSpecific requirements for hydrogen content:The hydrogen content shall be determined on each batch in the delivery condition in accordance withEN 3976.1 per batch 1 per batch3 Metho