AECMA PREN 4800-4-2002 Aerospace Series Titanium and Titanium Alloys Technical Specification Part 4 Wire Edition P1 [Replaced ASD-STAN PREN 3544-5]《航空航天系列.钛和钛合金 技术规范.第4部分 线材.P1版》.pdf

《AECMA PREN 4800-4-2002 Aerospace Series Titanium and Titanium Alloys Technical Specification Part 4 Wire Edition P1 [Replaced ASD-STAN PREN 3544-5]《航空航天系列.钛和钛合金 技术规范.第4部分 线材.P1版》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 4800-4-2002 Aerospace Series Titanium and Titanium Alloys Technical Specification Part 4 Wire Edition P1 [Replaced ASD-STAN PREN 3544-5]《航空航天系列.钛和钛合金 技术规范.第4部分 线材.P1版》.pdf（21页珍藏版）》请在麦多课文档分享上搜索。

1、AECMA STANDARDNORME AECMAAECMA NORMprEN 4800-3Edition 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 3: TubeSrie arospatialeTitane et alliages de titaneSpcification techniquePartie 3: TubesLuft- und RaumfahrtTitan und Titanlegierungen KneterzeugnisseTechnische LieferbedingungenTeil 3: RohreThis “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA-ST

3、AN (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 the publication of this Prestandard,

4、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 adraft European Standard to CEN (European

5、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 the date of publication toAECMA-STANG

6、ulledelle 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-,-,-Page 2prEN 4800-3: 2002ContentsPage0 Int

7、roduction. 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 appropriate . 16Copyright Association E

8、uropeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3prEN 4800-3: 20020 IntroductionThis standard is part of the series of EN metallic material standards for aerospace appli

9、cations. The generalorganisation 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 tubes. It shall be applied when referred to and in conjunction with the EN materialstand

10、ard 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 appropriate places in the text and the publications are l

11、istedhereafter. 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 referred to applies.ISO 6772 Aerospace Fluid syst

12、ems Impulse testing of hydraulic hose, tubing and fittingassembliesEN 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 A

13、erospace series Test methods for metallic materials Part 2: Tensile testing at elevatedtemperature 1)EN 2002-8 Aerospace series Metallic materials Test methods Part 8: Micrographic determinationof grain size 1)EN 2002-17 Aerospace series Test methods for metallic materials Tube used under pressure P

14、art 17: Integrity test 1)EN 2002-18 Aerospace series Test methods for metallic materials Part 18: Hydraulic distension testfor tube 1)EN 2002-20 Aerospace series Test methods for metallic materials Part 20: Eddy current testing ofcircular cross-section tubes 1)EN 2003-9 Aerospace series Test methods

15、 Titanium and titanium alloys Part 9 : Determination ofsurface contamination 1)EN 2032-1 Aerospace series Metallic materials Part 1: Conventional designationEN 2032-2 Aerospace series Metallic materials Part 2: Coding of metallurgical condition in deliveryconditionEN 2078 Aerospace series Metallic m

16、aterials Manufacturing schedule, inspection schedule,inspection and test report Definition, general principles, preparation and approvalEN 2955 Aerospace series Recycling of titanium and titanium alloy scrapEN 3042 Aerospace series Quality assurance EN aerospace products Qualification procedureCopyr

17、ight 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 4800-3: 2002EN 3114-1 Aerospace series Test method Microstructure of ( + ) titanium alloy wrought

18、 products Part 1: General requirements 1)EN 3684 Aerospace series Test methods Titanium alloy wrought products Determination of transus temperature Metallographic method 1)EN 3718 Aerospace series Test method for metallic materials Ultrasonic inspection of tubes 1)EN 3976 Aerospace series Titanium a

19、nd titanium alloys Test method Chemical analysis for thedetermination of hydrogen content 1)EN 4258 Aerospace series Metallic materials General organization of standardization Linksbetween types of EN standards and their useEN 4259 Aerospace series Metallic materials Definition of general terms 1)EN

20、 4268 Aerospace series Metallic materials Heat treatment facilities General requirements 2)EN 10233 Metallic Materials Tube Flattening TestEN 10234 Metallic Materials Tube Drift Expanding TestTR 2410 Aerospace series Metallic materials Relationship between dimensional standards andmaterial standards

21、 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 dimensional stan

22、dard; product designation, when required; forwarding address; nature and type of packing, if required;5 Health and safetyProducts in the delivery condition shall fulfil the health and safety laws of the area of the country when andwhere it is to be delivered.A product safety data sheet shall be avai

23、lable.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 publication of this standardCopyright Association Europeene des Constructeurs de Materiel Aerospatial

24、Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5prEN 4800-3: 20026 Technical requirements6.1 GeneralThe product shall be manufactured in accordance with the requirements of the relevant material standardand the applicab

25、le 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 shall be free fromirregularities prejudicial to the subsequent manufacture or use of this produc

26、t.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 requirements in tables 1 and 2 shall apply in conjunction with those of therelevant material standard.

27、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 material standard details specific qualification requirements. If a specific line number is notsh

28、own 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.6.2 Qualification requirementsQualification requirements when invoked by the material standard

29、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 Release requirements6.3.1 Release testsRelease testing shall be the responsibility of the manufact

30、urer.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 manufacturer shall inform the purchaser of the planned dates for extraction of samplesand relea

31、se 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 particular inspection and/or test for release shall be carried out ifcorresponding acceptance criteria

32、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 the original frequencyafter rectification of the original cause of failure.When failure cannot be

33、 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 were obtained unless already withdrawn by the manufacturer after suitable identification of the ca

34、useof 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 accepted, or partially or fully re-heat treated if heat treatment can rectify the cause of the failu

35、re 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.Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under licens

36、e with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6prEN 4800-3: 20026.3.3 RejectionAny failure to meet the requirements of the material standard shall be cause for rejection.6.3.4 Special testsSpecial tests may be required by the purchaser. In such c

37、ases, 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 Capability clauseWhere capability clause is invoked and where sufficient statistical evidence exists, t

38、he 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 indicates that the product does notcomply with the requirements, the batch shall be rejected.If suffi

39、cient 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 testing, other than that defined in 6.3.5 above, may be negotiated with thepurchaser on the bas

40、is 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 2078stating the following: manufacturers name and address and, if appropriate, identification of the

41、 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; batch and/or test samples heat treatment condition; results of the tests and retests if any.6.4 T

42、raceabilityEach 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 Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or ne

43、tworking permitted without license from IHS-,-,-Page 7prEN 4800-3: 2002Table 1 Technical requirements for lines 1 to 29, where appropriateFrequency of testingMaterial standard linereferenceNo TitleRequirementsQualification Release1 Material designation See EN 2032-1. The test samples used for chemic

44、al 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 be at the discretion of the manufacturer unless otherwise stated in the materialstandard or or

45、der. 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 compositionSpecifi

46、c 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 Method of melting Method of melting consists of multiple melt using combination of non-consumable electrode, consumableelectrode and

47、 cold hearth (electron beam or plasma arc) melting practices. Some of the followingrequirements are dependent on the actual melting route, non-consumable electrode melting should beused for consolidation purpose only.1 Raw material:Raw materials shall be purchased only from suppliers approved by the

48、 manufacturer and registered inhis list of approved suppliers.Approval of suppliers shall be made in accordance with written procedures contained within the qualityassurance system of the manufacturer.Titanium sponge and alloying elements:The requirements shall be specified by the manufacturer who shall also establish the followingprocedures for the evaluation and acceptance testing of each batch. titanium sponge: manufacturing method, level of impurities, particle size, freedom from surfacecontamination ; alloying elements: chemical composition including level of impurities, particle si