1、 ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN TR 4858 Edition P1 March 2018 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Rue Montoyer 10 - 1000 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8131 - www.asd-stan.org ICS: Descriptors: ENGLISH
2、VERSION Aerospace series Pipe couplings materials and surface treatments Luft- und Raumfahrt Rohrverschraubungen, Werkstoffe und Oberflchenschutz Srie arospatiale Systme de raccordement, commandes de vol matriaux et traitements de surface This “Aerospace Series” Prestandard has been drawn up under t
3、he responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published 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 publica
4、tion 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 review by users and formal agreement of ASD-STAN, the ASD-STAN prEN will be submitted as
5、 a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any nati
6、onal standards conflicting with the EN. ASD-STAN Technical Committee approves that: “This document is published by ASD-STAN for the needs of the European Aerospace Industry. The use of this standard is entirely voluntary, and its applicability and suitability for any particular use, including any pa
7、tent infringement arising therefrom, is the sole responsibility of the user.” ASD-STAN reviews each standard and technical report at least every five years at which time it may be revised, reaffirmed, stabilized or cancelled. ASD-STAN invites you to send your written comments or any suggestions that
8、 may arise. All rights reserved. No parts of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without prior written permission of ASD-STAN. Order details: E-mail: salesasd-stan
9、.org Web address: http:/www.asd-stan.org/ Edition approved for publication 1stMarch 2018 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain TR 4858:2018 (E) 2 Contents Page Foreword 3 Avant-propos. 3 Vorwort . 3 1 Scope 4 1 Domaine dapplication 4 1
10、Anwendungsbereich 4 2 Normative references 5 2 Rfrences normatives . 6 2 Normative Verweisungen . 6 3 Codes for designation origins . 7 3 Codes origines de la dsignation . 7 3 Kodifizierung fr Herkunftsangaben . 7 4 Low alloy steels/Aciers faiblement allis/Niedriglegierte Sthle . 8 5 Corrosion resis
11、ting steels/Aciers rsistant la corrosion/Korrosionsbestndige Sthle . 9 6 Low alloy steels of carburizing/Aciers faiblement allis de cmentation/Niedriglegierte Sthle Einsatzhrtung 11 7 Low alloy steels for structure/Aciers faiblement allis de construction/Niedriglegierte Sthle fr Struktur Bauweise 12
12、 8 Titanium alloy/alliage de titane/Titanlegierung . 13 9 Sealing Material/Matriau de scellement/Dichtungsmaterial . 14 10 Mechanical characteristics . 15 10 Caractristiques mcaniques. 15 10 Mechanische Eigenschaften 15 11 Surface treatments/Traitements de surface/Oberflchenbehandlung . 16 12 Qualif
13、ication . 17 12 Qualification . 17 12 Qualifizierung 17 Bibliography Bibliographie Literaturhinweise . 18 TR 4858:2018 (E) 3 Foreword The main task of ASD-STAN Domains is to prepare EN standards. In exceptional circumstances, however, the publication of a Technical Report of one of the following typ
14、es may be proposed: type 1, the subject is still under technical development requiring wider exposure; type 2, a Domain has collected data of a different kind from that which is normally published as a European Standard. Hydraulic Domain decided to publish this document in the form of a Technical Re
15、port of type 2 in order to facilitate the updating of this document. Avant-propos La tche principale des Domaines ASD-STAN est dlaborer des normes EN. Cependant, titre exceptionnel, la publication dun Rapport Technique de lun des types suivants peut tre propose: type 1, le sujet en question est enco
16、re en cours de dveloppement technique et requiert une plus grande exprience ; type 2, un Domaine a runi des donnes de nature diffrente de celles qui sont normalement publies comme norme europenne. Le Domaine Hydraulique a dcid de publier ce document sous la forme dun Rapport Technique de type 2 pour
17、 en faciliter la mise jour. Vorwort Die Hauptaufgabe der Domain der ASD-STAN ist es, EN-Normen zu erarbeiten. In Sonderfllen kann jedoch die Verffentlichung eines Fachberichtes folgender Typen beantragt werden: Typ 1, das betroffene Thema befindet sich noch in technischer Entwicklung und bentigt wei
18、tere Erfahrung; Typ 2, das Domain hat Angaben zusammengetragen, die blicherweise nicht Gegenstand einer europischen Norm sind. Das Mechanik Domain Hydraulik hat beschlossen, dieses Dokument in Form eines Fachberichtes von Typ 2 zu verffentlichen, um dessen berarbeitung zu erleichtern. TR 4858:2018 (
19、E) 4 1 Scope This Technical Report gives the EN standardized materials or, on the national level, the materials standardized by ASD member countries to be used for manufacturing the relevant products to insure their functional interchangeability. This Technical Report is not to be taken as a table o
20、f equivalent materials. The use of EN standardized materials shall be given priority. This Technical Report applies when it is referenced. 1 Domaine dapplication Le prsent Rapport Technique indique les matriaux normaliss EN ou, sur le plan national, les matriaux normaliss par les pays membres de lAS
21、D utiliser pour la fabrication des produits concerns afin dassurer leur interchangeabilit fonctionnelle. Il ne sagit pas dune table dquivalence de matriaux. Les matriaux normaliss EN doivent tre utiliss en priorit. Le prsent Rapport technique sapplique chaque fois quil est cit en rfrence. 1 Anwendun
22、gsbereich Dieser Fachbericht fhrt die EN genormten Werkstoffe und die von den ASD Lndern auf nationaler Ebene genormten Werkstoffe auf, die angewandt werden, um Erzeugnisse herzustellen, die ihre funktionelle Austauschbarkeit gewhrleisten. Er ist nicht als ein Verzeichnis austauschbarer Werkstoffe z
23、u verwenden. EN-genormte Werkstoffe sind vorrangig zu verwenden. Dieser Fachbericht ist immer dann anzuwenden, wenn auf ihn verwiesen wird. TR 4858:2018 (E) 5 2 Normative references The following documents are referred to in the text in such a way that some or all of their content constitutes requir
24、ements of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2399, Aerospace series Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) Rm 900 MPa Bars for forged bolts D 25 m
25、m EN 2407, Aerospace series Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) Solution treated and precipitation treated Sheet, strip and plate 0,2 mm a 10 mm EN 2491, Aerospace series Molybdenum disulphide dry lubricants Coating methods EN 2662, Aerospace series Heat resisting alloy NI-PH3601 (NiCr
26、22Mo9Nb) Annealed Sheet, strip and plate 0,2 mm a 10 mm EN 2663, Aerospace series Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Solution treated Sheet, strip and plate 0,2 mm a 10 mm EN 2694, Aerospace series Aluminium alloy AL-P6061-T6 or T62 Sheet and strip 0,4 mm a 6 mm EN 2786, Aerospace series E
27、lectrolytic silver plating of fasteners EN 2798, Aerospace series Fluorocarbon rubber (FKM) Low compressions set Hardness 80 IRHD EN 3021, Aerospace series Molybdenum disulphide dry film lubricants graphite and halogen free Technical specification EN 3311, Aerospace series Titanium alloy TI-P64001 (
28、Ti-6Al-4V) Annealed - Bar for machining D 110 mm EN 3112, Aerospace series Bolts, normal hexagonal head, threaded to head, in alloy steel, cadmium plated Classification: 900 MPa (at ambient temperature)/235 C EN 3314, Aerospace series Titanium alloy TI-P64001, solution treated and aged; bar for mach
29、ining D 75 mm EN 3315, Aerospace series Titanium alloy TI-P64001, solution treated and aged Forgings De 75 mm EN 3120, Aerospace series Titanium alloy TI-P64003 Cold worked and stress relieved Seamless tube for pressure systems 4 mm D 51 mm 690 MPa Rm 1 030 MPa EN 3363, Steel FE-CM68 solution treate
30、d Rm 485 MPa Sand or investment casting EN 3468, Steel FE-PA13 softened 500 Rm 700 MPa Forgings De 100 mm EN 3487, Aerospace series Steel FE-PA3601 (X6CrNiTi18-10) Air melted Softened Bar for machining a or D 250 mm 500 MPa Rm 700 MPa TR 4858:2018 (E) 6 EN 3671, Aerospace series Heat resisting alloy
31、 NI-PH3601 (NiCr22Mo9Nb) Non heat treated Forging stock a or D 250 mm EN 3761, Aerospace series Heat resisting alloy FE-PA2601, softened and cold worked; bar for forged fasteners D 50 mm, 1100 MPa Rm 1300 MPa EN 4315, Aerospace series Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treate
32、d and precipitation treated, bar and section a or D 100 mm, Rm 900 MPa EN 4318, Aerospace series Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated, bar and section De 100 mm, Rm 960 MPa EN 4379, Aerospace series Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
33、Solution treated, forging De 200 mm EN 10027-1, Designation systems for steels Part 1: Steel names TR 3900, Metallic materials Relationship between AECMA designation systems1)2 Rfrences normatives Les documents de rfrence suivants sont indispensables pour lapplication du prsent document. Pour les rf
34、rences dates, seule ldition cite sapplique. Pour les rfrences non dates, la dernire dition du document de rfrence sapplique (y compris les ventuels amendements). 2 Normative Verweisungen Die folgenden Dokumente werden im Text in solcher Weise in Bezug genommen, dass einige Teile davon oder ihr gesam
35、ter Inhalt Anforderungen des vorliegenden Dokuments darstellen. Bei datierten Verweisungen gilt nur die in Bezug genommene Ausgabe. Bei undatierten Verweisungen gilt die letzte Ausgabe des in Bezug genommenen Dokuments (einschlielich aller nderungen). 1) Published as ASD-STAN Technical Report at the
36、 date of publication of this European standard. http:/www.asd-stan.org/ TR 4858:2018 (E) 7 3 Codes for designation origins In Tables of this technical report, countries and other designation origins are designated with the following codes: ASD Aerospace and Defence Industries Association of Europe2)
37、; ECISS European Committee for Iron and Steel Standardization3); FR France; DE Germany; GB United Kingdom; US United States. 3 Codes origines de la dsignation Dans les tableaux du prsent rapport technique, les pays et les autres origines de la dsignation sont dsigns par les codes suivants: ASD Aeros
38、pace and Defence Industries Association of Europe2); ECISS European Committee for Iron and Steel Standardization3); FR France; DE Allemagne; GB Royaume-Uni; US tats-Unis. 3 Kodifizierung fr Herkunftsangaben In den Tabellen der Herausgabe dieses Fachberichts werden die Lnder und andere Herkunftsangab
39、en mit folgenden Kennbuchstaben bezeichnet: ASD Aerospace and Defence Industries Association of Europe2); ECISS European Committee for Iron and Steel Standardization3); FR Frankreich; DE Deutschland; GB Grobritannien; US Vereinigte Staaten. 2) For designations, see TR 3900./Pour les dsignations, voi
40、r TR 3900./Fr die Bezeichnungen, siehe TR 3900. 3) For designations, see EN 10027-1./Pour les dsignations, voir EN 10027-1./Fr die Bezeichnungen, siehe EN 10027-1. TR 4858:2018 (E) 8 4 Low alloy steels/Aciers faiblement allis/Niedriglegierte Sthle Table 1 Tableau 1 Tabelle 1 Application Application
41、Anwendung MaterialaMatriauaWerkstoffaDesignation origincOrigine de la dsignationcHerkunftsangabecDesignationbDsignationb Bezeichnungb Standard Norme Norm TBD aMaterial designation does not take into account designation of heat treatment condition, please consult the applicable specification./La dsig
42、nation matriau ne prend pas en compte la dsignation des conditions de traitement thermique, veuillez consulter la spcification applicable./Die Materialbezeichnung bercksichtigt nicht die Bezeichnung des Wrme-behandlungszustand, bitte die anzuwendende Specification beachten.bFormer designations are i
43、ndicated in brackets./Les anciennes dsignations sont indiques entre parenthses./Die vormaligen Bezeichnungen sind in Klammern angegeben.cSignification of these codes is indicated in Clause 4./La signification de ces codes est indique lArticle 4./Die Bedeutungdieser Kennbuchstaben ist in Abschnitt 4
44、angegeben.TR 4858:2018 (E) 9 5 Corrosion resisting steels/Aciers rsistant la corrosion/Korrosionsbestndige Sthle Table 2 Tableau 2 Tabelle 2 Application Application Anwendung MaterialaMatriauaWerkstoffaDesignation originc Origine de la dsignationcHerkunftsangabecDesignationbDsignationb Bezeichnungb
45、Standard Norme Norm Aerospace Series pipe couplings 37 in heat resistance steel; Inch Series Steel FE PA13 Softened De 100 mm 500 Rm 700 MPa - Forgings - EN 3468 similar to 1.4544.9/1.4549.9 C.R.S. AISI 321 AMS 5643 BS S129/S130 EN Aerospace Series pipe couplings 37 in heat resistance steel; Inch Se
46、ries Steel FE-PA3601 (X6 CrNiTi18-10) - Air melted - Softended - D 250 mm 500 Rm 700 MPa - Bar for machining EN 3487 similar to 1.4544.9/1.4546.9 C.R.S AISI 321 AMS 5645/AMS-QQ-S-763 BS S130 EN Aerospace Series Flange Couplings Swivel flange with fastener holes; or Weld couplings up to 21 000 kPa In
47、ch Series Heat resisting alloy FE-PA2601 - Softened and cold worked bar for forged fastener D 50 mm; 1 100 MPa Rm 1 300 MPa EN 3761 EN Aerospace Series Flange Couplings Swivel flange with fastener holes; or Weld couplings up to 21 000 kPa Inch Series Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)
48、 -Solution treated and precipitation treated, bar and section a or D 100 mm; Rm 900 MPa EN 4315 EN Aerospace Series Flange Couplings Swivel flange with fastener holes; or Weld couplings up to 21 000 kPa Inch Series Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) -Solution treated and precipitation treated, bar and section De 100 mm; Rm 960 MPa EN 4318 EN Aerospace Series Flange Couplings Swivel flange with fastener holes; or Weld couplings up to 21 000 kPa Inch Series Heat resisti
