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Tiêu đề Heat Resisting Steel Fe-Pa2601 (X6NiCrTiMoV26-15)
Trường học The British Standards Institution
Chuyên ngành Aerospace Engineering
Thể loại British Standard
Năm xuất bản 2008
Thành phố London
Định dạng
Số trang 10
Dung lượng 447,42 KB

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BS EN 2398 2008 ICS 49 025 10 NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAW BRITISH STANDARD Aerospace series — Heat resisting steel FE PA2601 (X6NiCrTiMoV26 15) — Rm = 900 MP[.]

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BS EN 2398:2008

ICS 49.025.10

NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAW

BRITISH STANDARD

Aerospace series

— Heat resisting

steel FE-PA2601

(X6NiCrTiMoV26-15) —

Rm = 900 MPa — Bars

for machined bolts —

D = 25 mm

Incorporating

January 2011 corrigendum

BS EN 2398:2008

Incorporating corrigenda January 2011 and February 2013

Aerospace series

— Heat resisting

steel FE-PA2601

(X6NiCrTiMoV26-15) —

Rm ≥ 900 MPa — Bars

for machined bolts —

D ≤ 25 mm

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BS EN 2398:2008

National foreword

This British Standard is the UK implementation of EN 2398:2008.

The UK participation in its preparation was entrusted to Technical Committee ACE/61, Metallic materials for aerospace purposes.

A list of organizations represented on this committee can be obtained on request to its secretary.

This publication does not purport to include all the necessary provisions

of a contract Users are responsible for its correct application.

Compliance with a British Standard cannot confer immunity from legal obligations.

Together with BS EN 2399:2008, it supersedes BS HR 650:1972, which

is withdrawn.

This British Standard

was published under

the authority of the

Standards Policy and

Strategy Committee on 30

September 2009

© BSI 2011

Amendments/corrigenda issued since publication

31 January 2011 Addition of supersession details to national foreword

ISBN 978 0 580 73738 1

BS EN 2398:2008

National foreword

This British Standard is the UK implementation of EN 2398:2008.

The UK participation in its preparation was entrusted to Technical Committee ACE/61, Metallic materials for aerospace purposes.

A list of organizations represented on this committee can be obtained on request to its secretary.

This publication does not purport to include all the necessary provisions

of a contract Users are responsible for its correct application.

Compliance with a British Standard cannot confer immunity from legal obligations.

Together with BS EN 2399:2008, it supersedes BS HR 650:1972, which

is withdrawn.

This British Standard

was published under

the authority of the

Standards Policy and

Strategy Committee on 30

September 2009

© BSI 2011

Amendments/corrigenda issued since publication

31 January 2011 Addition of supersession details to national foreword

ISBN 978 0 580 73738 1

BS EN 2398:2008

ISBN 978 0 580 81193 7

Amendments/corrigenda issued since publication

31 January 2011 Addition of supersession details to national foreword

30 June 2013 Implementation of CEN reissued title page

This British Standard was

published under the authority

of the Standards Policy and

Strategy Committee on

30 September 2009

© The British Standards

Institution 2013

Published by BSI Standards

Limited 2013

The UK participation in its preparation was entrusted by Technical Committee ACE/61, Metallic materials for aerospace purposes, to Subcommittee ACE/61/-/15, Steels for Aerospace Purposes.

A list of organizations represented on this subcommittee can be obtained

on request to its secretary.

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EUROPEAN STANDARD

NORME EUROPÉENNE

EUROPÄISCHE NORM

EN 2398

March 2008

ICS 49.025.10

English Version

Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm = 900 MPa - Bars for machined bolts

- D = 25 mm

Série aérospatiale - Acier résistant à chaud FE-PA2601

(X6NiCrTiMoV26-15) - Rm = 900 MPa - Barres pour

boulonnerie usinée D = 25 mm

Luft- und Raumfahrt - Hochwarmfester Stahl FE-PA2601 (X6NiCrTiMoV26-15) - Rm = 900 MPa - Stangen zur Spanabhebenden Formgebung für Schrauben - D = 25 mm

This European Standard was approved by CEN on 10 November 2007

CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member

This European Standard exists in three official versions (English, French, German) A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions

CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom

EUROPEAN COMMITTEE FOR STANDARDIZATION

C O M IT É E U R O P É E N D E N O R M A LIS A T IO N EUROPÄISCHES KOMITEE FÜR NORMUNG

Management Centre: rue de Stassart, 36 B-1050 Brussels

© 2008 CEN All rights of exploitation in any form and by any means reserved

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BS EN 2398:2008

EN 2398:2008 (E)

2

Foreword

This document (EN 2398:2008) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN)

After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN

This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by September 2008, and conflicting national standards shall be withdrawn at the latest by September 2008

Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights

According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom

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BS EN 2398:2008

EN 2398:2008 (E)

3

Introduction

This standard is part of the series of EN metallic material standards for aerospace applications The general organization of this series is described in EN 4258

This standard has been prepared in accordance with EN 4500-3

1 Scope

This standard specifies the requirements relating to:

Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15)

Rm ≥ 900 MPa Bars for machined bolts

D ≤ 25 mm

for aerospace applications

2 Normative references

The following referenced documents are indispensable for the application 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 2002-16, Aerospace series — Metallic materials — Test methods — Part 16: Non-destructive testing — Penetrant testing. 1)

EN 2344, Aerospace series — Round bars, machined in heat resisting alloys — Diameter 10 mm D 180 mm — Dimensions

EN 2399, Aerospace series — Heat resisting steel FE-PA92-HT — Rm ≥ 900 MPa — Bars for forged bolts

D 25 mm 2)

EN 2951, Aerospace series — Metallic materials — Test method — Micrographic determination of content of non-metallic inclusions 1)

EN 4258, Aerospace series — Metallic materials — General organization of standardization — Links between types of EN standards and their use

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 4500-3, Aerospace series — Metallic materials — Rules for drafting and presentation of material standards — Part 3: Specific rules for heat resisting alloys 1)

EN 4700-2, Aerospace series — Steel and heat resisting alloys — Wrought products — Technical specification — Part 2: Bar and section.1)

1) Published as ASD Prestandard at the date of publication of this standard

2) Published as ASD Standard at the date of publication of this standard

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BS EN 2398:2008

EN 2398:2008 (E)

4

2 Chemical

composition

%

Delivery condition Softened, cold worked, solution treated

and machined Softened, cold worked, solution treated, precipitation treated and machined 6.1

Heat treatment

900 °C ± 10 °C / t = 1 h / air cool or faster

Cold worked d + 980 °C ± 10 °C / t = 1 h / air cool or faster

900 °C ± 10 °C / t = 1 h / air cool or faster

Cold worked d + 980 °C ± 10 °C / t = 1 h / air cool or faster + 720 °C ± 10 °C / t = 16 h / air cool

Use condition Softened, cold worked d, solution treated,

precipitation treated and machined Delivery condition

7

16

T

26

C

Elongation at

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BS EN 2398:2008

EN 2398:2008 (E)

5

(micro cleanliness)

6 A or D may be tested either on the products or at an earlier stage of manufacturing

98 Notes – a Bracketed figures indicate composition expressed as parts per million (p.p.m.) The method

of analysis for lead shall be agreed between manufacturer and purchaser

b The method of melting required shall be agreed between manufacturer and purchaser

c Bars for upset forgings are defined by EN 2399

d After the softening treatment, all bars shall be reduced 15 % to 25 % in cross section during final drawing or rolling at a temperature of not more than 870 °C

e Combination notched/unnotched test piece; rupture shall occur in the unnotched portion of test piece Stess may be increased after 48 h to promote rupture

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BS EN 2398:2008

EN 2398:2008 (E)

6

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This page has been intentionally left blank

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