Bsi bs en 02933 1996 (1999)

www bzfxw com BRITISH STANDARD AEROSPACE SERIES BS EN 2933 1996 Bolts, T head, relieved shank, long thread, in heat resisting nickel base alloy NI P100HT (Inconel 718) — Classification 1275 MPa (at am[.]

BRITISH STANDARD AEROSPACE SERIES BS EN

2933:1996

Bolts, T-head, relieved

shank, long thread, in

heat resisting nickel

base alloy NI-P100HT

(Inconel 718) —

Classification:

1275 MPa (at ambient

temperature)/650 °C

The European Standard EN 2933:1996 has the status of a

British Standard

ICS 49.040.20

This British Standard, having

been prepared under the

direction of the Engineering

Sector Board, was published

under the authority of the

Standards Board and

comes into effect on

15 June 1996

© BSI 12-1999

The following BSI references

relate to the work on this

standard:

Committee reference ACE/12

Draft for comment 88/76308 DC

ISBN 0 580 25929 3

Committees responsible for this British Standard

The preparation of this British Standard was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, upon which the following bodies were represented:

Association of Electronic, Telecommunications and Business Equipment Industries

British Industrial Fasteners Federation Ministry of Defence

Society of British Aerospace Companies

Amendments issued since publication

Amd No Date Comments

BS EN 2933:1996

Contents

Page

National foreword

This British Standard has been prepared by Technical Committee ACE/12 and is

the English language version of EN 2933:1996 Aerospace series — Bolts,

T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718) — Classification: 1 275 MPa (at ambient temperature)/650 °C, published by the European Committee for

Standardization (CEN)

EN 2933:1996 was produced as a result of international discussions in which the United Kingdom took an active part

A British Standard does not purport to include all the necessary provisions of a contract Users of British Standards are responsible for their correct application

Compliance with a British Standard does not of itself confer immunity from legal obligations.

Cross-references Publication referred to Corresponding British Standard

EN 2424:1995 BS EN 2424:1995 Marking of aerospace products

ISO 3353:1992 BS 2A 231:1993 Rolled threads and bolts Lead and

runout requirements

ISO 5855-2:1988 BS 6293 Aerospace MJ threads

Part 2:1994 Limit dimensions for bolts and nuts

Summary of pages

This document comprises a front cover, an inside front cover, pages i and ii, the EN title page, pages 2 to 8, an inside back cover and a back cover

This standard has been updated (see copyright date) and may have had amendments incorporated This will be indicated in the amendment table on the inside front cover

EUROPEAN STANDARD

NORME EUROPÉENNE

EUROPÄISCHE NORM

EN 2933 March 1996

ICS 49.040.20

Descriptors: Aircraft industry, screw, nickel alloy, heat resistant material, classification, dimension, designation

English version Aerospace series — Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718) — Classification: 1 275 MPa

(at ambient temperature)/650 °C

(ISO 2861:1988)

Série aérospatiale- Vis à tête en T, fût dégagé

filetage long, en alliage résitant à chaud à base

e nickel NI-P100HT (Inconel 718) —

Classification: 1 275 MPa (à temperature

ambiante)/650 °C

Luft-und Raumfahrt — T-Kopfschrauben, Dünnschaft, langes Gewinde, aus

hochwarmfester Nickelbasislegierung NI-P100HT (Inconel 718) — Klasse: 1 275 MPa (bei Raumtemperatur)/650 °C

This European Standard was approved by CEN on 1995-08-31 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 Central Secretariat 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 Central Secretariat has the same status as the official versions

CEN members are the national standards bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom

CEN

European Committee for Standardization Comité Européen de Normalisation Europäisches Komitee für Normung

Central Secretariat: rue de Stassart 36, B-1050 Brussels

© 1996 Copyright reserved to CEN members

Ref No EN 2933:1996 E

Foreword

This European Standard has been prepared by the

European Association of Aerospace

Manufacturers (AECMA)

After inquiries and votes carried out in accordance

with the rules of this Association, this Standard has

successively received the approval of the National

Associations and the Official Services of the

members countries of AECMA, 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 1996, and conflicting national standards

shall be withdrawn at the latest by September 1996

According to the CEN/CENELEC Internal

Regulations, the national standards organizations

of the following countries are bound to implement

this European Standard: Austria, Belgium,

Denmark, Finland, France, Germany, Greece,

Iceland, Ireland, Italy, Luxembourg, Netherlands,

Norway, Portugal, Spain, Sweden, Switzerland and

United Kingdom

EN 2933:1996

1 Scope

This standard specifies the characteristics of T-headed bolts with relieved shank, long thread,

in NI-P100HT, for aerospace applications

Classification: 1 275 MPa1)/650 °C2)

2 Normative references

This 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 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 publication referred to applies

ISO 3353, Aerospace — Rolled threads for bolts — Lead and runout requirements

ISO 5855-2, Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts

EN 2424, Aerospace series — Marking of aerospace products

EN 2583, Aerospace series — Bolts in heat resisting nickel base alloy NI-P100HT (Inco 718) —

Classification: 1 275 MPa/650 °C — Technical specification3)

EN 2952, Aerospace series — Heat resisting alloy NI-PH2601 — Solution treated and cold worked — Bar

for forged fasteners — D k 50 mm — 1 270 MPa k R m k 1 550 MPa3)

EN 3219, Aerospace series — Heat resisting nickel base alloy (NI-P100HT) — Cold worked and softened —

Bar and wire for continuous forging or extrusion for fasteners – 3 k D k 30 mm3)

3 Required characteristics

3.1 Configuration — Dimensions — Tolerances — Masses

See Figure 1 and Table 1 and Table 2 Dimensions and tolerances are in millimetres

3.2 Materials

EN 2952 or EN 3219

Table 1

1) Minimum tensile strength of the material at ambient temperature

2) Maximum test temperature of the parts

3) Published as AECMA Prestandard at the date of publication of this standard

Code Designation ± 0,1 ± 0,13 ± 0,5

0,003

0,12

0,15

1 0MJ10×1,25-4h6h0 11,1 9,19 16,5 5,3 7,9 13 0,0025

a In accordance with ISO 5855-2

+0,5

0 +0,50 +0,30

Figure 1

Table 2 Length code N

4,42

6,61

9,55

13,59

24,55

a Mass quoted in kg/1 000 parts

EN 2933:1996

4 Designation

EXAMPLE:

NOTE If necessary, the code 19005 shall be placed between the description block and the identity block.

5 Marking

EN 2424, style A, as indicated on Figure 1

6 Technical specification

EN 2583

BS EN 2933:1996

© BSI 12-1999

List of references

See national foreword

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