00945928 PDF Li ce ns ed C op y A ki n K ok sa l, B ec ht el L td , 1 8 A pr il 20 03 , U nc on tr ol le d C op y, ( c) B S I BRITISH STANDARD AEROSPACE SERIES BS EN 3643 1997 Rivets, solid, 100° coun[.]
Trang 1Licensed Copy: Akin Koksal, Bechtel Ltd, 18 April 2003, Uncontrolled Copy, (c) BSI
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Trang 2BRITISH STANDARD AEROSPACE SERIES BS EN
3643:1997
Rivets, solid, 100°
countersunk normal
head, in titanium
TI-PO2, anodized, inch
based series
The European Standard EN 3643:1996 has the status of a
British Standard
ICS 49.030.99
Trang 3This 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 January 1997
© BSI 11-1998
The following BSI references
relate to the work on this
standard:
Committee reference ACE/12
Draft for comment 90/76226 DC
ISBN 0 580 27026 2
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 Electronics, Telecommunications and Business Equipment Industries
British Industrial Fasteners Federation Ministry of Defence
Society of British Aerospace Companies Ltd
Amendments issued since publication
Amd No Date Comments
Trang 4BS EN 3643:1997
Contents
Page Committees responsible Inside front cover
List of references Inside back cover
Trang 5ii © BSI 11-1998
National foreword
This British Standard has been prepared by Technical Committee ACE/12 and is
the English language version of EN 3643:1996 Aerospace series — Rivets,
solid, 100° countersunk normal head, in titanium TI-PO2, anodized, inch based series, published by the European Committee for Standardization (CEN).
EN 3643:1996 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 8080:1985 BS M 58:1986 Specification for anodic coating of
titanium and titanium alloys by the sulphuric acid process
Summary of pages
This document comprises a front cover, an inside front cover, pages i and ii, the EN title page, pages 2 to 6, 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
Trang 6EUROPEAN STANDARD
NORME EUROPÉENNE
EUROPÄISCHE NORM
EN 3643
September 1996
ICS 49.040.20
Descriptors: Aircraft industry, rivet, countersunk head rivet, titanium, characteristic, dimension, dimensional tolerance, designation
English version
Aerospace series – Rivets, solid, 100°
countersunk normal head, in titanium TI-PO2,
anodized, inch based series
Série aérospatiale — Rivets ordinaires, à tête
fraisée 100° normale, en titane TI-PO2;
anodisés, série base inches
Luft- und Raumfahrt — Vollniete, mit 100° normalem Senkopf, aus Titan TI-PO2, anodisiert, Zoll-Reihe
This European Standard was approved by CEN on 1996-06-29 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
The European Standards exist 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 3643:1996 E
Trang 72 © BSI 11-1998
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
received the approval of the National Associations
and the Official Services of the member 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
March 1997, and conflicting national standards
shall be withdrawn at the latest by March 1997
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
the United Kingdom
Trang 8EN 3643:1996
1 Scope
This standard specifies the characteristics of solid
rivets, with 100° countersunk normal head, in
titanium TI-PO2, anodized, inch based series, for
maximum operating temperature 315 °C
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 8080, Aerospace — Anodic treatment of
titanium and titanium alloys — Sulfuric acid
process.
ISO 10299, Aerospace — Identification marking of
solid rivets1)
EN 2424, Aerospace series — Marking of aerospace
products.
EN 3378, Aerospace series — Titanium TI-PO2 —
Annealed — 330 # R c # 410 MPa – Wire for
rivet — 1,6 # d # 10 mm2).
EN 3627, Aerospace series — Titanium solid
rivets — Technical specification1)
3 Required characteristics
3.1 Configuration — Dimensions — Masses
See Figure 1 and Table 1 and Table 2 Dimensions and tolerances are expressed in millimetres and apply after surface treatment
3.2 Material
EN 3378
3.3 Surface treatment
ISO 8080
1) In preparation at the date of publication of this standard
2) Published as AECMA Prestandard at the date of publication of this standard
Trang 94 © BSI 11-1998
Table 1 Figure 1
Diameter
code
D1 D2b D3 D4 D5 L2 L3 L4 L5 L6 R
max min min max min min max min ± 0,08
024 2,45 2,35 4,45 4 3,54 1,9 1,6 0,9 0,05 0,38 2,4 0,8 0,5
0,15
032 3,25 3,15 5,95 5,35 4,82 2,6 2,3 1,1 0,06 0,47 2,6 1
0,7
036 3,65 3,55 6,7 6 5,46 2,9 2,5 1,3 0,07 0,52 2,9 1,1
0,25
040 4,05 3,94 7,4 6,6 5,79 3,2 2,8 1,4 0,08 0,68 3 1,2 0,8
048 4,85 4,73 8,9 7,95 7,39 3,8 3,3 1,8 0,1 0,63 3,8 1,5 1
a D1 max may increase by 0,03, over length (L5 – L2).
b Maximum condition
0 0,08 –
Trang 10EN 3643:1996
Table 2
Diameter code 024 032 036 040 048 Length a Massb a Massb a Massb a Massb a Massb
004 4 X X 0,101 X X 0,191 X X 0,257
005 5 X X 0,121 X X 0,227 X X 0,302
006 6 X X 0,142 X X 0,263 X X 0,344 X X 0,432
007 7 X X 0,162 X X 0,299 X X 0,384 X X 0,488
008 8 X X 0,183 X X 0,335 X X 0,427 X X 0,544 X X 0,808
009 9 X X 0,203 X X 0,371 X X 0,469 X X 0,600 X X 0,889
010 10 X X 0,223 X X 0,408 X X 0,511 X X 0,656 X X 0,970
011 11 X X 0,244 X X 0,444 X X 0,552 X X 0,712 X X 1,051
012 12 X X 0,264 X X 0,480 X X 0,595 X X 0,769 X X 1,134
013 13 X X 0,285 X X 0,516 X X 0,637 X X 0,825 X X 1,215
014 14 X X 0,305 X X 0,552 X X 0,678 X X 0,882 X X 1,297
015 15 X X 0,325 X X 0,589 X X 0,720 X X 0,938 X X 1,378
016 16 X X 0,346 X X 0,625 X X 0,764 X X 0,995 X X 1,460
017 17 X 0,366 X X 0,661 X X 0,805 X X 1,051 X X 1,541
018 18 X 0,387 X X 0,697 X X 0,847 X X 1,108 X X 1,623
019 19 X 0,407 X 0,733 X X 0,890 X X 1,164 X X 1,704
020 20 X 0,427 X 0,770 X X 0,932 X X 1,221 X X 1,785
a Tail end code (see Figure 1)
b Approximate values (kg/1 000 pieces), calculated on the basis of 4,45 kg/dm3, given for information purposes only
L1 + 0,50
Trang 116 © BSI 11-1998
4 Designation
EXAMPLE:
NOTE If necessary, the code 19005 shall be placed between the description block and the identity block.
5 Marking
5.1 Rivet
EN 2424, style G
5.2 Material
ISO 10299
6 Technical specification
EN 3627
Trang 12BS EN 3643:1997
© BSI 11-1998
List of references
See national foreword
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London
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