BS ISO 10299-2001 Aerospace - Rivets solid - Material and metric series identification《航空航天 实心铆钉 材料和米制的标示》.pdf

1、| | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | BRITISH STANDARD BS ISO 10299:2000 ICS 49.

2、030.60 NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAW Aerospace Rivets, solid Material and metric series identificationThis British Standard, having been prepared under the direction of the Engineering Sector Committee, was published under the authority of the Standards Commi

3、ttee and comes into effect on 15 February 2001 BSI 02-2001 ISBN 0 580 36691 X BS ISO 10299:2000 Amendments issued since publication Amd. No. Date Comments National foreword This British Standard reproduces verbatim ISO 10299:2000 and implements it as the UK national standard. The UK participation in

4、 its preparation was entrusted by Technical Committee ACE/12, Aerospace Fasteners and Fastening Systems, Details and Parts, to Subcommittee ACE/12/1, Aerospace Fasteners and Fastening Systems, Details and Parts (international), which has the responsibility to: aid enquirers to understand the text; p

5、resent to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related international and European developments and promulgate them in the UK. A list of organizations represented on this subcommittee

6、 can be obtained on request to its secretary. Cross-references The British Standards which implement international or European publications referred to in this document may be found in the BSI Standards Catalogue under the section entitled “International Standards Correspondence Index”, or by using

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8、om legal obligations. Summary of pages This document comprises a front cover, an inside front cover, the ISO title page, pages ii and iii, a blank page, pages 1 to 4, an inside back cover and a back cover. The BSI copyright notice displayed in this document indicates when the document was last issue

9、d.INTERNATIONAL STANDARD ISO 10299 First edition 2000-08-15 Reference number ISO 10299:2000(E) Aerospace Rivets, solid Material and metric series identification Aronautique et espace Rivets ordinaires Identification du matriau et de la srie mtriqueISO 10299:2000(E) iiISO 10299:2000(E) iii Foreword I

10、SO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO technical com- mittees. Each member body interested in a subject for which a technical

11、 committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liai- son with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of el

12、ectrotechnical standardization. International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 3. Draft International Standards adopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard require

13、s approval by at least 75 % of the member bodies casting a vote. Attention is drawn to the possibility that some of the elements of this International Standard may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. International Standard

14、 ISO 10299 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 4, Aerospace fastener systems.INTERNATIONAL STANDARD ISO 10299:2000(E) 1 Aerospace Rivets, solid Material and metric series identification 1 Scope This International Standard specifies the marks al

15、lowed to identify material and metric series on solid rivets for use in aerospace construction. It applies when reference is made to this International Standard in the product standard or definition document. 2 Normative reference The following normative document contains provisions which, through r

16、eference in this text, constitute provisions of this International Standard. For dated references, subsequent amendments to, or revisions of, any of these publica- tions do not apply. However, parties to agreements based on this International Standard are encouraged to investi- gate the possibility

17、of applying the most recent edition of the normative document indicated below. For undated references, the latest edition of the normative document referred to applies. Members of ISO and IEC maintain reg- isters of currently valid International Standards. ISO/TR 12198:1998, Aerospace Rivets, solid

18、Materials. 3 Requirements 3.1 Marking Marks shall be legible. 3.2 Material identification The identification of the material shall be marked on the head of the rivet, see Tables 1 and 2. Location is left to the manufacturers discretion. However, marking shall not cause interference when setting. Tab

19、le 1 positions marks in relation to shank diameter drawn up in dotted lines. Only materials given in ISO/TR 12198 are indicated Table 1. 3.3 Metric series identification See Figure 1. Marking shall not cause interference when setting. This symbol shall be legible to the unaided eye. 3.4 Complementar

20、y requirements Complementary requirements (for example coloration) shall be specified in the product standard or definition document.ISO 10299:2000(E) 2 Table 1 Material identification Material Symbol a Family Designation Aluminium alloys Al99,5 (1050A) (no marking) Al4Cu0,7Mg0,7Mn (2017A) embossed

21、Al4,4Cu1,5Mg0,6Mn (2024) embossed Al2,6Cu0,3Mg (2117) indented Al6,3Cu0,3Mn0,06Ti (2219) indented Al5Mg0,3Mn (5056A) embossed Al6,2Zn2,3Cu2,2Mg0,1Zr (7050) embossed Al4Cu0,4Mn0,2Mg (V65) (no marking) Corrosion-resistant steels X2CrNi19-11 (AISI 304L) indented X6NiCrTiMoV26-15 (A286) embossed Nickel

22、alloys Ni30Cu (Monel 400) embossed Ni19Cr0,4Ti (Nimonic 75) indented NiCr22Fe18Mo9 (Hastelloy X) embossed Ni16Cr7Fe3Ti1Nb1Al (Inconel X750) indented Titanium (commercially pure) (T40) embossed Titanium alloy Ti44,5Cb indented a Dimensions are given in Table 2.ISO 10299:2000(E) 3 Table 2 Dimensions o

23、f symbols Dimensions in millimetres Symbol Height or depth Position Width embossed 0,2 max. indentedISO 10299:2000(E) 4 4D r i l ls t a r t The drill start option will be indicated by a code in the rivet designation. The dimensions of the drill start, located in the centre of the rivet head, are as

24、follows: d i a m e t e r : m a x . ; depth: max. Dimensions in millimetres Key 1 Shank diameter 2 Radiused tail end diameter a Dot, indented on the tail end to a depth of 0,2 max. Figure 1 0,8 mm 0,2 mmBS ISO 10299:2000 BSI 389 Chiswick High Road London W4 4AL | | | | | | | | | | | | | | | | | | | |

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