EN 4162-2016 en Aerospace series - Screws 100 ountersunk normal head offset cruciform recess coarse tolerance normal shank medium length thread in alloy steel cadmium plated - Clas.pdf
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1、BSI Standards PublicationBS EN 4162:2016Aerospace series Screws100 countersunk normalhead, offset cruciform recess,coarse tolerance normal shank,medium length thread, inalloy steel, cadmium plated -Classification: 1 100 MPa (atambient temperature) / 235CBS EN 4162:2016 BRITISH STANDARDNational forew
2、ordThis British Standard is the UK implementation of EN 4162:2016. Itsupersedes BS EN 4162:2009 which is withdrawn.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can b
3、eobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2016. Published by BSI StandardsLimited 2016ISBN 978 0 580 90781 4ICS 49.030.20Compliance
4、with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 31 March 2016.Amendments issued since publicationDate Text affectedBS EN 4162:2016EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE
5、 NORM EN 4162 March 2016 ICS 49.030.20 Supersedes EN 4162:2009English Version Aerospace series - Screws 100 countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature) / 235
6、 C Srie arospatiale - Vis tte fraise 100 normale, empreinte cruciforme dporte, tige normale tolrance large, filetage moyen, en acier alli, cadmies - Classification: 1 100 MPa ( temprature ambiante) / 235 C Luft- und Raumfahrt - 100 Senkschrauben mit Flgelkreuzschlitz, mittlere Gewindelnge, aus legie
7、rtem Stahl, erkadmet - Klasse: 1 100 MPa (bei Raumtemperatur) / 235 C This European Standard was approved by CEN on 27 September 2015. 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 s
8、tandard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version i
9、n any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech
10、Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EURO
11、PEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2016 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4162:2016 EBS EN
12、 4162:2016EN 4162:2016 (E) 2 Contents Page European Foreword 3 1 Scope 4 2 Normative references 4 3 Required characteristics 5 4 Designation 8 5 Marking . 8 6 Technical specification 9 Annex A (informative) Standard evolution form . 10 BS EN 4162:2016EN 4162:2016 (E) 3 European Foreword This documen
13、t (EN 4162:2016) 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
14、 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 2016 and conflicting national standards shall be withdrawn at
15、the latest by September 2016. 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. This document supersedes EN 4162:2009. According to the
16、CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hun
17、gary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 4162:2016EN 4162:2016 (E) 4 1 Scope This European Standard specifies the characteristics of screws
18、, 100 countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated. Classification: 1 100 MPa1) / 235 C2). 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are
19、 indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2133, Aerospace series Cadmium plating of steels with specified tensile strength 1 450 MPa, copper, c
20、opper alloys and nickel alloys EN 2137, Steel FE-PL75 1100 MPa Rm 1250 MPa Bars De 100 mm Aerospace series EN 2424, Aerospace series Marking of aerospace products EN 2442, Steel FE-PL711 1100 MPa Rm 1300 MPa Bars and wires De 25 mm3)EN 3514, Steel FE-PL711 Hardened and tempered 1100 MPa Rm 1300 MPa
21、Bar and wire for bolts De 25 mm EN 9100, Quality Management Systems Requirements for Aviation, Space and Defense Organizations EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard parts ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled extern
22、al threads ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts ISO 5856, Aerospace Screws, 100 degrees normal countersunk head, internal offset cruciform ribbed or unribbed drive, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strengt
23、h classes less than or equal to 1 100 MPa Dimensions ISO 7689, Aerospace Bolts, with MJ threads, made of alloy steel, strength class 1 100 MPa Procurement specification 1)Minimum tensile strength of the material at ambient temperature. 2)Maximum temperature that the bolt can withstand without contin
24、uous change in its original characteristics, after return to ambient temperature. The maximum temperature is determined by the surface treatment. 3)For new design, see EN 3514. BS EN 4162:2016EN 4162:2016 (E) 5 ISO 7913, Aerospace Bolts and screws, metric Tolerances of form and position ISO 14275, A
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