SIST EN 3820:2017
(Main)Aerospace series - Metric bolts, normal hexagon head, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
Aerospace series - Metric bolts, normal hexagon head, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal
shank, short thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa1) / 315 °C2).
Luft- und Raumfahrt - Metrische Sechskantschrauben, kurzes Gewinde, aus Titanlegierung, anodisiert, MoS2-geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/315 °C
Série aérospatiale - Vis métriques à tête hexagonale normale, fût normal à tolérance large, filetage court, en alliage de titane, anodisées, lubrifiées MoS2 - Classification : 1 100 MPa (à température ambiante)/315 °C
Aeronavtika - Metrični sorniki, normalna šestroba glava, široka toleranca, kratek navoj, iz titanove zlitine, anodizirani, mazani z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/315 °C
Ta standard določa lastnosti anodiziranih sornikov iz titanove zlitine z normalno šestrobo glavo, široko toleranco in kratkim navojem, mazanih z MoS2.
Klasifikacija: 1 100 MPa1)/315 °C2).
General Information
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Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Metrische Sechskantschrauben, kurzes Gewinde, aus Titanlegierung, anodisiert, MoS2-geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/315 °CSérie aérospatiale - Vis métriques à tête hexagonale normale, fût normal à tolérance large, filetage court, en alliage de titane, anodisées, lubrifiées MoS2 - Classification : 1 100 MPa (à température ambiante)/315 °CAerospace series - Metric bolts, normal hexagon head, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C49.030.20Sorniki, vijaki, stebelni vijakiBolts, screws, studsICS:Ta slovenski standard je istoveten z:EN 3820:2017SIST EN 3820:2017en,fr,de01-december-2017SIST EN 3820:2017SLOVENSKI
STANDARDSIST EN 3820:20091DGRPHãþD
SIST EN 3820:2017
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3820
October
t r s y ICS
v {ä r u rä t r Supersedes EN
u z t rã t r r xEnglish Version
Aerospace series æ Metric boltsá normal hexagon headá coarse tolerance normal shanká short threadá in titanium alloyá anodizedá MoS t lubricated æ Classificationã
s
s r r Série aérospatiale æ Vis métriques à tête hexagonale normaleá fût normal à tolérance largeá filetage courtá en alliage de titaneá anodiséesá lubrifiées MoS t æ
Luftæ und Raumfahrt æ Metrische Sechskantschraubená kurzes Gewindeá aus Titanlegierungá anodisiertá MoS tæThis European Standard was approved by CEN on
t x June
t r s yä
egulations which stipulate the conditions for giving this European Standard the status of a national standard without any alterationä Upætoædate lists and bibliographical references concerning such national standards may be obtained on application to the CENæCENELEC Management Centre or to any CEN memberä
translation under the responsibility of a CEN member into its own language and notified to the CENæCENELEC Management Centre has the same status as the official versionsä
CEN members are the national standards bodies of Austriaá Belgiumá Bulgariaá Croatiaá Cyprusá Czech Republicá Denmarká Estoniaá Finlandá Former Yugoslav Republic of Macedoniaá Franceá Germanyá Greeceá Hungaryá Icelandá Irelandá Italyá Latviaá Lithuaniaá Luxembourgá Maltaá Netherlandsá Norwayá Polandá Portugalá Romaniaá Serbiaá Slovakiaá Sloveniaá Spainá Swedená Switzerlandá Turkey and United Kingdomä
EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre:
Avenue Marnix 17,
B-1000 Brussels
9
t r s y CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN
u z t rã t r s y ESIST EN 3820:2017
EN 3820:2017 (E) 2 Contents
Page European foreword . 3 1 Scope . 4 2 Normative references . 4 3 Required characteristics . 5 3.1 Configuration – Dimensions – Masses. 5 3.2 Tolerances of form and position . 5 3.3 Materials . 5 3.4 Surface treatment . 5 4 Designation. 8 5 Marking . 8 6 Technical specification . 8 6.1 Approval of manufacturers . 8 6.2 Qualification of bolts . 8 6.3 Requirement deleted . 8
(informative)
Standard evolution form . 9
SIST EN 3820:2017
EN 3820:2017 (E) 3 European foreword This document (EN 3820:2017) 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 April 2018, and conflicting national standards shall be withdrawn at the latest by April 2018. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN shall not be held responsible for identifying any or all such patent rights. This document supersedes EN 3820:2006. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countrie
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