SIST EN 2647:2009
(Main)Aerospace series - Nuts, hexagonal, self-locking, ball seat, in alloy steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C
Aerospace series - Nuts, hexagonal, self-locking, ball seat, in alloy steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C
This standard specifies the characteristics of self-locking hexagonal nuts with ball seat in alloy steel, cadmium plated, MoS2 lubricated.
Classification: 900 MPa ) / 235 °C )
They are intended to be used with washers to EN 2648 or suitable parts, see Annex A.
Luft- und Raumfahrt - Sechskantmuttern, selbstsichernd, für Neigungsausgleich, aus legiertem Stahl, verkadmet, MoS2-geschmiert - Klasse: 900 MPa (bei Raumtemperatur)/235 °C
Diese Norm legt die Eigenschaften von selbstsichernden Sechskantmuttern für Neigungsausgleich, aus legiertem Stahl, verkadmet, MoS2 geschmiert, fest.
Klasse: 900 MPa ) / 235 °C )
Sie werden in Verbindung mit Scheiben nach EN 2648 oder mit geeigneten Teilen verwendet, siehe Anhang A.
Série aérospatiale - Écrous hexagonaux, à freinage interne, orientables, en acier allié, cadmiés, lubrifiés MoS2 - Classification: 900 MPa (à température ambiante)/235 °C
Aeronavtika - Matice, šestrobe, samozapiralne, z izravnavo nagiba, iz legiranega jekla, prevlečene s kadmijem, namazane z MoS2 - Klasifikacija: 900 MPa (pri temperaturi okolice)/235 °C
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Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Sechskantmuttern, selbstsichernd, für Neigungsausgleich, aus legiertem Stahl, verkadmet, MoS2-geschmiert - Klasse: 900 MPa (bei Raumtemperatur)/235 °CSérie aérospatiale - Écrous hexagonaux, à freinage interne, orientables, en acier allié, cadmiés, lubrifiés MoS2 - Classification: 900 MPa (à température ambiante)/235 °CAerospace series - Nuts, hexagonal, self-locking, ball seat, in alloy steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 2647:2006SIST EN 2647:2009en,de01-april-2009SIST EN 2647:2009SLOVENSKI
STANDARDSIST EN 2647:20011DGRPHãþD
SIST EN 2647:2009
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 2647
June 2006 ICS 49.030.30 Supersedes EN 2647:1995 English Version
Aerospace series - Nuts, hexagonal, self-locking, ball seat, in alloy steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C
Série aérospatiale - Écrous hexagonaux, à freinage interne, orientables, en acier allié, cadmiés, lubrifiés MoS2 - Classification: 900 MPa (à température ambiante)/235 °C
Luft- und Raumfahrt - Sechskantmuttern, selbstsichernd, für Neigungsausgleich, aus legiertem Stahl, verkadmet, MoS2-geschmiert - Klasse: 900 MPa (bei Raumtemperatur)/235 °C This European Standard was approved by CEN on 3 February 2006.
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, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
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B-1050 Brussels © 2006 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2647:2006: ESIST EN 2647:2009
EN 2647:2006 (E) 2 Contents Page Foreword.3 1 Scope.4 2 Normative references.4 3 Required characteristics.5 4 Designation.7 5 Marking.7 6 Technical specification.7 Annex A (informative)
Assembly.8
SIST EN 2647:2009
EN 2647:2006 (E) 3 Foreword This European Standard (EN 2647:2006) has been prepared by the AeroSpace and Defense Industries Asso-ciation of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has re-ceived 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 December 2006, and conflicting national standards shall be withdrawn at the latest by December 2006. 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. According to the CEN/CENELEC Internal Regulations, the national standards
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