SIST EN 2585:2004
(Main)Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensions and loads
Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensions and loads
This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self- lubricating liner, narrow series, for elevated load at ambient temperature, with or without swaging groove, intended for use in the fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range - 55° C to + 163° C.
Luft- und Raumfahrt - Gelenklager aus korrosionsbeständigem Stahl mit selbstschmierender Beschichtung - Breite Reihe - Hohe Belastung bei Raumtemperatur - Maße und Belastungen
Diese Norm legt die Eigenschaften von Gelenklagern aus korrosionsbeständigem Stahl mit selbstschmierender Beschichtung, breite Reihe, für hohe Belastung bei Raumtemperatur, mit oder ohne Montagenut fest, die für die starren oder beweglichen Flugwerkteile und deren Betätigungsmechanismen bestimmt sind.
Sie sind im Temperaturbereich von - 55 °C bis + 163 °C zu verwenden.
Série aérospatiale - Rotules en acier résistant a la corrosion a garniture autolubrifiante - Série large a charge élevée a température ambiante - Dimensions et charges
La présente norme spécifie les caractéristiques des rotules en acier résistant a la corrosion, a garniture autolubrifiante, série large, a charge élevée a température ambiante, avec ou sans gorge de sertissage, destinées a etre utilisées dans les éléments fixes ou mobiles de la structure des aéronefs et de leurs mécanismes de commande.
Elles doivent etre utilisées dans l'intervalle de température de - 55 °C a + 163 °C.
Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensions and loads
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensions and loadsLuft- und Raumfahrt - Gelenklager aus korrosionsbeständigem Stahl mit selbstschmierender Beschichtung - Breite Reihe - Hohe Belastung bei Raumtemperatur - Maße und BelastungenSérie aérospatiale - Rotules en acier résistant a la corrosion a garniture autolubrifiante -Série large a charge élevée a température ambiante - Dimensions et chargesAerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensions and loads49.035Sestavni deli za letalsko in vesoljsko gradnjoComponents for aerospace constructionICS:Ta slovenski standard je istoveten z:EN 2585:2001SIST EN 2585:2004en01-maj-2004SIST EN 2585:2004SLOVENSKI
STANDARDSIST EN 2585:20011DGRPHãþD
SIST EN 2585:2004
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 2585October 2001ICS 49.035Supersedes EN 2585:1992English versionAerospace series - Bearings, spherical plain in corrosionresisting steel with self-lubricating liner - Wide series - Elevatedload at ambient temperature - Dimensions and loadsSérie aérospatiale - Rotules en acier résistant à lacorrosion à garniture autolubrifiante - Série large à chargeélevée à température ambiante - Dimensions et chargesLuft- und Raumfahrt - Gelenklager auskorrosionsbeständigem Stahl mit selbstschmierenderBeschichtung - Breite Reihe - Hohe Belastung beiRaumtemperatur - Maße und BelastungenThis European Standard was approved by CEN on 29 December 2000.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the Management Centre or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any other language made by translationunder the responsibility of a CEN member into its own language and notified to the Management Centre has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2001 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 2585:2001 ESIST EN 2585:2004
EN 2585:2001 (E)2ForewordThis 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 hasreceived the approval of the National Associations and the Official Services of the member countries ofAECMA, prior to its presentation to CEN.This European Standard shall be given the status of a national standard, either by publication of an identicaltext or by endorsement, at the latest by April 2002, and conflicting national standards shall be withdrawn atthe latest by April 2002.According to the CEN/CENELEC Internal Regulations, the national standards organizations of the followingcountries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark,Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal,Spain, Sweden, Switzerland and the United Kingdom.SIST EN 2585:2004
EN 2585:2001 (E)31ScopeThis standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self-lubricating liner, narrow series, for elevated load at ambient temperature, with or without swaging groove,intended for use in the fixed or moving parts of the aircraft structure and control mechanisms.They shall be used in the temperature range – 55° C to + 163° C.2Normative referencesThis 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 listedhereafter. For dated references
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