SIST EN 2588:2009

Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads

This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, with assembly slots, with or without lubrication holes and groove, intended for use in fixed or moving parts of aircraft structure and control mechanisms.
They may be used in the temperature range from - 54 °C to 150 °C.
However, as they are lubricated with the following greases (see EN 2337):
-   ester type very high pressure grease (code letter A), operating range from - 73 °C to 121 °C or,
-   synthetic hydrocarbon type very high pressure grease general purpose (code letter B), operating range from - 54 °C to 177 °C.
Their field of application when lubricated with grease code letter A is limited to 121 °C.

Luft- und Raumfahrt - Gelenklager aus korrosionsbeständigem Stahl mit Einführnut - Maße und Belastungen

Diese Norm legt die Eigenschaften für Gelenklager aus korrosionsbeständigem Stahl mit Einführnut der metrischen Reihe mit oder ohne Schmierloch und Schmiernut fest, die für starre oder bewegte Flugwerkteile und deren Betätigungseinrichtungen bestimmt sind.
Sie können in einem Temperaturbereich von -54 °C bis 150 °C verwendet werden.
Da sie mit den folgenden Fetten geschmiert werden (siehe EN 2337)
-   Hochdruckfett auf Esterbasis (Kennbuchstabe A, Betriebstemperaturbereich von -73 °C bis 121 °C oder
-   Hochdruckfett auf der Basis von synthetischen Kohlenwasserstoffen zur allgemeinen Verwendung (Kennbuchstabe B), Betriebstemperaturbereich von -54 °C bis 177 °C
ist der Anwendungsbereich für Schmierung mit Fett A auf 121 °C eingeschränkt.

Série aérospatiale - Rotules lisses en acier résistant à la corrosion avec encoches d'assemblage - Dimensions et charges

Aeronavtika - Ležaji, krogelni, drsni, iz korozijsko odpornega jekla z utorom - Mere in nosilnosti

General Information

• Status: Withdrawn
• Publication Date: 26-Jan-2009
• Withdrawal Date: 03-Nov-2024
• ICS: 49.035 - Components for aerospace construction
• Technical Committee: I13 - Imaginarni 13
• Current Stage: 9900 - Withdrawal (Adopted Project)
• Start Date: 04-Nov-2024
• Due Date: 27-Nov-2024
• Completion Date: 04-Nov-2024
• Ref Project: EN 2588:2006 - Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads

Relations

• Replaces: SIST EN 2588:2001/AC1:2001 - Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads
• Effective Date: 01-Mar-2009
• Replaces: SIST EN 2588:2001 - Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads
• Effective Date: 01-Mar-2009
• Revised: SIST EN 2588:2024 - Aerospace series - Bearing, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads
• Effective Date: 03-May-2023

Standards Content (Sample)

SLOVENSKI STANDARD
01-marec-2009
1DGRPHãþD
SIST EN 2588:2001
SIST EN 2588:2001/AC1:2001
Aeronavtika - Ležaji, krogelni, drsni, iz korozijsko odpornega jekla z utorom - Mere
in nosilnosti
Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly
slots - Dimensions and loads
Luft- und Raumfahrt - Gelenklager aus korrosionsbeständigem Stahl mit Einführnut -
Maße und Belastungen
Série aérospatiale - Rotules lisses en acier résistant à la corrosion avec encoches
d'assemblage - Dimensions et charges
Ta slovenski standard je istoveten z: EN 2588:2006
ICS:
49.035 Sestavni deli za letalsko in Components for aerospace
vesoljsko gradnjo construction
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 2588
NORME EUROPÉENNE
EUROPÄISCHE NORM
May 2006
ICS 49.035 Supersedes EN 2588:1988
English Version
Aerospace series - Bearings, spherical plain in corrosion
resisting steel with assembly slots - Dimensions and loads
Série aérospatiale - Rotules lisses en acier résistant à la Luft- und Raumfahrt - Gelenklager aus
corrosion avec encoches d'assemblage - Dimensions et korrosionsbeständigem Stahl mit Einführnut - Maße und
charges Belastungen
This European Standard was approved by CEN on 13 January 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.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36  B-1050 Brussels
© 2006 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2588:2006: E
worldwide for CEN national Members.

Contents Page
Foreword .3
1 Scope.4
2 Normative references.4
3 Terms and definitions.4
4 Symbols and abbreviations.5
5 Required characteristics.5
5.1 Configuration, dimensions and masses .5
5.2 Surface roughness.5
5.3 Clearances and loads .7
5.4 Materials.8
5.5 Surface treatment.8
6 Designation.9
7 Marking.9
8 Technical specification.9

Foreword
This European Standard (EN 2588:2006) has been prepared by the European Association of Aerospace
Manufacturers - Standardization (AECMA-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
AECMA, 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 November 2006, and conflicting national standards shall be withdrawn
at the latest by November 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.
This European Standard supersedes EN 2588:1988.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: 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 the United Kingdom.
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