Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush - Dimensions and loads

This standard specifies the characteristics of rigid single row ball bearings in corrosion resisting steel with an extended inner ring and a solid or lightweight flanged alignment bush, designed to withstand only slow rotations and slight oscillations under load.
They are intended for use in airframe fixed and moving elements and in flight control linkages.
The bearings defined in this standard shall be used in the temperature range from - 54 °C to 150 °C.
However, as they are lubricated with the following greases (see EN 3727):
   ester type very high pressure grease (code letter A), operating range from - 73 °C to 121 °C or,
   synthetic hydrocarbons 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 code letter A grease is limited to 121 °C.

Luft- und Raumfahrt - Flugwerklager - Einreihige Rillenkugellager aus korrosionsbeständigem Stahl mit einseitig verlängertem Innenring und selbsteinstellendem Flansch - Maße und Belastungen

Diese Norm legt die Eigenschaften von einreihigen Rillenkugellagern aus korrosionsbeständigem Stahl mit verlängertem Innenring und selbsteinstellendem Voll- oder Teilflansch fest, die so ausgelegt sind, dass sie unter Belastung nur langsamen Dreh  und geringen Schwenkbewegungen standhalten.
Sie sind zur Verwendung zwischen festen und beweglichen Flugwerkteilen und in Flugsteuerungsgestängen vorgesehen.
Die in der vorliegenden Norm festgelegten Flugwerklager sind im Temperaturbereich von  54 °C bis 150 °C zu verwenden.
Da sie jedoch mit folgenden Fetten geschmiert werden (siehe EN 3727):
   Hochdruckfett auf Esterbasis (Kennbuchstabe A), Betriebstemperaturbereich  73 °C bis 121 °C; oder
   Hochdruckfett auf der Basis von synthetischen Kohlenwasserstoffen (Kennbuchstabe B), Betriebs¬temperaturbereich  54 °C bis 177 °C.
Ihr Anwendungsbereich ist bei Schmierung mit Fett A auf 121 °C eingeschränkt.

Série aérospatiale - Roulements pour structures d’aéronefs - Roulements en acier résistant à la corrosion, rigides, à une rangée de billes, avec bague intérieure à jupe et bague d’alignement à collerette - Dimensions et charges

Aeronavtika - Kotalni ležaji za letala - Enoredni žlebasti kroglični ležaji iz korozijsko odpornega jekla, z enostransko podaljšanim notranjim obročem in samonastavljivo prirobnico - Mere in nosilnosti

General Information

Status
Published
Publication Date
13-Jun-2006
Withdrawal Date
30-Dec-2006
Technical Committee
Drafting Committee
Current Stage
9093 - Decision to confirm - Review Enquiry
Completion Date
31-May-2017

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Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Flugwerklager - Einreihige Rillenkugellager aus korrosionsbeständigem Stahl mit einseitig verlängertem Innenring und selbsteinstellendem Flansch - Maße und BelastungenSérie aérospatiale - Roulements pour structures d’aéronefs - Roulements en acier résistant à la corrosion, rigides, à une rangée de billes, avec bague intérieure à jupe et bague d’alignement à collerette - Dimensions et chargesAerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush - Dimensions and loads49.035Sestavni deli za letalsko in vesoljsko gradnjoComponents for aerospace constructionICS:Ta slovenski standard je istoveten z:EN 4041:2006SIST EN 4041:2009en,de01-julij-2009SIST EN 4041:2009SLOVENSKI
STANDARD



SIST EN 4041:2009



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4041June 2006ICS 49.035 English VersionAerospace series - Bearings, airframe rolling - Rigid single rowball bearings in corrosion resisting steel, with extended innerring and flanged alignment bush - Dimensions and loadsSérie aérospatiale - Roulements pour structures d'aéronefs- Roulements en acier résistant à la corrosion, rigides, àune rangée de billes, avec bague intérieure à jupe et bagued'alignement à collerette - Dimensions et chargesLuft- und Raumfahrt - Flugwerklager - EinreihigeRillenkugellager aus korrosionsbeständigem Stahl miteinseitig verlängertem Innenring und selbsteinstellendemFlansch - Maße und BelastungenThis European Standard was approved by CEN on 20 April 2006.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 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 translationunder the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.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 STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2006 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4041:2006: ESIST EN 4041:2009



EN 4041:2006 (E) 2 Contents Page Foreword.3 1 Scope.4 2 Normative references.4 3 Terms and definitions.5 4 Symbols and abbreviations.5 5 Required characteristics.5 6 Designation.10 7 Marking.10 8 Technical specification.10
SIST EN 4041:2009



EN 4041:2006 (E) 3 Foreword This European Standard (EN 4041:2006) 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 December 2006, and conflicting national sta
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