SIST EN 4036:2009
(Main)Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads
Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads
This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing with reduced internal radial clearance and threaded shank in corrosion resisting steel, designed to withstand only slow rotations and oscillations under load.
They consist of:
- a rod end comprising:
- circumferential groove to identify location;
- either seals or shields;
- an optional longitudinal groove for locking purpose;
- an inner ring with balls.
These rod ends are intended for use with flight control rods or rods for aerospace structures.
They are intended to be used in the temperature range: - 54 °C to 150 °C.
However, being lubricated with the following greases:
- very high pressure grease, ester type (code A), operational range - 73 °C to 121 °C or
- very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range - 54 °C to 177 °C (see EN 2067),
their field of application when lubricated with code A grease is limited to 121 °C.
Luft- und Raumfahrt - Einstellbare Ösenköpfe mit zweireihigem Pendelkugellager und Gewindeschaft aus korrosionsbeständigem Stahl, reduzierte radiale Lagerluft - Maße und Belastungen
Diese Norm legt die Eigenschaften von einstellbaren Ösenköpfen mit zweireihigem Pendelkugellager, mit reduzierter radialer Lagerluft und Gewindeschaft aus korrosionsbeständigem Stahl fest, die so ausgelegt sind, dass sie unter Belastung nur langsamen Dreh und Kippbewegungen standhalten.
Sie bestehen aus:
einem Ösenkopf, der:
mit einer Ringnut zur Kontrolle der Einschraubtiefe versehen ist;
mit Dicht oder Deckscheiben ausgerüstet ist;
eine Längsnut zur Sicherung aufweisen kann;
einem Innenring mit Kugeln.
Diese Ösenköpfe sind für Bediengestänge für Flugsteuerungen oder für Strukturstangen von Luftfahrzeugen vorgesehen.
Sie sind für den Einsatz in folgendem Temperaturbereich vorgesehen: -54 °C bis 150 °C.
Da sie jedoch mit folgenden Fetten geschmiert werden:
Hochdruckfett auf Esterbasis (Kennbuchstabe A), Betriebstemperaturbereich -73 °C bis 121 °C; oder
Hochdruckfett auf der Basis von synthetischen Kohlenwasserstoffen, zur allgemeinen Verwendung (Kennbuchstabe B), Betriebstemperaturbereich -54 °C bis 177 °C (siehe EN 2067),
ist ihr Anwendungsbereich bei Schmierung mit Fett mit dem Kennbuchstaben A auf 121 °C eingeschränkt.
Série aérospatiale - Embouts réglables à rotule sur deux rangées de billes et à tige filetée en acier résistant à la corrosion, jeu radial réduit - Dimensions et charges
Aeronavtika - Nastavljivi drsni zgibi s samovarovalnim dvorednim nihalnim krogličnim ležajem in navojnim steblom iz korozijsko odpornega jekla, z zmanjšanim radialnim ohlapom ležaja - Mere in nosilnosti
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Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.QLKDOQLPLuft- und Raumfahrt - Einstellbare Ösenköpfe mit zweireihigem Pendelkugellager und Gewindeschaft aus korrosionsbeständigem Stahl, reduzierte radiale Lagerluft - Maße und BelastungenSérie aérospatiale - Embouts réglables à rotule sur deux rangées de billes et à tige filetée en acier résistant à la corrosion, jeu radial réduit - Dimensions et chargesAerospace series - Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads49.035Sestavni deli za letalsko in vesoljsko gradnjoComponents for aerospace constructionICS:Ta slovenski standard je istoveten z:EN 4036:2006SIST EN 4036:2009en,de01-september-2009SIST EN 4036:2009SLOVENSKI
STANDARD
SIST EN 4036:2009
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4036May 2006ICS 49.035 English VersionAerospace series - Rod ends, adjustable with self-aligningdouble row ball bearing and threaded shank in corrosionresisting steel, reduced internal radial clearance - Dimensionsand loadsSérie aérospatiale - Embouts réglables à rotule sur deuxrangées de billes et à tige filetée en acier résistant à lacorrosion, jeu radial réduit - Dimensions et chargesLuft- und Raumfahrt - Einstellbare Ösenköpfe mitzweireihigem Pendelkugellager und Gewindeschaft auskorrosionsbeständigem Stahl, reduzierte radiale Lagerluft -Maße und BelastungenThis European Standard was approved by CEN on 16 March 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 4036:2006: ESIST EN 4036:2009
EN 4036:2006 (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.9 7 Marking.9 8 Technical specification.9
SIST EN 4036:2009
EN 4036:2006 (E) 3 Foreword This European Standard (EN 4036:2006) 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. 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. SIST EN 4036:2009
EN 4036:2006 (E) 4 1 Scope This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing with reduced internal radial clearance and threaded shank in corrosion resisting steel, designed to withstand only slow rotations and oscillations under load. They consist of: a rod end comprising: circumferential groove to identify location; either seals or shields; an optional longitudinal groove for locking
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