EN 4035:2021

Aerospace series - Rod end, adjustable, with self-aligning double row ball bearing, in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads

This document specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load.
They consist of:
-   a rod end comprising:
-   circumferential groove to confirm that the assembled rod-end is "in safety" emphasized with the application of red paint;
-   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 - Einstellbarer Ösenkopf mit zweireihigem Pendelkugellager aus korrosionsbeständigem Stahl, reduzierte radiale Lagerluft und Gewindeschaft aus Titanlegierung - Maße und Belastungen

Dieses Dokument legt die Eigenschaften von einstellbaren Ösenköpfen mit zweireihigem Pendelkugellager aus korrosionsbeständigem Stahl, mit reduzierter radialer Lagerluft und Gewindeschaft aus Titanlegierung fest, die so ausgelegt sind, dass sie unter Belastung nur langsamen Dreh- und Kippbewegungen standhalten.
Sie bestehen aus
—   einem Ösenkopf, der
—   mit einer Ringnut versehen ist, zur Bestätigung, dass sich der zusammengebaute Ösenkopf „in Sicherheit“ befindet, unterstrichen durch Auftragen von roter Farbe,
—   mit Dicht- oder Deckscheiben ausgerüstet ist,
—   eine Längsnut zur Sicherung aufweisen kann und
—   einem Innenring mit Kugeln.
Diese Ösenköpfe sind für Bediengestänge für Flugsteuerungen oder für Strukturstangen von Luftfahrzeugen bestimmt.
Sie sind bestimmt für den Einsatz im Temperaturbereich von: −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 - Embout réglable, à roulement à rotule sur deux rangées de billes, en acier résistant à la corrosion, jeu interne radial réduit et tige filetée en alliage de titane - Dimensions et charges

Le présent document spécifie les caractéristiques des embouts réglables à roulement à rotule sur deux rangées de billes en acier résistant à la corrosion, à jeu interne radial réduit et tige filetée en alliage de titane, conçus pour supporter (en charge) uniquement des rotations lentes et des oscillations faibles.
Ils sont constitués :
- d'un corps d'embout comprenant :
- une gorge circulaire permettant de confirmer que l’embout est assemblé « en sécurité », soulignée par l’application de peinture rouge ;
- soit des joints d'étanchéité, soit des flasques de protection ;
- éventuellement une gorge longitudinale de verrouillage ;
- d'une bague intérieure sur billes.
Ces embouts sont destinés aux bielles pour commandes de vol ou aux bielles de structures aérospatiales.
Ils sont destinés à être utilisés dans une plage de températures comprise entre −54 °C et 150 °C.
Cependant, comme ils sont lubrifiés avec les graisses suivantes :
- graisse extrême pression, type ester (code A), plage d'utilisation comprise entre −73 °C et 121 °C ; ou
- graisse extrême pression, type hydrocarbures synthétiques, usage général (code B), plage d'utilisation comprise entre −54 °C et 177 °C (voir l’EN 2067) ;
en cas de lubrification avec de la graisse code A, leur champ d'application est limité à 121 °C.

Aeronavtika - Nastavljivi drsni zgibi s samovarovalnim dvorednim nihalnim krogličnim ležajem iz korozijsko odpornega jekla, z zmanjšanim radialnim ohlapom ležaja in navojnim steblom iz titanove zlitine - Mere in nosilnosti

General Information

• Status: Published
• Publication Date: 09-Mar-2021
• Withdrawal Date: 29-Sep-2021
• ICS: 49.035 - Components for aerospace construction
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3/S 1 - Parts of Mechanical Systems
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 10-Mar-2021
• Completion Date: 10-Mar-2021
• Ref Project: SIST EN 4035:2021 - Aerospace series - Rod end, adjustable, with self-aligning double row ball bearing, in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads

Relations

• Replaces: EN 4035:2006 - Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads
• Effective Date: 17-Mar-2021

Standards Content (Sample)

SLOVENSKI STANDARD
01-maj-2021
Nadomešča:
SIST EN 4035:2009
Aeronavtika - Nastavljivi drsni zgibi s samovarovalnim dvorednim nihalnim
krogličnim ležajem iz korozijsko odpornega jekla, z zmanjšanim radialnim ohlapom
ležaja in navojnim steblom iz titanove zlitine - Mere in nosilnosti
Aerospace series - Rod end, adjustable, with self-aligning double row ball bearing, in
corrosion resisting steel, reduced internal radial clearance and threaded shank in
titanium alloy - Dimensions and loads
Luft- und Raumfahrt - Einstellbarer Ösenkopf mit zweireihigem Pendelkugellager aus
korrosionsbeständigem Stahl, reduzierte radiale Lagerluft und Gewindeschaft aus
Titanlegierung - Maße und Belastungen
Série aérospatiale - Embout réglable, à roulement à rotule sur deux rangées de billes, en
acier résistant à la corrosion, jeu interne radial réduit et tige filetée en alliage de titane -
Dimensions et charges
Ta slovenski standard je istoveten z: EN 4035:2021
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.

EN 4035
EUROPEAN STANDARD
NORME EUROPÉENNE
March 2021
EUROPÄISCHE NORM
ICS 49.035 Supersedes EN 4035:2006
English Version
Aerospace series - Rod end, adjustable, with self-aligning
double row ball bearing, in corrosion resisting steel,
reduced internal radial clearance and threaded shank in
titanium alloy - Dimensions and loads
Série aérospatiale - Embout réglable à rotule sur deux Luft- und Raumfahrt - Einstellbarer Ösenkopf mit
rangées de billes en acier résistant à la corrosion, jeu zweireihigem Pendelkugellager aus
radial réduit et à tige filetée en alliage de titane - korrosionsbeständigem Stahl, reduzierte radiale
Dimensions et charges Lagerluft und Gewindeschaft aus Titanlegierung -
Maße und Belastungen
This European Standard was approved by CEN on 13 February 2021.

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 CEN-CENELEC 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
translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management
Centre has the same status as the official versions.

CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia,
Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway,
Poland, Portugal, Republic of North Macedonia, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and
United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2021 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4035:2021 E
worldwide for CEN national Members.

Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms, definitions and symbols . 5
4 Required characteristics . 5
5 Designation . 9
6 Marking . 10
7 Technical specification . 10
8 Quality management systems . 10
Bibliography . 11

European foreword
This document (EN 4035:2021) has been prepared by the Aerospace and Defence Industries Association of
Europe – Standardization (ASD-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 ASD,
prior to its presentation to CEN.
This document shall be given the status of a national standard, either by publication of an identical text or by
endorsement, at the latest by September 2021, and conflicting national standards shall be withdrawn at the
latest by September 2021.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. CEN shall not be held responsible for identifying any or all such patent rights.
This document supersedes EN 4035:2006.
According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this document: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech
Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia,
Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Republic of North Macedonia,
Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom.

1 Scope
This document specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing
in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy,
designed to withstand only slow rotations and oscillations under load.
They consist of:
— a rod end comprising:
— circumferential groove to confirm that the assembled rod-end is “in safety” emphasized with the
application of red paint;
— either seals or shields;
— an optional longitudinal groove for locking pu
...