SIST EN 4035:2021
(Main)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
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
No Scope available
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
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Standards Content (Sample)
SLOVENSKI STANDARD
SIST EN 4035:2021
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
SIST EN 4035:2021 en,fr,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
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SIST EN 4035:2021
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SIST EN 4035:2021
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.
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SIST EN 4035:2021
EN 4035:2021 (E)
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
2
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SIST EN 4035:2021
EN 4035:2021 (E)
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.
3
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SIST EN 4035:2021
EN 4035:2021 (E)
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
...
SLOVENSKI STANDARD
oSIST prEN 4035:2020
01-september-2020
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: prEN 4035
ICS:
49.035 Sestavni deli za letalsko in Components for aerospace
vesoljsko gradnjo construction
oSIST prEN 4035:2020 en,fr,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
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oSIST prEN 4035:2020
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oSIST prEN 4035:2020
DRAFT
EUROPEAN STANDARD
prEN 4035
NORME EUROPÉENNE
EUROPÄISCHE NORM
July 2020
ICS 49.035 Will supersede 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 roulement à Luft- und Raumfahrt - Einstellbarer Ösenkopf mit
rotule sur deux rangées de billes, en acier résistant à la zweireihigem Pendelkugellager aus
corrosion, jeu interne radial réduit et tige filetée en korrosionsbeständigem Stahl, reduzierte radiale
alliage de titane - Dimensions et charges Lagerluft und Gewindeschaft aus Titanlegierung -
Maße und Belastungen
This draft European Standard is submitted to CEN members for enquiry. It has been drawn up by the Technical Committee ASD-
STAN.
If this draft becomes a European Standard, 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.
This draft European Standard was established by CEN 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.
Recipients of this draft are invited to submit, with their comments, notification of any relevant patent rights of which they are
aware and to provide supporting documentation.
Warning : This document is not a European Standard. It is distributed for review and comments. It is subject to change without
notice and shall not be referred to as a European Standard.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2020 CEN All rights of exploitation in any form and by any means reserved Ref. No. prEN 4035:2020 E
worldwide for CEN national Members.
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oSIST prEN 4035:2020
prEN 4035:2020 (E)
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
2
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oSIST prEN 4035:2020
prEN 4035:2020 (E)
European foreword
This document (prEN 4035:2020) 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 is currently submitted to the CEN Enquiry.
This document will supersede EN 4035:2006.
3
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oSIST prEN 4035:2020
prEN 4035:2020 (E)
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 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 ran
...
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