Aerospace series - Bush, flanged, corrosion resisting steel, with self-lubricating liner - Dimensions and loads

This document specifies the characteristics of flanged bushes in corrosion resisting steel with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 163 °C and assembly with an interference fit into fixed and moving aerospace parts.

Luft- und Raumfahrt - Buchse mit Flansch aus korrosionsbeständigem Stahl mit selbstschmierender Beschichtung - Maße und Belastung

Série aérospatiale - Bague à épaulement, en acier resistant à la corrosion, à garniture autolubrificante - Dimensions et charges

Aeronavtika - Puše s prirobnico iz korozijsko odpornega jekla s samomazalno oblogo - Mere in obremenitve

Ta dokument določa lastnosti drsnih puš s prirobnico iz korozijsko odpornega jekla s samomazalno oblogo ter priporočilo za projektiranje gredi in ohišij.
Puše so predvidene za uporabo v temperaturnem območju od –55 °C do 163 °C in s sestavom z nateznim spojem v fiksnih in gibljivih delih aeronavtičnih vozil.

General Information

Status
Published
Publication Date
11-Mar-2019
Technical Committee
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
04-Mar-2019
Due Date
09-May-2019
Completion Date
12-Mar-2019

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Standards Content (Sample)

SLOVENSKI STANDARD
SIST EN 2288:2019
01-maj-2019
1DGRPHãþD
SIST EN 2288:2001
Aeronavtika - Puše s prirobnico iz korozijsko odpornega jekla s samomazalno
oblogo - Mere in obremenitve
Aerospace series - Bush, flanged, corrosion resisting steel, with self-lubricating liner -
Dimensions and loads
Luft- und Raumfahrt - Buchse mit Flansch aus korrosionsbeständigem Stahl mit
selbstschmierender Beschichtung - Maße und Belastung
Série aérospatiale - Bague à épaulement, en acier resistant à la corrosion, à garniture
autolubrificante - Dimensions et charges
Ta slovenski standard je istoveten z: EN 2288:2019
ICS:
49.030.99 Drugi vezni elementi Other fasteners
SIST EN 2288:2019 en,fr,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 2288:2019

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SIST EN 2288:2019


EN 2288
EUROPEAN STANDARD

NORME EUROPÉENNE

February 2019
EUROPÄISCHE NORM
ICS 49.030.99 Supersedes EN 2288:1989
English Version

Aerospace series - Bush, flanged, corrosion resisting steel,
with self-lubricating liner - Dimensions and loads
Série aérospatiale - Bague à épaulement, en acier Luft- und Raumfahrt - Buchse mit Flansch aus
resistant à la corrosion, à garniture autolubrificante - korrosionsbeständigem Stahl mit selbstschmierender
Dimensions et charges Beschichtung - Maße und Belastung
This European Standard was approved by CEN on 18 June 2018.

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, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, 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
© 2019 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2288:2019 E
worldwide for CEN national Members.

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SIST EN 2288:2019
EN 2288:2019 (E)
Contents
Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Requirements . 4
4 Designation. 8
5 Marking . 8
6 Technical specification . 8
7 Design recommendation . 9
8 Quality management system . 9



2

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SIST EN 2288:2019
EN 2288:2019 (E)
European foreword
This document (EN 2288:2019) 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 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 August 2019, and conflicting national standards shall
be withdrawn at the latest by August 2019.
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 2288:1989.
According to the CEN-CENELEC Internal Regulations, the national standards organizations of the
following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria,
Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta,
Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland,
Turkey and the United Kingdom.
3

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SIST EN 2288:2019
EN 2288:2019 (E)
1 Scope
This European standard specifies the characteristics of flanged bushes in corrosion resisting steel with
self-lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 163 °C and assembly
with an interference fit into fixed and moving aerospace parts.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
EN 2311, Aerospace serie
...

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