EN 3545-001:2005
(Main)Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specification
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specification
This standard specifies the technical requirements of rectangular connectors with sealed and non-sealed rear, plastic housing, locking device, for operating temperatures from - 55 °C to 175 °C.
Luft- und Raumfahrt - Elektrische Rechtecksteckverbinder mit und ohne hintere Abdichtung, Plastikgehäuse, Verriegelungssystem, Betriebstemperaturen von - 55 °C bis 175 °C - Teil 001: Technische Lieferbedingungen
Diese Norm legt die technischen Anforderungen an Rechtecksteckverbinder mit und ohne hintere Abdichtung, mit Plastikgehäuse und Verriegelung, für Betriebstemperaturen von -55 °C bis 175 °C fest.
Série aérospatiale - Connecteurs électriques, rectangulaires, étanches et non étanches à l'arrière, à boîtier en plastique, à verrouillage, températures d'utilisation - 55 °C à 175 °C - Partie 001 : Spécification technique
Aeronavtika – Konektorji, električni, pravokotni, s tesnilno kapo ali brez nje, plastičnim ohišjem, zapornim mehanizmom, z delovno temperaturo med –55 °C in 175 °C – 001. del: Tehnična specifikacija
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specificationSérie aérospatiale - Connecteurs électriques, rectangulaires, étanches et non étanches a l'arriere, a boîtier en plastique, a verrouillage, températures d'utilisation - 55 °C a 175 °C - Partie 001 : Spécification techniqueLuft- und Raumfahrt - Elektrische Rechtecksteckverbinder mit und ohne hintere Abdichtung, Plastikgehäuse, Verriegelungssystem, Betriebstemperaturen von - 55 °C bis 175 °C - Teil 001: Technische LieferbedingungenTa slovenski standard je istoveten z:EN 3545-001:2005SIST EN 3545-001:2006en49.060ICS:SLOVENSKI
STANDARDSIST EN 3545-001:200601-julij-2006
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3545-001
November 2005 ICS 49.060 English Version
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specification
Série aérospatiale - Connecteurs électriques, rectangulaires, étanches et non étanches à l'arrière, à boîtier en plastique, à verrouillage, températures d'utilisation - 55 °C à 175 °C - Partie 001 : Spécification technique
Luft- und Raumfahrt - Elektrische Rechtecksteckverbinder mit und ohne hintere Abdichtung, Plastikgehäuse, Verriegelungssystem, Betriebstemperaturen von -55 °C bis 175 °C - Teil 001: Technische Lieferbedingungen This European Standard was approved by CEN on 26 September 2005.
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 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 translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions.
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, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36
B-1050 Brussels © 2005 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3545-001:2005: E
Cables, electrical, for general purpose
Operating temperatures between – 55 °C and 200 °C
Part 002: General. EN 2591-100 *, Aerospace series
Elements of electrical and optical connection
Test methods
Part 100: General. EN 3155-001, Aerospace series
Electrical contacts used in elements of connection
Part 001: Technical specification. 1) EN 3155-003, Aerospace series
Electrical contacts used in elements of connection
Part 003: Contacts, electrical, female, type A, crimp, class S
Product standard. EN 3155-008, Aerospace series
Electrical contacts used in elements of connection
Part 008: Contacts, electrical, male, type A, crimp, class S
Product standard. EN 3155-070, Aerospace series
Electrical contacts used in elements of connection
Part 070: Contacts, electrical, male, type A, crimp, class S
Product standard.2) EN 3155-071, Aerospace series
Electrical contacts used in elements of connection
Part 071: Contacts, electrical, female, type A, crimp, class S
Product standard.2) EN 3197, Aerospace series
Installation of aircraft electrical and optical interconnection systems.1) EN 3545-002, Aerospace series
Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C
Part 002: Specification of performance and contact arrangements. EN 3545-008, Aerospace series
Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures – 55 °C to 175 °C
Part 008: Tools for assembly/removal of coding and attachment systems
Product standard.2) EN 4529-002, Aerospace series
Elements of electrical and optical connection
Sealing plugs
Part 002: Index of product standards. 1) EN 9133, Aerospace series
Quality management systems
Qualification procedure for aerospace standard parts.
* And all parts quoted in this standard. 1) Published as AECMA Prestandard at the date of publication of this standard. 2) In preparation at the date of publication of this standard.
3) Published by: Society of Automotive Engineers, Inc. (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA. 4) Published by: Department of Defense (DOD), the Pentagon, Washington, D.C. 20301 USA.
4.3 Materials 4.3.1 General The materials which are not specified or are not specially described, shall be as light as possible for the required application. Materials are chosen according to safety criteria as defined by the authority of certification. When dissimilar metals are in close contact, adequate protection against corrosion shall be provided such that the electromotive force of the galvanic couple shall not exceed 0,25 V. 4.3.2 Housings These are made of rigid material with high dielectric qualities which will not deteriorate under normal conditions of operation and ageing. 4.3.3 Contacts Contacts shall comply with the requirements of EN 3155-001. 5 Design 5.1 Housings In the sealed and non-sealed types, the grommet shall be attached to the housing. Identification of the various positions used for coding by the position indicator which appears on the attachments is given in EN 3545-002. Identification of the contact cavities shall be consistent with Figures 3 to 10 in EN 3545-002.
Key 1 0,9 min. (see NOTE 1) 2 2,4 max. for contact size 20 2,3 max. for other sizes (see NOTE 2) 3 1 to 1,9 (see NOTE 3) 4 0,03 to 0,58 for arrangements 01 to 06 0,05 to 0,60 for arrangements 07 and 08 5 1,27 min. for quadrax contacts (see NOTE 1) 6 Connector with male contacts 7 Male coding and attachment system 8 Female coding and attachment system 9 Connector with female contacts a Applicable dimensions for contact arrangement 07 and 08
NOTE 1 Electrical engagement of contacts. NOTE 2 Extreme limit position of electrical point of female contact. NOTE 3 Extreme limit position of male contact, maximum axial clearance: 0,5 Figure 1
Figure 2
Figure 4 7.5 Arrangement 04 21 contacts, size 16 See Figure 5.
Figure 5
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