SIST EN 3716-001:2009
(Main)Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 001: Technical specification
Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 001: Technical specification
This standard applies to single-way connectors with triaxial interfaces used in the transmission of digital data, with the two-core shielded cables in accordance with EN 3375-003, EN 3375-004 and EN 3375-005.
This standard defines the general characteristics of connectors with screw couplings usable up to a frequency of 5 MHz. It specifies the conditions of qualification, acceptance and quality assurance. It defines the test programmes and groups.
Temperature class: - 65°C to 150°C
Luft- und Raumfahrt - Steckverbinder, triaxial für digitale Datenübertragung in einer Richtung - Teil 001: Technische Lieferbedingungen
Diese Norm gilt für einpolige, triaxiale Steckverbinder, die zur Übertragung von digitalen Daten mit zweiadri¬gen, geschirmten Leitungen nach EN 3375 003, EN 3375 004 und EN 3375 005 verwendet werden.
Diese Norm legt die allgemeinen Eigenschaften von Steckverbindern mit Schraubkupplung zur Verwendung bis zu einer Frequenz von 5 MHz fest. Sie gibt die Qualifikations , Abnahme und Qualitätssicherungsbe¬dingungen an. Sie legt die Prüfprogramme und Prüfgruppen fest.
Temperaturklasse: 65 °C bis 150 °C
Série aérospatiale - Connecteur, monovoie, avec interface triaxiale, pour transmission de données numériques - Partie 001: Spécification technique
Aeronavtika - Konektorji, enosmerni, triaksialni, za digitalni prenos podatkov - 001. del: Tehnična specifikacija
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Steckverbinder, triaxial für digitale Datenübertragung in einer Richtung - Teil 001: Technische LieferbedingungenSérie aérospatiale - Connecteur, monovoie, avec interface triaxiale, pour transmission de données numériques - Partie 001: Spécification techniqueAerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 001: Technical specification49.060Aerospace electric equipment and systemsICS:Ta slovenski standard je istoveten z:EN 3716-001:2006SIST EN 3716-001:2009en,de01-julij-2009SIST EN 3716-001:2009SLOVENSKI
STANDARD
SIST EN 3716-001:2009
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 3716-001May 2006ICS 49.060 English VersionAerospace series - Connector, single-way, with triaxial interface,for transmission of digital data - Part 001: Technical specificationSérie aérospatiale - Connecteur, monovoie, avec interfacetriaxiale, pour transmission de données numériques - Partie001 : Spécification techniqueLuft- und Raumfahrt - Steckverbinder, triaxial für digitaleDatenübertragung in einer Richtung - Teil 001: TechnischeLieferbedingungenThis European Standard was approved by CEN on 20 February 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 3716-001:2006: ESIST EN 3716-001:2009
EN 3716-001:2006 (E) 2 Contents Page Foreword.3 1 Scope.4 2 Normative references.4 3 Terms and definitions.5 4 Description.5 5 Design.5 6 Definition drawings and masses.6 7 Tests.11 8 Quality assurance.17 9 Designation and marking.20 10 Packaging.21 11 Packing.21 12 Storage.21
SIST EN 3716-001:2009
EN 3716-001:2006 (E) 3 Foreword This European Standard (EN 3716-001:2006) 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 3716-001:2009
EN 3716-001:2006 (E) 4 1 Scope This standard applies to single-way connectors with triaxial interfaces used in the transmission of digital data, with the two-core shielded cables in accordance with EN 3375-003, EN 3375-004 and EN 3375-005. This standard defines the general characteristics of connectors with screw couplings usable up to a frequency of 5 MHz. It specifies the conditions of qualification, acceptance and quality assurance. It defines the test programmes and groups. Temperature class: − 65°C to 150°C 2 Normative references The following referenced documents are indispensable for the application 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 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 3375-003, Aerospace series — Cables, electrical, for signal data transmissions — Part 003: Cable, bifilar, double-braid — Product standard. 2) EN 3375-004, Aerospace series — Cables, electrical, for signal data transmissions — Part 004: Cable, bifilar, single-braid — Product standard. 2) EN 3375-005, Aerospace series — Cables, electrical, for signal data transmissions — Part 005: Cable, bifilar, double-braid, high immunity — Product standard. 2) EN 3716-*, Aerospace series — Connector, single-way, with triaxial interface, for transmission of digital data. EN 9133, Aerospace series — Quality management systems — Qualification Procedure for aerospace standard parts. MIL-DTL-5624U, Turbine fuel, aviation, grades JP-4 and JP-5. 3) MIL-HDBK-454A, General guidelines for electronic equipment. 3) MIL-PRF-7808L, Lubricating oil, aircraft turbine engine, synthetic base, NATO code number O- 148. 3) MIL-PRF-23699F, Lubricating oil, aircraft turbine engine, synthetic base, NATO code number O-156. 3) MIL-PRF-87937D, Cleaning compound aerospace equipment. 3) QPL-5606-31, Hydraulic fluid, petroleum base; aircraft; missile and ordnance. 3)
* And all parts quoted. 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: Department of Defense (DOD), The Pentagon, Washington D.C. 20301, USA. SIST EN 3716-001:2009
EN 3716-001:2006 (E) 5 FED-STD-H28, Screw thread standards for federal services. 3) AMS1424D, Fluid, Deicing/Anti-Icing, Aircraft, SAE Type I. 4) 3 Terms and definitions For the purposes of this standard, the terms and definitions given in EN 2591-100 and EN 3155-001 apply. 4 Description 4.1 General The triaxial connectors are the solder or crimp contact type, with mechanical end stop. The coupling system is the screw type; at the end of coupling the housings are mechanically stopped. 4.2 Receptacle Fixing is by nut, anti-vibration washer and gasket seal. 4.3 Plug The knurled coupling ring mounted permanently on the plug allows the connectors to be coupled and decoupled. 4.4 Materials and surface treatment When dissimilar metals are in close contact, adequate protection against corrosion shall be used to ensure that the electro-chemical potential difference does not exceed 0,25 V. a) Housing Copper alloy, tin plated. b) Contact Copper alloy, gold-plated over an appropriate undercoat. c) Insert The materials used shall have electrical and mechanical characteristics compatible with the required use. d) Ferrule Material identical to that used for housing. 5 Design The insert is not removable.
4) Published by Society of Automotive Engineers Inc. (SAE) 400 Commonwealth Drive, Warrendale, PA 15096-001, USA. SIST EN 3716-001:2009
EN 3716-001:2006 (E) 6 It is retained mechanically in the housing. The fronts of the inserts are designed to guarantee the seal when the connectors are mated. 6 Definition drawings and masses 6.1 General The general definition drawings and masses of the receptacles, plugs and flight caps are given in the product standards. 6.2 Receptacle mating dimensions 6.2.1 With socket contact See Figures 1 and 2. Dimensions and tolerances are in millimetres.
Key 1 5/16 – 32 UNEF 2A according to FED-STD-H28 Figure 1 SIST EN 3716-001:2009
EN 3716-001:2006 (E) 7
Key 1 End of socket contact 2 ∅ compatible with intermediate pin 3 End of pin contact 4 Point of contact with a flat-ended pin ∅ 1,850 ± 0,005 5 Reference plane Figure 2 SIST EN 3716-001:2009
EN 3716-001:2006 (E) 8 6.2.2 With pin contact See Figure 3. Dimensions and tolerances are in millimetres.
Key 1 End of insulator 2 ∅ compatible with intermediate pin 3 End of pin contact 4 Point of contact with a flat-ended pin ∅ 1,850 ± 0,005 5 Reference plane Figure 3 SIST EN 3716-001:2009
EN 3716-001:2006 (E) 9 6.3 Mating dimensions of plug 6.3.1 With pin contact See Figure 4. Dimensions and tolerances are in millimetres.
Key 1 End of insulator 2 End of contact ∅ 1,85 3 Point of contact with a flat-ended pin ∅ 6,080 ± 0,005 4 5/16 – 32 UNEF 2A according to FED-STD-H28 5 ∅ compatible with external pin ∅ 6,08 ± 0,04 6 ∅ compatible with internal pin ∅ 0,61 ± 0,03 7 Reference plane (mechanical stop) Figure 4 SIST EN 3716-001:2009
EN 3716-001:2006 (E) 10 6.3.2 With socket contact See Figure 5. Dimensions and tolerances are in millimetres.
Key 1 End of contact ∅ 0,61 2 Point of contact with a flat-ended pin ∅ 6,080 ± 0,005 3 End of socket contact 4 Point of contact with a flat-ended pin ∅ 1,850 ± 0,005 5 5/16 – 32 UNEF 2A according to FED-STD-H28 6 ∅ compatible with external pin ∅ 6,08 ± 0,04 7 ∅ compatible with internal pin ∅ 1,85 ± 0,03 8 Reference plane (mechanical stop) Figure 5 SIST EN 3716-001:2009
EN 3716-001:2006 (E) 11 6.4 Mating dimensions See Figure 6. Dimensions are in millimetres.
Key 1 52,20 before mating 2 41,53 max. after mating Figure 6 7 Tests See Table 1. SIST EN 3716-001:2009
EN 3716-001:2006 (E) 12 Table 1 EN 2591- Title Details 101 Visual examination With naked eye Initial examination: presence of all components; general appearance. Final examination: no loosening of parts, no cracking, no wear affecting the function, no part detached. 102 Examination of dimensions and mass As per 6 and product standard 201 Contact resistanc
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