1、 g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58metallic shells and screw-locking Part 001: Technical specificationThe European Standard EN 3218-00
2、1:2006 has the status of a British StandardICS 49.060Aerospace series Connectors, rectangular, with BRITISH STANDARDBS EN 3218-001:2006BS EN 3218-001:2006This British Standard was published under the authority of the Standards Policy and Strategy Committee on 29 September 2006 BSI 2006ISBN 0 580 491
3、76 5Amendments issued since publicationAmd. No. Date CommentsThis publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.National forewordTh
4、is British Standard was published by BSI. It is the UK implementation of EN 3218-001:2006.The UK participation in its preparation was entrusted by Technical Committee ACE/6, Aerospace avionic electrical and fibre optic technology, to Subcommittee ACE/6/-/3, Aerospace Connectors.A list of organizatio
5、ns represented on ACE/6/-/3 can be obtained on request to its secretary.EUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 3218-001April 2006ICS 49.060English VersionAerospace series - Connectors, rectangular, with metallic shellsand screw-locking - Part 001: Technical specificationSrie arospatiale -
6、 Connecteurs rectangulaires botiersmtalliques et verrouillage par vis - Partie 001 :Spcification techniqueLuft- und Raumfahrt - Rechtecksteckverbinder mitmetallischem Gehuse und Schraubverriegelung - Teil 001:Technische LieferbedingungenThis European Standard was approved by CEN on 27 February 2006.
7、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 app
8、lication 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 t
9、he 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,
10、Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 2006 CEN All rights of exploitation in any form and by any means reservedworldwid
11、e for CEN national Members.Ref. No. EN 3218-001:2006: EEN 3218-001:2006 (E) 2 Contents Page Foreword 3 1 Scope .4 2 Normative references .4 3 Terms and definitions.5 4 Conditions of use5 5 Description 5 5.1 General 5 5.2 Materials 6 6 Design6 6.1 Housings6 6.2 Accessories.6 6.3 Sealing .6 6.4 Polari
12、zation of housings.6 6.5 Mounting of receptacles.7 6.6 Threads7 6.7 Contact characteristics 7 6.8 Identification of contacts and inserts7 7 Definition drawings and masses7 7.1 General 7 7.2 Dimensions of receptacle.7 7.3 Dimensions of plug.9 7.4 Coding .12 8 Tests 12 8.1 Tests according to EN 2591-1
13、00 12 8.2 Special tests 12 8.3 Tests 13 9 Quality assurance .20 9.1 General 20 9.2 Conditions for initial qualification .20 9.3 Maintenance of qualification25 10 Designation and marking .27 10.1 Designation .27 10.2 Marking 27 11 Delivery conditions.28 12 Packing 28 13 Storage 28 Annex A (normative)
14、 Gauge for test EN 2591-410: Insert retention in housing (axial)29 EN 3218-001:2006 (E) 3 Foreword This European Standard (EN 3218-001:2006) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance wi
15、th 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 id
16、entical text or by endorsement, at the latest by October 2006, and conflicting national standards shall be withdrawn at the latest by October 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 he
17、ld 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,
18、 Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 3218-001:2006 (E) 4 1 Scope This standard specifies the general characteristics of rectan
19、gular connectors with metallic shells and screw-locking, for use in a temperature range from 65 C to 150 C on board aircraft. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For un
20、dated references, the latest edition of the referenced document (including any amendments) applies. EN 2242, Aerospace series Control of tools used for crimping of electrical cables with conductors defined by EN 2083 and EN 2346. 1)EN 2265-002, Aerospace series Cables, electrical, for general purpos
21、e Operating temperatures between 55 C and 150 C Part 002: General. 1)EN 2266-002, Aerospace series Cables, electrical, for general purpose Operating temperatures between 55 C and 200 C Part 002: General. EN 2282, Aerospace series Characteristics of aircraft electrical supplies. EN 2591-100, Aerospac
22、e 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 3155-023, Aerospace series Electrical contacts used in elements of connection Part 023: Cont
23、act, electrical, female 023, type A, crimp, class R Product standard. EN 3218-002, Aerospace series Connectors, rectangular, with metallic shells and screw-locking Part 002: Specification of performance and contact arrangements. EN 3218-005, Aerospace series Connectors, rectangular, with metallic sh
24、ells and screw-locking Part 005: Plug with non-removable size 22 solder contacts Product standard. EN 3218-006, Aerospace series Connectors, rectangular, with metallic shells and screw-locking Part 006: Receptacle with non-removable size 22 solder contacts Product standard. EN 3218-007, Aerospace se
25、ries Connectors, rectangular, with metallic shells and screw-locking Part 007: Plug with rear-removable size 20 crimp contacts Product standard. EN 3218-008, Aerospace series Connectors, rectangular, with metallic shells and screw-locking Part 008: Receptacle with rear-removable size 20 crimp contac
26、ts Product standard. EN 9133, Aerospace series Quality management systems Qualification Procedure for aerospace standard parts. Including all its parts quoted. 1) Published as AECMA Prestandard at the date of publication of this standard. EN 3218-001:2006 (E) 5 MIL-PRF-7808L, Lubricating oil, aircra
27、ft turbine engine, synthetic base, NATO code number O 148. 2)MIL-PRF-7870C, Lubricating oil: general purpose, low temperature, NATO code number O-142. 2)MIL-PRF-23699F, Lubricating oil, aircraft turbine engine, synthetic base, NATO code number O-156. 2)MIL-PRF-87937D, Cleaning compound aerospace equ
28、ipment. 2)QPL-5606-31, Hydraulic fluid, petroleum base; aircraft; missile and ordnance. 2)FED-STD-H28:1978, Aerospace series Screw thread standards for federal services. 2)AS 1241C, Fire resistant phosphate ester hydraulic fluid for aircraft. 3)AMS 1424F, Deicing/Anti-Icing fluid, Aircraft, SAE Type
29、 I. 3)3 Terms and definitions For the purposes of this standard, the terms and definitions given in EN 2591-100 and the following apply. 3.1 dummy insert insert without a cavity and used instead of an insert fitted with contacts 4 Conditions of use Operating voltage: see EN 2282 5 Description 5.1 Ge
30、neral A pair of connectors is characterized by its rectangular shell, its screw coupling system located at both ends and by the inserts which can be removed from the shell. The shells provide polarization of the coupling as well as locating and polarizing of inserts. The male contacts are rectangula
31、r in cross-section and female contacts are of the tuning-fork type; their size is comparable to a size 22 or 20 circular contact, according to the individual case. These connectors use removable crimp contacts, sizes 20 and 22, or non-removable solder contacts size 22. Receptacles and plugs can acco
32、mmodate inserts containing either male or female contacts. When male contacts are fitted in the plug, the connector is “scoop-proof“. The inserts can be removed from the shell. 2) Published by: Department of Defense (DOD), The Pentagon, Washington D.C. 20301, USA. 3) Published by Society of Automoti
33、ve Engineers Inc. (SAE) 400 Commonwealth Drive, Warrendale, PA 15096-001, USA. EN 3218-001:2006 (E) 6 Coding, carried out by the user, is provided by two removable keys located at each end of the housings and capable of assuming four positions, thus giving 16 coding options. Different configurations
34、 of housings and contact arrangements are provided in EN 3218-002. There are two sizes of housing (size 1 and size 2). 5.2 Materials The materials used shall be corrosion-resistant. When dissimilar metals or alloys are in close contact, adequate protection shall be provided so that the electromotive
35、 force of the galvanic couple shall not exceed 0,25 V. The contacts shall be covered with a gold plating over a nickel undercoat. The thickness of the gold shall be at least 1,27 m in the active zone of the contacts. The housings shall be made of aluminium alloy with, according to the version, the f
36、ollowing finishing: anodized coating: code A; cadmium plating: code C; nickel plating: code N. The threaded items and accessories shall be made of stainless steel. The materials used shall satisfy the requirements of the mould growth test (EN 2591-306). 6 Design 6.1 Housings The housings can take on
37、e or two inserts, their position are identified by the letters A and B. One or other of these inserts may be replaced by a dummy insert or by an insert not fitted with its contacts. 6.2 Accessories The receptacle and plug housings shall have a cable-clamp fitting. 6.3 Sealing Sealing shall be provid
38、ed at the rear of the contacts by an elastomer seal in the case of crimp contacts or by a heat-shrinkable sleeve in the case of solder contacts. At the interface, a seal located on the insert holding the male contacts, shall provide sealing at the coupling. 6.4 Polarization of housings Polarization
39、of the receptacle and plug is achieved by the mating faces of the housings being non-symmetrical. Polarization of A and B inserts is achieved by non-symmetry of the inserts and the internal face of the housings. EN 3218-001:2006 (E) 7 6.5 Mounting of receptacles The receptacles are panel mounted, ei
40、ther rear mounted or side mounted. In the case of rear mounting, washers shall be used to compensate for differences in panel thickness. The assembly drawings shall be included in the product standards for the different versions. 6.6 Threads Threads shall comply with FED-STD-H28. Screws shall be sel
41、f-locking. 6.7 Contact characteristics See EN 3155-001. Solder contacts are an integral part of the insert. Crimp contacts shall be removed from the insert from the rear. 6.8 Identification of contacts and inserts Contacts: the position of contact No. 1 in the row shall be identified on the front fa
42、ce of the insert by marking with a contrasting colour. Identification of contacts or cavities shall be done on a side face or the rear face of the insert. Rows: the side faces A and B of inserts and housings shall be marked. 7 Definition drawings and masses 7.1 General The general dimensions and mas
43、ses of the plugs and receptacles are given in EN 3218-005, EN 3218-006, EN 3218-007 and EN 3218-008. Dimensions and tolerances are in millimetres. 7.2 Dimensions of receptacle See Figures 1 to 3 and Table 1. EN 3218-001:2006 (E) 8 Key 1 Coding, see 7.4. a Accessories includedFigure 1 Table 1 Size N
44、a A C D F G H M max. 0,15 0 0,6 0,2 0,15 0,15 1 9 22,63 51,5 44,45 29 32,3 32,3 36,22 2 19 47,78 77,0 69,85 54,4 57,7 57,7 61,47 aN = Pitch EN 3218-001:2006 (E) 9 Figure 2 Position of contacts and mating faces Key 1 For hexagonal wrench 2,78 across flats 2 Screw 3 Three spacers thickness: 0,80 0,05
45、4 Effective depth 7,5 min. Thread: 6-32 UNC 2B Figure 3 Locking and unlocking systems 7.3 Dimensions of plug See Figures 4 to 6 and Table 2. Dimensions and tolerances are in millimetres. EN 3218-001:2006 (E) 10 Key 1 Coding, see 7.4. a Accessories includedFigure 4 Table 2 Size N a A C D F G M max. 0
46、,15 0 0,6 0,2 0,15 1 9 22,63 51,5 44,45 28,8 32,3 35,30 2 19 47,78 77,0 69,85 54,2 57,7 60,70 aN = Pitch a EN 3218-001:2006 (E) 11 Figure 5 Position of contacts and mating faces Key 1 Thread: 6-32 UNC 2A 2 For hexagonal wrench 2,78 across flats 3 Captive screw Figure 6 Locking and unlocking systems
47、EN 3218-001:2006 (E) 12 7.4 Coding See Figure 7 and EN 3218-002. NOTE The coding keys can be put in any one of four positions, each 90 apart. Figure 7 8 Tests 8.1 Tests according to EN 2591-100 The tests of EN 2591-100 applicable in the context of this standard as well as the details necessary for i
48、mplementing them and for inspecting connector characteristics are given in Table 3. 8.2 Special tests 8.2.1 Durability of insert retention system The accessories shall be removed to allow extraction and insertion of inserts. The connectors shall be mated and unmated 10 times. Ten extraction and inse
49、rtion cycles of each insert tested shall be performed using the tools specified. 8.2.2 Handling at low temperature The connectors, wired and mated, shall be exposed to 25 C for 2 h. Immediately after removal from the cold chamber, the connector shall be unmated, mated and unmated again. The inserts and the crimp contacts shall be extracted and re-inserted using appropriate tools. 8.2.3 Tightening torque Wired a
