1、STD-AECMA PREN 40b7-001-ENGL I777 I LOL23LL 00L33b3 A21 W AECMA STANDARD NORME AECMA AECMA NORM prEN 4067-001 Edition P 1 September 1997 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 11 ICs: Desc
2、riptors: ENGLISH VERSION Aerospace series Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 OC peak Part O01 : Technical specification Srie arospatiale Luft- und Raumfahrt Connecteurs lectriques circulaires, contact protg, accouplement
3、 par bague filete, rsistant au feu, temprature 260 OC en pointe Partie O01 : Spcification technique Elektrische Rundsteckverbinder, Kontaktgeschtzt Schraubkupplung, feuerbestndig Betriebstemperaturen, 260 OC Spitze Teil 001 : Technische Lieferbedingungen This “Aerospace Series Prestandard has been d
4、rawn up under the responsibility of AECMA The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to th
5、e publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre NPS) and formal agreement of th
6、e Official Services of the Member countries it will be submitted as a draft European Standard to CEN European Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX I Comment
7、s should be sent within six months after the date of publication to I Edition approved for publication 1997-09-30 AECMA Gulledelle 94 B-1200 BRUXELLES C2 Chairman Mr Pezzetta aecma 1997 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA
8、Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 prEN 4067-001 : 1997 Contents list O 1 2 3 4 10 11 12 Introduction Scope Normative references . Terminology Description Design . Definition drawings and masses Tests Quality assurance . Designation and marking
9、. Delivery conditions Packaging Storage . Page 3 3 3 4 4 6 6 23 34 39 39 39 39 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 4067-001: 19
10、97 O Introduction This family of connectors is derived from MIL-C-83723 series III type T, EN 2997-001 and MIL-C-39029 for the contacts. It is particularly suitable for use on aircraft engines and in zones of severe environmental conditions on board aircraft, applying EN 2282. These connectors are d
11、istinguishable from EN 2997-001 by: - the contact protection effectiveness (scoop-proof). 1 Scope This standard specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for threaded ring coupling circular conne
12、ctors, fire-resistant, intended for use in a temperature range from - 65 OC to 260 OC peak. 2 Normative references This European Standard incorporates by dated or undated reference provisions from others publications. These normative references are cited at the appropriate places in the text and the
13、 publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 26
14、3 EN 2234 EN 2267-002 EN 2282 EN 2591 * EN 2997-001 EN 3042 EN 3155-001 EN 3197 EN 4067-002 IS0 inch screw threads - General plan and selection for screws, bolts and nuts - Fiameter range 0,06 to 6 in Aerospace series - Fire-resistant electrical cables - Technical specification 1) Aerospace series -
15、 Cables, electrical, for general purpose - Operating temperatures between - 55 OC and 260 OC - Part 002: General 1) Aerospace series - Characteristics of aircraft electrical supplies Aerospace series - Elements of electrical and optical connection - Test methods - General Aerospace series - Connecto
16、rs, electrical, circular, coupled by threaded ring, fire- resistant or non fire-resistant, operating temperatures 175 OC continuous, 200 OC continuous, 260 OC peak - Part O01 : Technical specification Aerospace series - Quality assurance - EN aerospace products - Qualification procedure Aerospace se
17、ries - Electrical contacts used in elements of connection - Part 001: Technical specification 1) Aerospace series - Installation of aircraft electrical and optical interconnection systems 1 Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire- resistant, operating temp
18、erature 260 OC peak - Part 002: Specification of performance and contact arrangements 1) * Including all its parts. 1) Published as AECMA Prestandard at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license wi
19、th AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN qOb7-00L-ENGL 1777 LOL23LL 00L33bb 530 D Page 4 prEN 4067-001: 1997 M IL-A-8243D M IL-C-25 769 J MIL-C-39029D MIL-C-83723E MIL-H-5606E MI L-L-7808 J M IL-L-7 8 70A MIL-L-23699C MIL-STD-454M AS 1
20、241A TR 4257 Anti-icing and deicing-defrosting fluids 2) Cleaning compound, aircraft surface, alkaline water base 2) Contacts, electrical connector, general specification for 2) Connectors, electrical, (circular, environment resisting), receptacles and plugs, general specification for 2) Hydraulic f
21、luid, petroleum base, aircraft, missile and ordnance 2) Lubricating oil, aircraft turbine engine, synthetic base, NATO code number 0-1 48 2) Lubricating oil, general purpose, low temperature 2) Lubricating oil, aircraft turbine engine, synthetic base 2) Electronic equipment, standard general require
22、ments for 2) Fire resistant phosphate ester hydraulic fluid for aircraft 3) Aerospace series - Elements of electrical and optical connection - Relationship between the numbering systems for parts of EN 2591 4) 3 Terminology See EN 2591. 4 Description Different housings and contact arrangements are p
23、rovided according to the models depending on the service conditions. These connectors use crimp or solder contacts of sizes 20 and 16. The receptacles and plugs contain either male contacts or female contacts. The contacts fitted in the model YE receptacles are exclusively of the male solder type. T
24、he connectors are polarized by means of keyways and keys ; polarization shall be obtained before the male contacts enter the insert of the female contacts and before the coupling ring is engaged. The position of the keying arrangement is given in table 4. The visual check of coupling is obtained by
25、masking of a blue colour band on the receptacle. 2) Published by: Department of Defense (DODI, the Pentagon, Washington, D.C. 20301 USA. 3) Published by: Society of Automotive Engineers, Inc. (SAE) 400 Commonwealth Drive, Warrendale, 4) Published as AECMA Technical Report at the date of publication
26、of this standard PA 15096-001 USA. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 40b7-001-ENGL 1777 LOL231L DOL33b7 47-7 Page 5 prEN 4
27、067-001 : 1997 4.1 Receptacle The receptacle may be attached by: - square flange; - nut, with sealing by O-ring at the attachment; - round soldered, brazed or welded flange for model YE connectors. The receptacle contains five keyways in which the keys of the plug engage. The main keyway is fixed an
28、d is wider than the others. Polarization is ensured by the different positions which the secondary keyways may take. The position of the insert is fixed relative to the main keyway. 4.2 Plug The plug contains five keys which engage in the keyways of the receptacle. The main key is wider than the oth
29、ers. Polarization is ensured by the different positions which the secondary keys may take. The position of the insert is fixed relative to the main key. The coupling ring permanently fitted on the plug enables the connectors to be coupled and uncoupled. The screwing up torque shall be lower than the
30、 unscrewing torque. The internal thread of the coupling ring may be treated with a suitable lubricant compatible with the performance required in this standard. The plug of model SE is fitted with a grounding spring device ensuring electrical continuity between the coupled connector housings. 4.3 Ma
31、terials and surface treatment When dissimilar metals are in close contact, adequate protection against corrosion shall be used for the electromotive force of the cell not to exceed 0,25 V (see EN 31971. 4.3.1 Housings The material of the housing for the connectors and for the fittings shall be passi
32、vated stainless steel (see EN 4067-002). 4.3.2 Contacts Unless otherwise specified, the contacts shall be in ferrous alloy for model YE and in copper alloy for the other models. They shall be gold-plated on an appropriate undercoat. Selective protection is authorized provided that it is sufficient t
33、o ensure that performance is met. Measurement of the thickness of the protective treatment shall be effected in accordance with EN 2591-508. 4.3.3 Nonmetallic materials The materials used for insert, seals and grommets shall have a hardness and mechanical and electrical characteristics consistent wi
34、th the required use. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN Ob7-00L-ENGL 1777 2012311 00133bB 303 Page 6 prEN 4067-001 : 1997 5
35、 Design 5.1 Housings The connector housings shall be in one unit. They shall contain teeth at the rear over the entire periphery and shall accomodate cable outlet accessories. The receptacle shall furthermore be fitted with an O-ring seal for sealing the coupled housings. Receptacles for attachment
36、by nut shall contain an O-ring seal. The nut shall have holes for the passage of locking wire. The threads shall conform to IS0 263. The coupling ring shall be designed so that the male and female contacts engage when it is turned in a clockwise direction and disengage when turned anticlockwise. The
37、 coupling threads may have a lubricant applied during manufacture. On completion of tightening of the coupling ring, mechanical contact shall exist between the receptacle and the plug. Masking of the colour band (see figure 1) shall show that the connectors are correctly coupled. The outlet accessor
38、ies shall compress the grommet of the connectors without twisting it. A blue colour band indicating that the crimp contacts of the connectors are intended for rear removal shall be provided: - behind the flange of the receptacles with square flange; - on the flange of receptacles for nut attachment;
39、 - on the coupling ring of the plugs. The position of the colour bands shall be such that at least one of them is visible when the connectors are fitted and when they are coupled or uncoupled. 5.2 Inserts The insert carrying the male and female contacts shall be in hard material and have a cross sec
40、tion and radii such that no cracks, flaking or breaks can occur in normal operation. The insert for contacts shall be non-removable ; it shall be mechanically held in the housing. Sealing shall be provided between the housing and insert. The front face of the insert shall be such that sealing is ens
41、ured when the connectors are coupled. The interfacial seal of the insert of the male contacts shall be bonded on the hard insert. The grommet shall permit sealing for all cable diameters indicated in EN 4067-002 and shall not be removable. The mechanical contacts retention system shall be integrated
42、 in the hard insert. The design of non-hermetic connectors shall permit individual installation of the contacts without removal of the insert or grommet. Fitting and removal of the contacts shall be from the rear with the tools specified in the contact product standards. 6 Definition drawings and ma
43、sses The general dimensions and the masses of receptacles and plugs are given in the product standards. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,
44、-6.1 Receptacle mating dimensions The mating dimensions of receptacles are shown in figure 1 and details A, B, C and D as well as in tables 1 and 2. Dimensions and tolerances are in millimetres. Detail A A Thread R 0.3* 0.1 Bluecolour band !I I I I I 1.73 11.13 Detail C 16.66 16,28 interfacial $eat
45、II / Optionalshape Hard insert Housing size 08 : 1,50 r0.08 - Sea dia. Housing sizes 10 to 24 : 1,78*0.08 16.98 Detail B 2,15 1.81 I I II 1 I 0.89 Detail D (5:l) 2,oo I90 )-L * Blue band shall be located on receptacle so as to be visible when unmated and fully covered when completely mated. This col
46、our band designs also the rear release contact connectors. Figure 1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 40b7-00L-ENGL 1777 D
47、 LOL23LL 0033370 TbL Page 8 prEN 4067-001 : 1997 Housing size 08 10 12 14 16 18 20 22 24 Table 1 Thread, C D 5 T class 2A 1) max. 7,37 9,86 12,58 1,93 12,45 1,80 16,28 16,15 20,60 20,47 22,35 22,22 25,58 25,45 2,26 28,27 2,13 28,14 31,45 31,32 34,62 34,49 37,80 37,67 10,62 10,49 13,59 13,46 17,91 17
48、,78 19,66 19,53 22,88 22,76 25,58 25,45 28,75 28,62 31,93 31,80 35,lO 34,97 0,562 UNEF 24 0,688 UNEF 24 14,17 15,93 19,61 0,875 UNEF 20 0,938 UNEF 20 1,062 UNEF 18 21,84 1,188 UNEF 18 25,02 1,312 UNEF 18 28,19 1,438 UNEF 18 31,37 1,562 UNEF 18 1,50 1,24 2,06 1,80 20 16 I 1) IS0 263 3,OO 1,17 2,28 2,
49、90 1 ,O7 2,14 3,81 1,75 2,88 3,71 1,65 2,73 Table 2 0.99 3,00 2,38 2,28 2,98 1,61 2,88 I 3f81 1 1,56 2,44 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 9 prEN 4067-001 : 1997 6.2 Plug mating dimensions The coupling dimensions for plugs are shown in figu
