AECMA PREN 3155-012-2000 Aerospace Series Electrical Contacts Used in Elements of Connection Part 012 Contacts Electrical Triaxial Size 8 Male Type D Solder Class R Product Standar.pdf

1、STDaAECMA PREN 3355-012-ENGL 2000 U 301231L 0038334 i99 m Edition approved for publication 2000-05-31 AECMA STANDARD NORME AECMA AECMA NORM Comments should be sent within six months C2 Chairman after the date of publication to AECMA Guiledelle 94 Mr Peuetta B-1200 BRUXELLES prEN 31 55-012 Edition P

2、2 May 2000 ICs: 49.060 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 Supersedes edition P 1 March 1993 Descriptors: Aerospace industry, aircraft equipment, element of electrical connection, ele

3、ctrical contact, characteristic, marking ENGLISH VERSION Aerospace series Electrical contacts used in elements of connection Part O1 2: Contacts, electrical, triaxial, size 8, male, type D, solder, class R Product standard Srie arospatiale Luft- und Raumfahrt Contacts lectriques utiliss dans les org

4、anes de connexion Partie 012: Contacts lectriques triaxiaux, taille 8, mles, type D, souder, classe R Elektrische Kontakte zur Verwendung in Verbindungselementen Teil O1 2: Elektrische triaxiale Stiftkontakte, Gre 8, Typ D, zum Lten, Klasse R Norme de produit Produ ktnorm This “Aerospace Series“ Pre

5、standard has been drawn 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 countr

6、ies. Subsequent to the 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

7、formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. aecrna 201 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with

8、 AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD.AECMA PREN 3155-OLZ-ENGL 2000 LOL23LL OOL83L5 625 m Page 3 prEN 31 55-01 2: 2000 O Introduction The contacts defined by this standard are derived from and interchangeable with those of MIL-C-39029/90A. They

9、are also interchangeable with those of standard EN 31 55-01 O. 1 Scope This standard specifies the required characteristics and tests applicable to size 8, male triaxial electrical contacts O1 2, type D, solder, class R, used in elements of connection according to EN 31 55-002. It shall be used toge

10、ther with EN 31 55-001. The associated female contacts are defined in EN 31 55-01 1 and EN 31 55-01 3. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the te

11、xt and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies.

12、 EN 2591* EN 3155-001 EN 31 55-002 EN 31 55-01 O EN 3 EN 3 55-01 1 55-01 3 EN 3375-003 EN 3375-004 EN 3375-005 MIL-A-8243D MI L-C-25769J MlL-C-39029/90A MI L-H-5606E MIL-1-81 969/14 MIL-L-7808J MI L-L-7870A MI L-L-23699C SAE AS 1241A Aerospace series - Elements of electrical and optical connection -

13、 Test methods - General Aerospace series - Electrical contacts used in elements of connection - Part 001: Technical specification 1) Aerospace series - Electrical contacts used in elements of connection - Part 002: List and utilization of contacts 1) Aerospace series - Electrical contacts used in el

14、ements of connection - Part 010: Contacts, electrical, triaxial, size 08, male, type D, crimp, class R - Product standard 1) Aerospace series - Electrical contacts used in elements of connection - Part 011: Contacts, electrical, triaxial, size 8, female, type D, crimp, class R - Product standard 1)

15、Aerospace series - Electrical contacts used in elements of connection - Part 013: Contacts, electrical, triaxial, size 8, female, type D, solder, class R - Product standard 1) Aerospace series - Cables, electrical, for signal data transmissions - Part 003: Cables, bifilar, single braid - Product sta

16、ndard 2) Aerospace series - Cables, electrical, for signal data transmissions - Part 004: Cables, bifilar, double braid - Product standard 2) Aerospace series - Cables, electrical, for signal data transmissions - Part 005: Cables, bifilar, double braid, high immunity - Product standard 2) Anti-icing

17、 and deicing-defrosting fluids 3) Cleaning compound, aircraft surface, alkaline water base 3) Contact, electrical connector, concentric twinax, pin, size 8 3) Hydraulic fluid, petroleum base, aircraft, missile and ordnance 3) Installing and removal tools, connector electrical contact, type 111, clas

18、s 2, composition B 3, Lubricating oil, aircraft turbine engine, synthetic base, NATO code number 0-1 48 3) Lubricating oil, general purpose, low temperature 3) Lubricating oil, aircraft turbine engines, synthetic base 3) Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft (March 83) 4) And a

19、ll its 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 DC 20301 USA 4) Published by Society of Automotive Engineers, Inc. (S

20、AE), 400 Commonwealth Drive Warrendale, PA 15096-0001 Previous page is blank 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 3155-012-EN

21、GL 2000 1012311 001831b 5bL = Pane 4 prN 31 55-01 2: 2000 3 Definitions For the purposes of this standard, the definitions given in EN 31 55-001 apply. 4 Required characteristics 4.1 Specific characteristics Type D contacts are contacts with screening feature, class R corresponds to an operating tem

22、perature range from - 65 “C to 150 OC. They may be delivered in different conditions defined in table 9 of EN 31 55-001. 4.2 Dimensions and mass See figure 1 for dimensions. Dimensions and tolerances are given in millimetres. Contact mass: 3,50 g ma. 0.58 max. Key 1 Diameter of outside after wiring

23、2 Corelcentre contact solder zone 3 Corefintermediate contact solder zone 4 Braid/outer contact solder zone 5 Point of contact with a flat ended gauge pin of diameter 2,870 I 0,005 6 End of contact centre pin 7 Diameter compatible with intermediate pin diameter 2,870 f 0,025 8 Permitted flat 40,2 ma

24、. 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 3155-OLZ-ENGL 2000 = 1012311 0018317 4TB = Page 5 prEN 3155-012: 2000 4.3 Mat

25、erial, surface treatment 4.3.1 Material Body: copper alloy 4.3.2 Protective coating Gold on appropriate undercoat for copper alloy parts. Thickness not specified. 4.3.3 Dielectric ETFE Fluoropolymer 4.3.4 Heat-shrinkable tubing Radiation crosslinked polyvinylidene fluoride. 4.4 Permissible cables Se

26、e table 1. Table I I i I I Cable reference 1 Permissible cable group codes I A I EN 3375-003 I I B I EN 3375-004 I C I EN 3375-005 I 4.5 Dimensions are in millimetres. See figure 2 to figure 17. Stripping of cables and wiring method Pre-position the screening feature ferrule on the cable - Figure 2

27、Expose the braid by stripping the insulation Figure 3 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 3355-032-ENGL 2000 = 3032313 00383

28、38 334 Page O prEN 31 55-01 2: 2000 Pick up and roll back the braid. Pick up and roll back the first braid. Single braid EN 3375-003 Double braid Double braid - Mu metal EN 3375-004 EN 3375-005 Figure 4 Figure 5 Figure 6 Cut the Mu metal strip Figure 7 Align the two wires of the pair Cut the filler

29、Strip the conductors I I 2 *os Figure 9 Pick up and roll back the second braid Figure 0 Flux (RMA flux) and tin plate the conductors with Sn63 Pb37 Recut the conductors to the lengths indicated (white and coloured wires of the pair). I I 3,5*0.s Key 1 White colour Figure 10 Copyright Association Eur

30、opeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECIA PREN 3155-012-ENGL 2000 W LO12311 00183L9 270 Page 7 prEN 3155-012: 2000 Insert the conductors in the contacts: - whit

31、e conductor: centre contact; - colour conductor: intermediate contact; - introduce the cable to butt into the contact (centre conductor); - check the position of the colour conductor and the position of the sleeve as indicated. -4 Key 1 Colour conductor 2 3 Oto1 rnax. 4 Cable/contact butt The sleeve

32、 covers the jacket of the colour conductor Figure 11 After having checked the alignment of the V of the cable clamp with the positioner; insert the contacticable assembly in the positioner. See figure 12. Turn on the heating tool for at least 30 s before Set-up. Position the contact in the heating z

33、one using the holding fixture. 3 4-LJ Key 1 Reflector 2 Positioner 3 Clamp 4 Holding tool Figure 12 2 Heat until the two solder preforms have completely melted. Leave the assembly to cool for a minimum of 15 s before withdrawing the contact from the fixture. Copyright Association Europeene des Const

34、ructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD.AECMA PREN 3155-012-ENGL 2000 I 10123Ll 0018320 T92 Page 8 prEN 31 55-01 2: 2000 Checking the contact Set-up. See figure 13. The contact can

35、 only be correctly Set-up if all of the following conditions are visually observed: - the two solder preforms have disappeared; - respecting the overlap of the colour conductor. 2.5 max. I j U_* Key 1 Overlap 2 Melted solder rings NOTE is not affected. A slight browning of the kynar sleeve is accept

36、able given that the performance of the product used Figure 13 Bring back the braid(s) over the body of the contact. See figure 14. Cut the braid according to the dimension indicated. Figure 14 Introduce the screening feature ferrule to butt into the contact shoulder. See figure 15. Figure 15 Copyrig

37、ht 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 3155-012-ENGL 2000 LO12311 0018321 q2q m Page 9 prEN 3155-012: 2000 Heat the screening feature

38、ferrule until solder has completely melted through the holes. See figure 16. Hold the ferrule with a tool while heating. Leave the assembly to cool for a minimum of 15 s before withdrawing the contact from the tool. Figure 16 Checking the ferrule Set-up The braid shall be correctly wetted by the sol

39、der and shall be visible through at least 2 holes in the screening feature ferrule. Figure 17 4.6 Tooling Conform to MIL-I-81969/14 Insertion: not necessary Extraction: M-81969/14-O6 I- 0.25 max. Contact termination: the hot air generator is of a minimum usable capacity of 800 Wand the temperature i

40、n the heating zone shall be (420 f 20) OC. The drawing of the tool is given for information purposes: the positioner has an interface for the male contact on side P and the female contact on side S (see figure 12); the function of the cable clamp is to hold the parts in place during the heating and

41、cooling phases. 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-,-,-X X X Cable as per table 1 - Prok distance: (150 f 2) mm Test temperature: ambient Oute

42、r Not applicable 4.7 Tests See table 2. Table 2 - Tests Not ipplicable Applicable EN 2591 - Test According EN 31 55-001 to I Remarks 1 o1 Visual examination i 02 Examination of dimensions and mass Contact resistance - low level 201 Maximum contact resistance Contact 1-1 Intermediate 55 1 66 I 202 Co

43、ntact resistance at rated current Cable as per table 1 - Prob distance: (150 f 2) mm Maximum contact resistance rnR Rated I I I I initiai Y2lL-I tests tests 661 94 111 Centre I I I I Outer I 6,3 I 7,5 I 10,7 I 12 204 DiscontinuiGf contacts in the microsecond range Method B Duration of discontinuity:

44、 5 Gn At15O“C 2GR 206 Measurement of insulation resistance Method C Proof tect voltage at sea level: 1 O00 V r.m.s. between centre contact and intermediate contacl and 500 V r.m.s. between intermediate contact and outei contact. Proof test voltage at altitude: 125 V r.rn.s. at 1,l kPa pressure (33 O

45、00 m). Leakage current: 2 mA 207 Voltage proof test 21 o Electrical overload :ontinued) 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

46、3155-032-ENGL 2000 = LOL23LL 0038323 7Tl Page 11 prEN 31 55-01 2: 2000 The contacts shall be connected to a cable which complies with EN 3375 then fitted in the connectors. The connectors fitted with appropriate cable clamps shall I be mated and mounted on the fixture using appropriate mounting syst

47、ems. The cables are clamped a minimum of 200 mm from the rear of the contacts at a fixed point of the assembly. Discontinuity: I 1 O0 ns Test at (23 f 51 “C Not applicable Applicable According to I Remarks EN 31 55-001 2apacity measurement rransfer impedance X X Under investigation Shielding effecti

48、veness from 1 O0 MHz to I GHz Indurance at temperature - X X Method B Duration: 1 O00 h Mould growth Salt mist X X Resistance to fluids X See table 3. Sinusoidal and random vibraions i fi continued) Method A, severity 300. The contacts shall be connect= with a cable as per EN 3375 then fitted in con

49、nectors. The connectors fitted Witt appropriate cable clamps shal be mated and mounted or Table 2 (continued) :N 2591- Test 21 1 21 2 21 3 301 305 qapid change of temperature 306 307 31 5 402 Shock X 403 406 Mechanical endurance XI 1 Damage by test probe Robustness of the contact to flexion Tensile resistance of crimped connections 41 5 41 6 41 7 XI XI -1 41 8 Gauge