ASD-STAN PREN 6047-001-1995 Aerospace Series Connectors Electrical Circular Coupled by Threaded Ring for High Current Operating Temperature + 200 Degrees Celsius Continuous and Fir.pdf

1、 AECflA PRENmb047- 001 95 I 10123LL 0009L 9T7 I Edition approved for publication AECMA STANDARD NORME AECMA AECMA NORM AIB/TFJ Chairman Comments should be sent within six months after the date of publication to prEN 6047-00 I Edition PI October 1995 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE

2、 INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (32) 2 775 81 10 - Fax. (32) 2 775 81 11 ICs : Descriptors : ENGLISH VERSION Aerospace series Connectors, electrical, circular, coupled by threaded ring, for high current operating temperature + 200 OC continuous, and fire resistant Part 00

3、1 - Technical specification Srie arospatiale Luft- und Raumfahrt mit Schraubkupplung, fr hohe Strme Betriebstemperaturen + 200 OC konstant, und feuerbestndig Teil O01 - Technische Lieferbedingungen Connecteurs lectriques circulaires, Elektrische Rundsteckverbinder accouplement par bague filete, pour

4、 hautes intensits temprature dutilisation + 200 OC continu, et tenant au feu Partie O01 - Spcification technique This “Aerospace Series“ Prestandard 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

5、 AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically o

6、r functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre INPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardizatio

7、n) for formal vote. 1995-10-31 AECMA Gulledelle 94 B-1200 BRUXELLES Mr Luck aecma 1995 AECMA PREN*b047- O01 75 .I 1012311 0007882 833 Page 2 prEN 6047-001 : 1995 Contents list Scope Normative references Terminology Description Design Definition drawings and masses Tests Quality assurance Designation

8、 and marking 1 O Delivery conditions 11 Packaging 12 Storage AECMA PREN*h047- OOL 95 e L0123LL 0009883 77T Page 3 prEN 6047-001 : 1995 1 scope This standard defines the characteristics of circular electrical connectors, coupled by threaded ring, for high current, operating temperature +200 OC contin

9、uous, and fire resistant, and determines quality assurance requirements. It is applicable whenever referenced, particularly suitable for use on engine and in zones of severe environmental conditions. 2 Normative references EN 2000 EN 2591 * EN 2854-003 EN 3042 EN 3197 EN 6047-002 EN 6047-003 EN 6047

10、-004 FED-STD-H28 MI L-STD-454M M IL-H-5606E M IL-L-7808J MIL-L-7870A Aerospace series - Quality assurance - EN Aerospace products - Approval of the quality of manufacturers. Aerospace series - Elements of electrical and optical connection - Test methods - General. Aerospace series - Electrical cable

11、 over 5 mm2 for general purpose. Operating temperatures between -55 “c and +260 “c - Part 003 - Product Standard ) Aerospace series - Quality assurance - EN Aerospace products - Qualification procedure. Aerospace series - Installation of aircraft electrical and optical interconnection systems . Aero

12、space series - Connector, electrical, circular, coupled by threaded ring, for high current, operating temperature +200 OC continuous, and fire resistant - Part 002 - Specification of performance and contact arrangements 2, Aerospace series - Connector, electrical, circular, coupled by threaded ring,

13、 for high current, operating temperature +200 OC continuous, and fire resistant - Part 003 - Square flange receptacle - Product standard 2, Aerospace series - Connector, electrical, circular, coupled by threaded ring, for high current, operating temperature +200 OC continuous, and fire resistant - P

14、art 004 - Plug - Product standard *) Issue march 1978 - Screw thread standards for several services. 3, Standard general requirements for electronic equipment - Requirement 4 : Fungus-inert material. 3, Hydraulic fluid, petroleum base, aircraft, missile and ordnance. 3, Lubricating oil, aircraft tur

15、bine engine, synthetic base. 3, Lubricating oil, general purpose, low temperature. 3, * and all its parts quoted in table 3. 1) In preparation at the date of publication of this standard 2) Published as AECMA Prestandard at the date of publication of this standard 3) Published by : Department Of Def

16、ense (DOD), the Pentagon, Washington, D.C. 20301, USA. Page 4 prEN 6047-001 : 1995 MI L-A-8243 D MlL-L-23699C MI L-C-25769J EUROCAE ED-148 Anti-icing and de-icing / defrosting fluid. 3, Lubricating oil, aircraft turbine engine, synthetic base. 3, Cleaning compound, aircraft surface, alkaline water b

17、ase. 3, Environemental conditions and test procedures for airborne equipment 4, 3 Terminology See EN 2591. 4 Description The pair of connectors is characterized : - by the receptacle with a square flange and threaded coupling ring ; - by the plug with a self-locking coupling screw. These connectors

18、use crimp contacts. The receptacles and plugs contain either male contacts or female contacts. The connectors are polarized by a master key ; polarization shall be obtained before the male contacts enter the insulator of the female contacts and before the coupling ring is engaged. The visual control

19、 of coupling is obtained by color markings on the plugs coupling ring. 4.1 Materials 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. 4.1.1 Housings The material of the

20、 connector housing shall be steel protected against corrosion by a passivated cadmium plating. 3) Published by : Department Of Defense (DOD), the Pentagon, Washington, D.C. 20301, USA. 4) Published by : EUROCAE (Organisation Europeenne pour IEquipement Electronique de lAviation Civile) 11, rue Hamel

21、in 75783 PARIS CEDEX 16. AECMA PREN*b047- O01 95 I 1022311 0009885 542 I Page 5 prEN 6047-001 : 1995 4.1.2 Insulators The materials used for the seals and grommets shall have a hardness and mechanical and electrical characteristics consistent with the required use. Non-resilient material used in the

22、 production of the insulators shall have electrical and mechanical characteristics compatible with the required use. 5 Design 5.1 Housings They shall be in one unit. The plug shall also be fitted with an O-ring to ensure that the housings are tightly sealed when mated. The coupling ring shall be des

23、igned so that the male and female contacts engage when it is screwed to the right and disengage when it is unscrewed to the left. The coupling ring shall be knurled. On completion of tightening of the coupling ring, mechanical contact shall exist between the receptacle and the plug. Appearance of co

24、lor (orange or red) in six lock displays located on the coupling ring shall show that the connectors are correctly coupled. The contacts are fitted in the housings by compressing them with the various insulators. These insulators are fixed inside the connector housings and held in place by tightenin

25、g a rear screw fitting that shall have at least three holes for passage of a lockwire. Threads shall comply with FED-STD-H28. 5.2 Insulators The insulator supporting the male and female contacts shall be in rigid material and have a cross section and radii such that no cracks, flaking or breaks can

26、occur in normal operation. The front face of the insulator shall be such that sealing is ensured when the connectors are coupled. The interface seal of the insulator of the male contacts shall be bonded on the rigid insulator. The grommet shall permit suitable sealing for all cable diameters indicat

27、ed in EN 6047-002. It shall be removable. The insulators shall be removable and mechanically polarized by a keyikeyway system and held tight in place by the connector backshell. An O-ring shall be fitted to ensure correct sealing between the rear insulators and the housings. AECMA PRENub047- 001 95

28、= LOL23LL 0009b 489 Page 6 prEN 6047-001 : 1995 6 Definition drawings and masses The general dimensions and the mass of receptacles and plugs are given in EN 6047-003 and EN 6047-004. 6.1 Receptacle mating dimensions The mating dimensions of receptacles are shown in figure 1. Dimensions and toleranc

29、es are in millimeters. -. 1 k L 15,87 min. 1,45 min., 0,85 + 0,lO . 6.58 max. Thread 3-1 6UN-2A Figure 1 AECMA PRENab047- O01 95 1012311 0009887 315 Page 7 prEN 6047-001 : 1995 6.2 Plug mating dimensions The mating dimensions of plugs are shown in figure 2. All mating dimensions are given when conne

30、ctors are mated and when mating surfaces are against each other. Dimensions and tolerances are in millimeters. Point of Lock indicator ref. when 19,13 connectors are mated 18.26 0,36 max. 2,29 7 li 1,78 Polarizing groove , 1 1 0 69,34 c 0 68,96 Thread 3-1 6UN-2B c View as per F Lock display Unmated

31、Mated Figure 2 AECMA PREN*b097- O01 95 1012311 0009888 251 Page 8 prEN 6047-001 : 1995 6.3 Contact arrangements and polarizing The contact arrangements are specified by figure 3 which show the front face of the female insulators. see EN 6047-002. The following tolerances apply to the inserts fitted

32、in the housings : - Center of each hole : 1+100,50 I A I B 1 1-1D1,62 i A /B I - Center of each contact end : Identification of the contact position shall be permanently designed in contrasting color on the front face of the insert or interfacial seal and on the rear face of the rear separator. Mark

33、ing shall not be raised or recessed on the sealing surfaces. Polarizing of a receptacle and plug having the same size of shell is achieved by rotation of the insert relative to the main key or groove (see figure 4). The various angular positions which may be adopted are shown in table 1. Dimensions

34、and tolerances are in millimeters. Shell size, contact arrangements and polarizing I I I Contact size code 48-35 Figure 3 AECMA PRENwb047- 001 95 L0123Ll 0009889 198 H Code a in degree Page 9 prEN 6047-001 : 1995 Alternate insert positions N W X Y Z O - - - - 1 Center line of master key I or keyway

35、of shell Indexing radius of insert Housing (shell size) 48 -. I -I -I-. - Arrangement Number of Contact Symbol code contacts size 35 4 4/0 Engaging face of pin insert ; (socket insert opposite) Figure 4 Table 1 : Polarizing Table 2 : Contact arrangements AECMA PRENrb047- O01 75 I L01Z311 0007890 90T

36、 I Page 10 prEN 6047-001 : 1995 6.4 Dimensions of contacts Dimensions of contacts are given in the contact standard indicated by EN 6047-002. 6.5 Assembly instructions The assembly instructions of the connectors are indicated by EN 6047-002. 7 Tests 7.1 Special test 7.1.1 Holding force of plug coupl

37、ed with receptacle With a receptacle attached to a support, couple the plug without its contacts and coupling ring and apply a rotational torque on the plug of 10 N.m. Results :Visual examination 1 O1 of EN 2591. No damage to polarizing key. 7.2 Connector tests according to standard EN 2591 The test

38、s in clause 3 of EN 2591 applicable in the context of this specification - as well as the details necessary for implementing them and for inspecting connector characteristics - are given in table 3. AECMA PREN*b047- O01 95 m 1012311 0007871 846 m Title Page 11 prEN 6047-001 : 1995 Table 3 Jisual exa

39、mination Examination of dimensions and mass Zontact resistance . low level :ontact resistance at rated :urrent Electrical continuity at microvolt level Discontinuity of contacts in the microsecond ranae Details nitial examination : examination of connectors, ittings, loose parts (contacts, etc .) le

40、tails to be examined : Identification Appearance . Marking - Surface finish =inal examination : no loosening of parts, no crack, :race of carbon, excessive wear, detached parts shall be observed. kcording to clause 4. VOTE : In the case of a qualified inspection system the piece parts, unrelated to

41、the production batches of finished products may be used for the dimensional check. Not applicable. Measuring points on the cable, the two points 150 mm apart. Contact size size drop tests Not applicable. Duration of micro-discontinuity : 1 ps Method B. (continu AECMA PRENLb047- O01 95 II 1012311 000

42、9892 782 uleasurement of insulation ,esistanCe : at room temperature : at high temperature : aiter test 31 3 : aiter tests 31 5 and 31 6 : during tests 303 and 321 : Joltage proof test Page 12 prEN 6047-001 : 1995 Method A, connector unmated, unless otherwise specified below. Minimum insulation resi

43、stance : 5000MSZ 1 O00 M SZ 1 O00 M SZ (connectors mated) 1 O00 M SZ 1 O0 M SZ (connectors mated) Method A, connectors mated and unmated except after tests 31 1 and 31 3 where they must be mated. For tests at low pressure, voltage is applied after 30 minutes at the pressure indicated. Table 3 (conti

44、nued) remperature rise due to rated :urrent EN 2591- Maximum leakage current : 2 mA. NOTE : Where unmated connectors are used, the specifications in EN 31 97 should be followed. Room temperature : +120 OC. 205 206 207 208 Title Details iousing electrical continuity I Not applicable. Pressure Voltage

45、 value : Sea level 12,l kPa (15 O00 m) Connectors Vrms (continued AECMA PRENpb047- 001 75 m 1012311 0007873 619 W Contact size - 4/0 Page 13 prEN 6047-001 : 1995 Intensity Duration (A) (SI 325 300 435 5 Table 3 (continued) EN 2591- 209 21 o 21 3 21 6 301 302 303 304 305 Title Recommendation for dete

46、rmining CurrenVtemperature de-rating Electrical overload Shielding effectiveness 100 MHz to 1 GHz Contact insertion safety Temperature endurance Climatic sequence Cold/low pressure and dry heal Continuous dry heat test Rapid temperature variations Details Not applicable for qualification. Heating du

47、e to current flow shall not cause the maximum temperature to be exceeded. To confirm this, the user shall take account of this recommendation. To be performed during test 208. Not applicable. Not applicable. Temperature : (+200 f 3)“C. Duration : 1 O00 hours. Not applicable. Connectors mated. Five c

48、ycles. Minimal temperature : (-65 f 2 )“C. Not applicable. Connectors mated. TA = (-65 - g )Oc TB = +200 + 8 )OC (continued ) Page 14 prEN 6047-001 : 1995 Table 3 (continued) Title Details EN 2591- 306 Mould growth Method A. Duration : 28 days. Development O. No prior washing. No surface etching. 30

49、7 Salt spray The connectors are suspended in the test chamber with non-metallic cords, so that no accumulation of condensed saline solution can occur. The unmated connectors are exposed to the salt smav for 96 h. 308 Sand and dust Not applicable. 309 Dry heat Not applicable. 31 O Not applicable. Cold Low air pressure Air leakage Artificial rain 31 1 Appl icable. Not applicable. Appl icable. 31 2 31 3 31 4 Immersion at low air pressure Not applicable. Resistance to fluids Fluid type, number of cycles, temperature and duration of immersion and