AECMA PREN 3373-001-2006 Aerospace Series Terminal Lugs and In-Line Splices for Crimping on Electric Conductors Part 001 Technical Specification Edition P 3《航空航天系列终端接线片和卷曲电力电缆轴向接合..pdf

《AECMA PREN 3373-001-2006 Aerospace Series Terminal Lugs and In-Line Splices for Crimping on Electric Conductors Part 001 Technical Specification Edition P 3《航空航天系列终端接线片和卷曲电力电缆轴向接合..pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 3373-001-2006 Aerospace Series Terminal Lugs and In-Line Splices for Crimping on Electric Conductors Part 001 Technical Specification Edition P 3《航空航天系列终端接线片和卷曲电力电缆轴向接合..pdf（23页珍藏版）》请在麦多课文档分享上搜索。

1、ASD STANDARD NORME ASD ASD NORM prEN 3373-001 Edition P 3 May 2006 PUBLISHED BY AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8110 - Fax. + 32 2 775 8111 - www.asd-stan.orgICS: 49.060 Supersedes edition P 2 November 1999 De

2、scriptors: ENGLISH VERSION Aerospace series Terminal lugs and in-line splices for crimping on electric conductors Part 001: Technical specification Srie arospatiale Cosses et prolongateurs pour sertissage sur conducteurs lectriques Partie 001 : Spcification technique Luft- und Raumfahrt Kabelschuhe

3、und Stoverbinder zum Crimpen von elektrischen Leitern Teil 001: Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (Aerospace and Defence Industries Association of Europe - Standardization). It is published for the needs of the Eur

4、opean Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, wit

5、hout re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national

6、 members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 31 May 2006 Comments should be sent within six months after the date of publication to ASD-S

7、TAN Electrical Domain Copyright 2006 by ASD-STAN Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:20062 Foreword This standard was review

8、ed by the Domain Technical Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. Contents Page 1 Scope . 3 2 Normative references 3 3

9、 Terms and definitions . 3 4 General. 3 4.1 Physical characteristics . 3 4.2 Functional characteristics . 4 4.2.1 Recommended cables 4 4.2.2 Crimping tools. 4 5 Tests 4 5.1 General. 4 5.2 Special tests. 4 5.2.1 Crimping at low temperature 4 5.2.2 Sleeve strength. 5 5.2.3 Sealing 5 5.2.4 Flammability

10、. 5 5.3 Qualification tests for crimped connections on copper cable. 5 5.4 Qualification tests for crimped connections on aluminium cable . 12 6 Quality assurance 14 6.1 General. 14 6.2 Initial qualification conditions. 14 6.2.1 General. 14 6.2.2 Sampling and definition of samples. 14 6.2.3 Preparat

11、ion of specimens 15 6.2.4 Programme of qualification tests. 22 6.3 Acceptance and inspection conditions 23 6.4 Quality control. 23 6.5 Maintaining qualification . 23 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo re

12、production or networking permitted without license from IHS-,-,-prEN 3373-001:20063 1 Scope This standard specifies the general characteristics, the conditions of qualification, acceptance and quality assurance, as well as the test programs and groups for terminal lugs and in-Iine splices designed f

13、or crimping on copper and copper alloy conductors and on aluminium and aluminium alloy conductors. 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 lates

14、t edition of the referenced document (including any amendments) applies. IEC publication 50, International Electrotechnical Vocabulary Chapter 581: Electromechanical components for electronic equipment. EN 2083, Aerospace series Copper or copper alloy conductors for electrical cables Product standar

15、d. EN 2242, Aerospace series Control of tools used for crimping of electrical cables with conductors defined by EN 2083 and EN 2346. 1)EN 2591*, Aerospace series Elements of electrical and optical connection Test methods General. EN 3719, Aerospace series Aluminium or aluminium alloy conductors for

16、electrical cables Product standard. 1)EN 9133, Aerospace series Quality management systems Qualification Procedure for aerospace standard parts. 3 Terms and definitions For the purposes of this document, the following terms and definitions apply. IEC publication 50, International Electrotechnical Vo

17、cabulary Chapter 581: Electromechanical components for electronic equipment. 4 General 4.1 Physical characteristics The forms and dimensions, masses, materials and operating temperature ranges are defined in the product standards. * All its parts quoted in this standard. 1) Published as ASD Prestand

18、ard at the date of publication of this standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:20064 4.2 Functional characteristics 4.

19、2.1 Recommended cables The terminal lugs and in-line splices shall allow the correct connection (in accordance with EN 2242) of copper cables conforming to EN 2083 and of aluminium cables conforming to EN 3719. 4.2.2 Crimping tools The tools which are referred to in the product standards regarding t

20、erminal lugs and in-line splices shall be designed so that: they ensure the correct positioning of the crimping area; they have a full closure mechanism which ensures that the crimping cycle is fully completed; the crimping operation does not damage the terminal lug or the in-line splice and does no

21、t cause any significant burring; a reference mark identifying the gauge is made in the crimping area, if possible. 5 Tests 5.1 General Unless otherwise specified, the tests shall be selected from those in EN 2591. These tests are listed in Tables 1 and 3. The tests shall be carried out on each combi

22、nation of gauge, material and plating of the crimp barrel crimped on the appropriate section of each type of cable (material and plating), for each type of crimping tool. When a crimping barrel is designed to accommodate a range of cables for a s specific type of tool or for a type or size of die or

23、 stop, the tests shall be carried out on only the smallest and largest permitted cable sections. To rationalise the test procedures and avoid confusion between the tests for copper and aluminium cables, the tests have been grouped together, and are defined as Group Cu 0, Cu 1, Cu 2, etc. for copper

24、cables and Group Al 0, AI 1, AI 2, etc. for aluminium cables. For the purposes of these groups, copper and copper alloy cables are included within test Groups Cu 0, Cu 1, Cu 2, etc. Likewise aluminium and aluminium alloy cables are included within the test Groups AI 0, AI 1, AI 2, etc. 5.2 Special t

25、ests 5.2.1 Crimping at low temperature Keep the components (cable, terminal lugs or in-line splices and crimping tools) at a temperature of ( 15 2) C for 1 h, then crimp at that temperature. Keep the specimens at a temperature of ( 65 2) C for 1 h. Recover at (20 5) C for 1 h. Copyright Association

26、Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:20065 5.2.2 Sleeve strength The insulating sleeve shall have a good grip on the terminal lug barrel before and

27、 after crimping and, when held by a fork passed around the crimping barrel, the displacement shall not be more than 1 mm under an axial load of 35 N. 5.2.3 Sealing The cable shall be placed in a tube connected to a compressed air supply; the pressure shall be increased in 105Pa stages every 5 min up

28、 to 2 105Pa and maintained at this value for 1 h (see Figure 1). The specimen shall be immersed with the end of the barrel approximately 50 mm below the water level. There shall not be any leakage in the crimping area. Key 1 60 mm to 100 mm 2 Terminal lug 3 Cable 4 Collar clamp 5 Compressed air supp

29、ly pipe Figure 1 Assembly for the sealing test 5.2.4 Flammability The specimen shall be suspended in a still air chamber above a Bunsen burner with a 100 mm long tube and an internal diameter of (9,5 0,5) mm. The end of the 25 mm blue flame produced by the Bunsen burner shall be applied for 20 s to

30、half the length of the insulation of the specimen. There shall be no flame or incandescence 15 s after the flame is withdrawn. 5.3 Qualification tests for crimped connections on copper cable See Table 1. NOTE Where a requirement for an individual test is not quoted, see Table 7 for sequence of furth

31、er tests. 3145 2 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:20066 Table 1 Designation of the test Details EN 2591-101 Visual examin

32、ation With the naked or normally corrected eye on crimped specimens. An optical magnification of 6 to 10 may be used if required. Check that: the combined section of cable/barrel size or in-line splice/crimping tool conforms; the form and position of crimping are correct; there are no major cracks o

33、r burrs on the barrel; the cable core is correctly inserted in the barrel; the cable core and insulation are not damaged; the identification marks stamped on the crimp by the die are correct (if applicable). EN 2591-102 Examination of dimensions and mass Before crimping, dimensions and masses shall

34、conform to the requirements of the product standard. EN 2591-206 Measurement of insulation resistance The insulation resistance measured between the outer surface of the insulating sleeve and the cable core shall be a minimum of 1 000 M. EN 2591-217 Voltage drop under specified current for terminal

35、lugs and in-line splices See Figures 2 and 3. EN 2591-218 Ageing of terminal lugs and in-line splices by temperature and current cycling Test current as per Table 2. Requirement: see EN 2591-218. EN 2591-219 Voltage strength for insulated terminal lugs and in-line splices Test applicable to terminal

36、 lugs and in-line splices with insulated barrels. Requirement see EN 2591-219. EN 2591-301 Endurance at temperature Method B. 120 h in a dry heat chamber at a temperature 15 C above the operating temperature of the terminal lug or in-line splice. Test applicable terminal lugs and in-line splices wit

37、h insulated barrels. EN 2591-305 Rapid change of temperature TA= operating temperature of the terminal lug or in-line splice plus 15 C TB= 65 C EN 2591-307 Salt mist 48 h unless otherwise specified in the product standard. Check that no flaking of the protective treatment has occurred. continued Cop

38、yright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:2006 7 Table 1 (concluded) Designation of the test Details EN 2591-314 Immersion at low air

39、 pressure The in-line splice, fitted with its sealing accessories, shall be immersed in the solution. The ends of the cables shall protrude from the solution with neither the sealing accessories and the crimps being subjected to any stress. Pressure of chamber 4 kPa. EN 2591-315 Fluid resistance Tes

40、t applicable to terminal lugs and in-line splices with insulated barrels. EN 2591-403 Sinusoidal and random vibration Method A. Assembly as per Figure 4. No sign of fracture. Applicable to terminal lugs only. EN 2591-417 Tensile strength (crimped connection) See Figure 5. The specimen shall not brea

41、k at a value less than those specified in Table 2. EN 3373-001 Crimping at low temperature See 5.2.1. EN 3373-001 Sleeve strength See 5.2.2. EN 3373-001 Flammability See 5.2.4. Test applicable to terminal lugs and in-line splices with insulated barrels. Copyright Association Europeene des Constructe

42、urs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:20068 Key 1 Reference cable 2 Measurement point 3 Supply terminal Figure 2 Assembly for measuring the voltage drop in terminal lugs in

43、 accordance with EN 2591-217 L1500 min. L12UrUs213 500 min.3Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:20069 Key 1 Reference cable

44、2 Measurement point 3 Supply terminal Figure 3 Assembly for measuring the voltage drop in in-line splices in accordance with EN 2591-217 3 500 min.1L1Ur2 L1Us500 min. 2 3Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleN

45、o reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:200610 Key 1 Fixed point 2 Movement point 3 Attachment by nut and spring washer R = 5 external diameter of cable Figure 4 Assembly for the vibration test R 20 20 X YZR 1321Copyright Association Europeene des Constructe

46、urs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:2006 11 Key 1 Upper jaws of tensile testing machine 2 Cable 3 In-line splice 4 Terminal lug 5 Lower jaws of tensile testing machine Fi

47、gure 5 Principle of tensile testing machine 1 2 324 5 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:200612 Table 2 Tensile strength an

48、d voltage drop (copper conductor) Current cycling Measurementcurrent Maximum voltage drop for one crimp b Nominal section of the cables Minimum tensile strength cEN 2083 code mm2AWG a A A Initial mV After testing mV N 001 0,15 26 3,7 3 3 5 39 002 0,25 24 5,6 4,5 2 4 55 004 0,40 22 11,3 9 1 3 60 006 0,60 20 13,8 11 1 3 90 010 1 18 18 16 1 3 150 012 1,20 16 27,5 22 1 3 180 020 2 14 40 32 1 3 300 030 3 12 51,3 41 1 3 450 050 5 10 68,8 55 1 3 700 090 9 8 92,3 73 1 3 1 080140 14 6 126,3