ASD-STAN PREN 3662-006-2005 Aerospace Series Circuit Breakers Three-Pole Temperature Compensated Rated Current 20 A to 50 A Part 006 With Polarized Signal Contact Bus-Bar Version P.pdf

上传人:registerpick115 文档编号:452348 上传时间:2018-11-23 格式:PDF 页数:11 大小:106.85KB
下载 相关 举报
ASD-STAN PREN 3662-006-2005 Aerospace Series Circuit Breakers Three-Pole Temperature Compensated Rated Current 20 A to 50 A Part 006 With Polarized Signal Contact Bus-Bar Version P.pdf_第1页
第1页 / 共11页
ASD-STAN PREN 3662-006-2005 Aerospace Series Circuit Breakers Three-Pole Temperature Compensated Rated Current 20 A to 50 A Part 006 With Polarized Signal Contact Bus-Bar Version P.pdf_第2页
第2页 / 共11页
ASD-STAN PREN 3662-006-2005 Aerospace Series Circuit Breakers Three-Pole Temperature Compensated Rated Current 20 A to 50 A Part 006 With Polarized Signal Contact Bus-Bar Version P.pdf_第3页
第3页 / 共11页
ASD-STAN PREN 3662-006-2005 Aerospace Series Circuit Breakers Three-Pole Temperature Compensated Rated Current 20 A to 50 A Part 006 With Polarized Signal Contact Bus-Bar Version P.pdf_第4页
第4页 / 共11页
ASD-STAN PREN 3662-006-2005 Aerospace Series Circuit Breakers Three-Pole Temperature Compensated Rated Current 20 A to 50 A Part 006 With Polarized Signal Contact Bus-Bar Version P.pdf_第5页
第5页 / 共11页
亲,该文档总共11页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、AECMA STANDARD NORME AECMA AECMA NORM prEN 3662-006 Edition P 3 May 2005 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8110 - Fax. + 32 2 775 8111 - www.aecma-stan.orgICS: 49.060 Supersedes edition P 2 January 1999 D

2、escriptors: ENGLISH VERSION Aerospace series Circuit breakers, three-pole, temperature compensated, rated current 20 A to 50 A Part 006: With polarized signal contact Bus-bar version Product standard Srie arospatiale Disjoncteurs tripolaires compenss en temprature, intensits nominales 20 A 50 A Part

3、ie 006 : Avec contact de signalisation polaris Version barre-bus Norme de produit Luft- und Raumfahrt Schutzschalter, dreipolig, Temperaturkompensiert, Nennstrme von 20 A bis 50 A Teil 006: Mit polarisiertem Signalkontakt Sammelschienenversion Produktnorm This “Aerospace Series“ Prestandard has been

4、 drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. 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 review by users and formal agreement of AECMA-STAN, it will be submitted as a d

6、raft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national 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

7、 standards conflicting with the EN. Edition approved for publication 31 May 2005 Comments should be sent within six months after the date of publication to AECMA-STAN Electrical Domain Copyright 2005 by AECMA-STAN prEN 3662-006:20052 Foreword This standard was reviewed by the Domain Technical Coordi

8、nator of AECMA-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of AECMA-STAN defined in AECMA-STANs General Process Manual, this standard has received approval for Publication. Contents Page 1 Scope . 3 2 Normative references 3 3 Dimensions and mass 3 4 Ch

9、aracteristics 5 5 Designation. 10 6 Rated current code. 10 7 Delivery codes. 11 8 Marking 11 9 Technical specification 11 prEN 3662-006:20053 1 Scope This standard specifies the characteristics of three-pole circuit breakers, temperature compensated with a rated current from 20 A to 50 A, used in ai

10、rcraft on-board circuits at a temperature between 55 C and 90 C and at an altitude of 15 000 m max. These circuit breakers are operated by a push-pull type single push button (actuator), with delayed action “trip-free“ tripping with a polarized signal contact which is open when main contacts are clo

11、sed, and inversely. They are connected on supply side by means of bus-bar. They will continue to function up to the short-circuit current. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited ap

12、plies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 3155-016, Aerospace series Electrical contacts used in elements of connection Part 016: Contacts, electrical, male, type A, crimp, class S Product standard.1)EN 3662-001, Aerospace ser

13、ies Circuit breakers, three-pole, temperature compensated, rated current 20 A to 50 A Part 001: Technical specification.1)EN 3841-305, Aerospace series Circuit breakers Test methods Part 305: Short-circuit performance. EN 6113, Aerospace series Circuit breaker, connecting and attachment hardware.1)T

14、R 6083, Aerospace series Cut-outs for installation of electrical components.2)MIL-I-81969/1A, Installing and removal tools, connector electrical contact, type III, class 2, composition C.3)MIL-I-81969/14C, Installing and removal tools, connector electrical contact, type III, class 2, composition B.3

15、)MIL-S-19500, Semiconductor device, diode, silicon, fast recovery.3)FED-STD-595B, Colours used in Government Procurement. 3 Dimensions and mass 3.1 Dimensional characteristics The circuit breakers do not have to correspond to the pictorial illustration, only the dimensions given shall be adhered to.

16、 Dimensions are in millimetres. See Figure 1. 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published as AECMA Technical Report at the date of publication of this standard. 3) Published by: Department of Defense (DOD), the Pentagon, Washington D.C. 20301 USA. prEN

17、3662-006:20054 Key 1 Push button released 9 1 to 3 max. 2 Green colour according to FED-STD-595B No. 34090 10 3 White Gauge 20 connection pins according to EN 3155-016M2018 4 Marking area, see Clause 8. 11 Indicative value 25 (see note) 5 Connecting screw and washer 12 6 Push button pressed Position

18、ing lug in accordance with the panelcut-out, as per TR6083C202 7 Lockwasher 13 Rated current marking (white on green) 8 Attachment nut 14 3 holes 5,5 010,+NOTE Tools noted in Subclause 4.2.4 shall be applied without interfering with the terminal 2 connection. Even if the circuit breakers are grouped

19、. Figure 1 Configuration Dimensions Tolerances 110,5 A135C2 C1A153C2 B2 A2A1 B1 C1531,50-0,223M12 x 0,753 min.2 0,3A43max.7 min.10,5 0,5815,1 min.F225 B119,5 max.0,5A120,5A0,7F1 and F2 : see EN 3662-001, table 354 max.9,5 0,134 max.42 max.15,1 min.15,1 min.17,5 0,217,5 0,214r 2,5max.17,5 0,8 17,5 0,

20、810 min.10 min. 9,2 0,3926,5 0,3180-123 148 128 max.6,6 0,640,2 max.48,254+1025 max.4534021A20,5A0,5A19,5 0,2B271106Side view of terminals 1F1Bus-bar side 10,2 0,3F1 and F2: see EN 3662-001, Table 3. prEN 3662-006:20055 3.2 Electrical diagram See Figure 2. Terminal No.: 1 and 2: Main contacts 3 and

21、5: Signal contacts Figure 2 Electrical diagram 3.3 Mass 185 g max. (delivery code A including hardware). 3.4 Panel mounting See EN 3662-001. 4 Characteristics 4.1 Material, surface treatment See EN 3662-001. 4.2 Mechanical characteristics 4.2.1 Fasteners See EN 6113. 4.2.2 Recommended tightening tor

22、que of attaching nut for installation (5,25 0,25) Nm 4.2.3 Recommended tightening torque of connection hardware for installation (2,35 0,15) Nm A2 A1B2 B1C2 C13 5Push-button releasedA2 A1B2 B1C2 C13 5Push-button pressed3 5or3 5orprEN 3662-006:20056 4.2.4 Recommended tools for contacts of auxiliary c

23、ontact insertion and extraction plastic MIL-I-81969/14-11; metallic MIL-I-81969/1-02. 4.2.5 Resistance to vibrations 4.2.5.1 Combined test: ambient temperature at 70 C and vibrations Sinusoidal: 10 gn, see EN 3662-001. Random: 5,8 gn, see EN 3662-001. Low frequencies: 10 gn, see EN 3662-001. 4.2.5.2

24、 Combined test: ambient temperature at 85 C, altitude and vibrations Sinusoidal: 3 gn, see EN 3662-001. 4.2.6 Resistance to shocks 50 gn, see EN 3662-001. 4.2.7 Mechanical endurance See Table 6. 4.3 Environment characteristics 4.3.1 Humidity See EN 3662-001. 4.3.2 Corrosion See EN 3662-001. 4.3.3 Co

25、ntaminating liquids See EN 3662-001. 4.3.4 Overvoltage caused by lightning See EN 3662-001. 4.4 Electrical characteristics 4.4.1 Nominal voltages of main contacts See Table 1. Table 1 Nominal voltage 115/200 V a.c., 360 Hz to 800 Hz prEN 3662-006:20057 4.4.2 Diode of signal contact characteristic Ma

26、ximum current at 125 C: 0,5 A. Peak repetitive reversal voltage: 800 V min. Quality standard: JANTX according to MIL-S-19500. 4.4.3 Voltage drop at nSee Table 2. Table 2 Ratings A 20 25 30 35 40 45 50 U max. at n V 0,15 0,15 0,15 0,15 0,12 0,12 0,12 Signal circuit: 28 V d.c.; I = 3 mA : U 1,0 V. NOT

27、E When a signal contact has been operated with a power greater than 60 mW and/or with a voltage higher than 28 V d.c., it loses its low current quality. 4.4.4 Minimum and maximum tripping thresholds See Table 3. Table 3 Overload (in % of n) Minimum thresholds value 1 h Maximum thresholds value 1 h A

28、mbient temperatures C Ratings On ground At 15 000 m On ground 23 5 110 105 145 55 5 110 105 165 70 5 105 100 145 90 5 All 100 90 145 NOTE 1 For detection of minimum threshold, all the poles are connected in series. NOTE 2 For detection of maximum threshold, load value is: increased by about 20 % whe

29、n one pole is submitted to the load and other poles are not loaded; increased by about 10 % when two poles are submitted to the load and the other one is not loaded; not increased when the two other poles are loaded at 0,9 n. prEN 3662-006:20058 4.4.5 Overload trip See Table 4. Table 4 Overload (in

30、% of n) 200 500 1 000 3 poles 1 pole 3 poles 1 pole 3 poles 1 pole Ambient temperatures C Ratings A Trip time s 23 5 2 to 20 2 to 22 55 5 60 110 90 5 All 1,5 1,5 0,15 to 4,00 0,15 to 5,20 0,05 to 1,00 0,06 to 1,30 NOTE 1 When 3 poles are loaded, they will be connected in series. NOTE 2 When 1 pole i

31、s loaded, the two other poles are not loaded. 4.4.6 Short-circuit values See Table 5. Table 5 Nominal voltage 115/200 V a.c., 360 Hz to 800 Hz 0,8 cos 1 Prospective currents 2 000 A r.m.s. Test altitudes On the ground and at maximum altitude (15 000 m, 12 100 Pa) Number of operations 1 CO a+ 2 OCO b

32、aBreak operation (for definition see EN 3841-305). bMake operation (for definition see EN 3841-305). prEN 3662-006:20059 4.4.7 No-load and load endurance See Table 6. Table 6 Number of operations to be provided No-load Load 5 000 2 500 Main contacts Applicable Inductive 0,6 cos 0,7 n, 115/200 V a.c.

33、 - 360 Hz to 800 Hz All ratings Signal contacts Applicable Resistive 3 mA, 28 V d.c. Resistive 3 mA, 5 V d.c. Lamp 0,2 A, 28 V d.c. Resistive 0,5 A, 28 V d.c. NOTE 1 One operation corresponds to one closing + one opening. NOTE 2 Tolerances 5 % on current, voltage and frequency values. 4.4.8 Dielectr

34、ic rigidity See Table 7. Table 7 Closed position Z = 0 m Z = 15 000 m A1, B1, C1 with attachment A1, B1, C1 with 3 A1, B1, C1 with 5 A1, A2 with B1, B2 and C1, C2 B1, B2 with A1, A2 and C1, C2 1 500 V 400 V 3 with 5 3 and 5 with attachment 500 V 150 V Open position Z = 0 m Z = 15 000 m A1, B1, C1 wi

35、th A2, B2, C2 A1, B1, C1, A2, B2, C2 with attachment 3 and 5 with A1, B1, C1 3 and 5 with A2, B2, C2 A1, A2 with B1, B2 and C1, C2 B1, B2 with A1, A2 and C1, C2 1 500 V 400 V 3 and 5 with attachment 500 V 150 V prEN 3662-006:200510 4.4.9 Insulation resistance According to EN 3662-001, Table 5. 4.4.1

36、0 Overload endurance Not applicable 5 Designation EXAMPLE Description block CIRCUIT BREAKER Identity block EN3662-006A20AA Number of EN standard Design code, A: green button Rated current code (see Table 8) Delivery code A (see Table 9) NOTE If necessary, the code I9005 shall be placed between the d

37、escription block and the identity block. 6 Rated current code See Table 8. Table 8 Rating current n (A) 20 25 30 35 40 45 50 Marking on actuator 20 25 30 35 40 45 50 Rated current code 20A 25A 30A 35A 40A 45A 50A prEN 3662-006:200511 7 Delivery codes See Table 9. Table 9 Connection and attachment ha

38、rdware kits EN 6113 Delivery conditions Delivery code Kit part-No. aIncluded parts Pieces per part Fitted Supplied separately Connecting screw 6 Connecting lock washer 6 Attachment nut 1 A EN 6113C Attachment lock washer 1 X Attachment nut 1 B EN 6113B Attachment lock washer 1 X aSpare parts could b

39、e ordered separately, informations see EN 6113. 8 Marking As defined on the drawing and unless otherwise specified by contract, marking shall include: the designation defined in Clause 5 on the packaging; the manufacture date (year, week); the manufacturers name or trademark; the electrical diagram

40、and the terminal identification; the manufacturers part number (corresponding to the part number which includes connection and attachment hardware supplied separately in a bag). NOTE The marking could be on both opposite sides. For electrical diagram printed on the circuit breaker and/or terminal identification numbers see Figure 1. 9 Technical specification See EN 3662-001.

展开阅读全文
相关资源
  • ASD-STAN PREN 4022-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead Welded (Edition P1)《航空航天系列 钛合金制830管接头 90焊接穿壁弯头 第P1版[替代 ASD-STAN.pdfASD-STAN PREN 4022-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead Welded (Edition P1)《航空航天系列 钛合金制830管接头 90焊接穿壁弯头 第P1版[替代 ASD-STAN.pdf
  • ASD-STAN PREN 4021-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead (Edition P1)《航空航天系列 钛合金制830管接头 90穿壁弯头 第P1版[替代 ASD-STAN PREN 325.pdfASD-STAN PREN 4021-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead (Edition P1)《航空航天系列 钛合金制830管接头 90穿壁弯头 第P1版[替代 ASD-STAN PREN 325.pdf
  • ASD-STAN PREN 4018-2007 Aerospace series Pipe coupling 8 degree 30 in titanium alloy Elbows 90 degree with thrust wire nut (Edition P2)《航空航天系列 钛合金制830管接头 旋转螺母、带止推金属丝帽的90弯头 第P2版.pdfASD-STAN PREN 4018-2007 Aerospace series Pipe coupling 8 degree 30 in titanium alloy Elbows 90 degree with thrust wire nut (Edition P2)《航空航天系列 钛合金制830管接头 旋转螺母、带止推金属丝帽的90弯头 第P2版.pdf
  • ASD-STAN PREN 3256-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 45 Degree Swivel Nut Welded (Edition P 2 )《航空航天系列 钛合金制830管接头 旋转螺母、焊接式45弯头 第P2版[替代为 AS.pdfASD-STAN PREN 3256-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 45 Degree Swivel Nut Welded (Edition P 2 )《航空航天系列 钛合金制830管接头 旋转螺母、焊接式45弯头 第P2版[替代为 AS.pdf
  • ASD-STAN PREN 3254-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead Welded (Edition P 2)《航空航天系列 钛合金制830管接头 焊接式穿壁90弯头 第P2版[替代为 ASD-STAN.pdfASD-STAN PREN 3254-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead Welded (Edition P 2)《航空航天系列 钛合金制830管接头 焊接式穿壁90弯头 第P2版[替代为 ASD-STAN.pdf
  • ASD-STAN PREN 3253-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead (Edition P 2 )《航空航天系列 钛合金制830管接头 穿壁90弯头 第P2版[替代为 ASD-STAN PREN 402.pdfASD-STAN PREN 3253-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead (Edition P 2 )《航空航天系列 钛合金制830管接头 穿壁90弯头 第P2版[替代为 ASD-STAN PREN 402.pdf
  • ASD-STAN TR AMS2750-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdfASD-STAN TR AMS2750-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdf
  • ASD-STAN TR AMS2750 FRENCH-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdfASD-STAN TR AMS2750 FRENCH-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdf
  • ASD-STAN TR 9536-2008 Aerospace series Declarable Substances Recommended Practice《航空航天系列 需申报物质 建议做法》.pdfASD-STAN TR 9536-2008 Aerospace series Declarable Substances Recommended Practice《航空航天系列 需申报物质 建议做法》.pdf
  • ASD-STAN TR 9535-2008 Aerospace series Substance declaration (Edition 1)《航空航天系列 物质声明 第1版》.pdfASD-STAN TR 9535-2008 Aerospace series Substance declaration (Edition 1)《航空航天系列 物质声明 第1版》.pdf
  • 猜你喜欢
    相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ASD

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1