ASD-STAN PREN 2591-222-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 222 Insertion Loss (I L ) (Edition P 1)《航空航天系列 电气和光学连接部件的试验方法 第222部分 插入.pdf

上传人:twoload295 文档编号:451183 上传时间:2018-11-23 格式:PDF 页数:11 大小:84.21KB
下载 相关 举报
ASD-STAN PREN 2591-222-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 222 Insertion Loss (I L ) (Edition P 1)《航空航天系列 电气和光学连接部件的试验方法 第222部分 插入.pdf_第1页
第1页 / 共11页
ASD-STAN PREN 2591-222-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 222 Insertion Loss (I L ) (Edition P 1)《航空航天系列 电气和光学连接部件的试验方法 第222部分 插入.pdf_第2页
第2页 / 共11页
ASD-STAN PREN 2591-222-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 222 Insertion Loss (I L ) (Edition P 1)《航空航天系列 电气和光学连接部件的试验方法 第222部分 插入.pdf_第3页
第3页 / 共11页
ASD-STAN PREN 2591-222-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 222 Insertion Loss (I L ) (Edition P 1)《航空航天系列 电气和光学连接部件的试验方法 第222部分 插入.pdf_第4页
第4页 / 共11页
ASD-STAN PREN 2591-222-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 222 Insertion Loss (I L ) (Edition P 1)《航空航天系列 电气和光学连接部件的试验方法 第222部分 插入.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 2591-222 Edition P 1 February 2005PUBLISHED 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: Descriptors: ENGLISH VERSION Aerospace s

2、eries Elements of electrical and optical connection Test methods Part 222: Insertion Loss (I.L.) Srie arospatiale Organes de connexion lectrique et optique Mthodes dessais Partie 222 : Pertes dinsertion Luft- und Raumfahrt Elektrische und optische Verbindungselemente Prfverfahren Teil 222: Einfgungs

3、dmpfung This “Aerospace Series“ Prestandard has been 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 concerne

4、d 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, without re-identification of the standard. After examination and review by users and formal

5、agreement of AECMA-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 members have then to implement the EN at national level by giving the EN the status of

6、 a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 28 February 2005 Comments should be sent within six months after the date of publication to AECMA-STAN Electrical Domain Copyright 2005 by AECMA-STAN Page 2 prEN 2591-222:2005Fore

7、word This standard was reviewed by the Domain Technical Coordinator 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 S

8、cope 3 2 Normative references. 3 3 Preparation of specimens. 3 4 Apparatus 4 5 Procedure 4 6 Requirement . 5 7 Detail to be specified 5 Annex A (normative) Definition of S parameters 7 Page 3 prEN 2591-222:20051 Scope This standard specifies a measurement method of insertion loss, in the required fr

9、equency bandwith of coax contacts or connectors with characteristic impedance. It shall be used together with EN 2591-100. The measurement is carried out according to vectorial method using “S” parameters (see definition in Annex A). 2 Normative references The following referenced documents are indi

10、spensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2591-100, Aerospace series Elements of electrical and optical connection Test methods Par

11、t 100: General 1)3 Preparation of specimens The sampling shall include, for each specified cable, a minimum of two section of coaxial cable with connector in both ends. The first section called “Reference” is constituted as follow (see Figure 1): 60 cm 2,5 mm of coaxial cable 1 male coaxial connecto

12、r (SMA, N or TNC type ) 1 female coaxial connector (SMA, N or TNC type ) Key 1 Coaxial (Std) female connector 2 Coaxial (Std) male connector 3 Coaxial cable; Lg. = 60 cm 2,5 mm Figure 1 1) Published as AECMA Prestandard at the date of publication of this standard 1 23Page 4 prEN 2591-222:2005The coa

13、xial connectors shall be selected to offer optimum performances for each used cable and measured frequency range. They must have a reflection coefficient better than 0,1 ( 20 dB) in the test frequency rouge. It is necessary to use the same type of connector on each section of cable. The second secti

14、on called “Measure” (see Figure 2) is constituted by the same elements as “Reference Section”, the sample to be measured shall be installed in the middle of the section of the cable. Key 1 Coaxial (Std) female connector 2 Device under test 3 Coaxial (Std) male connector 4 Coaxial cable; Lg. = 2 30 c

15、m 2,5 mm Figure 2 4 Apparatus The apparatus shall comprise: Measure equipment include (see Figure 3): vector network analyser calibration kit standard precision adapters a 75 kit of transformation, to perform measurement from 50 network analyser, when it is necessary. 5 Procedure 5.1 Calibration Sel

16、ect measure frequency range and sampling points number. Carry out the complete calibration of network analyse, Part 1 and Part 2 (“S” Parameters, S11, S12, S21and S22) Using calibration kit according to instructions specified by network analyser manufacturer. 3 41 4 2Page 5 prEN 2591-222:20055.2 Mea

17、surement Connect reference section on network analyser, using if necessary, standard precision adapter. Perform the measurement, and run the curves tracer or record the values (S12, S21parameters). Move “reference section”, connect the “measure section” on the equipment, run the measurement and curv

18、e tracer, or record the values as above. 6 Requirement Sample insertion loss, which is measured, is the result of: (section insertion loss reference insertion loss). Insertion loss shall not exceed the values specified in the product standard. (The insertion loss of one contact or connector shall be

19、 the insertion loss of the contact or connector pair divided by two). 7 Detail to be specified The following items shall be specified: coaxial cables part number standard coaxial connectors part number network analyser, manufacturer, type and serial number frequency range sampling point number stand

20、ard precision adapter part number measurement impedance (50 or 75 ) for coaxial contact, connection length wiring instruction and tooling for thread coupling connectors, the coupling torque of the coupling ring Page 6 prEN 2591-222:2005Key 1 Vector network analyser 2 RF generator and “S” parameter t

21、est set Legend Precision hermaphroditic connectors Standard Precision Adapters Figure 3 Hermaphrodite Interface Standard Coaxial Connector Interface Device Under Test Interface 1 2 Page 7 prEN 2591-222:2005Annex A (normative) Definition of S parameters A.1 Effective Power of a Sinusoidal source Cons

22、ider an E.M.F. source, E, measured in Vrmswith an internal impedance Zgand a load impedance Z. The applied power P dissipated in Z is defined as () ()Z eZZE*Z*Z*EZZZEe*I V e Pggg+=+=22)()(P is a maximum when *ZZg= (balanced load). This maximum power is known as the effective or RMS nota Root Mean Sq

23、uared power for a given source (E, Zg) and can be expressed as Prms= )(2gdZeEP=4In general, when Z has a different value to Zg, we define P as +=221)(gggZZ*Z-ZZeEP4where ggZZ*ZZ+is known as the Power Reflection Coefficient. The power dissipated in Z can be expressed as the difference of two powers,

24、and when the source (E, Zg) power is maximum and when Z Zg, the amount of power reflected towards the source is equal to 2ggZZ*Z-Z+Page 8 prEN 2591-222:2005A.2 Waves Incident and Reflected (Kurokawa Waves) Let us define an impedance, Z, in terms of a potential difference, V, and a current I. We also

25、 define an Incident Wave, a, and a Reflected Wave, b, with respect to a Reference Resistance, Rg, as follows: the power dissipated in Z = P = |a|2 |b|2 the effective power generated by the source (E, Rg) = Prms= |a|2Expressing a and b in terms of V, I, Rg, gives: ggRI R Va2+= ggRI R Vb2= If Z is sup

26、plied by the source (E, Rg) we can state that E = V + Rg.I which automatically validates Prms = |a|2. NOTE - Rgis known as the Reference Resistance for the “waves“ a and b - The word wave is written inside speech marks because a and b do not show the typical electromagnetic behaviour associated with

27、 classical waves they are rather Power Waves - The definition of a and b is independent of that fact that the dipole Z is fed by a source of an internal resistance Rg- The power dissipated in Z is independent of the characteristics of the source and is always equal to |a|2|b|2- The ratio of the wave

28、s b to a is equal to (when V = Z.I) ggR ZR - Zab+= which is the Reflection Coefficient of the impedance Z with respect to the reference resistance Rg. Page 9 prEN 2591-222:2005A.3 S Parameters of a quad pole Let us apply the precedent definition to the input and output of a quad pole device. This ti

29、me we define an incident and reflected wave, a1and b1, for the input side and incident and reflected wave, a2and b2, for the output side, relative to the input and output reference resistances, R1and R2. 111112 R I RVa+= 222222 R I RVa+= 111112 R I RVb= 222222 R I RVb= We can state that the system i

30、s linear and we can therefore re-write the above equations to express on variable in function of two of the other unknowns. b1= S11 a1+ S12 a2b2= S21 a1+ S22 a2These S Parameters are also known as the system distribution parameters and characterise the quad pole in function of its input and output r

31、eference resistances, R1and R2. NOTE These S Parameters define the quad pole at a given frequency A.4 Physical Signification and Interest of S Parameters A.4.1 Physical significance of S11If S11= b1/a1, where a2= 0, then a2is equivalent to V2= R2.I2, the output of the quad pole is therefore closed l

32、oop on R2and if Zeis the input impedance of Q, then in these conditions, we can state that V1 = Ze.I1and S11is the input reflection coefficient with respect to R1when the output impedance = R2. 1111RZRZSee+=Page 10 prEN 2591-222:2005A.4.2 Physical significance of S22In the same way, if S22= b2/a2the

33、n when a1= 0, the input is closed loop on R1and under these conditions if Zois the output impedance, we obtain S22is the input reflection coefficient with respect to R2when the input impedance = R1. The Smmparameters are therefore defined as the Reflection Coefficients. A.4.3 Physical significance o

34、f S21If S21= b2/a1then when a2= 0, the output is closed loop on R2and therefore 111222211221IRVIRVRRabS+= If we assume that the quad pole Q is supplied by a source (E, R1) then E = V1+ R1.I1and V2= R2.I2The quad pole being supplied by a source of impedance R1and with a load R2will have a S Parameter

35、 S21proportional to a voltage gain called the System Transmission Coefficient. If we take the square of S21then we obtain )/12122221222221RMS PowerinRMS Power 44R (E, R RERVRREVS = where |S21|2is the Composite Power Gain. 2222RZRZSss+=EVRRS221212=Page 11 prEN 2591-222:2005A.4.4 Physical significance

36、 of S12We can do a similar calculation as above and we will find that, for a quad pole Q supplied by a source (E, R2) and whose input is closed loop on R1, the S12parameter is defined by EVRRS112212= S21is called the Inverse Transmission Coefficient. These S Parameters are used to characterise the j

37、unctions in high frequency applications because they possess a number of advantages: these parameters are measurable at R1and R2. In practice we choose standard values for resistances R1and R2such as 50 ohms or 75 ohms. It is much easier to measure variables over a known resistance than on an open c

38、ircuit (Z Parameters) or in a short circuit (Y Parameters). in closing each side of the circuit allows frequency sweeping. as the termination resistances R1and R2are dissipative, the risks of instability during the analysis of the active quad pole are decreased (which is not the case for open or short-circuits). a simple device already exists to separate a and b waves at high frequencies. This device is the directional coupler.

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