AECMA PREN 3745-100-2007 Aerospace series Fibres and cables optical aircraft use Test methods Part 100 General Edition P 1《航空航空航天系列 　航空用光缆和光纤　试验方法.第100部分 总则》.pdf

《AECMA PREN 3745-100-2007 Aerospace series Fibres and cables optical aircraft use Test methods Part 100 General Edition P 1《航空航空航天系列 　航空用光缆和光纤　试验方法.第100部分 总则》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 3745-100-2007 Aerospace series Fibres and cables optical aircraft use Test methods Part 100 General Edition P 1《航空航空航天系列 　航空用光缆和光纤　试验方法.第100部分 总则》.pdf（7页珍藏版）》请在麦多课文档分享上搜索。

1、ASD STANDARD NORME ASD ASD NORM prEN 3745-100 Edition P 1 May 2007 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Avenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: 49.060 Descriptors: ENGLISH VERS

2、ION Aerospace series Fibres and cables, optical aircraft use Test methods Part 100: General Srie arospatiale Fibres et cbles optiques usage aronautique Mthodes dessais Partie 100 : Gnralits Luft- und Raumfahrt Faseroptische Leitungen fr Luftfahrzeuge Prfverfahren Teil 100: Allgemeines This “Aerospac

3、e Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain follo

4、wing 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 agreement of A

5、SD-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 a national stan

6、dard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 31 May 2007 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2007 by ASD-STAN Copyright European Association of Aerospace Industries

7、 Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3745-100:20072 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms and definitions .3 4 Test conditions 6 5 List of test methods.6 Foreword This standard w

8、as reviewed 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. Copyright European Association of Aerospace

9、 Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3745-100:20073 1 Scope This standard defines terms for optical fibres and cable. 2 Normative references The following referenced documents are indispensable fo

10、r 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. IEC 50(731), International Electrotechnical Vocabulary Chapter 731: Optical fibre communication. 3 Terms

11、 and definitions For the purposes of this document, the following terms and definitions apply. 3.1 optical fibre a dielectric waveguide whose core consists of optically transparent material of low attenuation and whose cladding consists of optical transparent material of lower refractive index than

12、that of the core (see Figure 1) NOTE In general the optical fibre is furnished with a primary coating (see Figure 1). 3.2 core the central region of an optical fibre through which most of the optical power is transmitted (see Figure 1) 3.3 cladding dielectric material surrounding the core of the opt

13、ical fibre (see Figure 1) 3.4 fibre coating the first protective coating directly applied to the fibre during its manufacture (see Figure 1) NOTE Its purpose is to maintain original optical performance of the fibre and to provide minimum mechanical properties. 3.5 optical cable an assembly consistin

14、g of optical fibre, inner sheath and where applicable strength members and jacket (see Figure 1) 3.6 multiple fibre cable a construction in which a number of fibres are placed together in a cable 3.7 buffer a material which surrounds and is immediately adjacent to a primary coating and provides mech

15、anical protection (see Figure 1) 3.8 strength members a protective envelope added to the inner sheath when necessary to improve the properties of mechanical resistance (see Figure 1) Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo repr

16、oduction or networking permitted without license from IHS-,-,-prEN 3745-100:20074 3.9 jacket a external protective covering (see Figure 1) 3.10 refractive index profile the distribution of the refractive index along the diameter of an optical fibre NOTE The refractive index profile for simple struct

17、ures can be approximated by: ararnrng= for)/(21)(1arnnrn = for21)(12with 2221212/)( nnn = where: r is the radial distance from the centre of fibre, n1is the maximum refractive index value of the core material, n2is the refractive index value of the cladding material, a is the core radius, g is the p

18、rofile parameter which defines the form of the profile: 10 g step index profile 1 g 3 graded index profile 3 g 10 quasi step index profile 3.11 core diameter the core diameter ( cr) is the diameter of the circle which best fits the core area. For a cross section of an optical fibre the core area is

19、that within which the refractive index everywhere (excluding any index dip) exceeds that of the innermost homogeneous cladding by a given fraction of the difference between the maximum of the refractive index of the core (n1) and the refractive index of the innermost homogeneous cladding (n2) NOTE I

20、t is contained within the focus of points where the refractive index n3is given by: n3= n2+ k (n1 n2) n1= maximum refractive index value of core n2= refractive index value of the innermost homogeneous cladding k = a constant (unless otherwise specified a k value of 0,05 is assumed). 3.12 cladding di

21、ameter the cladding diameter ( cd) is the physical diameter of the optical fibre 3.13 concentricity error core/cladding the distance between the centre point of the core and the centre point of the cladding divided by the core diameter 3.14 non circularity of core the difference between the longest

22、and the shortest chords passing through the core centre, divided by the core diameter Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3745-100:20075 3.15 non circul

23、arity of cladding the difference between the longest and the shortest chords passing through the cladding centre, divided by the cladding diameter 3.16 attenuation the attenuation A at the wavelength lambda between two cross sections 1 (input) and 2 (output) separated by the distance L of the fibre

24、is defined by: A = 10 log10(P1/P2) (dB) P1= optical power traversing the cross section 1 P2= optical power traversing the cross section 2 Attenuation coefficient: (alpha) = A/L (dB/unit length) NOTE For practical use, generally, these parameters are given under modal equilibrium conditions (this is

25、not normally the case in avionic applications where lengths are short). 3.17 numerical aperture the numerical aperture NA is the maximum theoretical numerical aperture defined by: NA = 2221nn where: n1= maximum of the refractive index value of the core n2= the refractive index value of the innermost

26、 homogeneous cladding 3.18 bandwidth the value numerically equal to the lowest frequency at which the magnitude of the baseband transfer function of an optical fibre decreases to a specified fraction, generally to one half (3 dB), of the zero frequency value Key 1 Cladding 2 Buffer (if present) 3 Ja

27、cket 4 Core 5 Fibre coating 6 Strength members (if present) Figure 1 Optical cable 1 2 3 6 5 4 Optical fibre Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3745-10

28、0:20076 4 Test conditions Unless stated otherwise in the test methods, the technical specification or the product standard the test conditions shall be: Temperature: (20 5) C Atmospheric pressure: 86 KPa to 106 KPa Relative humidity: 45 % to 75 % The temperature and humidity shall remain constant du

29、ring a series of measurement. 5 List of test methods Table 1 General designation EN 3745 part Test designation 201 202 203 204 205 Visual examination Fibre dimensions Cable dimensions Wall thickness Cable longitudinal dimensional stability Table 2 Optical tests EN 3745 part Test designation 301 302

30、303 304 305 306 Attenuation Numerical aperture Bandwidth Backs cattering Immunity to ambient light coupling Variation of attenuation during temperature cycling Table 3 Environmental tests EN 3745 part Test designation 401 402 403 404 405 406 407 408 409 410 411 412 Accelerated ageing Temperature cyc

31、ling Thermal shock Cold bend test Flammability Thermal life Resistance to fluids Humidity resistance Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3745-100:20077

32、Table 4 Mechanical tests EN 3745 part Test designation 501 502 503 504 505 506 507 508 509 510 511 512 513 Optical fibre proof test Tensile strength for short length of optical fibres Scrape abrasion Micro bending test Cable tensile strength Impact resistance Cut-through Torsion Kink test Bending te

33、st Cable to cable abrasion Flexure endurance Crush resistance Table 5 Sundry tests EN 3745 part Test designation 601 602 603 Smoke density Toxicity Nuclear radiation Table 6 Handling tests EN 3745 part Test designation 701 702 703 704 705 Strippability Durability of manufacturers marking Contrast measurement Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-