SAE AIR 6236A-2016 In-House Verification of EMI Test Equipment.pdf
《SAE AIR 6236A-2016 In-House Verification of EMI Test Equipment.pdf》由会员分享,可在线阅读,更多相关《SAE AIR 6236A-2016 In-House Verification of EMI Test Equipment.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref
2、rom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2016 SAE InternationalAll rights reserved. No part of this publi
3、cation may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AIR6236AAEROSPACEINFORMATION REPORTAIR6236 REV. AIssued 2015-12Revised 2016-08Superseding AIR
5、6236In-House Verification of EMI Test EquipmentRATIONALEThe only change to this revision is within the Rationale as follows: MIL-STD-461 no longer requires the routine calibration of many types of EMI test equipment. This AIR provides the EMI test facility with procedures that can be performed in-ho
6、use using their own EMI test equipment to check that the devices no longer requiring calibration nevertheless are performing properly to manufacturers specifications. These procedures can be performed to check that the transducer factors entered into EMI test software havent changed, or in the case
7、where a MIL-STD-461 measurement system integrity check indicates a problem, they serve as a quick check of the transducers integrity.INTRODUCTIONMIL-STD-461G does not require certain types of test equipment to be periodically calibrated in a traceable manner. This aerospace information report provid
8、es guidance on how to self-check such devices, using equipment commonly found in EMI test facilities. The purpose is not to calibrate these devices, but to check that they have not varied significantly from manufacturers specifications.1. SCOPEThis AIR provides guidance to the EMI test facility on h
9、ow to check performance of the following types of EMI test equipment:Current probeLine Impedance Stabilization Network (LISN)Directional couplerAttenuatorCable lossLow noise preamplifierRod antenna basePassive antennasAll performance checks can be performed without software. A computer may be requir
10、ed to generate an electronic or hard copy of data. This is not to say that custom software might not be helpful; just that the procedures documented herein specifically eschew the necessity of automated operation. SAE INTERNATIONAL AIR6236A Page 2 of 91.1 PurposeThe purpose of this AIR is not to rep
11、roduce the procedures used by an accredited calibration facility, but rather to provide simple and accurate methods available using only test equipment found in an EMI test facility. For simplicity, all set-ups are shown using a network analyzer, but a spectrum analyzer or EMI receiver with built-in
12、 tracking generator may be used in lieu of a network analyzer, and if that isnt available, a separate signal generator may replace the tracking generator. The effects of these substitutions are discussed in Section 4. Measurement methods offered herein are not exclusive, but found to work well with
13、a minimum of complexity.2. APPLICABLE DOCUMENTSThe following publications form a part of this document to the extent specified herein. The latest issue of SAE publicationsshall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In theeve
14、nt of conflict between the text of this document and references cited herein, the text of this document takes precedence.Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has beenobtained.2.1 U.S. Government PublicationsCopies of these document
15、s are available online at http:/quicksearch.dla.mil.MIL-STD-4613. PERFORMANCE CHECKS3.1 Current ProbeVarious models of current probes based on transformer action are used from frequencies as low as 1 Hz to at least 1 GHz. All these probes may be calibrated as per Figure 1.In Figure 1, the network an
16、alyzer source drives a current through the calibration fixture, which the current probe senses. The attenuator values (excepting the 10 dB pad on the input side of the calibration fixture) are so chosen that the ratio of the current probe output (T-port) to the reference (R) input is directly the tr
17、ansfer impedance in dB Ohms, with no data reduction required. They also perform impedance matching functions reducing vswr-related errors at higher frequencies. The 10 dB pad is solely for impedance matching and vswr-reducing, and need not be included if unnecessary, typically at audio frequencies w
18、here extra signal level into the calibration fixture is required. Its value does not affect the transfer impedance calculation.Figure 1 - Current probe calibration - T/R ratio is the transfer impedance in dB ohmsAt radio frequencies where there is plenty of dynamic range, the source setting should b
19、e set 10 dB below maximum in order to place 10 dB of impedance matching attenuation between the source and coaxial transmission line. Also at radio frequencies where loss in the coaxial cable becomes appreciable, the length and type of coaxial connection between current probe output and “T” port and
20、 between the 20 dB pads on the output of the calibration fixture and the “R” input must be the same. SAE INTERNATIONAL AIR6236A Page 3 of 94. LISNWhile there are several methods for measuring the LISN impedance specified in MIL-STD-461, none has the simplicity and ease of measuring the insertion los
21、s the LISN presents to a 50 Ohm signal source. Insertion loss is the potential measured at the LISN port relative to at a 50 Ohm load. Above 1 MHz, where the 50 uH LISN approximates 50 Ohms, the insertion loss is 0 dB. At lower frequencies, insertion loss increases with decreasing frequency. Figure
22、2 shows the measurement set-up, and Figure 3 shows expected results, including error bars representing the MIL-STD-461 20% tolerance on LISN impedance. This method and limit account for the 0.25 uF blocking capacitor loss. Note that the upper tolerance above 1 MHz is strictly academic; there is no w
23、ay the LISN impedance can be higher than 50 Ohms, so the insertion loss cannot exceed 0 dB. At frequencies where coaxial cable loss is significant, the type and length of the cables connecting to the “T”and “R” ports must be the same. The connection between splitter and LISN input power connector mu
24、st be short enough to have no significant loss. Insertion loss is measured as the T/R ratio.Figure 2 - LISN insertion loss measurement set-upFigure 3 - MIL-STD-461 50 uH (upper curve) and 5 uH LISN insertion loss (lower curve), including losses in the 0.25 uF blocking capacitor with 50 uH curveSAE I
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAIR6236A2016INHOUSEVERIFICATIONOFEMITESTEQUIPMENTPDF

链接地址:http://www.mydoc123.com/p-1020379.html