SAE ARP 1256D-2011 Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines《航空涡轮发动机连续采样气体排放测量程序》.pdf
《SAE ARP 1256D-2011 Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines《航空涡轮发动机连续采样气体排放测量程序》.pdf》由会员分享,可在线阅读,更多相关《SAE ARP 1256D-2011 Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines《航空涡轮发动机连续采样气体排放测量程序》.pdf(19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 there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 SAE International All rights reserved. No part of this publication m
3、ay 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: 724-776-4970 (outside USA)
4、 Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/ARP1256D AEROSPACE RECOMMENDED PRACTICE ARP1256 REV. D Issued 1971-10 Revised 2011-07 Supersedin
5、g ARP1256C Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines RATIONALE Define the set point temperature range of the hydrocarbon analyzer. 1. SCOPE This SAE Aerospace Recommended Practice (ARP) describes the continuous sampling and analysis of g
6、aseous emissions from aircraft gas turbine engines. The measured gas species include carbon monoxide (CO), carbon dioxide (CO2), nitric oxide (NO), nitrogen dioxide (NO2), hydrocarbons (HC) and water vapor (H2O). This ARP excludes engine operating procedures and test modes, and is not intended for i
7、n-flight testing, nor does it apply to engines operating in the afterburning mode. It is recognized that there will probably be major advances in the gas analysis measurement technology. It is not the intent of this ARP to exclude other analysis techniques, but to form the basis of the minimum amoun
8、t of conventional instruments (those in common industry usage over the last fifteen years) required for the analysis of aircraft engine exhaust. It is the responsibility of the analyst to demonstrate the alternative measurement technology has comparable (or better) performance than the techniques de
9、scribed in this ARP. The measurement of other exhaust gas species is beyond the scope of this ARP. It should be noted the measurement of oxygen (O2) is generally accepted as essential for assessing data quality, but is not covered by this ARP. Sulfur dioxide (SO2) is normally not measured using conv
10、entional systems but is calculated from fuel sulfur content. Again this is not covered by this ARP. 2. REFERENCES 2.1 APPLICABLE DOCUMENTS The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of
11、 other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document supersedes applicable laws and regulations unless a specifi
12、c exemption has been obtained. 2.1.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. ARP1533 Procedure for the Analysis and Evaluation of Gaseous Emissions from
13、 Aircraft Engines SAE ARP1256D Page 2 of 19 3. SECTIONS This document is divided into the following sections: 4. Definitions and Terminology 5. Equipment 6. Analyzer Routines 7. Calibration Gases 8. System Layout 9. Test Procedure 10. Sampling 11. Information and Data to be Recorded 12. Calculation
14、of Results and Measurement Uncertainty 4. DEFINITIONS AND TERMINOLOGY 4.1 ACCURACY The closeness of agreement between a measured value and a true value. 4.2 AIRCRAFT GAS TURBINE ENGINE Any gas turbine engine used for aircraft propulsion or power generation, including those commonly called turbojet,
15、turbofan, turboprop, or turbo-shaft type engines. 4.3 CALIBRATION GAS A certified and traceable gas mixture of specified and known concentration used for adjustment of the analyzer gain to establish the basis for interpretation of the values of quantities indicated by the measuring instrument and th
16、ose values realized by the calibration gas mixture(s). 4.4 CERTIFIED AND TRACEABLE Documentory evidence awarded to an instrument, process or gas mixture that defines the property of the result of a measurement or the value of a standard whereby it can be related to stated references, usually nationa
17、l or international standards, through an unbroken chain of comparisons all having stated uncertainties. 4.5 CHEMILUMINESCENT DETECTOR (CLD) An instrument specific to Nitric Oxide (NO) that operates by detecting the light emitted when NO is reacted with ozone (O3). The same instrument in a different
18、measurement mode, can be used to analyse Oxides of Nitrogen (NOx) by catalytically converting the NOx to NO. The difference between this NOx and the original NO measurement is assumed to be Nitrogen Dioxode (NO2). 4.6 CONCENTRATION The volume fraction of the component of interest in the gas mixture
19、expressed as volume percentage or as parts per million by volume (ppmv). SAE ARP1256D Page 3 of 194.7 CONTINUOUS SAMPLING The presentation of a flowing sample to a gas analyzer so as to obtain a continuous measurement of concentration of the components of interest. 4.8 FLAME IONIZATION DETECTOR (FID
20、) A hydrogen-air diffusion flame detector that produces a signal nominally proportional to the mass-flow rate of hydrocarbons entering the flame, and generally assumed responsive to the number of carbon ions dissociated from the hydrocarbons entering the flame. 4.9 FUEL/AIR RATIO The mass rate of fu
21、el flow to the engine divided by the mass rate of dry airflow through the engine. 4.10 GAS DIVIDER A certified and traceable device that mixes a calibration gas with a diluent gas in precise fractions to produce a range of gas concentrations with which to demonstrate analyzer linearity. Gas dividers
22、 are commercially available and include gas mixing pumps, capillary and sonic nozzle type devices. Gas dividers are generally more accurate than a range of calibration gases to demonstrate analyzer linearity, and help reduce calibration gas cylinder inventory. 4.11 GASEOUS EMISSIONS The gas phase co
23、mponents in the exhaust stream of an aircraft gas turbine engine that for the purposes of this ARP are restricted to the measured carbon monoxide, carbon dioxide, nitric oxide, nitrogen dioxide and hydrocarbon gases. 4.12 INTERFERENCE Analyzer response due to presence of components other than the ga
24、s (or vapor) that is to be measured. 4.13 LINEARITY The response from an instrument described by the best mathematical straight-line between an instrument zero and full scale, for a given analyzer range.4.14 NOISE Analyzer noise has a frequency of 0.5 Hz or greater, and can be regular or irregular v
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