SAE AIR 4979A-2012
基于北大西洋公约组织(NATO)航天研发顾问团(AGARD)一致性引擎检测规程的引擎检测中不确定性测量的评估

Estimation of Measurement Uncertainty in Engine Tests Based on Nato Agard Uniform Engine Test Program


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标准号
SAE AIR 4979A-2012
发布日期
2012年05月29日
实施日期
废止日期
中国标准分类号
V30
国际标准分类号
49.050
发布单位
US-SAE
引用标准
ANSI/ASME MFC-2M-1983 ISO 90-1977 SAE AIR 1678-1985 831439 942140 SP-674
被代替标准
SAE AIR 4979-1996
适用范围
This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. The primary objective of this document is to describe the systematic and random measurement uncertainties which may be expected when testing gas turbine engines in a range of different test facilities. The documentation covers a "traditional" method for estimating pretest uncertainties and a "new" method for computing and comparing posttest uncertainties. To determine these posttest uncertainties, data generated during the AGARD Uniform Engine Test Program (UETP) were analyzed and compared to the pretest estimates. The proposed procedure provides a mechanism for determining the expected accuracy of test results obtained from facilities which were not previously cross calibrated. Furthermore, the method can be used to assist in making cost-effective management decisions on the level of validation/cross calibration necessary when bringing a test facility on line. This document is also intended to act as a guide for improving uncertainty analyses in a broad spectrum of related industries. Measurement uncertainty and measurement system approaches and practices for the UETP are presented in a systematic format. Readers can use these uncertainty approaches and practices for comparison to their own measurement systems. The approach chose was to analyze three of the UETP test conditions at eight test facilities along with the individual measurement system approaches and practices. The test program provided a wide range of performance measurements and corresponding pretest uncertainty estimates encompassing a variety of test and measurement approaches and practices. Included in the analysis are the basic gas turbine performance measurements of temperature, pressure, airflow, fuel flow, area, speed, thrust, and typical performance parameter functions and associated uncertainty estimates.




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