AIRCRAFT ENGINE GAS PATH DIAGNOSTIC METHODS: PUBLIC BENCHMARKING RESULTS

被引:0
|
作者
Simon, Donald L. [1 ]
Borguet, Sebastien [2 ]
Leonard, Olivier [2 ]
Zhang, Xiaodong [3 ]
机构
[1] NASA Glenn Res Ctr, Cleveland, OH 44135 USA
[2] Univ Liege, Liege, Belgium
[3] Wright State Univ, Dayton, OH 45435 USA
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 4 | 2013年
关键词
D O I
暂无
中图分类号
G40 [教育学];
学科分类号
040101 ; 120403 ;
摘要
Recent technology reviews have identified the need for objective assessments of aircraft engine health management (EHM) technologies. To help address this issue, a gas path diagnostic benchmark problem has been created and made publicly available. This software tool, referred to as the Propulsion Diagnostic Method Evaluation Strategy (ProDiMES), has been constructed based on feedback provided by the aircraft EHM community. It provides a standard benchmark problem enabling users to develop, evaluate and compare diagnostic methods. This paper will present an overview of ProDiMES along with a description of four gas path diagnostic methods developed and applied to the problem. These methods, which include analytical and empirical diagnostic techniques, will be described and associated blind-test-case metric results will be presented and compared. Lessons learned along with recommendations for improving the public benchmarking processes will also be presented and discussed.
引用
收藏
页数:13
相关论文
共 50 条
  • [21] Systematic benchmarking of performance, environmental and sustainability impacts of utilization of alternative cleaner fuel in an aircraft gas turbine engine
    Halil Yalcin Akdeniz
    Environmental Science and Pollution Research, 2022, 29 : 51012 - 51029
  • [22] USE OF VIBRATION SPECTRUM CHARACTERISTICS FOR AIRCRAFT GAS TURBINE ENGINE FLOW PATH DIAGNOSTICS.
    Mironov, A.G.
    Doroshko, S.M.
    Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1986, 29 (02): : 51 - 55
  • [23] Systematic benchmarking of performance, environmental and sustainability impacts of utilization of alternative cleaner fuel in an aircraft gas turbine engine
    Akdeniz, Halil Yalcin
    ENVIRONMENTAL SCIENCE AND POLLUTION RESEARCH, 2022, 29 (34) : 51012 - 51029
  • [24] Aircraft Engine Gas-Path Monitoring and Diagnostics Framework Based on a Hybrid Fault Recognition Approach
    Luis Perez-Ruiz, Juan
    Tang, Yu
    Loboda, Igor
    AEROSPACE, 2021, 8 (08)
  • [25] EVOLUTION OF AIRCRAFT GAS-TURBINE ENGINE
    ZIPKIN, MA
    ISRAEL JOURNAL OF TECHNOLOGY, 1977, 15 (1-2): : 44 - 58
  • [26] MULTILEVEL METHODS IN THE DYNAMICS OF AIRCRAFT ENGINE ROTORS
    VOLMIR, AS
    MIKHNEV, VF
    TIKHOMIROV, AE
    KHORKHORDIN, VI
    SOVIET APPLIED MECHANICS, 1984, 20 (12): : 1137 - 1141
  • [27] Gas Path Fault Diagnosis of Turboshaft Engine Based on Novel Transfer Learning Methods
    Zhao, Yong-Ping
    Jin, Hui-Jie
    Liu, Hao
    JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2024, 146 (03):
  • [28] A Methodology for the Diagnostic of Aircraft Engine Based on Indicators Aggregation
    Rabenoro, Tsirizo
    Lacaille, Jerome
    Cottrell, Marie
    Rossi, Fabrice
    ADVANCES IN DATA MINING: APPLICATIONS AND THEORETICAL ASPECTS, 2014, 8557 : 144 - 158
  • [29] Methods for coupled fluid/solid heat transfer with application on aircraft engine gas turbine components
    Negulescu, D.A.
    Berbente, C.
    UPB Scientific Bulletin, Series D: Mechanical Engineering, 2002, 64 (04): : 81 - 99
  • [30] Gas path analysis of military aircraft engines
    zur Nieden, H
    Fiedler, K
    MONITORING AND DIAGNOSIS IN POWER PLANTS, 1997, 1359 : 401 - 414