发明名称 |
DATABASE CONSTRUCTION METHOD FOR MODELING OF AIRCRAFT ENGINE |
摘要 |
A database constructing method for modeling an aircraft engine with utilization of restricted flight test data is provided to construct a database fit to an operation environment of an aircraft simulation system by constructing the database through a comparing process, after finding out a correction coefficient by extracting the flight data, and standardizing important performance values of the engine. Various data for modeling the aircraft engine is inputted(S1). A gross temperature/pressure value considering effects according to a flight speed is found by using ambient temperature/pressure value among the input data(S2). A gross temperature/pressure ratio is calculated by dividing the gross temperature/pressure value by the standard ambient temperature/pressure(S3). The correction coefficient is calculated by using the gross temperature/pressure ratio(S4). A standardized engine performance value is calculated by standardizing a normal/transition state with the correction coefficient(S6). The engine performance value is compared/verified with flight test acceleration/deceleration data of the database(S7). The verified engine performance value is stored to the database in a form available to engine modeling(S8).
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申请公布号 |
KR20050029956(A) |
申请公布日期 |
2005.03.29 |
申请号 |
KR20030066249 |
申请日期 |
2003.09.24 |
申请人 |
KOREA AEROSPACE INDUSTRIES, LTD. |
发明人 |
JANG, KWANG KYU |
分类号 |
G06F17/30;(IPC1-7):G06F17/30 |
主分类号 |
G06F17/30 |
代理机构 |
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