发明名称 |
THRUST CONTROL MALFUNCTION ACCOMMODATION SYSTEM AND METHOD |
摘要 |
A system for detecting and correcting a thrust control malfunction in an aircraft engine. The system includes an electronic engine control (EEC) unit that includes a first processing subsystem and a second processing subsystem, and a thrust control malfunction accommodation (TCMA) circuit included in the first processing subsystem and the second processing subsystem. Additionally, the system includes a TCMA software package executed by the first processing subsystem and the second processing subsystem, thereby providing redundant execution of the TCMA software package.
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申请公布号 |
US2003191565(A1) |
申请公布日期 |
2003.10.09 |
申请号 |
US20020116655 |
申请日期 |
2002.04.04 |
申请人 |
OSTROM GRAZYNA BALUT;BROWN KEVIN S.;FUNG KENNY L.;GHAYEM SHAHROKH |
发明人 |
OSTROM GRAZYNA BALUT;BROWN KEVIN S.;FUNG KENNY L.;GHAYEM SHAHROKH |
分类号 |
F01D21/00;F01D21/14;F02C9/00;F02C9/46;(IPC1-7):G01M17/00 |
主分类号 |
F01D21/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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