发明名称 |
Control system of a gas turbine engine supplying power to an aircraft |
摘要 |
A system and method for controlling the operation of a gas turbine engine supplying power to an aircraft, where the engine is controlled according to a reading of an amount of power drawn from the supplied power. The reading is fed directly to a control system (102), which issues commands for controlling engine parameters comprising an acceleration reference signal, load shedding, variable geometry positioning, and fuel flow. The control system (102) may further issue commands for controlling the amount of power drawn. The control system may further use the reading to monitor the engine's condition. |
申请公布号 |
EP2685068(A2) |
申请公布日期 |
2014.01.15 |
申请号 |
EP20130173975 |
申请日期 |
2013.06.27 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
CHEN, BRYAN;CHMIEL, DARIUSZ;BEAUCHESNE-MARTEL, PHILLIPPE;JARVO, JAMES ROBERT |
分类号 |
F02C9/28;B64D31/06;F01D21/00;F02C7/042;F02C9/26;F02C9/54;G05B13/02 |
主分类号 |
F02C9/28 |
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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