发明名称 |
SYSTEM FOR OPTIMIZING POWER USAGE FROM DAMAGED FAN BLADES |
摘要 |
An aircraft jet engine system includes at least one gas turbine engine having a fan including a rotor and a plurality of fan blades. A sensor system in the fan section senses information about the operation of the blades and provides feedback on the condition of each blade to a control. The control is programmed to take in the sensed information and identify a safe operating range for the gas turbine engine based upon damage information developed from the sensed information with regard to each of the blades. An aircraft jet engine system incorporating a plurality of gas turbine engines wherein safe operating ranges are developed for each of the gas turbine engines is also disclosed as is a method of operating an aircraft jet engine system. |
申请公布号 |
US2013111915(A1) |
申请公布日期 |
2013.05.09 |
申请号 |
US201113289322 |
申请日期 |
2011.11.04 |
申请人 |
SCHWARZ FREDERICK M.;WOOD COY BRUCE |
发明人 |
SCHWARZ FREDERICK M.;WOOD COY BRUCE |
分类号 |
F02C9/00 |
主分类号 |
F02C9/00 |
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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