发明名称 |
HEATING SYSTEM FOR USE IN A TURBINE ENGINE AND METHOD OF OPERATING SAME |
摘要 |
A method of operating a turbine engine including coupling a heating assembly to the turbine engine for selectively heating a compressor casing. A sensor transmits a first monitoring signal indicative of a speed of a rotor assembly to a controller. The controller determines whether the turbine engine is operating in a first operating mode based at least in part on the received first monitoring signal, wherein during the first operating mode a minimum clearance distance is defined between the rotor assembly and the compressor casing. The compressor casing of the turbine engine is heated to increase the clearance distance between the compressor casing and the rotor assembly, if the turbine engine is in the first operating mode. |
申请公布号 |
US2012297781(A1) |
申请公布日期 |
2012.11.29 |
申请号 |
US201113114752 |
申请日期 |
2011.05.24 |
申请人 |
MANCHIKANTI MARUTHI PRASAD;MEMMER JOHN DAVID |
发明人 |
MANCHIKANTI MARUTHI PRASAD;MEMMER JOHN DAVID |
分类号 |
F02C1/00;F01D5/08 |
主分类号 |
F02C1/00 |
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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