发明名称 |
Fuel control method of a can annular combustor array |
摘要 |
Fuel is delivered in a gas turbine engine including a can annular combustor array that includes at least one combustor level subset within the array supplied by an independent fuel delivery system. Fuel is supplied only to one or more subsets during a first mode of operation. Fuel is supplied to the entire array of combustors during a second mode of operation.
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申请公布号 |
US8429917(B2) |
申请公布日期 |
2013.04.30 |
申请号 |
US201113085769 |
申请日期 |
2011.04.13 |
申请人 |
SNIDER DAVID AUGUST;ZIMINSKY WILLY STEVE;GENERAL ELECTRIC COMPANY |
发明人 |
SNIDER DAVID AUGUST;ZIMINSKY WILLY STEVE |
分类号 |
F02C7/22 |
主分类号 |
F02C7/22 |
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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