Invention Grant
US09279388B2 Gas turbine engine with two-spool fan and variable vane turbine 有权
带双线轴风扇和变叶片涡轮机的燃气轮机

Gas turbine engine with two-spool fan and variable vane turbine
Abstract:
A gas turbine engine and a method of operating the gas turbine engine according to an exemplary aspect of the present disclosure includes modulating a variable high pressure turbine inlet guide vane of a high pressure spool to performance match a first stage fan section of a low pressure spool and an intermediate stage fan section of an intermediate spool to maintain a generally constant engine inlet flow while varying engine thrust.
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