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GAS TURBINE ENGINE WITH TWO-SPOOL FAN AND VARIABLE VANE TURBINE
GAS TURBINE ENGINE WITH TWO-SPOOL FAN AND VARIABLE VANE TURBINE
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机译:带有两风扇和可变叶片涡轮的燃气轮机发动机
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摘要
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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