AIRCRAFT ENGINE OPERABILITY
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United States of America
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Issued Date -
Jan 9, 2020
app pub date -
May 14, 2019
filing date -
May 14, 2019
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Abstract
A gas turbine engine has a cycle operability parameter β in a defined range to achieve improved overall performance, taking into account fan operability and/or bird strike requirements as well as engine efficiency. The defined range of cycle operability parameter β may be particularly beneficial for gas turbine engines in which the fan is driven by a turbine through a gearbox.
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