Full-span forward swept airfoils for gas turbine engines
Rotor of a gas turbine engines having a rotor hub and a plurality of blades extending from the rotor hub, wherein each blade has a full-span forward sweep along a leading edge of the blade that starts at an airfoil root of the blade at the hub and extends to a blade tip, wherein a sweep of a blade i...
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Main Authors | , , , , , |
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Format | Patent |
Language | English |
Published |
31.03.2020
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Subjects | |
Online Access | Get full text |
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Summary: | Rotor of a gas turbine engines having a rotor hub and a plurality of blades extending from the rotor hub, wherein each blade has a full-span forward sweep along a leading edge of the blade that starts at an airfoil root of the blade at the hub and extends to a blade tip, wherein a sweep of a blade is a percentage of a root axial chord length of the respective blade. |
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Bibliography: | Application Number: US201615261011 |