Advanced booster rotor blade

Details Advanced booster rotor blade Advanced booster rotor blade

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/14 (2006.01)

Patent

CA 2611339

A airfoil [50] having a leading edge [52] extending from a root [54] to a tip [55], an inner span region [155] and an outer span region [156] the leading edge having a sweep angle profile such that the sweep angle increases from the root [54] to a first height location [151] at a first rate of change of sweep angle that is substantially constant and thereafter increases at a second rate of change of sweep angle that is substantially constant.

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