Advanced booster system

Details Advanced booster system Advanced booster system

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 3/06 (2006.01) F01D 5/14 (2006.01) F01D 9/02 (2006.01)

Patent

CA 2611336

A compression stage [8] having a plurality of stator vanes [40] and rotor blades [ 14] coaxial with a longitudinal centerline axis [15], each stator vane having an exit swirl angle distribution such that the exit swirl angle has a maximum value at an intermediate radius location and each rotor blade having a blade leading edge adapted to receive the flow from the stator vanes with the exit swirl angle distribution profile.

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