Reduced loss swept supersonic fan blade

Details Reduced loss swept supersonic fan blade Reduced loss swept supersonic fan blade

F - Mech Eng,Light,Heat,Weapons

01

D

170/81

F01D 5/14 (2006.01) B64C 11/18 (2006.01) F04D 29/38 (2006.01)

Patent

CA 1283366

ABSTRACT SUPERSONIC FAN BLADE A swept leading edge blade (10) rotates in a stream of air (26) and experiences supersonic relative air velocities over at least a portion of the blade surface. The maximum camber points (28, 40) of adjacent blade segments (20, 18) are located to prevent intensification of the compression wave generated by each segment (20, 18).

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