Improved bushing for a jet engine vane

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 17/16 (2006.01) F01D 9/02 (2006.01)

Patent

CA 2652851

A vane assembly for an engine is disclosed, the vane assembly having a vane (10) including a blade (12) having a spindle (16) disposed at one end thereof and a bushing mounted on the spindle. The bushing (40) includes first and second half portions (42), each half portion having a generally semicircular body (44) having protrusions (51) and complementary recesses on the sides of the bodies (44). The first and second half portions (42) are snap fit onto the spindle (16) of the vane (10) such that the protrusion (52) of the second half portion is located in the recess of the first half portion, and the protrusion (52) of the first half portion is located in the recess of the second half portion. Each of the first and second half portions (42) further include a semi-annular flange (46) disposed at the first end of the body portion, the semi-annular flange (46) lying in a plane which is substantially perpendicular to a longitudinal axis of the body.

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