Component lock for a gas turbine engine

摘要

A lock assembly includes a lock body with an undercut slot which receives a retaining wire of a polygon shape.

主权项

1. A rotor disk assembly for a gas turbine engine comprising:
a rotor disk defined about an axis of rotation, said rotor disk having a circumferentially intermittent slot structure that extends radially outward relative to said axis of rotation; a component defined about said axis of rotation, said component having a multiple of radial tabs which extend radially inward relative to said axis of rotation, said multiple of radial tabs engageable with said circumferentially intermittent slot structure; and a lock assembly engaged with at least one opening formed by said circumferentially intermittent slot structure to provide an anti-rotation interface for said component, said lock assembly comprising a retaining wire that defines a polygon shape.