Methods and apparatus for turbine nozzle locks

摘要

A method enables a gas turbine engine nozzle (56) to be secured within an engine casing (28) that includes an exterior surface. The method comprises the steps of forming a first opening (120) to extend through the engine casing, inserting a nozzle lock (130) through the first opening from the casing exterior surface, coupling the nozzle lock to a portion of the nozzle, and securing the nozzle lock to the engine casing.