Abstract: A method enables a gas turbine engine nozzle to be secured within an engine casing that includes an exterior surface. The method comprises the steps of forming a first opening to extend through the engine casing, inserting a nozzle lock 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.
Type:
Grant
Filed:
July 3, 2002
Date of Patent:
August 10, 2004
Assignee:
General Electric Company
Inventors:
Edward Atwood Rainous, Charles Louis Williams, Michael Peter Murphy, Janice Ilene Pirtle, James Harold Joy