Nozzle flap hinge joint

Claim 1

A flap assembly hinge joint for a gas turbine engine exhaust nozzle, comprising: (a) a first hollow flap having a first chamber defined therein and being adapted for promoting flow of cooling air therethrough, and a first plurality of linearly spaced apart first lug extensions defined along a first flap edge thereof and aligned along a pivot axis near said first flap edge; (b) a second hollow flap pivotally mounted to said first hollow flap and having a second chamber defined therein and being adapted for promoting flow of cooling air therethrough, and a second plurality of linearly spaced apart second lug extensions defined along a second flap edge thereof, said second flap disposed adjacent said first flap with corresponding said second lug extensions alternated with said first lug extensions along said pivot axis; (c) each of said first lug extensions and said second lug extensions including means defining passageways therethrough in communication with the corresponding said first chamber and said second chamber, and further including means defining axial openings of preselected size aligned along said pivot axis; and (d) a hollow, generally cylindrically shaped hinge pin, disposed along said pivot axis and received by said axial openings in alternate said first lug extensions and said second lug extensions, said pin further including a third plurality of openings disposed along the length of said pin, said openings located in communicating relationship with respective said passageways in said first lug extensions and said second lug extensions of the respective said first hollow flap and said second hollow flap.