초록 ▼

A nozzle system includes a multitude of circumferentially distributed convergent flaps, divergent flaps and inter-flap seals which circumscribe an engine centerline and define the radial outer boundary of an exhaust gas path. Each divergent flap includes longitudinal sides having a set of extension

A nozzle system includes a multitude of circumferentially distributed convergent flaps, divergent flaps and inter-flap seals which circumscribe an engine centerline and define the radial outer boundary of an exhaust gas path. Each divergent flap includes longitudinal sides having a set of extension which are located at different longitudinal stations such that the extensions on adjacent divergent flaps interfit when the nozzle is in a minimum dilated position yet provide support for the intermediate flap seal when the nozzle is in a maximum dilated position to thereby provide a relative increase in the nozzle area ratio range.

대표청구항 ▼

What is claimed is: 1. A convergent/divergent nozzle system comprising: a divergent flap seal pivotably mounted about a hinge axis which circumscribes a nozzle centerline, said divergent flap seal defining a flap seal longitudinal axis between a first flap seal longitudinal side and a second flap s

What is claimed is: 1. A convergent/divergent nozzle system comprising: a divergent flap seal pivotably mounted about a hinge axis which circumscribes a nozzle centerline, said divergent flap seal defining a flap seal longitudinal axis between a first flap seal longitudinal side and a second flap seal longitudinal side; a first divergent flap pivotably mounted about said hinge axis adjacent said first flap seal longitudinal side, said first divergent flap having a first divergent flap longitudinal side with at least one extension which extends therefrom which faces toward said flap seal longitudinal axis, said at least one extension located at a first longitudinal station; and a second divergent flap pivotably mounted about said hinge axis adjacent said second flap seal longitudinal side, said second divergent flap having a second divergent flap longitudinal side with at least one extension which extends therefrom which faces toward said flap seal longitudinal axis, said at least one extension located at a second longitudinal station different from said first longitudinal station such that said at least one extension which extends from said first divergent flap longitudinal side at least partially interfits with said at least one extension which extends from said second divergent flap longitudinal side when the nozzle is in a minimum position. 2. The convergent/divergent nozzle system as recited in claim 1, wherein said at least one extension which extends from said first divergent flap longitudinal side and said at least one extension which extends from said second divergent flap longitudinal side at least partially supports said divergent flap seal when the nozzle is in a maximum position. 3. The convergent/divergent nozzle system as recited in claim 1, further comprising a linkage mounted to said divergent flap seal, said linkage connected to said first divergent flap and said second divergent flap. 4. The convergent/divergent nozzle system as recited in claim 1, further comprising a first plow tip mounted to said first divergent flap and a second plow tip mounted to said second divergent flap, said first plow tip at least partially interfits with said second plow tip when the nozzle is in the minimum position. 5. A convergent/divergent nozzle system comprising: a multitude of divergent flap seals and a multitude of divergent flaps pivotably mounted about a hinge axis which circumscribes a nozzle centerline, said multitude of divergent flap seals and said multitude of divergent flaps movable between an maximum nozzle position and a minimum nozzle position, each of said multitude of divergent flaps including at least one extension on a first longitudinal side and at least one extension on a second longitudinal side such that said at least one extension on said first longitudinal side of one of said multitude of divergent flaps interfits with said at least one extension on said second longitudinal side on an adjacent divergent flap of said multitude of divergent flaps at said minimum nozzle position and at least partially support one of said multitude of divergent flaps seals intermediate said divergent flap and said adjacent divergent flap at said maximum nozzle position. 6. The convergent/divergent nozzle system as recited in claim 5, wherein each of said multitude or divergent flaps are pivotally mounted to an associated convergent flap. 7. A method of increasing an area ratio range of a convergent/divergent nozzle system with a multitude of divergent flap seals and a multitude of divergent flaps, each of said divergent flap seals distributed circumferentially intermediate a first and second adjacent divergent flap comprising the steps of: (1) interfitting at least one extension on a first longitudinal side of at least one of the multitude of divergent flaps with at least one extension on a second longitudinal side of an adjacent divergent flap the nozzle system is in a minimum nozzle position. 8. A method as recited in claim 7, further comprises the step of: (2) at least partially supporting a divergent flap seal intermediate the first and second adjacent divergent flaps with the at least one extension on the first longitudinal side of one of the divergent flaps and the at least one extension on the second longitudinal side of the other divergent flap when the nozzle is in a maximum nozzle position.