Reduced radar cross section exhaust nozzle assembly
An exhaust nozzle assembly includes a plurality of interfitting flap assemblies that are moveable between a maximum area ratio and a minimum area ratio. Each of the pluralities of flap assemblies includes a slot and a wing. The wing fits within an adjacent slot of an adjacent flap assembly. Each of the flap assemblies includes a divergent element that provides a specific geometric shape forming the trailing edge surfaces. The flap element is attached to the divergent element and extends to a static structure. The flap element and the divergent element combine to form a continuous faceted outer surface of the exhaust nozzle assembly substantially void of gaps throughout the range of motion between the maximum and minimum area ratios.
1. An exhaust nozzle assembly comprising:
a plurality of interfitting flap assemblies movable between a maximum area position and a minimum area position, each of said plurality of flap assemblies including a slot on one longitudinal side and a wing on a second longitudinal side, said wing fitting within a slot of an adjacent one of said plurality of interfitting flap assemblies, wherein each of said plurality of flap assemblies includes a divergent element attached to a flap element, said divergent element and said flap element include a portion of said wing, and said divergent element defines a trailing edge including an aft most portion, sweep surfaces extending from said aft most portion at a sweep angle and a top surface extending upwardly from said aft most portion at a wedge angle.
2. The assembly as recited in claim 1 , including a seal disposed between adjacent flap assemblies.
3. The assembly as recited in claim 1 , wherein said divergent element includes a slot side and a wing side, wherein said slot slide is configured for receiving a wing side of an adjacent divergent element.
4. The assembly as recited in claim 1 , wherein said divergent element includes an attachment segment for connection to a linkage element.
5. The assembly as recited in claim 1 , wherein said flap element includes a slotted side and a wing segment, said wing segment received within a slotted side of an adjacent flap assembly.
6. The assembly as recited in claim 2 , wherein said seal is disposed on a surface of said plurality of flap assemblies exposed to exhaust gases.
7. An exhaust nozzle assembly cornpnsing:
a plurality of interfitting flap assemblies movable between a maximum area position and a minimum area position, each of said plurality of flap assemblies including a slot on one longitudinal side and a wing on a second longitudinal side, said wing fitting within a slot of an adjacent one of said plurality of interfitting flap assemblies, wherein each of said plurality of flap assemblies includes a divergent element attached to a flap element, said divergent element and said flap element include a portion of said wing; and
a seal disposed between adjacent flap assemblies, said seal includes a notch corresponding to trailing edges of adjacent divergent elements.
8. The assembly as recited in claim 7 , wherein said notch is V-shaped.
9. The assembly as recited in claim 7 , wherein said seal includes a first surface and a tented surface disposed on a plane different than said first surface, said tented surface extending outward from said first surface.
10. The assembly as recited in claim 1 , wherein said wing disposed within an adjacent slot does not contact an interior surface of said adjacent flap assembly.
11. An exhaust nozzle assembly comprising:
a variable opening defining a serrated trailing edge; and
a plurality of flap assemblies including a wing portion disposed along a first longitudinal side and a slot disposed on a second longitudinal side for receiving a wing portion of an adjacent flap assembly and a divergent element that defined a portion of said serrated trailing edge wherein said divergent element comprises a portion of said wing and a portion of said slot, wherein said wing is disposed within a slot of an adjacent divergent element, and said divergent element comprises an aft most segment forming a point of said serrated training edge and an exterior surface extending radially outwardly from said aft most segment.
12. The assembly as recited in claim 11 , wherein said plurality of flap assemblies includes a corresponding plurality of flap elements attached to a corresponding plurality of divergent elements.
13. The assembly as recited in claim 12 , including a seal disposed on an inner surface of said exhaust nozzle assembly.
14. The assembly as recited in claim 13 , wherein said seal includes a notch corresponding to a portion of said serrated trailing edge.
15. The assembly as recited in claim 14 , wherein said notch is substantially V-shaped.
16. The assembly as recited in claim 14 , wherein said seal includes an angled surface between a substantially planar region and an edge of said notch.
17. The assembly as recited in claim 14 , wherein said seal includes a first substantially flat segment and a second tented portion angled outwardly from said first substantially flat segment, and said notch is disposed within said second tented portion.