Gary H Reynolds

US Patent:

62339206, May 22, 2001

Filed:

Jan 26, 2000

Appl. No.:

9/491683

Inventors:

Walter M. Presz - Wilbraham MA
Gary Reynolds - San Diego CA

Assignee:

Stage III Technologies, L.C.

International Classification:

F02K 100

US Classification:

60230

Abstract:

A contoured thrust reverser and lobed nozzle noise suppressor is meant for use with gas turbine engines that have conventional post-exit thrust reversers and that require only moderate levels of noise suppression. The contoured thrust reverser and lobed nozzle noise suppressor comprises a conventional tailpipe frame terminating in a lobed nozzle, and a conventional thrust reverser mechanism holding a pair of contoured blocker doors. In a deployed position, the blocker doors lie aft of the lobed nozzle, having been moved there by the thrust reverser mechanism. The blocker doors abut one another and form a fore-facing scoop, wherein any engine exhaust exiting the lobed nozzle is redirected towards the fore of the engine. In a stowed position, the blocker doors lie over the tailpipe frame and align and nestle together with the engine's cowling. Since the blocker doors partially overlap the lobed nozzle in this position, aft portions of each blocker door are contoured to correspond in shape to an exterior fore portion of the lobed nozzle of which they overlap.