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NASA NTRS ยท 19900000125

Stowable Mechanical Sound Suppressor

Abstract

Stowable sound suppressor conceived for high-speed commercial transport (HSCT) engines. Suppressor is located just aft of variable nozzle of engine. During takeoff, when suppression of noise required, multisegmented system of separators rotates out of center plug across nozzle stream. Actuation accomplished by single ball-screw drive and links, similar to spokes in umbrella. With iris nozzle translated forward, circumferential row of tubes exposed. Pattern of tubes and separators form suppressor configuration. Flow stream through slots and tubes sized to takeoff area. Useful on any turbo-jet engine in which active suppression of sound required.

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BibTeXRIS

Thompson, Edward R.. 1990-03-01. Stowable Mechanical Sound Suppressor. https://ntrs.nasa.gov/citations/19900000125

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