Turbine inlet silencer

Acoustics – Sound-modifying means – Muffler – fluid conducting type

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181229, E04F 1704

Patent

active

054913080

ABSTRACT:
In order to reduce noise transmission through the air inlet duct (16) of a turbine engine (10), the air inlet duct (16) provides a non-linear path defined by a bend (24) for air from a source, and the turbine engine (10) includes a sound attenuation assembly (26) in the form of a splitter dissipative silencer disposed near the bend (24) in the air inlet duct (16). More specifically, the turbine engine (10) is such that the splitter dissipative silencer (26) can be formed as a modular assembly (42) removably securable near the bend (24) in the air inlet duct (16) upstream of a radial compressor (12) for removal and/or replacement or availability as an optional component of the turbine engine (10).

REFERENCES:
patent: 3739872 (1973-06-01), McNair
patent: 3841434 (1974-10-01), Culpepper, Jr.
patent: 4266602 (1981-05-01), White et al.
patent: 4276954 (1981-07-01), Romano
patent: 4421455 (1983-12-01), Tomren
patent: 4723626 (1988-02-01), Carr et al.

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