Gas turbine inlet system

A gas turbine inlet system includes a main inlet portion (12), wherein an airflow is introduced to the gas turbine inlet system. Also included is a silencer assembly (18). The silencer assembly includes a first silencing panel (22), wherein the first silencing panel is oriented substantially perpend...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	MERCHANT, LAXMIKANT, VENUGOPAL SETTY, DINESH
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A gas turbine inlet system includes a main inlet portion (12), wherein an airflow is introduced to the gas turbine inlet system. Also included is a silencer assembly (18). The silencer assembly includes a first silencing panel (22), wherein the first silencing panel is oriented substantially perpendicularly to the airflow, and wherein the first silencing panel includes a first plurality of airflow apertures. The silencer assembly also includes a second silencing panel (22), wherein the second silencing panel is oriented substantially perpendicularly to the airflow, and wherein the second silencing panel includes a second plurality of airflow apertures.