Silencer for a gas turbine

The present disclosure relates to a generally rectangular frame including two spaced-apart and substantially parallel end members interconnected by two spaced part and substantially parallel length members. The length members defined inwardly facing channels. Two spaced-apart perforated members are...

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Bibliographische Detailangaben
Hauptverfasser:	DARRELL JAHN D, OEHLKE SCOTT E, FLITSCH RONALD E, NOREEN ROBERT A
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS
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Beschreibung
Zusammenfassung:	The present disclosure relates to a generally rectangular frame including two spaced-apart and substantially parallel end members interconnected by two spaced part and substantially parallel length members. The length members defined inwardly facing channels. Two spaced-apart perforated members are secured within the inwardly facing channels between the two spaced-apart length members. Sound absorbing material is compressed between the perforated members.