EXHAUST SYSTEM FOR GAS TURBINE ENGINE

An exhaust system for a gas turbine engine is provided. The exhaust system includes an exhaust diffuser having a diffuser axis. The exhaust diffuser includes an outer diffuser wall. The exhaust diffuser also includes an inner diffuser wall. The exhaust diffuser further includes a diffuser inlet form...

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Bibliographische Detailangaben
Hauptverfasser:	Guillot Stephen A, Stang Ulrich E, Ng Wing F, Samal Nihar R
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 WEAPONS
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Beschreibung
Zusammenfassung:	An exhaust system for a gas turbine engine is provided. The exhaust system includes an exhaust diffuser having a diffuser axis. The exhaust diffuser includes an outer diffuser wall. The exhaust diffuser also includes an inner diffuser wall. The exhaust diffuser further includes a diffuser inlet formed by the first and second upstream ends of the outer diffuser wall and the inner diffuser wall. The exhaust diffuser includes a diffuser exit. The exhaust system also includes an exhaust collector coupled with the exhaust diffuser and adapted to collect and redirect exhaust gases in a radial direction. The exhaust collector includes a circumferential wall. The exhaust collector also includes a forward wall. The exhaust collector further includes an aft wall, wherein the aft wall is angled with respect to the diffuser axis. The exhaust collector includes a splitter disposed between the forward wall and the aft wall of the exhaust collector.