GAS TURBINE ENGINGE FILTER CLEANING SYSTEM AND METHOD OF OPERATION

A filter cleaning system is provided for a gas turbine engine (12) including a compressor section (14) and a combustor section (16). A mechanism (32) is operatively connected to the gas turbine engine and is configured to be driven by the gas turbine engine in a first mode and configured to drive th...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MARTIN, KEVIN, L, CALLAS, JAMES, J, TONSOR, ANDREW, J, SOPKO, THOMAS, M, RENSHAW, CODY, P
Format:	Patent
Sprache:	eng ; fre
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 LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL SEPARATION TRANSPORTING WEAPONS
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