Filter assembly

An air inlet filter assembly and method of assembling an inlet air filter assembly for use with a turbine engine system 10. The method includes coupling an inlet hood 106 to an air filter enclosure 104, such that an airflow path 116 is defined between the inlet hood and the air filter enclosure. A p...

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Bibliographische Detailangaben
Hauptverfasser:	SIDDARTH UPADHYAY, RAHUL J CHILLAR
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL SEPARATION TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An air inlet filter assembly and method of assembling an inlet air filter assembly for use with a turbine engine system 10. The method includes coupling an inlet hood 106 to an air filter enclosure 104, such that an airflow path 116 is defined between the inlet hood and the air filter enclosure. A pre-filter 110 is coupled to the inlet hood 116, such that the pre-filter is positioned within the airflow path 116. A filter bypass assembly 112 is coupled to the pre-filter 110 for moving the pre-filter from an operating position to a bypass position during operation. Advantageously the air inlet filter assembly allows removal of an intake air pre-filter from operation without shutdown of an associated turbine engine. A further invention is directed to a gas turbine engine system including a compressor and a combustor and an air inlet filter assembly.