Gas turbine inlet fogging system

The present application provides an inlet air fogging system (100) for a gas turbine engine (110). The inlet air fogging system (100) may include a fogging nozzle array (270) and a fogging control system (320) in communication with the fogging nozzle array (270). The fogging control system (320) may...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Mitra, Chayan, Mestroni, Julio Enrique, Chillar, Rahul J, Maity, Sandip, Sharma, Rachit
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 INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES LIGHTING MEASURING MECHANICAL ENGINEERING PHYSICS TESTING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The present application provides an inlet air fogging system (100) for a gas turbine engine (110). The inlet air fogging system (100) may include a fogging nozzle array (270) and a fogging control system (320) in communication with the fogging nozzle array (270). The fogging control system (320) may include a droplet size measurement system (340) and a humidity level measurement system (390).