System for regulating a cooling fluid within a turbomachine

A system for regulating a cooling fluid within a turbomachine 100. The system may include a plurality of bypass chambers 310, wherein each of the plurality of bypass chambers 310 allows for the cooling fluid to pass from the compressor section 105 to the at least one wheelspace area 195. The system...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	MEENAKSH, RAVI, VEDHAGIRI, SIVARAMAN, TROUT, JESSE, PARKER, WILLIAM, SCICCHITANO, ERIC, MOROSO, JOSEPH
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 ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A system for regulating a cooling fluid within a turbomachine 100. The system may include a plurality of bypass chambers 310, wherein each of the plurality of bypass chambers 310 allows for the cooling fluid to pass from the compressor section 105 to the at least one wheelspace area 195. The system may also include a plurality of bypass plugs 340, wherein each of the plurality of bypass plugs 340 is insertable into a bypass chamber opening 320 on each of the plurality of bypass chambers 310.