Mixer for cooling and sealing air system for turbomachinery

A system for mixing flows from a compressor is provided. The system comprises an ejector (150) that combines a first flow (122) and a second flow (132), from the compressor, into a third flow (158). A bypass flow (142) is connected between the first flow (122) and the third flow (158). A mixer (300)...

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Bibliographische Detailangaben
Hauptverfasser:	BALL, DAVID W. JR, WHALING, KENNETH N, ELURIPATI, RAVI PRAVEEN S, DAVIS, JAMES L, SARAVANAN, NATTAMAI V, SENGAR, AJIT S
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 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING MIXING, e.g. DISSOLVING, EMULSIFYING, DISPERSING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A system for mixing flows from a compressor is provided. The system comprises an ejector (150) that combines a first flow (122) and a second flow (132), from the compressor, into a third flow (158). A bypass flow (142) is connected between the first flow (122) and the third flow (158). A mixer (300) combines the bypass flow (142) and the third flow (158) into a fourth flow (165). The fourth flow has a pressure and temperature intermediate the respective pressures and temperatures of the bypass flow and the third flow.