HIGH PRESSURE COMPRESSOR AUGMENTED BLEED WITH AUTONOMOUSLY ACTUATED VALVE

PROBLEM TO BE SOLVED: To provide a gas turbine engine compressor bleed system allowing cruise bleed to meet plenum pressurization requirements using a lower pressure compressor stage.SOLUTION: A compressor bleed assembly 40 comprises: an annular bleed plenum 43 radially disposed between outer and in...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	MICHAEL ANTHONY THOMAS JR, CURTIS WILLIAM MOECKEL, CARLOS IVAN FLORES, DAVID WILLIAM FASIG
Format:	Patent
Sprache:	eng ; jpn
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 NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!