Gas turbine engine with intercooling turbine section

A gas turbine engine (10) includes a fan section (22) and an intercooling turbine section (24) along an engine axis aft of the fan section (22) and forward of a combustor section (30).

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	Kupratis, Daniel B
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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A gas turbine engine (10) includes a fan section (22) and an intercooling turbine section (24) along an engine axis aft of the fan section (22) and forward of a combustor section (30).