AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE EXHAUST HEAT EXCHANGER

An aircraft propulsion system (20) is provided that includes a turbine engine (24) and an exhaust gas heat exchanger (28). The exhaust gas heat exchanger (28) includes a central conduit (52), an outer radial plenum (54), fluid conduits (46), and inter-conduit passages (48). The fluid conduits (46) a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SMITH, Scott, DUROCHER, Eric 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 GAS-TURBINE PLANTS HEAT EXCHANGE IN GENERAL HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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