GAS TURBINE ENGINE WITH AN ENGINE ROTOR ELEMENT TURNING DEVICE

A turbine engine 10 has a core 16 with a compressor 22, combustor 28, and turbine 29 sections in axial flow arrangement and with corresponding rotating elements mounted to a shaft 36, 38 defining engine rotor elements 40. The turbine engine 10 has a rotary driver 72 operably coupled to the engine ro...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	MARTELL, Raymond Floyd, HOPPER, Mark Leonard, MILLER, Brandon Wayne, WAUN, Scott Douglas
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 ELECTRICITY 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 STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A turbine engine 10 has a core 16 with a compressor 22, combustor 28, and turbine 29 sections in axial flow arrangement and with corresponding rotating elements mounted to a shaft 36, 38 defining engine rotor elements 40. The turbine engine 10 has a rotary driver 72 operably coupled to the engine rotor elements 40. The turbine engine 10 has at least one thermoelectric generator 70 in thermal communication with the core 16 and in electrical communication with the rotary driver 72 to provide power to the rotary driver 72 to turn the engine rotor elements 40.