TEMPERATURE ESTIMATION APPARATUS FOR AEROPLANE GAS TURBINE ENGINE

In a temperature estimation apparatus for an aeroplane gas turbine engine mounted on an aircraft and having a combustion chamber, a high-pressure turbine rotated by combustion gas exhausted from the combustion chamber, a low-pressure turbine located downstream of the high-pressure turbine to be rota...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MURAMATSU HIRONORI, SAITA TOMOHISA
Format:	Patent
Sprache:	eng
Schlagworte:	MEASURING MEASURING QUANTITY OF HEAT MEASURING TEMPERATURE PHYSICS TESTING THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
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