INLET PERFORMANCE MEASUREMENT SYSTEM FOR GAS TURBINE ENGINE

A performance measurement system (56) of an inlet of a gas turbine engine includes a probe strut (58) configured for installation to a case strut (52) of an inlet case (46) of a gas turbine engine. The probe strut (58) includes one or more probes (64) extending therefrom configured to measure one or...

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Bibliographische Detailangaben
Hauptverfasser:	HENDRICKS, Richard C, RICE, William W, COVINO, Alfred F, THOMESEN, Douglas H, HACKETT, Bryan J
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 ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MEASURING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS
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