A method of operation is provided. During this method, a first power system of an aircraft powerplant is operated to direct a first quantity of fuel into a flowpath of the aircraft powerplant for combustion. A second power system of the aircraft powerplant is tested during the operating of the first power system. The testing of the second power system includes: signaling the second power system to direct a second quantity of fuel into the flowpath for combustion; determining an operational parameter of the aircraft powerplant following the signaling; and evaluating operability of the second power system by comparing the operational parameter to a threshold.
TESTING SECONDARY POWER SYSTEM OF AIRCRAFT POWERPLANT
TESTEN EINES SEKUNDÄRSTROMSYSTEMS EINES FLUGZEUGTRIEBWERKS
TEST DE SYSTÈME D'ALIMENTATION SECONDAIRE D'UNE UNITÉ DE PUISSANCE D'AÉRONEF
2025-01-01
Patent
Electronic Resource
English
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke |
AIRCRAFT POWERPLANT DEVELOPMENT TESTING
SAE Technical Papers | 1944
|ADJUSTING AIRCRAFT POWERPLANT POWER SPLIT TO CONTROL POWERPLANT VIBRATIONS
European Patent Office | 2023
|