TAKEOFF POWER MANAGEMENT SYSTEM AND METHOD FOR GAS TURBINE ENGINES

A gas turbine engine (20) includes a control unit (46) to command the gas turbine engine (20) to perform one of a rolling takeoff procedure and an unrestricted takeoff procedure. The control unit (46) is configured to command the gas turbine engine (20) to perform the rolling takeoff procedure when...

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Bibliographic Details
Main Authors WALTHER, Ronald S, FEULNER, Matthew R
Format Patent
LanguageEnglish
French
German
Published 25.01.2023
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
CONTROLLING
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRANSPORTING
WEAPONS
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Summary:A gas turbine engine (20) includes a control unit (46) to command the gas turbine engine (20) to perform one of a rolling takeoff procedure and an unrestricted takeoff procedure. The control unit (46) is configured to command the gas turbine engine (20) to perform the rolling takeoff procedure when information required to determine whether the unrestricted takeoff procedure can be performed is unavailable to the control unit (46).
Bibliography:Application Number: EP20170160897