METHOD FOR CHECKING THE MAXIMUM AVAILABLE POWER OF A TURBINE ENGINE OF AN AIRCRAFT EQUIPPED WITH TWO TURBINE ENGINES

摘要

The invention concerns a method (100) for checking the maximum available power of a turbine engine (11, 12) of an aircraft (10) equipped with two turbine engines (11, 12) configured to operate in parallel and together to supply a necessary power (P₁₊₂) to the aircraft during a flight phase, said method comprising the following steps:- placing one of the turbine engines (11, 12) in a maximum take-off power regime (PMD), and - adjusting a power (P_2, P₁) supplied by the other turbine engine (12, 11), such that the turbine engines (11, 12) continue to supply the necessary power (P₁₊₂) to the aircraft during the flight phase; - determining a power (P₁, P₂) supplied by the turbine engine (11, 12) placed in the maximum take-off power regime (PMD), and - processing the supplied power (P1, P2) determined in this way, in order to deduce a piece of information relating to the maximum available power.