| 摘要 |
The aim of the invention is to remove the mechanical bleed constraints in the engines during the transient flight phases of an aircraft in order to optimize the operability of the engine assembly during said phases. To this end, a supply of power is provided, particularly during said phases, by an additional indirectly propulsive engine power source. The method for optimizing the operability of the propulsive unit of an aircraft comprising main engines (200) as main drive sources involves, using a main engine power unit GPP (1) as a power source, providing all the non-propulsive power (Enp) and also involves, during the transient engine phases, at most partially providing additional power (kEp, ktEpt) to the body HP of the main engines (200). |
